UNITED STATES AIR FORCE AIRCRAFT ACCIDENT INVESTIGATION BOARD REPORT RC-135V, T/N 64-14848 55TH WING OFFUTT AIR FORCE BASE, NEBRASKA LOCATION: OFFUTT AIR FORCE BASE, NEBRASKA DATE OF ACCIDENT: 30 APRIL 2015 BOARD PRESIDENT: LIEUTENANT COLONEL WILLIAM M. EVANS, JR. Conducted IAW Air Force Instruction 51-503 DEPARTMENT OF THE AIR FORCE HEADQUARTERS AIR COMBAT COMMAND JOINT BASE LANGLEY-EUSTIS VA OFFICE OF THE VICE COMMANDER 205 0000 BOULEVARD SUITE 203 JOINT BASE LANGLEY-EUSTIS VA 23665-2788 Am: 0 3 2015 ACTION OF THE CONVENING AUTHORITY The Report of the Accident Investigation Board, conducted under the provisions of 51-503, that investigated the 30 April 2015 mishap, near Offutt Air Force Base, Nebraska, involving an RC-135, 64-14848, assigned to the 343rd Reconnaissance Squadron, 55th Wing, Offutt Air Force Base, Nebraska, complies with applicable regulatory and statutory guidance; on that basis it is approved. IERKY D. HARRIS, JR. Major General, USAF Vice Commander Mama: EXECUTIVE SUMMARY AIRCRAFT ACCIDENT INVESTIGATION RC-135V, T/N 64-14848 OFFUTT AIR FORCE BASE, NEBRASKA 30 APRIL 2015 On 30 April 2015, at approximately 1825 local time (L), the mishap aircraft (MA), an RC-135V, Tail Number 64-14848, assigned to the 343rd Reconnaissance Squadron, 55th Wing, Offutt Air Force Base (AFB), Nebraska (NE), experienced a fire in the rear cabin during initial takeoff. The MA and its crew were conducting a routine training mission in support of an Air Force Special Operations Command exercise. The Mishap Crewmembers (MC) consisted of cockpit crew, electronic warfare officers, intelligence operators and in-flight maintenance technicians. The Mishap Pilot aborted the takeoff, and all 27 MC safely evacuated the MA. Four crewmembers received treatment for minor smoke inhalation. Fire crews arrived at approximately 1829L and extinguished the flames. The fire burned a hole through the upper fuselage above the rear galley area of the MA, causing structural damage and damage to aircraft control and mission related systems. Repair cost to the MA is estimated at $62.4 million. There were no injuries to civilians or damage to private property. The board president found by preponderance of the evidence that the cause of the mishap was a leak in the high-pressure oxygen system due to poor assembly of the system tubing at depot maintenance. Failure by L3 Communications depot maintenance personnel to tighten a retaining nut connecting a metal oxygen tube to a junction fitting above the galley properly caused an oxygen leak. This leak created a highly flammable oxygen-rich environment that ignited. The resulting fire melted the retaining nut causing the tubing to become detached from the junction fitting, feeding more oxygen to the fire, increasing its size, and causing severe damage to the airframe, galley, and mission equipment onboard the aircraft. Under 10 U.S.C. § 2254(d) the opinion of the accident investigator as to the cause of, or the factors contributing to, the accident set forth in the accident investigation report, if any, may not be considered as evidence in any civil or criminal proceeding arising from the accident, nor may such information be considered an admission of liability of the United States or by any person referred to in those conclusions or statements. SUMMARY OF FACTS AND STATEMENT OF OPINION RC-135V, T/N 64-14848 OFFUTT AIR FORCE BASE, NEBRASKA TABLE OF CONTENTS ACRONYMS AND ABBREVIATIONS ...................................................................................... iii SUMMARY OF FACTS ................................................................................................................ 1 1. AUTHORITY AND PURPOSE ...........................................................................................1 a. Authority .........................................................................................................................1 b. Purpose............................................................................................................................1 2. ACCIDENT SUMMARY.....................................................................................................1 3. BACKGROUND ..................................................................................................................1 a. 55th Wing (55 WG) .......................................................................................................2 b. 55th Operations Group (55 OG) .....................................................................................2 c. 343rd Reconnaissance Squadron (343 RS) .....................................................................2 d. RC-135V/W Rivet Joint..................................................................................................2 e. L-3 Communications ........................................................................................................3 4. SEQUENCE OF EVENTS ...................................................................................................3 a. Mission ............................................................................................................................3 b. Planning ..........................................................................................................................3 c. Preflight ...........................................................................................................................3 d. Summary of Accident .....................................................................................................4 e. Impact ..............................................................................................................................4 f. Egress and Aircrew Flight Equipment (AFE) .................................................................4 g. Search and Rescue (SAR) ...............................................................................................4 h. Recovery of Remains ......................................................................................................4 5. MAINTENANCE .................................................................................................................4 a. Forms Documentation .....................................................................................................4 b. Inspections ......................................................................................................................5 (1) Mishap Aircraft ....................................................................................................... 5 c. Maintenance Procedures .................................................................................................5 d. Maintenance Personnel and Supervision ........................................................................6 e. Fuel, Hydraulic, and Oil Inspection Analyses ................................................................6 f. Unscheduled Maintenance ...............................................................................................6 6. AIRFRAME SYSTEMS .......................................................................................................6 a. Structures and Systems ...................................................................................................6 b. Evaluation and Analysis .................................................................................................8 (1) Oxygen System: Overview ..................................................................................... 8 (2) Oxygen System: Inspection and Testing............................................................... 10 (3) Wiring and Electrical ............................................................................................ 14 7. WEATHER .........................................................................................................................15 a. Forecast Weather ...........................................................................................................15 b. Observed Weather .........................................................................................................15 c. Space Environment .......................................................................................................15 d. Operations .....................................................................................................................15 RC-135V, T/N 64-14848, 30 April 2015 i 8. CREW QUALIFICATIONS ...............................................................................................16 a. Mishap Crew .................................................................................................................16 9. MEDICAL ..........................................................................................................................17 a. Qualifications ................................................................................................................17 b. Health ............................................................................................................................17 c. Pathology.......................................................................................................................17 d. Lifestyle ........................................................................................................................17 e. Crew Rest and Crew Duty Time ...................................................................................17 10. OPERATIONS AND SUPERVISION .............................................................................18 a. Operations .....................................................................................................................18 b. Supervision ...................................................................................................................18 11. HUMAN FACTORS ........................................................................................................18 a. Introduction ...................................................................................................................18 b. Applicable Factors ........................................................................................................18 12. GOVERNING DIRECTIVES AND PUBLICATIONS ...................................................18 a. Publically Available Directives and Publications Relevant to the Mishap ...................18 b. Other Directives and Publications Relevant to the Mishap ..........................................19 c. Known or Suspected Deviations from Directives or Publications ................................19 13. ADDITIONAL AREAS OF CONCERN .........................................................................19 STATEMENT OF OPINION ....................................................................................................... 20 1. Opinion Summary ...............................................................................................................20 2. Cause ...................................................................................................................................21 3. Conclusion ..........................................................................................................................21 INDEX OF TABS ......................................................................................................................... 22 RC-135V, T/N 64-14848, 30 April 2015 ii ACRONYMS AND ABBREVIATIONS 1 Lt 25 AF 55 AMU 55 ISS First Lieutenant Twenty-Fifth Air Force 55th Aircraft Maintenance Unit 55th Intelligence Support Squadron 55 MXG 55th Maintenance Group 55 MXS 55th Maintenance Squadron 55 OG 55th Operations Group 55 WG 55th Wing 97 IS 97th Intelligence Squadron 343 RS 343rd Reconnaissance Group ACC Air Combat Command AF Air Force AFB Air Force Base AFE Air Flight Equipment AFEM Aircrew Flight Equipment Member AFI Air Force Instruction AFSEC Air Force Safety Center AIB Accident Investigation Board ATC Air Traffic Control Capt Captain CMSgt Chief Master Sergeant Col Colonel CTR Contractor DoD Department of Defense ECS Environmental Control System EOS Emergency Oxygen System EPS Emergency Power System FL Flight Lead FLCS Flight Control System FPM Feet Per Minute FPS Fire Protection System FRC Fault Reporting Codes ft Feet IASE Instructor Airborne Systems Engineer IAW In Accordance With IP Instructor Pilot IMDS Integrated Maintenance Data System KIAS kts L Lt Col MA Maj MAJCOM MAMS Knots Indicated Airspeed Knots Local Time Lieutenant Colonel Mishap Aircraft Major Major Command Mishap Airborne Mission Supervisor MASE Mishap Airborne Systems Engineer MCO Mishap Cryptologic Operator MCP Mishap Co-Pilot MFF Mishap Firefighter MHFC Mental Health Flight Commander MM Mishap Mechanic MMX Production Superintendent MN Mishap Navigator MP Mishap Pilot MR Mishap Raven MSgt Master Sergeant MTC Mishap Tactical Coordinator OG Operations Group Ops Tempo Operations Tempo OSS Operation Support Squadron PA Public Affairs PHA Physical Health Assessment PR Pre Flight PSI Pounds Per Square Inch QA Quality Assurance QT Quick Turn Inspection SIB Safety Investigation Board SrA Senior Airman SSgt Staff Sergeant TCTO Time Compliance Technical Order T/N Tail Number T.O. Technical Order TPS Technical Process Specification TSgt Technical Sergeant The above list was compiled from the Summary of Facts, the Statement of Opinion, the Index of Tabs, and Witness Testimony (Tab V). RC-135V, T/N 64-14848, 30 April 2015 iii SUMMARY OF FACTS 1. AUTHORITY AND PURPOSE a. Authority On 8 June 2015, Major General Jerry D. Harris, Jr., Vice Commander, Air Combat Command (ACC), appointed Lieutenant Colonel William M. Evans, Jr., to conduct an aircraft accident investigation of a mishap that occurred on 30 April 2015, involving an RC-135V aircraft, Tail Number (T/N) 64-14848, at Offutt Air Force Base (AFB), Nebraska (NE) (Tab Y-1). The aircraft accident investigation was conducted in accordance with Air Force Instruction (AFI) 51503, Aerospace and Ground Accident Investigations, at Offutt AFB, NE, from 12 June 2015 through 30 June 2015. Also appointed to the board were a Legal Advisor (Major), a Pilot member (Capt), a Maintenance member (Technical Sergeant), and a Recorder (Technical Sergeant) (Tabs Y-1, Y-2). b. Purpose In accordance with AFI 51-503, Aerospace and Ground Accident Investigations, this accident investigation board conducted a legal investigation to inquire into all the facts and circumstances surrounding this Air Force aerospace accident, prepare a publicly-releasable report, and obtain and preserve all available evidence for use in litigation, claims, disciplinary action, and adverse administrative action. 2. ACCIDENT SUMMARY On 30 April 2015, at approximately 1825 local time (L), the mishap aircraft (MA), an RC-135V, T/N 64-14848, assigned to the 343rd Reconnaissance Squadron (343 RS), 55th Wing (55 WG), Offutt AFB, NE, experienced a fire in the rear cabin during initial takeoff on Runway 12 at Offutt AFB, NE (Tabs N-2, CC-1, CC-2). The MA and its crew were conducting a routine training mission in support of an exercise in conjunction with Air Force Special Operations Command (Tab AA-1). The MA was traveling at approximately 45 knots when the Mishap Pilot (MP) successfully aborted takeoff. All 27 Mishap Crewmembers (MC) egressed the MA safely (Tab V-6.1). Four crewmembers received treatment for minor smoke inhalation (Tab V-6.1). The fire burned a sizable hole through the upper fuselage above the rear galley area of the MA and caused damage to aircraft structure, control systems and mission related systems (Tabs S1.11, Z-1.4, Z-1.5, Z-1.7). Repair cost to the MA is estimated at $62.4 million (Tab P-3). There were no injuries to civilians or damage to private property (Tabs P1-P3). 3. BACKGROUND The MA belonged to the 343 RS stationed at Offutt AFB, NE. The 343 RS is a squadron within the 55th Operations Group (55 OG). The 55 OG is, in turn, part of the 55 WG which is located at Offutt AFB, NE. RC-135V, T/N 64-14848, 30 April 2015 1 a. 55th Wing (55 WG) The 55 WG is Air Combat Command’s largest wing with a budget of more than $477 million annually, 49 aircraft, 32 squadrons and more than 7,000 employees. The wing conducts a global flying mission with worldwide reconnaissance and treaty verification tasked by our nation’s highest levels as well as the National Airborne Operations Center. Additionally, it provides base support to more than 50 associate units, including U.S. Strategic Command, the Air Force Weather Agency and a military community of more than 57,000. The wing is comprised of six groups, five located at Offutt AFB, NE, and one at Davis-Monthan AFB, Arizona (Tab DD-1). b. 55th Operations Group (55 OG) The 55 OG is the largest and most diverse operations group in the Air Force, flying all variants of the RC-135, OC-135, WC-135 and E-4B aircraft. The group operates these aircraft around the clock in every geographic command in support of the 55th’s global reconnaissance, contingency operations, treaty verification, National Command Authority support and command and control responsibilities. Permanent overseas operating locations include RAF Mildenhall, England, Souda Bay Naval Support Activity, Crete and Kadena Air Base (AB), Japan. The 55 OG is located at Offutt AFB, NE (Tab DD-2). c. 343rd Reconnaissance Squadron (343 RS) The mission of the 343rd Reconnaissance Squadron is to provide worldwide reconnaissance for national command authorities, Combatant Commands, the intelligence community, and war fighters. Flying the RC-135V/W Rivet Joint, the 343 RS provides near real-time on-scene intelligence collection, analysis and dissemination capabilities. The squadron supports worldwide missions of the Department of Defense to keep the United States aware of its potential adversaries (Tab DD-3). d. RC-135V/W Rivet Joint The RC-135V/W Rivet Joint reconnaissance aircraft supports theater and national level consumers with near real time on-scene intelligence collection, dissemination and analysis capabilities. The Rivet Joint is an extensively modified C-135 which contains an on-board sensor suite which allows the mission crew to detect, identify and geolocate signals throughout the electromagnetic spectrum. The mission crew can then forward gathered information in a variety of formats to a wide range of consumers via Rivet Joint's extensive RC-135V, T/N 64-14848, 30 April 2015 2 communications suite. The interior seats more than 30 people, including the cockpit crew, electronic warfare officers, intelligence operators and in-flight maintenance technicians. All Rivet Joint airframe and mission systems modifications are overseen by L-3 Communications (previously Raytheon), under the oversight of Air Force Materiel Command. (Tab DD-4). e. L-3 Communications L-3 Communications is a prime contractor in aerospace systems and national security solutions. L-3 is also a leading provider of a broad range of communication and electronic systems and products used on military and commercial platforms. L-3 Mission Integration Division is a world-class systems integration organization specializing in the complex ISR capabilities and equipment, aircraft modification and maintenance, command, control and communications, networkenabling technologies and full life-cycle systems support and sustainment (Tab DD-5). 4. SEQUENCE OF EVENTS a. Mission The mishap mission was planned and briefed to support an exercise in the southern continental United States (Tab AA-1). The MC, in conjunction with the exercise staff, planned an 8-hour mission that included air refueling and a mission orbit (Tab K-1.1). The 343 RS Commander and the squadron Operations Supervisor properly authorized the mission (Tab K-1.2). b. Planning The MC planned and conducted pre-mission briefings on the day prior to the mishap, in accordance with all applicable directives (Tabs AA-1, V-1.1, R-2.1). During the full-crew brief, the MC briefed expected and contingency mission scenarios (Tabs V-1.1, R-2.1). Additionally, the MC discussed general emergency procedures, takeoff emergencies, and egress procedures (Tabs V-1.1, R-2.1). c. Preflight On the day of the mission, the MC filed their flight plan and reviewed both weather and Notices to Airmen at the 343 RS prior to stepping to the aircraft (Tabs V-1.1, R-2.1, K-1, K-2). Takeoff emergencies were reviewed by the MC prior to engine start (Tabs V-1.1, R-2.1, K-1, K-2). As part of the preflight routine, the MC conducted an exterior and an interior inspection of the aircraft. These portions of the MC preflight were uneventful with two exceptions (Tabs V-1.1, R-2.1). The MC noted a minor issue with the lavatory located in the rear compartment (Tabs V1.1, R-2.1). The MC also noted a malfunctioning starter valve on the inboard left engine, which was rectified using a manual starter valve operation (Tabs V-1.1, R-2.1). The total delay caused by these two issues was approximately 30 minutes (Tab V-6.1). RC-135V, T/N 64-14848, 30 April 2015 3 d. Summary of Accident The MA taxied to Runway 12 without incident (Tabs V-1.1, R-2.1). The MC confirmed departure clearances and were cleared for takeoff at 18:24L (Tabs CC-2, N-2). The MP, sitting in the left seat, was planning to fly the takeoff with backup from the Mishap Co-Pilot (MCP) (Tabs V-1.1, R-2.1). The MP accomplished an engine check by increasing the engine throttles of the aircraft out of idle prior to releasing the brakes (Tabs V-1.1, R-2.1). The MP then released the brakes and passed control of the throttles to the MCP (Tabs V-1.1, R-2.1). The MCP then began to increase throttles to the planned takeoff setting which caused the aircraft to start moving down the runway (Tabs V-1.1, R-2.1). As the MA passed approximately 45 knots, multiple crewmembers in the rear compartment of the aircraft reported seeing a fire above the galley of the aircraft (Tabs R-6.1, R-8.1, R-12.1, V-2.1, V-3.1, V-4.1). e. Impact Not applicable. f. Egress and Aircrew Flight Equipment (AFE) All AFE was properly constructed, placed and inspected correctly (Tab H-4). After the radio call to the ATC tower reporting a fire, the aircraft was parked and cleared of all MC in approximately 4 minutes (Tabs CC-1, CC-2). The egress itself, from first person to the last person out of the aircraft, took approximately 2 minutes and 45 seconds (Tab CC-1). There were no egress related injuries. Four crewmembers received treatment for minor smoke inhalation (Tab V-6.1). g. Search and Rescue (SAR) Not applicable. h. Recovery of Remains Not applicable. 5. MAINTENANCE a. Forms Documentation At the time of the mishap, the MA total airframe time was 39,422.9 hours (Tab D-2.2). A review of the active AFTO 781 forms and AFTO 781 historical records for the time period 90 days preceding the mishap revealed no discrepancies indicating any electrical or oxygen system anomalies existed on the MA (Tabs D-2.1 through D-2.4, U-4). The Integrated Maintenance Data System (IMDS) historical records for 90 days prior to the mishap were used to validate and confirm all form entries (Tabs U-4, BB-2). No open Time Compliance Technical Orders (TCTOs) restricted the MA from flying (Tab D-2.4). A review of the historical records showed all TCTOs had been accomplished in accordance with applicable guidance (Tab U-4). There were no TCTO compliance issues relevant to the mishap (Tabs D-2.4, U-4). RC-135V, T/N 64-14848, 30 April 2015 4 The MA flew a 5.7 hour mission earlier on the day of the mishap (Tab D-2.2). The flight crew noted three minor discrepancies that were unrelated to the mishap (Tab D-2.3). There were no maintenance discrepancies that would have prevented the MA from accomplishing its tasked mission on 30 April 2015 (Tabs D-2.2 through D-2.4). Historical records revealed only two repeat/recur maintenance discrepancies with the MA, neither of which were related to the mishap and both were corrected prior to the date of the mishap (Tab U-4). b. Inspections (1) Mishap Aircraft Every 4 years, each RC-135 aircraft rotates through the depot facility for Programmed Depot Maintenance (PDM) (Tab BB-1). This process is an inspection and correction of defects requiring equipment and/or facilities not normally available at operating locations (Tab BB-1). The MA was delivered to Offutt AFB, NE, on 19 June 2014 after it had completed PDM (Tab U1). Isochronal inspections, also referred to as phase inspections, are regularly-scheduled maintenance inspections performed on Air Force aircraft (T.O. 1C-135-6WC-2). Isochronal inspections are conducted on RC-135 aircraft after a period of 24 months, 1,800 flying hours, or 1,000 landings, whichever comes first (T.O. 1C-135-6WC-2). The RC-135 also has a 900-hr inspection due every 900 hours or 12 months and a 60 day Hourly Post Flight (HPO) (T.O. 1C135-6WC-1, T.O. 1C-135-6WC-7). The last scheduled inspection accomplished on the MA was an HPO, which was accomplished on 23 March 2015 (Tab U-4.27). The next scheduled isochronal inspection was scheduled for 11 February 2016 (Tab D-2.4). The MA had approximately 287 days remaining before the next isochronal inspection due date (Tab D-2.4). Prior to its first flight on 30 April 2015, maintenance personnel conducted a preflight (PR) inspection on the MA (Tab D-2.2). PR inspections are accomplished prior to the first flight of the flying period and are valid for 72 hours (T.O. 1C-135-6WC-1). The preflight was signed off at 2230L on 29 April 2015 and had another 52.5 hours of validity as of the scheduled take off time for the MA (Tab D-2.2, T.O. 1C-135-6WC-1). Additionally, between flights personnel performed a QT inspection at 1500L on the day of the mishap (Tab D-2.2). This type of inspection is used when the aircraft downtime will not exceed 12 hours (T.O. 1C-135-6WC-1). The inspection was valid at the time of the mishap (Tab D-2.2). The maintenance documentation confirmed all inspections were accomplished satisfactorily in accordance with applicable maintenance directives (Tab D-2.2). c. Maintenance Procedures A review of active and historical AFTO Form 781 series aircraft maintenance forms revealed no discrepancies indicating a deviation from established maintenance procedures on the MA (Tabs D-2.1 through D-2.4, U-4). A thorough review of the active AFTO 781 forms and AFTO 781 historical records for the time period 90 days preceding the mishap revealed only minor inconsequential documentation errors; no actual maintenance deviation was identified RC-135V, T/N 64-14848, 30 April 2015 5 (Tabs D-2.1 through 2.4, U-4, BB-2). The IMDS historical records for 90 days prior to the mishap were used to validate and confirm all form entries (Tabs U-4,BB-2). Review of the AFTO 781 historical records revealed no oxygen system maintenance was accomplished or required in the area of the fire since the aircraft returned from PDM (Tab U-4). A 12-month hot gas purge of the oxygen system, which removes any residual moisture from the system, was complied with on 11 February 2015 (Tab U-4.37). Maintenance documentation indicates this task was accomplished satisfactorily in accordance with applicable maintenance directives (Tab U4.37). During PDM, L-3 Communications inspects, cleans, and reinstalls the oxygen system using documents known as Technical Process Specifications (TPS) to complete assigned tasks (Tabs U2, U-3). TPS3-100, Installation of Oxygen Systems, instructs the technician on proper alignment, initial torqueing, leak checking, and final torqueing of the oxygen system fittings (Tab U-2). According to L3 Communications’ work order number 76596949, L3 Communications personnel completed these tasks on 21 August 2013 (Tab U-3). d. Maintenance Personnel and Supervision All preflight activities were normal and all personnel involved in the preflight and launch of the MA were qualified (Tabs T-1 through T-8, V-5.1, V-9.1). Maintenance supervisors were engaged in daily maintenance activities and were actively involved in the repair and launch of aircraft (Tab V-5.1). A thorough review of individual military training records on all personnel who performed maintenance on the MA indicated maintenance personnel were trained on all assigned tasks (Tabs T-1 through T-8). e. Fuel, Hydraulic, and Oil Inspection Analyses Fuel, oil, hydraulic fluid and liquid oxygen samples were taken from the MA after the mishap. The tests revealed no abnormalities with any of the aircraft fluids (Tabs D-5.1 through D-5.4). f. Unscheduled Maintenance A review of all aircraft maintenance activities on the MA for 90 days preceding the mishap revealed no discrepancies related to the mishap (Tabs D-2.1 through D-2.4, U-1). A review of IMDS and AFTO 781 maintenance records (90 days prior to the mishap) revealed two repeat/recur Pilot Reported Discrepancies (PRD), neither of which were related to the mishap (Tab U-4). All corrective actions were completed in accordance with applicable technical data (Tabs D2.1 through D2.4, U-4). 6. AIRFRAME SYSTEMS a. Structures and Systems Damage to the MA was photographed immediately following the mishap (Tabs S-1.1 through S1.5). The aircraft sustained substantial structural damage, including fire damage to several vertical and lengthwise structural components to the fuselage known as frames and stringers. RC-135V, T/N 64-14848, 30 April 2015 6 The fire also burned a sizable hole through the aircraft skin (Tabs S-1.11, Z-1.4, Z-1.5, Z-1.7). Figure 1. Damage to Fuselage (Tabs S-1.11, Z-1.4, Z-1.5, Z-1.7) The mishap rendered a number of aircraft systems inoperable (Tab S-1.9). The MA sustained substantial damage to the oxygen system and electrical input to the rudder power control unit. An antenna located at the site of the hole in the fuselage was also damaged (Tabs S-1.2, S-1.9 through S-1.11). Portions of the crew rest area in the rear compartment and the entire aircraft galley were severely damaged (Tab S-1.3). See Figures 2 and 3. Additionally, the fire caused substantial damage to a number of aircraft mission systems (Tabs S-1.3, S-1.11). RC-135V, T/N 64-14848, 30 April 2015 7 Figure 2. Undamaged Galley Area, RC-135V/W (Tab Z-1.10) Figure 3. Galley Area of T/N 64-14848 (Tab S-1.9) b. Evaluation and Analysis (1) Oxygen System: Overview The Air Force Research Laboratory/Materials Integrity Branch (AFRL/RXSA) provided on-site and laboratory analysis of portions of the onboard oxygen system located in the galley area of the rear compartment of the MA (Tab J-6). Members of the team collected oxygen system RC-135V, T/N 64-14848, 30 April 2015 8 components and certain wiring harnesses from the galley area in order to conduct a further detailed laboratory analysis (Tab J-6). Figure 4 shows components of the oxygen system superimposed on an image of the MA. Figure 4 also has a numbering system for the junctions (also called joints or fittings) that will be used for reference in this report (Tab J-26). Prior to the mishap, Junction #5 was connected to Junction #11 via flex hose (Tab J-31). Figure 4. Oxygen System Tubing (Tab J-26). Fittings used in the oxygen system are shown in Figure 5. The T-shaped fittings may be replaced by elbow-shaped fittings as needed (Tab J-29). These fittings are commonly referred to as “AN” fittings because each fitting has a specification that begins with “AN” (Tabs J-8, J-28). These fittings consist of four components; a male threaded end, a female nut (referred to as a Bnut), a sleeve, and a flared tube. A schematic of the system shown in Figure 5 indicates that contact between the inside of the flared tube and the male fitting cone constitutes the sealing surface of the fitting (Tab J-28). The B-nut itself does not provide sealing force to the fitting (Tab J-28). When properly tightened, the B-nut and sleeve provide clamping force to the sealing surface between the flared tube and the male fitting cone (Tab J-28). RC-135V, T/N 64-14848, 30 April 2015 9 Figure 5. Oxygen System Fittings (Tab J-28). Tightening (or torqueing) “AN” fittings to the proper specification requires initial torqueing, leak checking and final torqueing (Tab U-2.15). Initial torqueing is a two-step process which involves hand tightening the B-nut (in accordance with the schematic in Figure 5) to ensure proper alignment and a firm seal between the male cone fitting and the flared tube, and then torqueing the B-nut using a torque wrench to an initial minimum torque value (Tabs U-2.15, V-11.1). The initial minimum torque value for 5/16 inch aluminum tubing used in the MA is 100 inch-pounds (in-lbs) (Tabs U-2.16, J-9, J-30). Leak checking involves pressurizing the oxygen system to operational specifications while examining all fittings and connections using a leak test compound (Tab U-2.17). Final torqueing is required if any leaks occur and involves increasing the torque value as necessary to stop the leak, up to a maximum specified torque value (Tab U-2.15). The maximum torque value for 5/16 inch aluminum tubing used in the MA is 125 in-lbs (Tabs U-2.16, J-9, J-30). Replacement or repair is necessary if leakage cannot be stopped at the maximum torque value (Tab U-2.15). (2) Oxygen System: Inspection and Testing Inspection of the fittings removed from the MA revealed that the B-nuts at Junction #4, Junction #5 and Junction #11 were all finger tight (Tab J-9). Inspection of the oxygen system tubing also RC-135V, T/N 64-14848, 30 April 2015 10 revealed there was no B-nut on the other side of Junction #11 (Tab J-8). A fragment of the missing B-nut was discovered in the debris (Tab J-8). Analysis of the fragment indicated that the B-nut had melted (Tabs J-8, J-29). There was no evidence that the B-nut had forcibly passed over either the sleeve or the flared end of the corresponding tube (Tab J-8). Figure 6 shows the male threaded end of the elbow fitting where the B-nut at Junction #11 should have been located (on the right side of the elbow) (Tab J-29). Upon disassembly of the fitting, difference in colors of the threads between the protected side (left) of the elbow fitting and the missing B-nut side (right) indicate that the left side was exposed to some combustion products (such as soot), but not as much as the missing B-nut side (Tab J-29). Figure 6. Elbow Fitting (Tab J-29). Further examination of the tubing system showed the inner liner of the flex hose between Junction #11 and Junction #5 was destroyed (Tab J-8). See Figure 7. Light passing through the flex hose indicates the inner tubing is completely destroyed near Junction #5 (Tab J-31). Images of the flex hose near Junction #11 shows rumpling deformation on the inner tube, indicating exposure to heat (Tab J-31). Figure 7. Flex Hose Between Junction #5 (Left) and Junction #11 (Right) (Tab J-31). Examination of the flared ends of the tubes for each fitting indicated they all had a circular contact impression from the sleeve, through the tube coating to the base metal, except the flare at Junction #11 (also referred to as Tube #11) (Tabs J-10, J-35). See Figure 8. While the torque value at Junction #11 could not be measured due to the melted B-nut, the lack of a contact scar on Tube #11 indicates it had the lowest torque value of all the fittings examined (Tabs J-10, J-12, J- RC-135V, T/N 64-14848, 30 April 2015 11 35) . Figure 8. Flared Tube Ends (Tab J-35). Additionally, the sleeve located at Junction #11 had significant pitting (i.e, tiny holes or “pits”) on one side (Tab J-10). The pitting on this sleeve indicates the damage was directional, since it was present on one side and not the other (Tab J-10). Pitting was also found more frequently on one side of the corresponding Tube #11, just past the area the sleeve covered (Tabs J-10, J-38). No pitting damage was found beneath the sleeve (Tab J-10). The damaged B-nut fragment also had localized melting, which is consistent with damage on one side of the tube, starting at the shoulder of the B-nut (Tab J-11). Physical evidence indicates the area of high heat was localized, causing damage predominantly to one side of the sleeve and Tube #11 (Tabs J-11, J-35). The location of Tube #11 prior to removal from the MA is shown in Figure 9 (Tabs J-26, S-1.9, Z-1.1 through 1.3). Figure 11. Location of Tube #11 Prior to Removal (Tabs J-26, S-1.9, Z-1.1 through 1.3). AFRL/RXSA also pressure tested the oxygen system in segments using compressed nitrogen at RC-135V, T/N 64-14848, 30 April 2015 12 normal operating pressures up to 300 pounds per square inch (PSI) in conjunction with a foaming leak detectant (Tab J-9). In order to test each fitting, the damaged flex hose (between Junction #5 and Junction #11) was replaced using the flex hose connected to Junction #1 (which was undamaged in the fire), after Junction #1 had been pressure tested (Tab J-9). As stated above, Junction #4, Junction #5 and Junction #11 were found to be finger tight during initial inspection, therefore these fittings were pressure tested finger tight (Tab J-9). In the case of Junction #11, the missing B-nut (from the other side of the elbow joint) was replaced with the B-nut from Junction #2 and tested finger tight (Tab J-9). The oxygen system leaked at 20 PSI from Junction #4 and Junction #11 (Tab J-9). The B-nut at Junction #4 was then tightened 1/10th of a turn, but still leaked at 50 PSI (Tab J-9). Except for Junction #4 and Junction #11, all other areas of the tubing system held 300 PSI with no leaks detected (Tab J-9). Following pressure testing, the tubing system was disassembled and the individual components examined (Tab J-9). The torque required to loosen each nut is known as breakaway torque (Tab J-9). Laboratory testing and analysis indicated that tightening torque was approximately 40 in-lbs higher than breakaway torque (Tab J-9). Therefore, adding 40 in-lbs to the measured breakaway torque values for each B-nut will indicate their approximate tightening torque values (Tab J-9). See Figure 9. Nut Number Breakaway Torque, in-lbs Estimated Tightening Torque, in-lbs 1 2 3 4 5 6 7 8 9 10 150 40 20 50 30 30 50 60 40 130 190 80 60 90 70 70 90 100 80 170 Figure 9. Measured and Estimated Torque Values (Tabs J-9 and J-39). Figure 9 indicates that only Junction #8 meets the minimum/maximum torque requirements of 100/125 in-lbs (Tabs J-9, J-39). Additionally, only Junctions #1 and #10 had breakaway torques over 100 in-lbs (Tabs J-9, J-39). As stated above, all fittings except Junctions #4 and #11 held 300 PSI prior to disassembly, notwithstanding the low estimated tightening torque values noted in Figure 5 (Tab J-9). The lack of leaking on B-nuts with very low torque values indicates that the difference between a leaking and non-leaking fitting is very small (Tab J-12). The laboratory experiments indicated that a slight rotation of the fitting can cause a large change in the leaking pressure (Tab J-12). RC-135V, T/N 64-14848, 30 April 2015 13 AFRL/RXSA also determined that the T-shaped fitting connecting Junctions #4, #5 and #6 (4/5/6 fitting) lacked required letter markings and appeared to have a parting line and a rough surface (Tab J-10). See Figure 10. Parting lines and rough surfaces are both typical of a casting, whereas a machined or forged part is required by the specifications (Tab J-10). The 4/5/6 fitting also showed uneven wear patterns, nicks, gouges, and large areas of exposed metal which would also be cause for rejection of the fitting (Tab J-10). AFRL/RXSA determined that fittings similar to the 4/5/6 fitting were last manufactured in 2003 (Tabs J-10, J-34). Figure 10. T-Shaped Fittings. Red circle indicates a correct marking (Tab J-34). (3) Wiring and Electrical Visual inspection of the damaged aircraft showed the fire damage was intense and well-focused in a specific area of the rear compartment near the galley (Tab J-6). The interior area with the most severe wire damage coincided with a large hole in the fuselage (Tab J-6). Electrical system components in the direct proximity of the fire-damaged region were severely compromised (Tab J-6). Portions of cables and wiring harnesses in this area completely lacked insulation and showed signs of having partially melted (Tab J-6). AFRL/RXSA removed portions of cables and wiring harnesses for further analysis (Tab J-6). The galley contained two refrigerators, microwave oven, convection oven, lighting, and receptacles for up to four separate beverage jugs, along with the galley control panel (Tabs J-6, J17). The electrical connections immediately behind the galley control panel were blackened due to smoke, but showed no evidence of arcing or insulation failure (Tab J-7). The wires associated with the beverage jugs were heavily damaged, but only in the region directly under the hole in the fuselage (Tab J-7). The wires associated with the microwave and convection ovens were blackened due to smoke, but showed no evidence of arcing or insulation failure (Tabs J-7, J-23). The beverage jugs and light switches were all found in the off position (Tabs J-7, J-17). RC-135V, T/N 64-14848, 30 April 2015 14 AFRL/RXSA examined two wire harnesses supplying power to the microwave and convection ovens within the galley (Tabs J-7, J-23). Both harnesses exhibited little damage; insulation was intact and only displayed slight discoloration in areas that would have been exposed to the fire as it was burning (Tabs J-7, J-23). A 3-foot section of coaxial cable removed from the MA was also analyzed (Tabs J-7, J-24). The outer shield and visible inner conductor displayed no visual evidence of electrical arcing (Tabs J-7, J-24). AFRL/RXSA also examined an 8-foot section of a wire harness that runs along the roof of the fuselage above the galley (Tab J-7). Overall, the harness showed exposure to a wide temperature range, with each end showing little to no heat damage, and the middle showing severe damage (Tabs J-7, J-18). Testing of the wires indicated exposure to temperatures greater than 450° Celsius for an extended period (Tabs J-7, J-18, J-19). Numerous wires had molten copper ends (Tabs J-7, J-19). Cross-sectioned samples of these ends contained voids (i.e., tiny holes), which are indicators of electrical arcing, as well as a structured grain pattern or morphology, which occurs from extended exposure to a high temperature environment (Tabs J-7, J-19). An analysis of the relatively undamaged ends of the 8-foot wire harness indicated no evidence of arcing, continuous overcurrent, or degradation to the insulation (Tab J-7). Although evidence of electrical arcs was present within the large wire bundle, many electrical lines were powered for some period after the fire occurred (Tabs J-7, J-13). It is likely that the highly localized flame removed the insulation from the wires very quickly, while power was still feeding the wires, and the wires in the bundle were then able to freely arc to each other (Tab J-13). 7. WEATHER a. Forecast Weather Weather at Offutt AFB, NE, was forecast for winds from 150 degrees (out of the southeast) at 06 knots, with few clouds at 25,000 feet (Tab F-1). Temperature was forecast to be +23 degrees Celsius with 7 miles visibility (Tab F-1). b. Observed Weather Reported weather at the time of the mishap was winds from 120 degrees (out of the southeast) at 05 knots with clear skies, a temperature of +22 degrees Celsius and visibility of 10 miles (Tab F-2). The ATC tower at Offutt AFB, NE, passed current runway winds to the MC as calm (Tab N-2). c. Space Environment Not applicable. d. Operations Weather was well within operational limits. There is no evidence to suggest that weather was a factor in this mishap. RC-135V, T/N 64-14848, 30 April 2015 15 8. CREW QUALIFICATIONS a. Mishap Crew The MC was current and qualified for this mission (Tabs G-1.1 through G-1.12, G-2.1 through G-2.12). A review of the 30/60/90 day look-back, flight evaluation folders, and training records for all members of the MC revealed no deficiencies related to the mishap (Tabs G-1.1 through G-1.12, G-2.1 through G-2.12). The MP was a qualified Aircraft Commander (Tab G-1.1). The mishap flight was to be his first sortie as Aircraft Commander following an initial qualification checkride on 2 April 2015 (Tab G-1.1). He had a total of 1108.7 hours, with 834.6 hours in the RC-135V/W (Tab G1.1.2). His recent flight time was as follows on the day of the mishap (Tab G-1.1.3): Hours 5.5 42.9 42.9 Last 30 Days Last 60 Days Last 90 Days Sorties 1 7 7 The MCP was a qualified and experienced Mission Copilot (Tab G-1.2). He had a total of 902.3 hours, with 660.3 hours in the RC-135V/W (Tab G-1.2.2). His recent flight time was as follows on the day of the mishap (Tab G-1.2.3): Hours 0 33.4 43.2 Last 30 Days Last 60 Days Last 90 Days Sorties 0 5 7 The MN was a qualified and experienced Mission Navigator (Tab G-1.3). He had a total of 1918.1 hours, with 1845.5 hours in the RC-135V/W (Tab G-1.3.2). His recent flight time was as follows on the day of the mishap (Tab G-1.3.3): Hours 11.5 16.7 16.7 Last 30 Days Last 60 Days Last 90 Days Sorties 3 4 4 The MTC was a qualified and experienced Instructor and Evaluator Electronic Warfare Officer (Tab G-1.5). He had a total of 2036.6 hours, with 1994.0 hours in the RC-135V/W and 259.2 hours as an Instructor (Tab G-1.5.2). His recent flight time was as follows on the day of the mishap (Tab G-1.5.3): RC-135V, T/N 64-14848, 30 April 2015 16 Hours 0 0 7.5 Last 30 Days Last 60 Days Last 90 Days Sorties 0 0 1 The MAMS was a qualified and experienced Instructor and Evaluator Airborne Mission Supervisor. He had a total of 2100.7 hours, all in the RC-135V/W, with 120.8 hours as an Instructor (Tab G-1.7.2). His recent flight time was as follows on the day of the mishap (Tab G-1.7.3): Hours 6.8 35.1 59.9 Last 30 Days Last 60 Days Last 90 Days Sorties 1 5 9 9. MEDICAL a. Qualifications At the time of the mishap, the MC was fully medically qualified for flight duty without medical restrictions or waivers (Tab AA-2). b. Health Th e medical records for the MC, as well as their 72-hour histories were reviewed (Tabs R1 through R-12). Medical records revealed all individuals were in good health and had no recent performance-limiting illnesses prior to the mishap. All members of the MC had current physical health assessments (Tab AA-3). No relevant medical information was noted in the medical records. Four crewmembers were treated for minor injuries related to smoke inhalation. None of these individuals required further treatment after initial treatment on the day of the mishap (Tab AA-3). c. Pathology Not applicable. d. Lifestyle There is no evidence to suggest lifestyle factors were a factor in the mishap. e. Crew Rest and Crew Duty Time Air Force Instructions require flight crew to have proper crew rest, as defined in AFI 11-202, Volume 3, General Flight Rules, 07 November 2014, prior to performing in-flight duties. Crew rest is compulsory for aircrew members prior to performing any duties involving aircraft RC-135V, T/N 64-14848, 30 April 2015 17 operations and is a minimum of 12 non-duty hours before the Flight Duty Period begins. Crew rest is free time and includes time for meals, transportation, and rest. This time must include an opportunity for at least 8 hours of uninterrupted sleep. Crew rest period cannot begin until after the completion of official duties. A review of the duty cycles of the MC leading up to the mishap indicated they all had adequate crew rest (Tabs G-1.1 through G-1.12, R-1 through R-12). The MC was near the beginning of their 16-hour duty day when this incident occurred (Tab V-6.1). 10. OPERATIONS AND SUPERVISION a. Operations None of the MC reported an elevated operations tempo (i.e. more than ten flights per month) leading up to the mishap or that operations tempo was negatively affecting their ability to accomplish the mission (Tabs G-1.1 through G-1.12, R-1 through R-12). There is no evidence to suggest that operations tempo was a factor in this mishap. b. Supervision The 343 RS reviewed and approved the mishap sortie (Tabs K-1.3, AA-1). There is no evidence to suggest that 343 RS supervision was a factor in this mishap. 11. HUMAN FACTORS a. Introduction AFI 91-204, Safety Investigations and Reports, 24 September 2008, Attachment 5, contains the Department of Defense Human Factors Analysis and Classification System, which lists potential human factors that can play a role in any mishap. Human factors consider how people’s tools, tasks and working environment systematically influence human performance. b. Applicable Factors There is no evidence that human factors contributed to this mishap. 12. GOVERNING DIRECTIVES AND PUBLICATIONS a. Publically Available Directives and Publications Relevant to the Mishap (1) (2) (3) Air Force Instruction 11-202, Volume 3, General Flight Rules, 7 November 2014 Air Force Instruction 11-2RC-135, Volume 3, RC/OC/WC/TC-135 Operations Procedures, 22 April 2010 Air Force Instruction 21-101, Aircraft and Equipment Maintenance Management, 21 May 2015 RC-135V, T/N 64-14848, 30 April 2015 18 (4) Air Force Instruction 51-503, Aerospace and Ground Accident Investigations, 14 April 2015 (5) Air Force Instruction 91-204, Safety Investigations and Reports, 12 February 2014 NOTICE: All directives and publications listed above are available digitally on the Air Force Departmental Publishing Office website at: b. Other Directives and Publications Relevant to the Mishap (1) TO. 00-25-4, Depot Maintenance of Aerospace Vehicles and Training Equipment, 15 January 2012 (2) TD. 00-20-1, Aerospace Equipment Maintenance Inspection, Documentation, Policies, and Procedures, 15 June 2013 (3) TPS3-100, Installation of Oxygen Systems (L-3 Communications), 22 May 2014 The following T.O.s are not publically available and are subject to the Arms Export Control Act of 1976. (4) TO. 1C-135-6WC-1, Pre?ight/Postflight/Hourly Post-F light Inspection Workcards, 9 January 2015 (5) TD. Periodic Inspection Workcards, 15 June 2015 (6) TO. Hourly Inspection Workcards, 15 June 2015 c. Known or Suspected Deviations from Directives or Publications Evidence indicates that L-3 Communications maintenance personnel deviated from TPS3-100, Installation of Oxygen Systems, dated 22 May 2014, by failing to tighten the B-nuts located at Junction Junction #5 and Junction #11 properly as required by paragraphs 3.5 through 3.5.2 and Table II of that publication (Tab U-2). 13. ADDITIONAL AREAS OF CONCERN Not applicable. 30 June 2015 WILLIAM M. EVANS, Jr, Lt Col, USAF President, Accident Investigation Board RC-I 35 V, 64-14848, 30 April 2015 19 STATEMENT OF OPINION RC-135V, T/N 64-14848 OFFUTT AIR FORCE BASE, NEBRASKA 30 APRIL 2015 Under 10 U.S.C. § 2254(d) the opinion of the accident investigator as to the cause of, or the factors contributing to, the accident set forth in the accident investigation report, if any, may not be considered as evidence in any civil or criminal proceeding arising from the accident, nor may such information be considered an admission of liability of the United States or by any person referred to in those conclusions or statements. 1. OPINION SUMMARY On 30 April 2015, at approximately 1825 local time (L), the mishap aircraft (MA), an RC-135V, Tail Number 64-14848, assigned to the 343rd Reconnaissance Squadron, 55th Wing, Offutt Air Force Base (AFB), Nebraska (NE), experienced a fire in the rear cabin during initial takeoff. The MA and its crew were conducting a routine training mission in support of an Air Force Special Operations Command exercise. The Mishap Crewmembers (MC) consisted of cockpit crew, electronic warfare officers, intelligence operators and in-flight maintenance technicians. The Mishap Pilot (MP) aborted the takeoff, and all 27 MC safely evacuated the MA. Four crewmembers received treatment for minor smoke inhalation. Fire crews arrived at approximately 1829L and extinguished the flames. The fire burned hole through the upper fuselage above the rear galley area of the MA, causing structural damage and damage to aircraft control and mission related systems. Repair cost to the MA is estimated at $62.4 million. There were no injuries to civilians or damage to private property. I find by preponderance of the evidence that the cause of the mishap was a leak in the highpressure oxygen system due to poor assembling of the system tubing at depot maintenance. Failure by L-3 Communications depot maintenance personnel to tighten a retaining nut connecting a metal oxygen tube to a junction fitting above the galley properly caused an oxygen leak. This created a highly flammable oxygen-rich environment that ignited. The resulting fire melted the retaining nut causing the tubing to become detached from the junction fitting, feeding more oxygen to the fire, increasing its size, and causing severe damage to the airframe, galley, and mission equipment onboard the aircraft. I developed my opinion by analyzing factual data from witness testimony and information provided by subject matter experts to include technical reviews, engineering and laboratory testing, and analysis of post-mishap aircraft components. RC-135V, T/N 64-14848, 30 April 2015 20 2. CAUSE The cause of the mishap was the failure of depot maintenance personnel to assemble the oxygen system properly, specifically the high-pressure oxygen hose connection above the galley of the MA. The improper assembly of tubing system caused an oxygen leak. This leak created a highly ?ammable oxygen?rich environment that ignited. The lack of a contact scar on the ?ared tube end of the connection above the galley and the improper torque values on other undamaged high-pressure oxygen system tubing connections in the MA, as tested by the Air Force Research Laboratory/Materials Integrity Branch, support the conclusion that the B-nut on the connection above the galley was torqued insufficiently. The work order indicates that the oxygen hose and oxygen tube assemblies were installed at programmed depot maintenance. There is no evidence that would indicate that any disassembly, reassembly, or adjustments were made to the high?pressure oxygen system tubing at the location of the fire after the mishap aircraft was delivered from programmed depot maintenance. In addition, I found no evidence that the MC caused, could have prevented, or substantially contributed to the damage to the MA. 3. CONCLUSION I find by preponderance of the evidence that the cause of the mishap was a leak in the high- pressure oxygen system due to poor assembling of the system tubing at depot maintenance. Failure by depot maintenance personnel to tighten a retaining nut connecting a metal oxygen tube to a junction fitting above the galley properly caused an oxygen leak. This leak created a highly ?ammable oxygen-rich environment that ignited. The resulting fire melted the retaining nut causing the tubing to become detached from the junction fitting, feeding more oxygen to the fire, increasing its size, and causing severe damage to the airframe, galley, and mission equipment onboard the aircraft. 30 June 2015 WILLIAM M. EVANS, Jr, Lt Col, USAF President, Accident Investigation Board V, 64-14848, 30 April 2015 21 INDEX OF TABS DISTRIBUTION MEMORANDUM AND SAFETY INVESTIGATOR INFORMATION ....... A NOT USED ..................................................................................................................................... B NOT USED .................................................................................................................................... C MAINTENANCE REPORT, RECORDS, AND DATA............................................................... D NOT USED ..................................................................................................................................... E WEATHER AND ENVIRONMENTAL RECORDS AND DATA .............................................. F PERSONNEL RECORDS ............................................................................................................. G EGRESS, IMPACT, AND CRASWORTHY ANALYSIS ........................................................... H DEFICIENCY REPORTS ............................................................................................................... I RELEASABLE TECHNICAL REPORTS AND ENGINEERING EVALUATIONS ................... J MISSION RECORDS AND DATA .............................................................................................. K DATA FROM ON-BOARD RECORDERS .................................................................................. L DATA FROM GROUND RADAR AND OTHER SOURCES .................................................... M TRANSCRIPTS OF VOICE COMMUNICATIONS ................................................................... N ANY ADDITIONAL SUBSTANTIATING DATA AND REPORTS ......................................... O DAMAGE AND INJURY SUMMARIES ..................................................................................... P AIB TRANSFER DOCUMENTS ................................................................................................. Q RELEASABLE WITNESS TESTIMONY..................................................................................... R RELEASABLE PHOTOGRAPHS, VIDEOS, AND DIAGRAMS ............................................... S INDIVIDUAL FLIGHT RECORDS AND ORDERS, NOT INCLUDED IN TAB G .................. T AIRCRAFT MAINTENANCE RECORDS, NOT INCLUDED IN TAB D ................................ U WITNESS TESTIMONY AND STATEMENTS ......................................................................... V RC-135V, T/N 64-14848, 30 April 2015 22 NOT USED ...................................................................................................................................W NOT USED .................................................................................................................................... X DOCUMENTS APPOINTING THE AIB MEMBERS ................................................................ Y PHOTGRAPHS, VIDEOS, DIAGRAMS, NOT INCLUDED IN TAB S ..................................... Z FLIGHT DOCUMENTS .............................................................................................................AA GOVERNMENT DOCUMENTS AND REGULATIONS ......................................................... BB MEMORANDA FOR RECORD ................................................................................................. CC FACT SHEETS ............................................................................................................................DD RC-135V, T/N 64-14848, 30 April 2015 23 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB A SAFETY INVESTIGATOR INFORMATION A1. ORDERS APPOINTING SIB .............................................................................................. 2 A1.1. AMMENDED ORDERS APPOINTING SIB ............................................................. 3 A1.2. WAIVER FOR HOME STATION PM AND MM ..................................................... 4 A2. CONTACT INFORMATION FOR SIB MEMBERS AND ADVISORS ........................ 5 A3. MEMORANDUM DOCUMENTING GUIDANCE TO INVESTIGATORS ON CONTROLLING INFORMATION ........................................................................................... 6 A4. NON-DISCLOSURE AGREEMENTS OF SIB ADVISORS ........................................... 8 A-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK A-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 A1. ORDERS APPOINTING SIB DEPARTMENT OF THE AIR FORCE HEADQUARTERS me COMBAT COMMAND JOWT BASE LANGLEY VA SPECIAL ORDER: F1540 5 May 15 Pursuant to AFI 91-204, and IAW authority to convene aircraft safety investigations under that instruction, ACC appoints the following individuals. organization indicated, as Safety Investigation Board members to investigate the Class A aircraft mishap involving a RC-135V, tail number 64-4848. Offutt AFB. NE which occurred on 30 April 2015. The Board will determine the cause(s) of this mishap and make recommendations to prevent recurrence. The Board will produce a formal mishap report as prescribed by AFI 91-204 and a ?nal AFSAS message as approved by HQ ACC and AFSCISEF. Board duties imposed on these individuals take precedence until the investigation is complete. The investigation is complete when COMACC releases the Board; Primary Board Members: Board President Col 25 AFIOC Lackiand AFB, TX Pilot Member Capt 82 ATRSIDO Offutt AFB, NE investigating Officer: Capt 552 ACWISE Tinker AFB. OK Maintenance Member: Lt Col 55 MXGICD Offutt AFB, NE Medical Member: Capt 99 Beale AFB, CA AFE Member 55 OSSIOSL Offutt AFB, NE Non-Primary Board Members: AFSEC Representative: Kirtland NM Recorder Capt 338 Offutt AFB, NE FOP THF RHMMAMHFR Colg?f, Director of Safety r2594}: Pawn?: RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 A1.1. AMMENDED ORDERS APPOINTING SIB A-4 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 A1.2. WAIVER FOR HOME STATION PM AND MM A-5 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 A2. CONTACT INFORMATION FOR SIB MEMBERS AND ADVISORS SIB ROLE NAME President Col Safety Center Rep CMSgt Investigating Officer Capt Medical Member Capt Pilot Member Capt Maintenance Member Lt Col AFE Member CONTACT INFORMATION SMSgt Recorder Capt Air Force Research Laboratory Advisor Mr. Air Force Research Laboratory Advisor Mr. Air Force Research Laboratory Advisor Mr. Air Force Research Laboratory Advisor Mr. A-6 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 A3. MEMORANDUM DOCUMENTING GUIDANCE TO INVESTIGATORS ON CONTROLLING INFORMATION A-7 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 I USAF Capt, usm AFSEC Representative SIB Record?r A-8 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 A4. NON-DISCLOSURE AGREEMENTS OF SIB ADVISORS A-9 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAFETY INVESTIGATION NON-DISCLOSURE it we; 20g are) l. Protoc?onofprivileged safety information acquired during safegr imrestigationa ofAirForoe mishapaia importantinorderto prevent?miremiahaps. I am performing services insupporl of an Air Force safety hiveatiga?on. Safety Investigation Non-Disclosure Agreemt 2. As a result I have to privileged safety information. Access is solely' for the pm-poae of mishap prevention and no other use of safety privileged information by me or my sponsoring organization [company or military organization) is authorized access to this information. I tmderaland Iamnotto make topics (typed, photo, eteJofany information or disseminate any information to anyone or organization not directly providing aendees to the safety investigation. I am expressly prohibited from providing any priw?leged safety investigation infonnation to my general counsel's o?ice. legal staff; or any personnel involved in litigation. 3. Iamrequiredtoreturnitto AdrForee safetyehannela. Retaining eopieaisnot authorized. 1 amnotto discuss privileged safety infonnationwith anyone other than personnel directly involvedwiththe Air Force safety 4. through inwatigationia considered of?cialAir Force information. 5. Prior oud'?anWrode Tumour-e Block RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAFETY INVESTIGATION NON-DISCLOSURE AGREEMENT Safety Investigation Non-Disclosure Agreement 5 2 my mate) 1. Protection of privileged safety information acquired during safety investigations of Air Force an Air Force safety investigation. 2. As a result I have aeoess to privileged safer information. Access is solely for the purpose of mishap prevention and no other use ofsafety lnivileged infonnation hyme or my sponsoring organization {oompany or ndlitery organization) is authorized access to this information. I understand 1 am not to make oopies (typed, photo, etc.) of any information or disseminate any infonnation to anyone or organization not providing services to the safety I am expressly prohibited from providing any privileged safety investigation infonnation to my general ootmsel's of?ce, 1ega1 staff, or any ptnsonnel involved in litigation 3. After] am finiahedwith any infonnationprovidedon any media] arnrequiredto return itto Air Force safety channels. Retaining copies is not authorized. I am not to disouss privileged safety information with anyone other than personnel directly involved with the Air Fares safety investigation. 4. I understand that information obtained through a. safety investigation is considered o?eial Air Foroe information. 5. Iunderstandtheahove termsand agreeto abide hythe conditions setfor?i, Prior FuuNm and?mb?t?i?mde? Implant-e Block A-ll RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAFETY INVESTIGATION NON -DISCLOSURE AGREEMENT Safety loves tie Non-Dis 1 re 1: corn Agreemon 8 it"; will!) 1. Protection of privileged safety information acquired dining safety inVeatigations ofAir Force mishaps is I am performing senicesin mmport of an Air Force safety investigation. 2. As a result I have necess to privileged safety information. Access is solely for the purpose of mishapprevention and no other use ofsafetypriy?eged infonnation by me or my sponsoring organization [eompany or military organization} is authorized access to this infonnation. I understand I am not to make copies (typed, photo. etc.) of any information or disseminate any infonnation to anyone or organization not directly providing senrices to the safety investigation. I am exp-ash prohibited from providing any privileged safety invastiga?m information to my general counsel?s of?ce, legal staff, or any personnel involved in litigation. 3. A?erlarn?nishedwith any itto Air Force auteur channels. Retaining eopies is not amhon'zed. I am not to discuss privileged safety io?arma?on with anyone other than personnel directly involved with the Air Force safety investigation. 4. I understand that information obtained through a safety investigation is considered of?cial Air Force information. 5. 02. Print FWle and Rmb?Grnde A-12 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB THIS TAB NOT USED B-l RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK B-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB THIS TAB NOT USED C-l RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK C-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB D MAINTENANCE REPORT, RECORDS, AND DATA D1. AIRCRAFT MAINTENANCE AND MATERIEL REPORT, AF FORM 711C ........... 2 D2. AIRCRAFT AFTO 781 FORMS ......................................................................................... 3 D2.1. AFTO FORM 781F, FLIGHT AND MAINTENANCE REPORT ........................... 3 D2.2. AFTO FORM 781H, FLIGHT AND MAINTENANCE STATUS............................ 5 D2.3. AFTO FORM 781A, DISCREPANCY AND WORK DOCUMENT ........................ 7 D2.4. AFTO FORM 781K, TCTOs AND DELAYED DISCREPANCIES ...................... 17 D2.5. AFTO 781A PULLED FORMS .................................................................................. 22 D2.5.1. AFTO 781A PULLED FORMS, 20150428 – 20150430....................................... 22 D2.5.2. AFTO 781A PULLED FORMS, 20150424 - 20150428 ....................................... 23 D2.5.3. AFTO 781A PULLED FORMS, 20150423 - 20150424 ....................................... 23 D2.5.4. AFTO 781A PULLED FORMS, 20150419........................................................... 24 D2.5.5. AFTO 781A PULLED FORMS, 20150411 - 20150414 ....................................... 25 D2.5.6. AFTO 781A PULLED FORMS, 20150407........................................................... 26 D2.6. MAINTENANCE SNAPSHOT INQUIRY, 900-HR INSPECTION ...................... 27 D3. RC-135 LOX WAIVER LETTER ..................................................................................... 34 D4. MAINTENANCE RECORDS FROM OTHER INVOLVED EQUIPMENT............... 35 D4.1. AFTO FORM 134, BREATHING OXYGEN SERVICING TRAILER LOGS .... 35 D5. FLUID SAMPLE TESTING .............................................................................................. 47 D5.1. TURBINE FUEL SAMPLES ...................................................................................... 47 D5.2. HYDRAULIC FLUID SAMPLES.............................................................................. 61 D5.3. OXYGEN SAMPLES .................................................................................................. 64 D5.4. LUBRICATING OIL SAMPLES ............................................................................... 66 D-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK D-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 D1. AIRCRAFT MAINTENANCE AND MATERIEL REPORT, AF FORM 711C D-3 64?14848, Class A, 30 April 15, AFSAS #739726 D2. AIRCRAFT AFIO 781 FORMS AF TO FORM 781F, FLIGHT AND MAINTENANCE REPORT 1. Doc 2. ASST use 556THRU *6 MIN 4 HR 46 THRU 51 MIN .a HR 3 THRU 8 MIN 1 HR 27 THRU :3 MIN 3 .5 HR 52 THRU 57 MIN HR 9THRU14MIN TABLE 15 THRU 20 MIN 3 HR 40 THRU @4600 1C 64-14848 . ANIZATION CATION STANBIFCODE 6811: KOTT PREVIOUS EDITION IS OBSOLETE D-4 A REPORT AND MAINTENANCE RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INSTRUCTIONS FOR FORM 781 AIRBORNE STUDENT ma mama FF - First Pilot 5P - Student Filol LL - 599? 0? Hm rp -1ngtrucrgr 9.er {err First Pilot in MulIr-Enuine Fit. - Right Saa! Landing on Hard Surfaca TE . Tough and Ga Landing on Hard cc - Command Pilot 5G surface Touch and an Landing at on AC - PIIOI Ham Sumo; RP Rad? Elm? ?It? LN - Lari Seat Landing at Night on Hard DP Print systems Operator Surface EP Flint Evaluator an . 3mm RN Flight Seat Landing at Night on Hart: E?luatur A0 - Assistant adorn Dparatdt sum? FM . Fug?! Mechanic FL - Front Seat. Landing an Hard Surface HM Ha? "3r ?Bahama 3L Badt Seat Landing an Hard Surface FN - Fran Seat Landing at Night on Hard FE - Flight Engineer Surface En Inear . New. am, 5E Mums 9' an: . Back Seat at Night an Hard - it: - Intaroapt Conn-allar Sum? 38 - :Ivavi?atoga?:nl::r::ur CS - System Operator Lw Le? Sam Wall}, ummg - swan. its so . Planar operator Rw - Right Seat Wamr Landing NE Warfare Of?cer E0 EGM 0mm? La? seal Water Landing {Night} IN - lnatructu-r Navigator FM, Aim? and Wammg apemmns WEI night 5331 Water Landing {nght?r ID - Instruntor Navigator TR Tow operamr 33 Ski Landing 11 - Instructor waa on Systems Of?cer 7 . AP ?we? JUMP common amst lE instructor Electronic Warfare WR Weather Reconnaissance AN - Auxiliary Natdgabri?bseruer as A Pamrescua Man - Tacllral cur Operational cg - command LM Lnadmasm Tactical or Oparatr? anal EU Systems Evaluator FT In?igl?rl Pals aangar Specially: :g?tgmwa Fl-l - Fright Nurse - Night MT - Medical Technician Wang,? AG - Mrlal Gunner all positions Full Equipment FLIGHT BURGEDN ,rra - ?mm game Staff 3w E5 - Ejatrrion Seat IS InauucinrrExamInar oxygen pmmr? F5 - Surgeon I 1 - Free Fall l0 - um natrun para or Opnm?nna] arm? FF - Fire?ghter Fl - Nat-aid Flt, Insp. Tann. A5 . Airborne Support - Parachutiat ?.Jumpmaa'tar - Student Parachutlat IHDIVIDUAL FLIGHT CHECKS (For use in Sumatra E, Form 731} PM: Navryardrriobsarwr Non Hamid PP quali?ca?nn DP - Quali?cation GP - Instrument YP Instrument CREDIT CODES FOR USE IN COLUMN U, 0F AFTCI ?ll - LEAVE STATUS NOT BREDITABLE FOR PROFICIENCY - NDT CREDITABLE FDR PAY OR PROFICIENCY EIHULATDFI DR TRAINER REMARKS GENERAL TD. Dir-2&5. Sadtion Ill Is the praacribing directive for tha preparation of AFTO Form T51. Columnar haadlnga clarify each talent: to be filled in. The abdua ?ying duty symbols reflect the authorized codes to be used. A line entry will be ?lled in for each type of dutyI perfumed by the Departure and arrival paints: landing. takeoff. and alapaad times: total llma; Iota! landings. In?ll Entities and mi?i?" i? the spaces provided an AFTO Form 731 AFTD FORM TS1F. 213080103 D-S RC-135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 D2.2. AF TO FORM 781H, FLIGHT AND MAINTENANCE STATUS SERMLNUMBER ?50 35V 64-14848 6. (3mm 01 PR. PRIBPO. PRITH. TH. BPO. GT. ICT. WM. PU WED TYPE ACOONPUSHED BY DATE (4 STATUS DATA STATUS TODAY PKFORMS 781A AND 781K FOR WWTION 0' CTN IYIIOLI a. was a was sums ENGIE cvcua oocwemmou mung No ENG no mo FULLSTOP Ton. No ?02 N03 m4 pasvnous s?wzg ENG ENG ENG 1 2 3 FLIGHTS 101 . AFro FORM 7am. 20100915 PREVIOUS EDWIN '3 08301-5115 AEROSPACE VEHICLE FLIGHT STATUS AND MAINTENANCE -- V, 64~1 4848, Class A, 30 April 15, AFSAS #739726 OM05 SERVICING DATA OIL W. quads420 ?200 semcmo ceanncmou (sum. Enuoyoo umber. mm a! We? swamDATE 2o {5 ow 30 "7 ?ms 0?430 EVA DATE zo?ovza AFTO FORM 781 H. 20100915 BY 13 AT BY AT RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 D2.3. AFTO FORM 781A, DISCREPANCY AND WORK DOCUMENT D-8 RC-135 V, 64-14848, Class A. 30 April 15, AFSAS #739726 IFROM: 20150430 TD: MDS: RC135V SER PAGE 2 OF I I JCN IDATE ICF 781AIXF 781KIDATB CORRECTED I IA150280272001I 20150128I I I DES IFAULT CODE ICAN 105 FAILS EPA I I I I I I --EMPLOYEB I I --nT4 . '31! v. ?4 AUTH I 445 30:? 7? ASTM 14 Pc-ur Pom: I C) in li?hn. T?al'. U. Ga: Ch :uma raplu Ima'. y: 1 .11 Acid Numb-"r (mg u. Ltluw Dispositlons GUI FED ?xrxaiys?is 1nncates at 11>} Jams--5 a MIL-unfa- 4099 type Lllk-l'li'itln; :11 With dutcutabla 'r lazil . inu. Approved By Date C, GN This rec-oz". v.1: eie-ttrc-ni-rair' delivered to: stern Standard fin-:4 1 Ems-art. D-69 V, 64?14848, Class A, 30 April 15, AFSAS #739726 LABORATORY REPORT A I rJ'- Inhb Yin-:er I5 1580-" hrr" Cue: Sample ?a Peportedzutle/l? 13w? hra' Sung-1e SuLmiLL-a: - -. to: Submissi--n: Aircx'afr ."Invid-enr Tun. Sil, [\izuuaf'. tb'u Class STD a Specification: 3 iu?t? Hy Sularulh-MI: . - {tr-1 .. Sump] m1: Methud nus' Min Max lesnl' - :5 \.Svp ?.4v 4 9? ACTH t- n: 3- 4:.1 1' 17?49 - 14 [h-xnt Hr. -r,4 SAE .Lcl - Numb-1 ?nlq lur'? 'Saf Chromatogzapm: Ahdl?jflf .?tl-Ih Disnositxonn: 6577131."; ana'ypi? :rn?crn-as that in; =amr.r: 1.: a typo th-ricari'ia oi: v-vH-i- vu-Ju?ul: Approved By Date Th1: re:crt was sle:tronica-lv delivered to: 982w LGI-UCL5 EazLern Standald TimuaEST) Repel: 05/ -n 14:30' 3?5: as. provid-?ad by customs" D-70 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB THIS TAB NOT USED E-l RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK E-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB F WEATHER AND ENVIRONMENTAL RECORDS AND DATA F1. WEATHER BRIEFINGS PROVIDED TO FLIGHT CREWS ........................................ 2 F2. ACTUAL WEATHER OBSERVATIONS AND CONDITIONS FOR EVENT ........... 12 F3. METEOROLOGICAL AERODROME REPORT .......................................................... 12 F4. TERMINAL AREA FORECAST ...................................................................................... 12 F-1 64?14848, Class A, 30 April 15, AFSAS #739726 F1. WEATHER BRIEFINGS PROVIDED TO FLIGHT CREWS -1 7 I NONE In I'm .arT p? mun A 2999 1501OKTI 37F I 03C 376 -GOC CONTACT TWR I .v ufF NONE - 300- GULF 3.4: i 2 3 .r a (.4- -.E . 7 240?300 n. r. . FAR WEST NE 002 NORTHERN GU15 25040KT I LGT OCNL MDT 240-340 - 5 25055KT I 48C LGT OCNL MDT 2?0?340 54Fr12c 7MONE I I. 46Ftoac 7INONE I. 72mm: I - esp/20c . . ll ATTACHMENTS PMSY Dem/aw ammun- ?x .nL'r' BRIEFS swarm; NJ E1900 NONE VDID TME EXTENDED 61? RENEE MEWLS TIMEINITIALS . - un-Laucama I- n. J.L RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 Pm VI MISSION FEEDBACK 53. MISSION FEEDBACM MET Tlr'f-IE. 3E Thu-.E Tuj- LITE: rum-LLI-jru THE ?aTI-i I: Er. oTulj-i-r: II-J n-I-f-Ir-Ir-P HI vl-i-?I-HP i-vcil?nrr-I - . -I Dynamic-EH ET EI-3-I PI L-J3- POOH GOOD 1 How would you rate rho accuracy ofy'our mission-manning fan-.5551How IMould you rate the accuracy of your mission forecast? 3 II. 5 3. How would you rare the ?meiinegs AND COURTE of your wamer service for Ibis MinionHow 'I'I'C'uid you rate 012 Pilot-to?Molro Service provided for this mission i'n? utilizedHow would you are me rerovonoy of the weather information provided oompa red ro your misoion pro?Oven" issessment l?ission Segment Ils Fomcasled Not as Forecaster! GD MCI-GD Take-Off Enroute MOP. I Orbit Air Refueling D?kinalion Additional Comments-[Suggestions - TRANSIEHI SUPPERT 51. OBTAINING WEATHER SUPPDFITWHILE IN TRANSIENT STATUS - aim?1": Ai- In'i I. 34115.:- .7 JIM-.1 hi; rrw- n-InrH-I .n ammo-1.1. .1lh1-'- Flu-:mr 1 ?i =1 I in: I'll-mi. ohl. II I L-ar-vz-aelc numooru II- or -. I nu: Fin-on! ?om-1 - anon I- if -M ill?B Ih- I I'll huh-u] I. a-rw IEL manor-"IQFE. mo:an Inch-1 gnan?. - :17! I ImmL- I. I- I uI-l huh-7 IF-I numb-1. - n1 app..- 1 1-. - or Irv-.1- PART WEATHER FLIGHT USE ONLY 5: Eai- r?aL'l TE 5-: Mun-3r. giro-In . I 65083.10? FORM SE JEEI- RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 rIll M5 33:45:1- -5 Hui?5.?53 ?52 ?51] ??uw i ?iv w? -- :52 -51 I-su 50 I, .51 {51f 4 II ll a {xi-5n H, 1 - 554% -49m-43m-45 45 ,5 - mm Flight LerelSal? 4 Madelrun?me?llThuJ?AprI?li Chart valid: lime: 2155 1111130341.- 2015 FL Wind xx FL Tm lamp - a I mm E-FID arm E- r-rr ICHP. "ii-HI. T'n- all-i" can mm GRID 255 ml:- GRID MIT mm- MID Thu in Apr 2915 211}:- GOH 25] mt: SHE W113 3-0 WEDTE RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 l' ?imi- 1' - MA- . 1 Mail .1. m. Ih_? ?1 ??515 ?an A-da?-d? :45 I "Jr Eillma?el: ?'inds,'l'tmp 3: D1731 "pagf I. . Flight 311313411.Ki/Mgm?' Model 11111 ?m e: 122. Thu 31?} Apr 2 ?'15 Er} ?i .3434: Chart Tllid Fri ?31 May EIHS U??i '43 1 (W FL want 3 3 5' . A "mia wily; 3'3 FL Tern "ll-H ?kill .?vH-im 311;"? I TEHR 1WMJDI (H Hay '25'5 I CON 5WD WNWTUHE 25] mi: Hm mm Fn I RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 WIL453Til-4:.354 512Lag 45549 :4 550*?4111 ?54 r_ 45 Int-Niel: ?1116.5, Temp 3: Val all I Flight 34a 49? 44 I444 Moael nm lime: 12: Thu J?Apr 2:115 ?de time: 031 Fri {11 May 2415 5' ?14.43, 43 I EvansImp. - a-[dial f1 'fLiQ --. - H5 3 3 1] ACT 25M Dew IEHR VALID Hay [13:39-15 CHIN I mq?m?ul RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 - r" 1. . .. ?gnj3-:50 --50 an ?=Elks?wt my LAB. {was if 115 vii??1?" ?wt ?ightLerel?d? 119-. 5 43L Mmielrun?me: 121. Ihu J??pr 2?015 "Ill Chautlli??me:??ll:ri?l?tyl?i? r? 43 EJ-?v?nluae Fara?'F a I Puma xx Temp - I can um: 2:GRID comm 26:: ml:- GRID MIT mm Dame C. 13mm mm at Hay m5 aw; I COM GFHD 25: mt- Hm mm Fan at mama: I RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 mum .5 GI- mm Ila-1mm? . I RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 ?3 . 1m mm ?Kill .W m:n ?m my. RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 mm Ktli??l runaw- um TMAWEW mu: ml .3: ?Eit? . RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 rm: KT I56 "run. ?In. ?Jun-m 11/2 :11. '2 . I - ll 1mrmmaw:a.m min ?h?lm ml J. F?ll RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 F2. ACTUAL WEATHER OBSERVATIONS AND CONDITIONS FOR EVENT F3. METEOROLOGICAL AERODROME REPORT METAR KOFF 302358Z AUTO 12005KT 10SM CLR 22/03 A2997 RMK AO2 SLP152 T02230032 10238 20217 55002 F4. TERMINAL AREA FORECAST TAF KOFF 3018/0124 VRB06KT 9999 SKC QNH3000INS BECMG 0111/0112 VRB06KT 9999 SCT080 QNH3009INS BECMG 0114/0115 17009KT 9999 BKN060 QNH3013INS BECMG 0120/0121 18009KT 9000 -SHRA BKN040 QNH3012INS TX24/3021Z TN02/0112Z F-12 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 TAB G PERSONNEL RECORDS G1. FLIGHT RECORDS ............................................................................................................ 6 G1.1. CAPT [Mishap Pilot] (MP) ................................................................... 6 G1.1.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ....................................... 6 G1.1.2. FLYING HISTORY REPORT .............................................................................. 7 G1.1.3. 30/60/90 FLYING HISTORY REPORT............................................................... 9 G1.1.4. INDIVIDUAL DATA SUMMARY ..................................................................... 12 G1.1.5. INDIVIDUAL FLYING TIME SUMMARY ..................................................... 14 G1.1.6. INDIVIDUAL FLIGHT RECORD ..................................................................... 18 G1.1.7. INDIVIDUAL TRAINING SUMMARY ............................................................ 21 G1.2. CAPT [Mishap Co-Pilot] (MCP) .......................................................................... 27 G1.2.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ..................................... 27 G1.2.2. FLYING HISTORY REPORT ............................................................................ 28 G1.2.3. 30/60/90 FLYING HISTORY REPORT............................................................. 30 G1.2.4. INDIVIDUAL DATA SUMMARY ..................................................................... 33 G1.2.5. INDIVIDUAL FLYING TIME SUMMARY ..................................................... 35 G1.2.6. INDIVIDUAL FLIGHT RECORD ..................................................................... 40 G1.2.7. INDIVIDUAL TRAINING SUMMARY ............................................................ 43 G1.3. CAPT [Mishap Navigator] (MN) ................................................................................... 49 G1.3.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ..................................... 49 G1.3.2. FLYING HISTORY REPORT ............................................................................ 50 G1.3.3. 30/60/90 FLYING HISTORY REPORT............................................................. 52 G1.3.4. INDIVIDUAL DATA SUMMARY ..................................................................... 55 G1.3.5. INDIVIDUAL FLYING TIME SUMMARY ..................................................... 57 G1.3.6. INDIVIDUAL FLIGHT RECORD ..................................................................... 60 G1.3.7. INDIVIDUAL TRAINING SUMMARY ............................................................ 62 G1.4. CAPT [Mishap Raven 1] (MR1) .......................................................................... 65 G1.4.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ..................................... 65 G1.4.2. FLYING HISTORY REPORT ............................................................................ 66 G1.4.3. 30/60/90 FLYING HISTORY REPORT............................................................. 67 G1.4.4. INDIVIDUAL DATA SUMMARY ..................................................................... 69 G-1 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.4.5. INDIVIDUAL FLYING TIME SUMMARY ..................................................... 71 G1.4.6. INDIVIDUAL FLIGHT RECORD ..................................................................... 74 G1.4.7. INDIVIDUAL TRAINING SUMMARY ............................................................ 77 G1.5. LT COL [Mishap Tactical Coordinator] (MTC) ...................................................................... 81 G1.5.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ..................................... 81 G1.5.2. FLYING HISTORY REPORT ............................................................................ 82 G1.5.3. 30/60/90 FLYING HISTORY REPORT............................................................. 83 G1.5.4. INDIVIDUAL DATA SUMMARY ..................................................................... 85 G1.5.5. INDIVIDUAL FLYING TIME SUMMARY ..................................................... 87 G1.5.6. INDIVIDUAL FLIGHT RECORD ..................................................................... 89 G1.5.7. INDIVIDUAL TRAINING SUMMARY ............................................................ 91 Airborne Systems G1.6. SRA [Mishap Engineer 1] (MASE1) ................................................................... 95 G1.6.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ..................................... 95 G1.6.2. FLYING HISTORY REPORT ............................................................................ 97 G1.6.3. 30/60/90 FLYING HISTORY REPORT............................................................. 98 G1.6.4. INDIVIDUAL DATA SUMMARY ................................................................... 100 G1.6.5. INDIVIDUAL FLYING TIME SUMMARY ................................................... 102 G1.6.6. INDIVIDUAL FLIGHT RECORD ................................................................... 105 G1.6.7. INDIVIDUAL TRAINING SUMMARY .......................................................... 108 Airborne Mission G1.7. MSGT [Mishap Supervisor] (MAMS) ............................................................... 111 G1.7.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ................................... 111 G1.7.2. FLYING HISTORY REPORT .......................................................................... 112 G1.7.3. 30/60/90 FLYING HISTORY REPORT........................................................... 113 G1.7.4. INDIVIDUAL DATA SUMMARY ................................................................... 115 G1.7.5. INDIVIDUAL FLYING TIME SUMMARY ................................................... 117 G1.7.6. INDIVIDUAL FLIGHT RECORD ................................................................... 120 G1.7.7. INDIVIDUAL TRAINING SUMMARY .......................................................... 122 Cryptologic G1.8. SRA [Mishap Operator] (MCO)............................................................................... 125 G1.8.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ................................... 125 G1.8.2. FLYING HISTORY REPORT .......................................................................... 126 G1.8.3. 30/60/90 FLYING HISTORY REPORT........................................................... 127 G1.8.4. INDIVIDUAL DATA SUMMARY ................................................................... 129 G1.8.5. INDIVIDUAL FLYING TIME SUMMARY ................................................... 131 G-2 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.8.6. INDIVIDUAL FLIGHT RECORD ................................................................... 133 G1.8.7. INDIVIDUAL TRAINING SUMMARY .......................................................... 134 Airborne G1.9. SRA [Mishap Systems Engineer 2] (MASE2) ............................................................................ 137 G1.9.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ................................... 137 G1.9.2. FLYING HISTORY REPORT .......................................................................... 138 G1.9.3. 30/60/90 FLYING HISTORY REPORT........................................................... 139 G1.9.4. INDIVIDUAL DATA SUMMARY ................................................................... 140 G1.9.5. INDIVIDUAL FLYING TIME SUMMARY ................................................... 142 G1.9.6. INDIVIDUAL FLIGHT RECORD ................................................................... 146 G1.9.7. INDIVIDUAL TRAINING SUMMARY .......................................................... 149 Airborne Systems G1.10. TSGT [Mishap (MASE3) ...................................................................... 152 Engineer 3] G1.10.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ................................. 152 G1.10.2. FLYING HISTORY REPORT ........................................................................ 153 G1.10.3. 30/60/90 FLYING HISTORY REPORT......................................................... 154 G1.10.4. INDIVIDUAL DATA SUMMARY ................................................................. 156 G1.10.5. INDIVIDUAL FLYING TIME SUMMARY ................................................. 158 G1.10.6. INDIVIDUAL FLIGHT RECORD ................................................................. 160 G1.10.7. INDIVIDUAL TRAINING SUMMARY ........................................................ 162 G1.11. 1LT [Mishap Raven 2] (MR2) ................................................................... 164 G1.11.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ................................. 164 G1.11.2. FLYING HISTORY REPORT ........................................................................ 165 G1.11.3. 30/60/90 FLYING HISTORY REPORT......................................................... 166 G1.11.4. INDIVIDUAL DATA SUMMARY ................................................................. 168 G1.11.5. INDIVIDUAL FLYING TIME SUMMARY ................................................. 170 G1.11.6. INDIVIDUAL FLIGHT RECORD ................................................................. 174 G1.11.7. INDIVIDUAL TRAINING SUMMARY ........................................................ 177 Signals, Search & G1.12. CMSGT [Mishap Development] (MSSD) ............................................................. 180 G1.12.1. CERTIFICATE OF AIRCREW QUALIFICATIONS ................................. 180 G1.12.2. FLYING HISTORY REPORT ........................................................................ 181 G1.12.3. 30/60/90 FLYING HISTORY REPORT......................................................... 183 G1.12.4. INDIVIDUAL DATA SUMMARY ................................................................. 186 G1.12.5. INDIVIDUAL FLYING TIME SUMMARY ................................................. 188 G1.12.6. INDIVIDUAL FLIGHT RECORD ................................................................. 190 G-3 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.12.7. INDIVIDUAL TRAINING SUMMARY ........................................................ 191 G2. FLIGHT EVALUATION AND TRAINING RECORDS. ............................................ 194 G2.1. CAPT [Mishap Pilot] (MP) ............................................................... 194 G2.1.1. AF FORM 8s ....................................................................................................... 194 G2.1.2. AF FORM 8A ...................................................................................................... 198 G2.1.3. AF FORM 942 ..................................................................................................... 200 G2.1.4. TRAINING RECORDS ..................................................................................... 201 G2.2. CAPT [Mishap Co-Pilot] (MCP) ........................................................................ 207 G2.2.1. AF FORM 8s ....................................................................................................... 207 G2.2.2. AF FORM 942 ..................................................................................................... 211 G2.3. CAPT [Mishap Navigator] (MN) ................................................................................. 212 G2.3.1. AF FORM 8s ....................................................................................................... 212 G2.3.2. AF FORM 942 ..................................................................................................... 225 G2.4. CAPT [Mishap Raven 1] (MR1) ........................................................................ 226 G2.4.1. AF FORM 8s ....................................................................................................... 226 G2.4.2. AF FORM 942 ..................................................................................................... 228 G2.4.3. TRAINING RECORDS ..................................................................................... 229 G2.5. LT COL [Mishap Tactical Coordinator] (MTC) .................................................................... 230 G2.5.1. AF FORM 8s ....................................................................................................... 230 G2.5.2. AF FORM 942 ..................................................................................................... 232 G2.5.3. TRAINING RECORDS ..................................................................................... 233 Airborne Systems Engineer G2.6. SRA [Mishap MASE1) ................................................................. 234 1] G2.6.1. AF FORM 8s ....................................................................................................... 234 G2.6.2. AF FORM 942 ..................................................................................................... 236 G2.6.3. TRAINING RECORDS ..................................................................................... 237 Airborne Mission G2.7. MSGT [Mishap Supervisor] (MAMS) ............................................................... 240 G2.7.1. AF FORM 8s ....................................................................................................... 240 G2.7.2. AF FORM 942 ..................................................................................................... 242 G2.7.3. TRAINING RECORDS ..................................................................................... 243 Cryptologic G2.8. SRA [Mishap Operator] (MCO)............................................................................... 244 G2.8.1. AF FORM 8s ....................................................................................................... 244 G2.8.2. AF FORM 942 ..................................................................................................... 246 Airborne G2.9. SRA [Mishap Systems Engineer 2] (MASE2) ............................................................................ 247 G-4 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.9.1. AF FORM 8s ....................................................................................................... 247 G2.9.2. AF FORM 942 ..................................................................................................... 253 G2.9.3. TRAINING RECORDS ..................................................................................... 254 Airborne Systems G2.10. TSGT [Mishap (MASE3) ...................................................................... 258 Engineer 3] G2.10.1. AF FORM 8s ..................................................................................................... 258 G2.10.2. AF FORM 942 ................................................................................................... 262 G2.10.3. TRAINING RECORDS ................................................................................... 265 G2.11. 1LT [Mishap Raven 2] (MR2) ................................................................... 272 G2.11.1. AF FORM 8s ..................................................................................................... 272 G2.11.2. AF FORM 942 ................................................................................................... 274 G211.3. TRAINING RECORDS .................................................................................... 275 Signals, Search & G2.12. CMSGT [Mishap Development] (MSSD) ............................................................. 276 G2.12.1. AF FORM 8s ..................................................................................................... 276 G2.12.2. AF FORM 942 ................................................................................................... 278 G2.12.3. TRAINING RECORDS ................................................................................... 281 G3. MAINTENANCE TRAINING RECORDS .................................................................... 282 G4. OTHER PERSONNEL EVALUATION AND TRAINING RECORDS. .................... 282 G-5 64?4848, Class A, 30 April 15, AFSAS #739726 G1. FLIGHT RECORDS G1.1. [Mishap Pilot] Gl.l.l. CERTIFICATE OF AIRCREW QUALIFICATIONS DATE 6 Mar 1015 50-Mme 343 R5 Lmardhm?nhan- PILOT NAME 53 a mes Icmluml (AG IMMII PUP/Unqual I 343 R5 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.1.2. FLYING HISTORY REPORT PREPARED 01 MAY 2615 28:35 FLYING HISTORY REPORT (PA) AS OF 91 MAY 2015 SAO36-F40 INQUIRY NAnE:[MiShap Pilot] SSAN: GRADE: CPT 1 1 arm; 66 ASC: 1A ASC DATE: 04 MAR 15 (MD: ACC w1~c:e343nc~s PR1 caw pus: PRI ACFT: RC13SV UNIT: 0343:2050 BASE: DFFUTT AFB AIRCRAFT TOTALS AIRCRAFT MDS FLT DTY CERT CODE MPAN MPAN MPAN MPAN MPAN MPAN UCAE DATE FIRST FLOHN DATE ND DATE NO DATE N0 DATE DATE LAST DATE NO DATE NO DATE NO DATE TOTAL TIME 14.7 20. 99.0 0.0 0.0 0.0 PRIMARY TIME 13. SECONDARY TIME INSTRUCTOR TIME EVALUATOR TIME OTHER TIME NIGHT PRIMARY INST PRIMARY SIM INST NVG TIME COMBAT TIME CMBT SUPPORT TIME COMBAT SORTIES (M81 SUPPORT TOTAL SORTIES 0 00000000061 . moa'cn'o'ea'c'm?na'mb?a 0000N0000\\l . . . . 0000H0000WWN 00000000000 00000000000 000000000000 000000000000000 00000000000000 (3 c>aara c:c~ 9.6:c3c: c:E:La ?zhaan.n PAGE I PREPARED 01 MAY 2015 20:35 NAME: [Mishap Pilot] CMD: ACC AIRCRAFT TOTALS AIRCRAFT MOS FLT DTY CERT CODE DATE FIRST FLOWN DATE LAST FLOWN TOTAL TIME PRIMARY TIME SECONDARY TIME INSTRUCTOR TIME EVALUATOR TIME OTHER TIME NIGHT PRIMARY INST PRIMARY SIM INST NVG TIME COMBAT TIME CMBT SUPPORT TIME COMBAT SORTIES CMBT SUPPORT SORTIES TOTAL SORTIES SP NO DATE NO DATE SSAN: PR1 caw POS: SP NO DATE NO DATE c: a FLYING HISTORY REPORT IPA) GRADE: CPT PRI ACFT: RCIBSV UCAE 20 MAR 12 11 FEB 14 160.1 82. 6 ?a No? anew?names INQUIRY UCAE 09 MAR 12 97 NOV 14 592.7 315.0 0' N. \1 PAGE 2 API: 1 1 OFDA: 66 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 AS OF 01 MAY 2015 ASC: 1A PCN ASC DATE: 04 MAR 15 UNIT10343RCNSO BASE: OFFUTT AFB UCAE 06 DEC 11 04 NOV 14 164.6 (110'! NO A ooawwomaa I?l U'l UCIN 05 MAR 12 25 FEB 14 38.9 19. CAREER TOTALS CREW POSITION PRIMARY TIME SECONDARY TIME INSTRUCTOR TIME EVALUATOR TIME OTHER TIME TOTAL TIME STUDENT TIME OTHER US MIL TIME FOREIGN MIL TIME CIVILIAN TIME COMBAT TIME COMBAT SUPT TIME TOTAL SORTIES COMBAT SORTIES COMBAT SUP SORTIES NVG TIME 0.0 DATE FIRST FLOWN 05 MAR 12 DATE LAST FLONN 02 APR 15 4 run: wzewmoeaas?aee GRAND TOTAL 1108./ PAGE 2 RC4 35 V. 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.1.3. 30/60/90 FLYING HISTORY REPORT PREPARED 26 MAY 2015 68.58 AIRCRAFT HISHAP INVESTIGATION (DA) AS OF 70 MAY 2815 PCN SA93G-F26 NAME: [Mishap Piiot] GRADE: (PT SSAN: m-u- 1 PAC: 1 ASC: 1A DAFSC: 911929 AGE: CMD: ACE WING: 0343RCN50 CRLH POSITION: ASC DATE: 94 MAR 2615 CURR RATING: AIRCRAFT TYPE: RC135V SERIAL NO: 64-4848 HISHAP DATE 39 APR 2915 MISHAP AIRCRAFT FRI sec INST EVAL OTHER TOTAL NIGHT 1~s SIM INS SORT Rc135v 322.9 279.7 9.9 9.9 19.7 697.4 322.6 65.8 79.6 2.9 73 LAST 39 DAYS LAST 66 DAYS 7.0 7.1 6.0 9.8 0.6 14.7 7.6 0.6 2.0 0.5 2 LAST 99 DAVS 7.0 7.1 9.0 6.8 0.6 14.7 7.9 0.9 2.9 9.5 2 OTHER AIRCRAFT PRI sac INST EVAL OTHER TOTAL NIGHT INS SIM Ius SORT RC135W 86.1 72.5 9.3 8-8 9.3 167.9 86.1 14.8 22.1 1.5 25 LAST 39 DAYS 9LAST 99 DAYS 3LAST 99 DAYS 3TCIBSH 32.9 15.5 9.9 9.9 11.9 59.3 32.9 15.7 11.3 2.1 12 LAST 30 DAYS 2LAST 68 DAYS 13.8 6.3 9.9 9.0 9.3 29.4 13.8 4.6 3.5 1.1 4 LAST 99 DAYS 13.9 6.3 9.9 9.9 9.3 29.4 13.9 4.9 3.5 1.1 4 AF37AT72 129.5 199.5 9-9 9.9 42.5 293.9 129.5 9.9 3.2 12.9 93 38 DAYS 1IAST 59 DAYS 1.5 A.s 9.9 9.9 9.9 12.9 I 9.9 9.9 9.9 4 LAST 99 DAYS 21.5 19.5 9.9 9.9 9.9 49.9 21.5 9.9 9.9 9.9 12 RC1355 0LAST 39 DAYS 9LAST 99 DAYS 9LAST 99 DAYS 9PAGE 1 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 29 MAY 2915 99:59 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 29 MAY 2915 PCN SA936-F20 NAME: [MiShap GRADE: CPT SSAN: API: 1 PAC: 1 ABC: 1A 911ch AGE: CMD: Acc WING: 9343RCNSO ORGANIZATION: CREW POSITION: NPAN ASC DATE: 94 MAR 2915 (DAR RATING: PILOT AIRCRAFT IYPE: Rc135v SERIAL 94-4949 MISHAP APR 2915 OTHER AIRCRAFT PRI sec INST EVAL OTHER TOTAL NIGHT INS SIM IHS SORT Rc13su 9LAST 39 DAYS 9LAST 99 DAYS 9LAST 99 DAYS 9Tc1355 9LAST 39 DAYS 9LAST 99 DAYS 9LAST 99 DAYS 9AF37AT72 129.9 199.5 9-9 9.9 42.5 263.6 129.5 9.9 3.2 12.9 93 LAST 39 DAYS LAST 99 DAYS 7.5 4.5 9.9 9.9 9.9 12.9 7.5 9.9 9.9 9.9 4 LAST 99 DAYS 21.5 19.5 9.9 9-9 9.9 49.9 21.5 9.9 9.9 9.9 12 Rc135w 86.1 72.5 9.9 9.9 9.3 197.9 99.1 14.9 22.1 1.5 25 LAST 39 DAYS 9LAST 69 DAYS 3LAST 99 DAYS 3T991A 9LAST 39 DAYS 9LAST 99 DAYS 9LAST 99 DAYS 9PAGE 2 6-10 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPAREO 29 MAY 2915 99 59 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 29 MAY 2915 PCN 5A936-F20 NAME: [Mishap Pilot] GRADE: CPT SSAN: APT: 1 MC: 1 ASC: 1A DAFSC: 9115429 AGE: CHD: ACC WING: 9343RCNSO ORGANIZATION: CREH POSITION: MPAN ASC DATE: 94 MAR 2915 CURR RATING: PILOT AIRCRAFT TYPE: Rc135v SERIAL NO: 94-4949 MISHAR APR 2915 OTHER AIRCRAFT PRI SEC INST EVAL OTHER TOTAL NIGHT INS 51H 1N5 SORT 1996A 9LAST 39 DAYS 9LAST 99 DAYS 9DAYS TCIBSS 9LAST 39 DAYS 9LAST 99 DAYS 9LAST 90 DAYS 0 9 6.8 0.0 9.0 0.9 0.6 6.9 6.6 0.0 6.8 Tc135w 32 9 15.5 9.9 9.9 11.9 59.3 32.9 15.7 11.3 2-1 12 LAST 39 DAYS 2LAST 99 DAYS 13.9 9.3 9.9 9.9 9.3 29.4 13.8 4.9 3.5 1.1 4 LAST 99 DAYS 13.9 9.3 9.9 9.9 9.3 29.4 13.9 4.9 3.5 1.1 a CAREER TOTALS CREW POSITION FIRST FLIGHT PRT SFC TNST EVAL OTHER TOTAL STUDENT COMBAT COMBAT SORT LAST FLIGHT TIME SUPPORT PILOT 95 MAR 2912 449.9 392.7 9.9 9.9 31.9 934.6 449.9 274.1 395.9 9.9 119 92 APR 2915 3 6-11 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.1.4. INDIVIDUAL DATA SUMMARY PREPARED 01 MAY 2015 29:35 INDIVIDUAL DATA SUMMARY (PA) AS OF 01 MAY 2015 PCN SA036-A76 INQUIRY NAME: [Mishap Pilot] SSAN: m-n GRADE: (PT cm: Acc WING: 0343RCNSO UNIT: 9343RCNSO BASE: OFFUTT AFB PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: DDT SECURITY CLEARANCE DATE: 30 MAR 99 MBR SVC CAT: RESTRICTED AREA BADGE NO: LAST PHYS DATE: PROFESSIONAL QUAL INDEX PHYS CODE: PROFESSIONAL OUAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: PHYSIOLOGICAL Tm; DATE: JUMP STATUS DUE DATE DATE ASSIGNED JUMP STATUS: DATE OF BIRTH: DUTY AFSC: 011325 EFFECTIVE DATE OF DUTY: 91 JUN 13 PAS CODE: SYSTEM MANAGEMENT SHORT TOUR HAM CODE: scap DATE RETURN FROM OVERSEAS: DEPLOYEO HARM CODE: DATE OF RANK: 27 MAY 13 DEPLOYED DATE: DATE OF REDEPLOYED DATE LAST STA: 25 AUG 11 SPECIAL CAT ID: WE ?115 57mm? 25 11 RECORDS REVIEU ACC DATE: 15 APR 15 PERSONNEL RECORD 19 RECORDS REVIEW DUE DATE: 31 AUG 15 PROJECTED DAFSU RECORDS REVIEU STATUS CODE: PROJECTED PAS CODE: PROJECTED DUTY LOCATION: PROJ DEPARTURE DATE: REPORTING DATE: PAC 3 EFFECTIVE DATE. USE CODE: PHA EMAIL 03/16/15 DMT I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE ACC PAGE 1 PAGE 1 6-12 PIIPARED 01 MAY 2815 20:35 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 1NDIVIDUAL DATA SUMMARY (PA) AS OF OI MAY 2915 PCN SAO36-A7D INQUIRY NAME: [Mishap Pilot] SSAN: GRADE: CPT CMD: ACC WING: O343RCNSO UNIT: 0343RCNSO BASE: DFFUTT AFB AIRCRAFT ASSIGNMENT DATA AERDNAUTICAL BADGE AIRCRAFT OPLOC: SGBP AERUNAUTICAL PILOT AIRCRAFT: 1C EFFECTIVE DATE: 11 ACFT SVC CAT: USAF PRIMARY ACFT: RC135V FLT DUTY CERT CODE: MPAN CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA LAST NPD DATE: 26 APR 10 LAST MPO REASON: A NONE PAY STOP DATE: 25 APR 22 LAST PRODUCTIVE FLIGHT DATE: 02 APR 15 PREVIOUS PRODUCTIVE FLIGHT DATEDT: AVIATION SERVICE DATA CURR PARA RATING: AVIATION SERVICE CODE: 1A CURR PARA RATING DATE: EFFECTIVE DATE: 04 MAR 15 ORIG PARA RATING: PRIOR ASC: 15 ORIG PARA RATING DATE: EFFECTIVE DATE: TE g1 MAR 15 STATUS AERO ORDER TERM DA 5 APR 22 OFFICER SERVICE DATE: 27 MAY 99 FORM CWRSE DATE AVIATION out: 25 APR 10 REFRESHER PHYSIOLOGICAL TRAINING ID APR 15 TRANSITION STATUS CODE: A INITIAL PHYSIOLOGICAL HYPOXIA TRAINING 36 APR 10 AVIATION POSITION 1 EFFECTIVE DATE: 01 JUN 13 PLYING ACTIVITY CATEGORY: 1 OFDA GATE 10/17: 69 OFDA GATE 15/15: 0 DFDA GATE 29/18: 0 OFDA TO 60 Your current DFDA is 60 manth(s). You need 36 additional mantMs) OFDA to meet your 12 Year gate requirement to receive continuous ACIP through 18 years of aviation service and you must maintain a valid flight physical. I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE ACC PAGE 2 PAGE 2 G?l3 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 28:08 INDIVIDUAL ELYING TIME SUMMARY IPA) AS OF 13 MAY 2015 PCN SA036-F70 REQUEST PERIOD FROM: 30 APR 2014 T0: 39 APR 2015 NAME: [Mishap Pilot] 55AN: m-u GRADE: CPT 901 mew p05: PR1 AIRCRAFT: RC135V CMD: ACC WING: 0343RCNSO UNIT: ACFT SGBP TAIL DUTY cue SIM nus DATE 0000 POSN 001 sec INST EVAL 0TH TOTAL SRT cne SRT SRT NITE 1N5 INS NVG RES AF37AT7 12 JUN 14 62-6003 MCAE 16003 MCAE 162-6002 HCAE 162-6002 MCAE 162-6002 NCAE 162?6002 MCAE 062-6002 MCAE 062-6002 MCAE 162-6002 UPIN 102-6002 UPIN 162-6002 UPIN 162-6003 UPIN 162-6003 UPIN 162-6002 0910 162?6003 UPIN 262-6003 UPIM 162-6003 UPIN 262-6003 UPIN 162-6002 UPIN 162-6902 UPIN 162-6002 UPIN 162-6002 UPIN 162-6002 0910 162-6002 UPIN 162-6003 UPIN 362-6002 UPIN 162-6002 UPIN 162-6802 UPIN 10.0 0.0 0.0 0.0 ACC PAGE I?l PAGE 1 6-14 PREPARED 13 MAY 2015 20:08 NAME, [Mishap Pilot] CMD: ACC MDS AF37AT7 DATE APR AF37AT72 SUMMARY PRI 0.0 60. 0. AIRCRAFT: SIMULATOR: RPA RC135V WING: TAIL NUMB 62-5002 62-5003 62-6003 62?6003 62-5003 62-5002 62-6003 62?6003 62-6002 62-6003 G:an 64~4845 64-4845 64?4845 64-4345 64-4845 64-4845 64-4345 64-4845 64-4845 54-4845 64-4845 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL FLYING TIME SUMMARY (PA) REQUEST PERIOD FROM: 30 APR 2014 UNIT: 0343RCNSO DUTY POSN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN I 0002 EGG-1 MCAE MCAE MCAE MCAE MCAE MCAE MCAE MCAE MCAE MCAE MCAE 30 r4 tha h?r? ruaantm uacntn caLm uwra aawwmambawp? EGGC [Tl r4 kJ?d k-L? Lr ED Ln (34$ u1r1 a a a m4? c.9-e Nl?l?pd SSAN: ACFT choc: SGBP U7 ammo OGGI 09053663536630 rn c:e 63039356990 PAGE coocwecooco MAY 2015 30 APR 2015 GRADE: (PT TOTAL SRT 3090659333093 PRI CREW P05: CMB SRT (D GGOGGOOQO 0.0 :0 O-I 9996999990? (39939606000 GEOGQQGOQOO .4 Gas: 665% to a e o?3cnum a are a bus PCN SA036-F70 PRI AIRCRAFT: RC135V SIM INS NVG 00.0 0.0 0.0 0.0 0.0 0.0 0.0 9.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.5 0.0 0.6 0.0 0.0 0-0 0.0 0.0 ACC PAGE 2 RES G)sz 0660 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:08 INDIVIDUAL FLYING TIME SUMMARY (pA) AS OF 13 MAY 2015 PCN 5A036-F70 REQUEST PERIOD FROM: 30 APR 2014 T0: 30 APR 2015 NAME: [M'Shap Pllotl 55m: GRADE: EPT PR1 CREW PRI AIRCRAFT: Rc135v CMO: Acc WING: 0343chso UNIT: 0343chso ACFT SGBP TAIL DUTY CMB SIM MDS DATE NUMB POSN PR1 sec INST EVAL 0TH TOTAL SRT cue SRT SRT NITE 1N5 INS ?vs RES RC135V 08 JUL 14 63-9192 MCAE 462-4126 MCAE 462-4131 UCAE 662?4135 UCAE 262-4126 UPIN 362?4126 UPIN 30.0 0.0 0.0 0.0 CMB SIM Rc135v SUMMARY PRI sec INST 0TH TOTAL SRT (MB SRT 5RT NITE 1us INS NVG AIRCRAFT: 65.4 50.3 0.0 0.0 3.9 127.6 17 0.0 0.0 0 2.0 9.5 1.6 0.0 SIMULATOR0.0 0.0 0.0 0.0 Rc13sw 19 MAR 15 62-4135 UPIN 30.0 1.0 0.0 0.0 cne SIM RCIBSW SUMMARY PR1 SEC INST EVAL 0TH TOTAL 5R1 (MB SRT SRT NITE INS INS uvs AIRCRAFI0.0 1.0 0.0 0.0 SIMULATOR0.0 0.0 0.0 0.0 RDA0.0 0.0 0-0 0.0 lCl35W 09 MAR 15 62?4127 262-4127 UPIN 562-4133 UPIN 462-4127 UPIN 20.0 0.0 0.6 0.0 ACC PAGE 3 PAGE 3 G?l6 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:08 INDIVIDUAL FLYING TIME SUMMARY (pA) AS OF 13 MAY 2015 PCN SA036-F70 REQUEST PERIOD FROM: 30 APR 2614 TO: 30 APR 2015 NAME: [MiShap SSAN: GRADE: CPT PRI CREN P05: PRI AIRCRAFT: RC135V CMD: Acc 0100: 9343RCNSO UNIT: 03430c~50 ACFT UPLOC: $000 TAIL 001v (NH US SIM M05 DATE MUMB PDSN PR1 SEC INST EVAL 0TH TOIAL 5m CMB SRT US 501 NITE INS INs NVG RES CME SIM TC 1350 SUMMARY PRI sn=c INST WM 010 TOTAL SRT m0 SRT 5m NITE INS INs Nv AIRCRAFT: 13.8 6.3 0.0 0.0 0.3 20SIMULATORRPAENE SIM GRAND IOIALS PRI SEC INST EVAL om IOTAL SRT (MB SRT SRT NITE INS INS Nv AIRCRAFT: 03.0 00.5 0.0 0.0 4.3 155SIMULATOR: 00-7 57.3 0.0 0.0 5.0 123.0 38 0.0 0.0 4.0 0. RPAAcc PAGE 4 PAGE a G-l7 6529c: babe RC-135V, 64-4848. Class A, 30 April 15. AFSAS #739726 G1.1.6. INDIVIDUAL FLIGHT RECORD PREPARED 91 MAY 2915 29:35 INDIVIDUAL FLIGHT 950199 REPORT (PA) as DF 91 MAY 2915 571935.579 INQUIRY umslelshap PIth 5549: 59995: CPT PR1 casw 995: PR1 AIRCRAFT: RC135V (99: ACC wmc: 934390159 9911-. 934390159 ACFT OPLOC: 5599 TAIL DUTY (MB 05 SIM DATE MDS DATE NUHB POSN PR1 SEC INST EVAL (NH 1014!. SR1 CMB SRT NIKE 1N5 1N5 NVG RES UPDAYED 24 APR 14 54-4945 14:29149595 RC13SV 25 APR 14 54-4945 MCAE 329149595 RC135V 3 APR 14 64-4845 MCAC 120140501 9.613511 07 MAY 14 64-4845 KAE 30.0 0.7 0.0 0.0 20140508 RC135V 99 MAY 14 54?4945 MCAE 429149512 RC135V 12 MAY 14 64-4845 OCAE 40.0 0.3 0.0 0.0 20140513 RC135V 13 MAY 14 64-4845 MCAE 20.0 0.0 20140515 RC135V 19 MAY 14 64-4845 MCAE 420140528 20 MAY 14 64-4845 KAE 520140522 RCB5V 23 MAY 14 64-4845 MCAE 30.0 0.9 0.5 0.0 20140528 mm 24 MAY 14 54-4945 MCAE 329149527 RC135V 29 MAY 14 54-4945 MCAE 429149529 RC135V 29 MAY 14 64-4845 MCAE 40.0 1.0 0.0 0.0 20140604 45374172 12 JUN 14 52-5993 MCAE 129149524 95374172 19 JUN 14 52-5993 MCAE 126149619 08 JUL 14 63-9792 MLAE 420140709 AF37AT72 29 JUL 14 62-6092 MCAE 120140731 95379172 31191 14 52-5992 MCAE 129149994 RC135V 07 AUG 14 62-4126 MCAE 420140819 AF37AT72 27 OCT 14 62 6002 HCAE 120141030 19374172 29 OCT 14 52-5992 MCAC 929141939 95374172 39 ocr 14 52-5992 HCAE 929141931 RC135V 03 NOV 14 62-4131 UCAE 620141105 AF37AT72 04 NOV 14 62-6002 MCAE 120141106 RC135V 97 nov 14 52-4135 UCAE 229141112 AFSIATIZ 02 DEC 14 62-6002 UPIN 120150126 ACC PAGE 1 1 CERTIFY 71m I HAVE asvxewso 1599 499 IT IS COMPLETE AND ACCURATE. 5159419913 9415 PAGE 1 G-18 PREPARED 01 MAY 2015 20:35 NAME: [Mishap Pilot] WING: CMD: ACC MDS AF37AT72 APJIAIIZ AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AFJ7AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 AF37AT72 RC135V 1 CERTIFY DATE THAT 1 DEC DEC JAN JAN JAN JAN JAN JAN JAN JAN JAN JAN JAN JAN JAN JAN FEB FEB FEB FEB FEB FEB FEB FEB MAR 0343RCNSO TAIL NUMB 62?6002 62-6002 62-6003 62-6003 62-6002 62-6003 62-6003 62-6003 62-6003 62-6002 62-6007 62-6002 62-6002 62-6002 62-6002 62-6003 62-6002 62-6002 62-6002 62?6002 62-6003 62-6003 62-0003 62-6003 62-6902 62-4126 UNIT: 0343RCNSO DUTY POSN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN FRI .ainla c:Ln?n buLnLn \Ih:nural? ulhi-dh?id hindrd h?th-F4 HAVE REVIEWED MY IFRR AND ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 SEC . . . . . . . . . . . . . - . . . . . . . . . . . . IT IS COMPLETE AND ACCURATE. 2 U1 4 INDIVIDUAL FLIGHT RECORD REPORT (PA) INQUIRY SSAN: ACFT OPLOC: seep EVAL OTH TOTAL SRT CNB C) Ea?ncacaEacaba csta cacaeacsla a>a>czcaa> CICDCB EXCSUDC: GICJCD CDC: GICDC: 6:636:13 saabta GIGDCD 53:3 c>a>a>?3 G>a>zn caeazs 6363!: 5353C: CDC: 6360!: CDCDI: CDC: CICIZDIS CICDED qu>Lu uTLucucn a~Ln Uihdla Lacuna a-c? tutu utcu hnhahdod hirihdtd pAhAhayaa? papa -auavd CDC: CDC: CICD1D CICDCD CICDCD CDC: CICJCD PAGE 2 6-19 GRADE: CPT CDC: CDC: CICD CJCB CDC: CDC: CDC: CICD GICD CD C31: C: Cit: SIGNATURE AS OF 01 MAY 2015 PR1 CREW P05: 6/5 SRT NITE 53(313 CIGDC: CDC: CICDC: CDC: GICDC: G) C3 C3 CDC: CDC: GJCD C: C3 C31: CDC: CDC: CDCD CJC: CBC: CBC: 63C: CBC: CDC: 6103!: 32!: GICJEDIB CICJ INS Fu 5) 53!: 63C: CDCD CDC: CDC: Cll: CDC: Cit: CBC: CBC: CIC: CD CDC: CD 62C: CDC: CDC: CD GJC: CD1: CD CDC: CDID CDC: 2H 01:: CDCDIS 53!: CICDC: CDC: CDC: CDC: GJCD GDCD PCN SA036-F70 PR1 AIRCRAFT: RC135V DAIE NVG RES UPDATED 20150126 20150126 20150126 20150126 20150126 20150126 20150114 20150114 20150114 20150115 20150121 20150123 20150123 20150126 20150127 20150127 20150129 20150205 20150206 20150212 20150219 20150219 20150219 20150225 20150225 20150305 CD CD CIC: CDC: CICD CDC: (DID CDC: C) <3 C: CDC: Ell: CIC: GJCD CDC: CICICDID ACC PAGE 2 DATE PREPARED 01 MAY 2015 20:35 [Mishap Pilot] WING: ACC MDS DATE TC135W 09 RC135V 12 AF37AT72 16 AF37AT72 17 RC135W 19 AF37AT72 20 24 TC13SW 30 TCISSU 02 AF37AT72 14 M05 SUMMARY AIRCRAFT: SIMULATOR: RPA: I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATEFRI 91.0 60.7 0.0 TAIL NUMB 62-4127 62-4126 62-6093 62-6003 62-4135 62-6002 52-4127 62-4133 62-4127 62-6003 UNIT: DUTY POSN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN UPIN I 0892 PR1 nn . . . 1, Gee!- RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 SEC 3 9993609006 05W: INQUIRY SSAN: ACTT OPLDC: SGBP EVAL 0TH TOTAL 0.0 0.0 4.4 0.0 0.2 7.5 0.0 0.0 3.0 0.0 0.0 3.0 0.0 0.1 7.8 0.0 0.0 3.0 0.0 0.0 5.5 0.0 0.0 5.0 0.0 0.3 5.5 0.0 0.0 3.0 TOTAL SRT 171.9 24 123.0 38 0.0 0 PAGE 3 6-20 ?5 La.4 ?a-4?4 nth-rd INDIVIDUAL FLIGHT RECORD REPORT (PA) GRADESIGNATURE PRI CREW P05: AS OF 01 MAY 2015 SRT NITE cacaa>u>a>cacacud>aa 0.0 0.0 OGQAGGQOOG 0669565990 SRT 0 5'3 2 COMO-I PCN 5A036-F70 PR1 AIRCRAFT: RC135V DATE NVG RES UPDATED 0.0 5 20150310 0.0 5 20150313 0.0 0 20150318 0.0 0 20150318 0.0 5 20150320 0.0 0 20150320 0.0 5 20150325 0.0 20150331 0.0 5 20150403 0.0 0 20150420 SIM INS INS NVG 15.5 2.7 0.0 0.0 4-0 0.0 0.0 0.0 0.0 ACC PAGE 3 DATE RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.1.7. INDIVIDUAL TRAINING SUNINIARY PREPARED 13 MAY 2015 19:44 NAME: [Mishap Pilot] PHYSICAL DUE DATEOUALIFICATION PROFILE PLT PLT PLT FLT ONLY (HR (NI AC ONLY CMR (NJ AC ONLY CMR (NI AC NLY CHR (NI Ac ONLY CMR (NJ AC ONLY (HR (N) AC ONLY CHE (N) AC (NU CMR (NJ Ac ONLY CMR (M) AC ONLY CHE AC ERR (M AC (NLY cm (N) MLY an At ONLY (HR (N) AC (NLY cm (N) Ac ONLY can (N) Ac ONLY (N) Ac ONLY can ((Mn (N) (N) GRADE: CPT INDIVIDUAL TRAINING SUMMARY CURRENT TRAINING PERIOD *fhuH- PHYSIOLOGICAL DUE DATE: 30 APR 20 TASK NAME OUT GO-ARO TOTAL RECEIVE REFUEL REC NIGHT AIR REC REFUEL KC-IG SIM ENG OUT SSE co ARND MIC A/n xc-Lo SIM TOTAL 39 FLP TDUEH co SIM va HGT LAND SIM OPP SEAT 3 ENG LNDG SIMR DAY SIMR NIIE OPP SEAT srnenc LOSS cons 0/1 EVAI TOT APPROACHES PREC APP APP PENETRATION TASK ID APJO ARGO AROA AROG ARIQ L012 MF29 NF MGGA H682 H687 $057 5066 5067 SRSO 1095 APOO APG2 APG3 APIU REO I it Ip' PAGE 1 ACCOHP GMAY 2015 CREW POSITION: HPAN RECORDS REVIEW DUE DATE: 31 AUG 15 DAVE LAST Acconp PHASE PCN SAGBE-TIO UNIT: 0343RCNSO ACC ova IN OA?l'f out our; PMS CODE ACC PAGE 1 W0 RC-I35V, 64-4848. Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:44 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2015 PCN 5A636-T10 CURRENT TRAINING PERIOD NAME: [MiShap Wot] GRADE: cp'r SSAN: caew POSITION: MPAN UNll: 0343RCNSO PHYSICAL DUE DATE: 93 AUG 15 PHYSIOLOGICAL our DATE: 30 APR 20 ascoaos nevnaw DUE DATE: 31 AUG 15 ACC pm TASK (MTV LAST OVR IN NEST CD QUALIFICATION PROFILE TASK NAME [0 RED ACEOMP REM ACCOMP IN PHASF DUE DUE PMS CODE cm (N) ("55 APP-HAN M?(N) CIRCLING APP FLT (HR (N) VFR APP ??FLT (HR (N) HOIJ) PATTERN APZS PIT (NR (N) GPS APP A929 (N) ENROUTE DESLENT AP37 FLT (NR (N) ILS GYRO AP39 RDVU ARES 3LT (N) REC NEAKAWAY M13 (N) ENCON 3 R02 ARZO PLT CPR (N) INSTR DEPART (N) TOTAL LNOG L009 PLT (MR (N) DAY LNDG (N) NIGHT LNDG L002 IN) IOUCH AND (30 L093 (N) U11) AL) (.3 L025 PLT CPR (N) DEG ELECTRO SPE "(PLT CMR (N) SIM VFR APP M588 FLT (NR (N) 51" HOLD PAT MF89 'PLT CNR (N) SIM ENROUTE DES MF91 HFQI (N) REC BRKAWAY MF93 Acc PAGE 2 PAGE 2 6-22 RC-I35V, 64-4848. Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19M INDIVIDUAL TRAINING SUMMARY As or 13 MAY 2015 SA036416 CURRENT TRAINING PERIOD NAME: [M'Shap GRADE: CPT SSAN: ?Ho- MPAN UNIT: 0343RCNSO PHYSICAL DATE: 93 AUG 16 PHYSIOLOGICAL DUE DATE: 30 APR 29 RECORDS REVIEW DUE DATE: 31 AUG 15 ACC P91 TASK DA7E LAST DATE OVH 1? WEST co QUALIFICATION mom: TASK NAME RED ACCONP am ACCOMP IN ms: om sue nu: was con: wu CH FLT CHE (N) SIM EHCONB H795 FLT (MR (N) SIM INSTR DEP 1 2 02 APR 15 I PLT (NR (N) SIM TOTAL LAND HF97 9 17 17 APR 15 I FLT (N) SIM LND GEAR EX NFQB PLT (MR SIM LUWAT OPS H603 1 0? awn 19 CH PLT CNR (N) 51" ALERY PROC M004 (N) 51" START PROC M595 (N) SIM 5Y5 '56 "696 PLT (NR (N) 51" RIVET JOINT RAP M003 PLT (N) 51" COBRA BALI RAP "609 6 a 1 CH PLT (N) SIM COMBAT SENT RAP M610 9 9 I (N PLT CIR (N) SIM TNIUM. "511 PLT (NR (N) SIN 135 LURHENCY M012 9 4 17 APR 15 I FLT CMR (N) 51" 7/0 ROLLING "$(N) SIM 7/0 SVATIC M610 "out "515 FLT CMK (N) PRO). "142 3 82 APR lb 1 CH FLT CMR (N) TOT SIM "1'FLT (N) AUTHENT $009 PLT (N) REF SORTIE SW5 (N) SIM PET-RAN 5014 FLT (HR (N) CIR APP 5015 1 a 92 APR 15 I ACC PAGE 3 PAGE 3 G-23 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:44 INDIVIDUAL TRAINING SUMMARY As or 13 MAY 2015 PCN SAOSG-TIG CURRENT TRAINING PERIOD MARE: [Mishap Pith GRADE: CPT 55sz casw POSITION: MPAN UNIT: 8343RCNSO PHYSICAL DUE DATE: 03 AUG 15 PHYSIOLOGICAL DUE DATE: 39 APR 20 RECORDS REVIEW nus DATE: 31 AUG 15 Acc pm TASK DATE LAST DATE UVH 1N CD QUALIFICATION PROFILE TASK NAME RED ACCOMP REM ACCORD IN PHASE DATF DIIF DUE PMS CODE W0 CH PLT (HR (N) SIH INST SORTIE 5017 PLT (MR (N) SIM PREC APP $018 (MR (N) SIM NPREE APP $019 3 17 Am 15 CH (N) PRE DEPLDY 5046 $047 (N) SXMR DAY LAND $054 (N) SZNR NIGHT LAND $055 3 67 APR 15 I CH FLT (HR (N) SIMR TCH 6 GO 5056 PLT (N) 2/3 ENGMIS 5073 PLT (MR (N) 51m TAKE OFF $074 (N) SIM RENDEZVOUS 5099 (N) TOT RAP SRGO RAP SRGB (saoec RAF SRGOR RAP SRBI SRGIC RAP SRBIR 1 CH PLT CM (N) PILOT PRO 2 2 87 APR 15 I (.N FLT (NR (N) TOT SAGE(N) BASIC SORTIE 5x03 Acc PAGE 4 PAGE 4 G-24 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19 44 INDIVIDUAL TRAINING SUMMARY AS or 13 MAY 2015 Pcu SA036-TIO CURRENT TRAINING PERIOD PHYSICAL DUE DATE: 03 AUG 16 GRADE: CPT SSAN: PHYSIOLOGICAL DUE DATE: 38 APR 20 CREW POSITION: NPAN UNIT: RECORDS REVIEW DUE DATE: 31 AUG 15 pm TASK DATE LAST . OVR CD QUALIFICATION PROFILE TASK NAHE TD RED ACCMP REM ACCOMP TN PHASE DATE DUE DUE 9H5 CODE WD CH PLT CM (N) TOT T088 (N) INITIAL T008 (N) ROLLING T009 (N) STATIC T019 GRND AFE FIT (NECK Ll97 a in MR GT GRND PILOT TRAINING GRND PILOT TRAINING ANTI-HIJACK GAOB GRND PILOT TRAINING GAOG GRND PILOT TRAINING POOMA GAZG GRND PILOT TRAINING H9 OUAL GRNII PILOT TRAINING ACAD GMB GRND PILOT TRAINING SEPT 6503 GRND PILOT TRAINING STAN EVAL TEST 6505 GRNO PILOT TRAINING (3506 GRND PILOT TRAINING OPLAN STUDY 6522 0 I7 PAR 14 GT GRND PILOT TRAINING AIL SERVICE 652GRND TRAINING FLY SAFETY TRNG 51:GRNO PILOT TRAINING RISNO CERT GSSO GRND PILOT TRAINING RISNO STUDV 6551 GRND PILOT TRAINING 8910 (2 PRO 6559 GRNO PILOT TRAINING SIE TEST SEC 657GRND PILOT TRAINING ISO PREP GRND PILOT TRAINING INTEL TRNG I585 GRND PILOT TRAINING AFE FAM TRNG LL01 a 15 NOV 11 ACC PAGE 5 PAGE 5 CF25 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:44 INDIVIDUAL TRAINING SUMMARY A5 0F 13 MY 2015 PCN CURRENT TRAINING PERIOD [Mishap Pilot] GRADE: CPT SSAN: CREW POSITION: MPAN UNIT: 0343RCNSO PHYSICAL DUE DATE: 03 AUG 16 PHYSIOLOGICAL DUE DATE: 36 APR 20 RECORDS REVIEW DUE DATE: 31 AUG 15 ACC pan TASK I. DATE LAST uAIc DVR IN RESI CD OUALIFICATION PROFILE TASK NATE In REO ACCONP REM ACCONP IN PHASE DATE DUE DUE PNs CODE GT GRNO PILOT TRAINING EGRESS INONIJI LL03 PILOT TRAINING ACOT LL04 GRNO PILOT TRAINING EGRESS WACDE LL05 a 15 Nov II II GRNO PILOT TRAINING APE TRNG LL06 PILOT TRAINING LOCAL AREA SURV 5591 II 12 nov II 5 GT GRNII PIIUI TRAINING (MST SURV TRNG ssez GRNO PILOT TRAINING (AC TRNG $503 GRND PILOT TRAINING NST 5505 GRND PILOT TRAINING AFRICOM (C51) 5507A 9 a GT GRND PILOT TRAINING CENTCOM (C51) 5507c GRNII PILOT TRAINING EUCON ICSI) 55975 a GT GRNIJ PILOT TRAINING ICSI) SSOTP 0 GT GRND TRAINING summon 55075 GRNII PILOT TRAINING SPEC SERE TRNG 5510 IIRND PILOT TRAINING s-vaa-A 5524 8 07 OCT 11 ACE PAGE 6 PAGE 6 G-26 64-4848, Class A, 30 April 15, AFSAS #739726 G1.2. CAPT (?Shep (MCP) G1.2.1. CERTIFICATE OF AIRCREW QUALIFICATIONS DAVE 6 Mar 2015 343 R5 Cenmatons rum I 2 - i NAME 3? Remus ??[Mishap Pilot] 1W1 MI LIMJ Commander, 343 RS G-27 Gl.2.2. FLYING HISTORY REPORT PREPARED 91 MAY 2015 20:24 NAME: [Mishap Co-Pilot] (MD: ACC AIRCRAFT TOTALS AIRCRAFT MDS FLT DTY CERT CODE MLAE DATE FIRST FLOWN 24 JAN 13 DATE LAST 28 JAN 15 TOTAL TIME 323.3 PRIMARY TIME 171.0 SECONDARY TIME 149.4 INSTRUCTOR TIME 9.0 EVALUATOR TIME 0-0 OTHER TIME 2.9 NIGHT 39.7 PRIMARY INST 32.9 PRIMARY SIM INST 6.4 NVG TIME 0-0 COMBAT TIME 88.8 CMBT SUPPORT TIME 0.0 COMBAT SORTIES 8 (NET SUPPORT SORTIES 0 TOTAL SORTIES 43 SSAN: PR1 caw POS: MCAE 15 FEB 13 Mar-- LO FLYING HISTORY REPORT (PA) GRADE: CPT PR1 ACFT. RC135V MCAE 10 JAN 13 .. . . ocoeoc-bsasnocno y?a INQUIRY "(PAGE 1 6-28 API: 1 FAC: 1 NCAE 14 DEC 14 14 DEC 14 13.5 GGDOGVOOGGN OFDA: 49 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 AS or 91 MAY 2915 ASC: 1A ECN SADBG-F40 ASC 15 FEB 13 OTTUTT AFB MCAE 16 OCT 12 16 APR 15 171DATE N0 DATE 0.9 533099630996 PAGE 1 PREPARED MAY 2015 26:24 [Mishap Co-Pilot] CMD: ACC AIRCRAFT TOTALS AIRCRAFT MDS DATE FIRST FLOWN DATE LAST FLOWN TOTAL TIME PRIMARY TIME SECONDARY TIME INSTRUCTOR TIME EVALUATOR TIME OTHER TIME NIGHT PRIMARY INST PRIMARY SIM INST NVG TIME COMBAT TIME CMBT SUPPORT TIME COMBAT SORTIES CMBT SUPPORT SORTIES TOTAL SORTIES FLT DTY CERT CODE SP NO DATE NO DATE (D RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 FLYING HISTORY REPORT (PAT INQUIRY SSAN: (aw P05: CAREER TOTALS CREW POSITION PILOT PRIMARY TIME 316.6 SECONDARY TIME 283.4 INSTRUCTOR TIME 0.0 EVALUATOR TIME 0.0 OTHER TIME 60.3 TOTAL TIME 660.3 STUDENT TIME 242.0 OTHER US MIL TIME 0.0 FOREIGN MIL TIME 0.0 CIVILIAN TIME 0-0 COMBAT TIME 183.8 COMBAT SUPT TIME 0.0 TOTAL SORTIES 92 COMBAT SORTIES 17 COMBAT SUP SORTIES NVG TIME 0.0 DATE FIRST FLOWN 10 JAN 13 DATE LAST 19 MAR 15 GRAND TOTAL 902.3 GRADE: CPT PRI ACFT: RC135V PAGE 2 API: 1 6-29 PAC: 1 AS OF 01 MAY 2015 OFDA: 49 ASC: 1A PCN SAOBO-F4O ASC 16 FEB 13 BASE: OFFUTT AFB PAGE 2 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.2.3. 30/60/90 FLYING HISTORY REPORT 20 MAY $15 09:01 NAME 1 LMD: ALL WLuu: CURR RATING: PILOT PRI SEC RC135V 171.0 149.4 LAST 30 DAYS 0.0 0.0 LAST 50 DAYS 0.0 0.0 LAST 90 DAYS 0.0 0.0 PR1 SEC RCIBSH 84.0 78.7 LAST 30 DAYS 0.0 0.0 LAST 60 DAYS 9.9 9.4 LAST 90 DAYS 9.0 9.4 TCIBSW 40.7 35.6 LAST 30 DAYS 0.0 0.0 LAST 50 DAYS 0.0 0.0 LAST 90 DAYS 2.7 2.7 RCIBSS 12.1 12.0 LAST 30 DAYS 0.0 0.0 LAST 50 DAYS 0.0 0.0 LAST 90 DAYS 6.0 0.0 RC13SU 7.0 6 0 LAST 30 DAYS 0.0 0.0 LAST 60 DAYS 0.0 0 0 LAST 90 DAYS 0.0 0 0 AIRCRAFT MISHAP INVESTIGATION (PA) A5 0" 20 MAY 2015 PCN 011R2G AGE: ASC DATE: 16 FEB 2013 MISHAP APR 2015 API: 1 PAC: 1 ASC: 1A ORGANIZATION: POSITION: MCAE AIRCRAFT TYPE: RC13SV SERIAL NO: 60-4848 NISHAP AIRCRAFT GRADE: CPT INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT 0.0 0.0 2.9 323 3 171.0 39.7 32OTHER AIRCRAFT INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT 0.0 0.0 15.9 178.6 84.0 45.8 270.0 0.0 15.0 330.0 0.0 150.0 0.0 23.9 100 2 40.7 16.7 100.0 0.0 15.6 39 7 12PAGE 1 6-30 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 79 "Av 2915 99:91 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 29 MAY 2915 PCN SA636-F20 NAME: [Mishap GRADE: CPT SSAN: API: 1 FAC: 1 ASC: 1A DAFSC: 911929 AGE: CMD: ACC WING: CREW POSITION: MCAE ASC DATE: 16 FEB 2013 CURE RATING: PILOT AIRCRAFT TYPE: RCIBSV SERIAL N0: 54?4848 MISHAP DATE: 30 APR 2015 OTHER AIRCRAFT PRI SEC INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT Tc1355 1LAST 30 DAYS 0LAST 60 DAYS 0LAST 99 DAYS 9AE37AT72 85.6 93.6 9.9 9.9 9.7 177.9 95.9 4.5 9.9 22.9 57 LAST 30 DAYS 2-8 3.0 0.0 0.0 0.2 6-0 2.8 0.0 0.0 1.0 IAST 60 DAYS 4.8 5.0 0.8 0.0 2.2 12.0 4.8 0.0 1.0 1.5 4 LAST 99 DAYS 7.3 7.5 9.9 9.9 2.2 17.9 7.3 9.9 1.9 3.9 9 T991A 9LAST 30 DAYS 0LAST 60 DAYS 0LAST 99 DAYS 9T999A 9LAST 39 DAYS 9LAST 99 DAYS 9LAST 99 DAYS 9PAGE 2 G-3 PREPARED 29 MAY 2015 09:01 [Mishap Co-Pilot] CMD: ACC WING: CURR RATING: PILOT PRI CREW POSITION FIRST FLIGHT PR1 LAST FLIGHT TIME PILOT 18 JAN 2013 316.6 283 4 10 MAR 2015 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AIRCRAFT MISHAP INVESTIGATION AS OF 28 MAY 2015 PCN DAFSC: 011R2G AGE: ASC DATE: 16 FEB 2013 MISHAP APR 2015 API: 1 1 ASC: 1A CREW POSITION: HCAE SERIAL NO: 64-4848 SSAN: ORGANIZATION: 0343120450 AIRCRAFT TYPE: Rc135v tn omen AIRCRAFT ?u INST EVAL OTHER TOTAL NIGHT INS CAREER TOTALS GRADE: CPT SIM INS SORT INST EVAL OTHER TOTAL STUDENT COMBAT COMBAT SORT SUPPORT 0.6 0,0 66.3 660.3 316.6 242.0 183.8 92 PAGE 3 G-32 Gl.2.4. INDIVIDUAL DATA SUNIMARY PREPARED 01 MAY 2615 20.24 [Mishap Co-Pilot] BASE: UFFUTT AFB INDIVIDUAL DATA SUMMARY (PA) SSAN: DUTY PHONE: OFFICE SYMBOL: HER SVC (AT: LAST PHYS DATE PHYS CODE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: PHYSIOLOGICAL TNG DATE: PHYSIOLOGICAL DUE DATE: DATE OF BIRTH: DUTY AFSC: EFFECTIVE DATE OF DUTY: PAS CODE: SHORT TOUR INDICATOR: DATE RETURN FROM OVERSEAS: DATE OF RANK: DATE OF DATE DEP LAST DUTY STA: DATE ARR THIS STATION: PERSONNEL RECORD STATUS: PROJECTED DAFSC: PROJECTED PAS CODE: PROJECTED DUTY LOCATION: PRDJ DEPARTURE DATE: PROJ REPORTING DATE: FAC 8 EFFECTIVE DATE: LOCAL USE CODE: I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. DOD-6000 USAF OIIRZG PERSONAL DATA INQUIRY GRADE: CPT CMD: ACC RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 AS OF 01 MAY 2015 WING: PCN SADSG-A7O UNIT: PAGE 1 6-33 SECURITY CLEARANCE: SECURITY CLEARANCE DATE: RESTRICTED AREA BADGE NO: PROFESSIONAL DUAL INDEX (POI): PROFESSIONAL DUAL INDEX DATE: JUMP STATUS DATE ASSIGNED JUMP STATUS: SYSTEM MANAGEMENT HARM CODE: DEPLOYED HARM CODE: DEPLOYEO DATE: REDEPLOYED DATE: SPECIAL CAT ID: RECORDS REVIEW ACC RECORDS REVIEW DUE DAIE: RECORDS REVTEW STATUS CODE: SIGNATURE 22 DEC 14 SGDP 24 FEB 15 29 FEB 16 ACC PAGE 1 PREPARED 91 MAY 2015 20:24 [Mishap Co.Pi ot] BASE: OFFUTT AFB AIRCRAFT ASSIGNMENT DATA AIRCRAFT OPLOC: CMO OF AIRCRAFT: ACFT SVC CAT: PRIMARY ACFT: FLT DUTY CERT CODE: CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA LAST MPO LAST MPO REASON: PAY STOP DATE: LAST PRODUCTIVE FLIGHT DATE: PREVIOUS PRODUCTIVE FLIGHT DATE: AVIATION SERVICE DATA AVIATION SERVICE CODE: EFFECTIVE DATE: PRIOR ASC: EFFECTIVE DATE: AERO ORDER TERM DATE: OFFICER SERVICE DATE: AVIATION SERVICE DATE: TRANSITION STATUS CODE: AVIATION POSITION INDICATOR: EFFECTIVE DATE: FLYING ACTIVIIY CATEGORY: PRE-ACIA-OFDA: DFDA GATE 10/12: OFDA GATE 15/15: OFDA GATE 20/18: OFDA TO DATERC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 SSAN: SGBP 1C USAF RC135V MLAE APR 11 NONE APR INDIVIDUAL DATA SUMMARY (PAT INQUIRY AS OF 01 MAY 2615 PCN 5AO36-A7O GRADE: CPT CMD: ACC WING: 6343RCNSO UNIT: 9343RCNSO AERONAUTICAL BADGE AERONAUTICAL RATING: EFFECTIVE DATE: PILOT 27 APR 12 GUS MTI RTG DT: CURR PARA RATING: CURR PARA RATING DATE: ORIG PARA RATING: OHIO PARA RATING DATE: STATUS FORMAL COURSE DATE Your current OFDA 15 a9 You need 47 additional month(s) OFDA to meet your 12 Year gate requirement to receive continuous ACIP through 18 years of aviation service and you must maintain a valid flight physical. I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE- SIGNATURE DATE ACC PAGE 2 PAGE 2 6-34 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:08 INDIVIDUAL FLVING TIME sum;an (FA) AS OF 13 MAY 2015 PCN SA036-F70 REQUEST PERIOD FROM: 30 APR 2014 TO: 30 APR 2015 NAME: [Mishap SSAN: GRADE: CPT PRI (999 P05: 991 AIRCRAFT: 9c135v (Mo: ACC 9199: 93939cuso uu11: 93439c~so ACFI 99191: 5999 1911 991v cue 519 995 DATE 9999 POSN 991 sec 1951 EVAL 919 TOTAL SRT cma 591 591 9119 195 INS uvc RES AF37AT7 19 MAY 14 92-9993 9999 16003 MCAE 192-9993 MCAE 192-9992 MCAE 962-6003 MCAE 162-6002 MCAE 192-9992 MCAE 292-9993 MCAE 192-9993 MCAE 362-6002 MCAE 192-9992 MCAE 19993 MCAE 162-6002 MCAE 162-6002 MCAE 192-9992 MCAE 19.9 9.9 1.9 9.9 CMB SIM AF37AT72 SUMMARY PRI SEC INST EVAL 0TH TOTAL SR1 CMB SRT SRT NITF INS INS NVG AIRCRAFT9.9 9.9 9.9 9.9 519919199: 21.9 19 1 9.9 9.9 3.2 92.9 15 979 979 9.9 1.9 9.9 9.9 RPA0.0 0.0 0.0 0.0 RC1355 10 NOV 14 62-4128 MCAE 062-4128 MCAE 162-4128 MCAE 162-4128 MCAE 262-4128 MCAE 062~4128 MCAE 3.7 3.7 0.0 0.0 3.0 10.4 1 0.0 0 0.0 0 0.0 2.0 0.0 0.0 ACC PAGE 1 9999 1 6-35 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:08 INDIVIDUAL FLYING TIME (pA) AS OF 13 MAY 2015 PCN SA036-F70 REQUEST PERIOD FROM: 30 APR 2014 T0: 39 APR 2015 SSAN: GRADE: CPT PRI CREW POS: PRI AIRCRAFT: (MD: ACC WING: G343RCNSO UNIT: ACTT 0010c: SGBP TAIL DUTY SIM N05 DATE NUNB POSN PR1 sec INST EVAL 0TH TOTAL SRT CMB SRT C/s SRT NITE 1N5 INS ch RES RC1355 12 DEC 14 62-4123 MCAN 20.0 0.3 0.0 0.0 CMB SIM Rc13ss SUMMARY PAT sec INST EVAL 0TH TOTAL SRT CMB SRT C/s SRT NITE INS INS ch AIRCRAFT: 12.1 12.0 0.0 0.0 15.6 39.7 7 0.0 0 0.0 0 3.1 4.1 0.3 0.0 SIMULATOR0.0 0.8 0.0 0.9 RPARC135U 14 DEC 14 64-4049 NCAN 7ENE SIM RC135U SUMMARY PRI sec INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE 1N5 INS NVG AIRCRAFT: 7.0 6.0 0.0 0.0 0.5 13.5 1 0.0 0 0.0 0 7.0 0.0 0.0 0.0 SIMULAIOR0.9 0.0 0.0 0.0 RPA9.9 9.9 0.0 0.0 nc135v 03 JUN 14 64-4845 MCAE 464'4345 MCAE 354-4845 MCAE 464-4845 MCAE 364-4645 MCAE 264-4845 MCAE 464-4845 MCAE 354-4845 MCAE 454-4845 MCAF 464-4645 MCAE 464-4845 MCAE 364-4845 MCAE 30.0 0.2 0.0 0.0 ACC PAGE 2 PAGE 2 6-36 RC-I35V, 64-4848, Class A, 30 April 15. AFSAS #739726 PREPARED 13 MAY 2015 20:08 INDIVIDUAL FLYING TIME SWARY (FA) AS OF 13 MAY 2615 SA036-F70 REQUEST PERIOD FROM: 30 APR 2014 TO: 30 APR 2015 60632 NAME: 5540: GRADE: CPT PRI caew P05: PRT AIRCRAFT: RC135V CMD: Acc WING: 0343RCN50 0343Rcuso ACFT OPLOC: SGBP TAIL DUTY CMB SIM MOS DATE NUMB POSN PRI SEC INST EVAL DTH TOTAL SRT CMB SRT SRT NITE INS 105 NVG RC135V 02 JUL 14 64-4345 MCAE 364-4645 MCAE 164-4645 MCAE 164-4845 HCAE 264-4345 MCAE 364-4845 MCAE 364-4845 MCAE 064-4645 MCAE 364-4845 MCAE 364-4845 MCAE 6.2 6.7 0.0 0.0 0.5 1364-4841 MCAE 364-4848 MCAE 462-4131 MCAE 364-4848 MCAE 264-4643 MCAE 40.0 0.0 0.0 0.0 CMB 51M Rc135v SUMMARY PR1 SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE 105 105 AIRCRAFT: 91.3 869.2 110.0 0.0 0.0 RPA0.0 0.0 0.0 RC135W 06 MAR 15 62 4139 MCAE 162-4130 MCAE 14130 MCAE 162-4135 MCAE 062-4135 MCAE 4.2 4.5 0.0 0.0 4.8 13.5 1 0.0 0.0 0 6.2 4.0 0.0 0.0 Acc PAGE 3 PAGE 3 G-37 1: 93? 6606'! RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:98 INDIVIDUAL FLYING TIME SUMMARY (FA) AS OF 13 MAY 2015 PCN SA036 F70 REQUEST PERIOD FROM: 30 APR 2014 T0: 30 APR 2015 SSAN: GRADE: CPT PR1 caew 005: PR1 AIRCRAFT: RC135V (MD: ACC UNIT: 0343RCN50 ACFT OPLOC: 5000 TAIL DUTY (MB SIM 005 DATE NUMB POSN PR1 SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE 1N5 INS ch RES CMB SIM RCIBSW SUMMARY PR1 SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS TNS NVG AIRCRAFT: 9.0 9.4 0.0 0.0 15.0 33.4 5 0.0 0 0.0 0 8.6 5.2 1.0 0.0 SIMULATOR0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 Tc1355 24 OCT 14 02-4133 MCAE 1CMB SIM TC13SS SUMMARY PR1 SEC INST 0TH TOTAL SRT CHB SRT SRT NITE INS INS NVG AIRCRAFT0.0 1.0 0.5 0.0 SIMULATOR0.0 0.0 0.0 0.0 RPA62-4127 MCAE 162-4127 MCAE 262-4127 MCAE 262-4127 MCAE 262-4133 MCAE 162~4127 MCAE 12.0 0.5 0.5 0.0 CMB SIM Tc13sw SUMMARY PR1 sec INST EVAL 0TH TOTAL SRT CMB SRT C/s SRT NITE INS INS NVG AIRCRAFT: 10.2 12.5 0.0 0.0 7.1 29.0 6 0.0 0 0.0 0 6.6 3.5 1.7 0.0 SIMULATOR0.0 0.0 0-0 0.0 RPA0.0 0.0 0.0 0.0 ACC PAGE 4 PAGE 4 6-38 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:08 INDIVIDUAL FLYING TIME SUMMARY (pA) AS OF 13 MAY 2015 PCN REQUESI PERIOD 30 APR 2914 39 APR 2015 Mishap MEfl NA SSAN: GRADE: CPT PRI CREW PDS: PRT AIRCRAFT: RCIBSV CMD: ACC WING: UNIT: 0343RCNSO ACFT OPLOC: SGBP CMB SIM GRAND TOTALS PRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SR1 NITE INS INS NVG AIRCRAFT: 131.4 128.3 0.0 9.0 42.5 302.2 47 0.0 0 0.0 0 34.5 25.7 6.9 0.0 SIMULATOR: 21.6 18.1 0.0 0.0 3.2 42.9 15 0.0 1.0 6.8 0.0 RPAACC PAGE 5 PAGE 5 6-39 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.2.6. INDIVIDUAL FLIGHT RECORD PREPARED 01 MAY 2015 28224 INDIVIDUAL FLIGHT RECORD REPORT (PA) A5 0" 91 MAY 1015 PCN 5A936-F7U INQUIRY NAME: [M'Shap SSAN: GRADE: c177 PR1 CREW P05: 6 PRI AIRCRAFT: RC135V 1140: 400 WING: 0343110150 01117: 0343110150 ACFT 00100: 5000 TAIL DUTY CHE 51? DATE HDS DATE NUMB 905" SEC INST EVAL 0TH TOTAL SRT CHE SR7 SR1 NIlt 1N5 INS RES UPDAFED 103501 12 MAY 14 62-4127 MCAE 120140513 1103714172 16 MAY 14 62-6003 MCAE 120140519 AF37A172 27 MAY 14 62-6093 MCAE 120149510 03 JUN 14 64-4045 MCAE 420140004 acnsv 04 JUN 14 64-4845 MCAE 320140604 RC135V 05 JUN 14 54-4845 MCAE 420140699 RC135V 98 JUN 14 54?4845 320149619 00135v 10 JUN 14 64-4845 MCAE 220140612 RC135V 11 JUN 14 64-4845 MCAE 420140016 RC135V 15 JUN 14 64-4845 320140618 RC135V 17 JUN 14 64-4845 MCAE 420140010 001350 101011 14 64-4845 MCAE 420140020 RC135V 24 JUN 14 54-4845 MCAE 423140625 RC135V 26 JUN 14 64-4845 MCAE 320140701 RC135V 30 JUN 14 64-4845 MCAE 320140701 RC135V 02 JUL 14 64-4045 MCAE 320140714 RC135V 06 JUL 14 64-4345 MCAE 129149719 RC135V 09 JUL 14 64-4845 MCAE 120140710 RC135V 10 JUL 14 64-4045 MCAE 220140716 RC135V 11 JUL 14 64-4845 320149714 NEW 16 JUL 14 64-4845 MCAE 320140717 RC135V 20 JUL 14 64-4345 MCAE 020140721 RC135V 23 JUL 14 64'4845 MAE 320140725 RC135V 24 JUL 14 64-4345 MCAE 320140720 RC135V 28 JUL 14 64-4045 MCAE 6.2 6.7 0.0 0.0 0.5 1320140006 AFBIAWZ 12 AUG 14 62-0003 MCAE 120140027 Acc PAGE 1 1 CERTIFY THAT I HAVE REVIEWED IFRR AND 17 IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 1 PREPARED 01 MAY 2015 20:24 RC-I 35 V, 64-4848, Class A, 30 April 15. AFSAS #739726 INQUIRY NAME: [Mbhap 55m: CMD: ACC UNIT: ACFT OPLOC: 5081? M05 RC135V AF37AT72 TCIBSW TC1350 RC135V AF37AT72 AF37AT72 RC135V TC1355 AF37AT72 RCIBSS RC1355 RC13SS RC1355 RC13SS RC1355 RC1350 AF37A172 RC135V AF37AT72 RC135V TC135U TC135V AF37AT72 DAT AUG AUG SEP SEP SEP SEP OCT OCT OCT NOV NOV NOV NOV NOV DEC DEC DEC DEC JAN JAN JAN JAN FEB FEB FEB I CERTIFY THAT I TAIL DUTY NUMB POSN PR1 INST EVAL 01'" TOTAL 14 64-4041 MCAE 362-6002 MCAE 062-4127 MCAE 2.1 0-0 0.0 1.0 5.2 14 62-4127 MCAE 262-4127 MCAE 264-4048 462-6003 MCAE 162-6002 MCAE 162-4131 MCAE 362-4133 MCAE 162-6002 MCAE 262-4128 MCAE 062?4128 MCAE 162-4128 MCAE 1.7 1.5 0.0 0.0 4.8 14 62-4128 HCAE 262-4120 MCAE 062-4128 MCAE 3.7 3.7 0.0 0.0 3.0 10.4 14 62-4128 MCAN 264-4849 MCAN 7.0 6.0 0.0 0.0 0.5 13.5 15 62-6003 MCAE 164-4848 MCAE 262-6003 MCAE 364-4848 MCAE 462-4133 MCAF 162-4127 MCAE 162-6002 MCAE 1.5 1.5 0.0 0.0 0.0 3.0 HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. PAGE 2 SET INDIVIDUAL FLIGHT RECORD REPORT (PA) GRADE: CMH SRT 3 cauzca Ca?azaia SIGNATURE 6-4 1 CP1 PRL CREW POS: AS OF 01 MAY 2015 SR7 NITE PCN SA036-F70 PRI AIRCRAFT: RC135V U13 DATE NVG RES UPDATED 20140819 20140904 20140912 20140912 20140918 20140923 20141006 20141017 20141030 20141029 20141106 20141111 20141119 20141205 20141205 20150107 20141211 20150112 20141216 20150109 20150128 20150430 20150130 20150205 20150217 20150217 ACC PAGE 2 DATE RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 01 MAY 2015 20:24 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS or 01 my 2015 pm INQUIRY NAME: W'me 90PM 557m: m-n- GRADE: CPT PR1 P05: 0 PR1 AIRCRAFT: Rc135v CMD: ACC WING: UNIT: 0343RCN50 ACFT OPLOC: SGBP TAI DUTY CMB 5 51M DATE MUS DATE NUHB POSN PR1 SEC INST EVAL 01'" TOTAL SRT CMB SRT SRT NITE 1N5 1N5 MIG RES UPDATED AF37AT72 20 FEB 15 62-6002 MCAE 120150305 00 MAR 15 52-4130 MCAE 120150310 RCISSW 07 MAR 15 62-4138 MCAE 120150317 RCIBSW 09 MAR 15 62-4130 MCAE 120150317 Rc13sw 09 MAR 15 52.4135 MCAE 020150317 10 MAR 15 62-4135 MCAE 4.2 4.5 0.0 0.0 4.8 1320150317 AF37AT72 13 MAR 15 62-5003 MCAE 120150317 AF37AT72 23 MAR 15 62-6002 MCAE 120150323 AF37AT72 16 APR 15 62-6002 MCAE 120150420 CMB SIM MDS SUMMARY FRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS AIRCRAFT: 131.4 120.3 0.0 0.0 42.5 302.2 47 0.0 0 0.0 0 34.5 25.7 0.0 0.0 SIMULATOR: 20-3 16.6 0.0 0.0 3.0 39.9 14 MA 0.0 1.0 5.0 0.0 RPA0.0 0.0 0.0 0.0 ACC PAGE 3 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 3 6-42 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.2.7. INDIVIDUAL TRAINING SUNINIARY PREPARED 13 MAY 2015 19:48 INDIVIDUAL TRAINING AS OF 13 MAY 2615 CURRENT TRAINING PERIOD NAME: GRADE: SSAN: no-" (new POSITION- MCAE UNIT: 0343RCNSO PHYSILAL um: um: 19 AUG 15 PHYSIOLOGICAL DUE DATE: 39 APR 16 RECORDS REVIEW DUE DATE: 29 FEB 16 ACC TASK 3 DATE LAST DATE DVR IN REST CD QUALIFICATION PROFILE TASK NAME ED RED ACECMP REM ACCONP IN WASP DATE DUE DUE PHS (ODE W0 cn cm aJ/cS/ce mus) care CPLT CHINE) TOT APPROACHES APOO CPLT (MINE) FREE CPLT CNNE) ?on-ma APP APGZ CPLT PENETRATION M703 (mm msnma/couv CPLT CHINE) MISS APP-MN AP19 .owe? mums APP CPLT CHINE) VFR APP APTaura/ca mm HOLD 9mm CHINE, 55 APP AP29 a 10 FEB 15 1 CN CPLT EMIOUTE DESCENT 2 36 [5 I CPLT CIIHF) Ilg GVRD ?'mcs/ca (mm TOTAL was 9 9 15 1 cu cm cumEPLT RECEIVE REFUEL ARGO musCPLT (FINE) REE BREAKAHAY A813 it! CPU CHINE) DION 3 RDZ ARZO 1 24 NOV 1? I CPLT CHINE) INS-TR DEPART DPBI CPLT TOTAL LNDG IDGO CPLT CHINEsums/ca cum? mm Luca weCPLT CURE) TOUCH AND GO L003 9 19 15 FEB I Acc PAGE 1 PAGE 1 G-43 RC-I 35 V, 64-4848. Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2915 19:48 INDIVIDUAL TRAINLNG SUMMARY A5 or 13 my 2515 pm ?935.119 CURRENT WAINTNG PERIOD NAME: [M'smp CPT SSAN: mm- CREW POSITION: MCAE umr: osasawso PHYSICAL nus DATE: 19 AUG 15 PHYSIOLOGICAL DUE DATE: 30 APP. 15 RECORDS nevxew cue 29 FEB 15 ACC pan TASK DATE LASI DATE 01m 1N new CD OUAUFICATIW PROFILE TASK NANE 10 RED ACCOMP IN PHASE DATE DUE OLE VHS CODE WU CH LND GEAR AL7 EX ?015 1 1m HE 14 I CPLT CHINE) DEG ELECTRO SPE 2 IN 24 JUN 14 (H EPLT SIM 1L5 CPLT 51" VFR APP MFBB CPLV W15) 51" HOLD PAT 51" GPSIGLS APP HFQD 2 2 0 24 15 I CPLT CHME) SIM ENROUTE DES "3?CPLT (NINECPLT CWNE) REC AIR BRKAHAV CPLT Stu ?(0'INSTR DEF F1ng CPLT SIN LAND MF97 15 59 24 15 I CPLT LND GEAR ALT CPLT SIM RECEIVER TOTM 9 5 13 I5 I (H Cm?) SIM ALERT PROC M694 CPLT CHINE, SIM START PROC M595 1 2 22 JAN 15 I CPLT CWHU SIH 5Y5 NAV LEG M605 6 9 26 MAR 14 CPLT OWE) SIM RIVET JOINT RAP M593 9 24 APR 1,5 I CH (FLT SIM COBRA BALL RAP M609 0 9 I CH CWBNI SEW MP M613 9 a I CPLT 51" IN) INITIAL 135 CURKBUCY H612 0 9 24 APR 15 I CHRHI) 51H "013 1 3 76 APR 15 I CPLT 51M STATIC M614 1 3 74 15 I Acc PAGE 2 PAGE 2 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:48 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2015 PCN SAOBE-TIO CURRENT TRAINING PERIOD NAME: [MBhap co'P'bt] GRADE: CPT SSAN: CREW POSITION: MCAE UNIT: 0343RCNSO PHYSICAL DUE 19 AUG 15 PHYSIOLOGICAL DUE DATE: 30 APR 16 RECORDS REVIEW DUE 29 FEB 16 Acc p511 TASK A DATE LAST DATE UVR IN REST CD QUALIFICATION moms TASK NAME 19 RED REM ACCOMP PHASE DATE DUE DUE Ens can: (H CPLT 0111):) MODE H615 1 1 03 NOV 14 (H CPLT SIM-E1101 PROF CELT CMRTE) TOT 5m M157 CPLT RJ/c5/ca (we) 515 LEG N591 CPLT CMRTE) AUWENT M11 CPLT CMRTE) TOT SIM RAE $009 CELT CRETE) 51R REF 50sz 5095 a 1 15 APR 15 I CELT 011115) 5111 Em?) 5014 CPLT CMRTE) 51R (1R AEE 5015 (Matt) 51)! TNST SORTTF son CELT (mus) 51R EREC APP 5018 CELT (MATE) 5m NEREC APP $019 CELT cmtE) PRE DEPLOY sm 5045 27 MAY I cu CELT (MATECPLT SIHR DAY LAND 5054 CELT (mus) 51m NIGHT LAND 5055 CPLT ONE) SIAR TCH 5. so 5056 23 24 APR 15 I CH AIR DAY 5066 1 13 MAR 15 CH CPU CMNF) 51m AIR NITE 506! 25 AUG 14 I CH CELT (1111(6) 2/3 5073 CPLT R1/c5/cu CMRTE) 51m TAKE on 5014 CPLT (mm) 51? RENDEZVOUS 5099 CELT R1/c5/Ca TOT RAE 51100 CPLT CRME) RJ RAE 51159 1) 11 19 MAR 15 1 ACC PAGE 3 PAGE 3 6-45 RC-I35V, 64-4848. Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:48 INDIVIDUAL TRAINING SUMMARY ,5 or 13 my 215 pcu ?936-710 CURRENT TRAINING PERIOD NAME: GRADE: CPT SSAN: "hm CREW POSITION: MCAE PHYSICAL DUE DATE: 19 AUG 15 PHYSIOLOGICAL DUE 30 APR 16 RECORDS REVIEW DUE DATE: 29 FEB 16 ACC TASK LAST DATE DVR IN CD QUALIFICATION PROFILE NAME 10 RED REM IN WASE DATE DUE DUE PHS CODE W0 CH CPLT CHRTE) RJ RAP C0 5859C CPLT (AME) R3 RAP SR59R CPLT CMTNE) CB RAP SHEET CPLT CB RAP C0 SRGOC 0 0 I CH CHRTE) CB MP SRGOR 12 DEC 1? 1 CH CPLT (WNET C5 MP 0 1 CH (FLT CS MP C0 SRGIC 0 9 I CH CPLT CS RAP 5R61R 0 LT 1 CH CPLT PILOT PRO SRTY SRTH 5 a 28 15 I CH CPLT CHRIS) TOT 5X90 (FLT BASIC SORTIE 5X93 CPLT CWNE) TOT T705 T000 CPLT INITIAL T093 CPLT CWNE) T099 CPLT CHTNE) STATIC T019 GRND AFE FIT CHECK LL07 0 5 97 APR 14 GT GRND PILOT ?GRND PILOT ANTLHIJACK GRND PILOT ?GRND PILOT TRAINIM PODHA (JANWWI.) VILOT WINIW "9 DUNGRND PILOT TMINIW ACAD GRND PILOT WINIW SCPT (1503 CRND PILOT WATNTM STAN EVAL TEST G505 ACC PAGE 4 PAGE a 6-46 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:48 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2015 SA036-T10 CURRENT TRAINING PERIOD NAME: [Mmap co?P'bt] GRADE: CPT SSAN: CREW POSITION: MCAE UNIT: PHYSICAL DUE DATE: 19 AUG 15 PHYSIOLOGICAL DUE DATE: 30 APR 16 RECORDS REVIEW DUE DATE: 29 FEB 16 Acc PGH TASK VOIIDUR DATE LAST DATE ova 1N REST CD WALIFICATION PROFILE TASK NAME 10 RED ACCOMP REM ACCOMP IN PHASE DATE DUE DUE (ODE WU GT GRNO PILOT TRAINING IRL G586 GRNO P1L01 TRAINING OPLAN sum G522 19 on 12 In GRNO PILOT TRAINING A/c SERVICI- 6525 GRNO PILOT TRAINLNG 5nmv 1m, (1520 TRAINING RISNO (LAT 6550 PILOT TRAINING RISND smov 6551 GINO PILOT TRAINING 9910 c2 PRO 6559 GRND PILOT TRAINING s1: TEST sec G572 1/25 A GT (3ND PILOT TRAINING ISO PREP "502 CRND PILOT TRAINING INTEL TRNG IEOS a 17 521: 14 311 562 15 GT GRNO PILOT TRAINING AFE FAN TRNG LL01 as an 12 6 GT GRNO PILOT TRAINING EGRESS (NONEJT LL03 (RND PILOT TRAINING Ach L194 GRNO PILOT TRAINING EGRESS 1105 a 05 OCT 12 . GT GRND PILOT TRAINING AFE TRNG 11CRND PILOT TRAINING LOCAL AREA SURV 5501 a 04 OCT 12 GT GRNO PILOT TRAINING CHBT SURV TRNG 5502 GRNO PILOT TRAINING CAC TRNG 5503 GRNO PILOT TRAINING NST 5505 GRND PILOT TRAINING (CSII 5597A Gr GRND PILOT TRAINING cemcon (c511 5507c 24 5111 13 31-) 51:11 16 GT GRND PILUT TRAINING :ucon (c511 5507: a GRND PILOT TRAINING r-Acm 551m 0 GT GRND PILOT TRAINIW SOUTHCOH (C51) 55075 0 ACC PAGE 5 PAGE 5 G-47 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:48 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2915 PCN CURRENT TRAINING PFRIOD NAME: [M'Shap GRADE: cm SSAN: m-N mew posmou: MCAE mm: asasacnso PHYSICAL DUE DATE: 19 AUG 15 PHYSIOLOGICAL DUE DATE: 30 APR 15 RECORDS REVIEW DUE DATE: 29 FEB 16 ACC TASK DATE LAST OUR R551 (0 QUALIFICATION PROFILE TASK NAME ID R50 ACCWP REM ACCONP IN WASH DUE DUE W5 CODE WW GT GRND PILDT SPEC SERE TRNG 5519 (51 GRND PILOT TRAINIHS S-V83-A $524 0 9 27 JUL 12 ACC PAGE 5 PAGE 6 G-48 GL3. CAPT [Mishap Navigator] (MN) 64?4848, Class A, 30 April 15, AFSAS #739726 G1.3.1. CERTIFICATE OF AIRCREW QUALIFICATIONS BAIL 6 Marlo? mm :1 Certi?cation; SQUADRON 343 RS unv '3 1 I: NAME 2 8 3 a 2 REMARKS I I 055/05saws/(p5 ialmnanuu', 343 RS G-49 Gl.3.2. FLYING HISTORY REPORT PREPARED 01 MAY 2015 20:12 "m5 :[Mishap Navigator] (MD: Acc mucmsasncus AIRCRAFT AIRCRAFT MDS FLT DTY CERT CODE MNAF DATE FIRST 12 JAN 69 DATE LAST 16 APR 15 TOTAL TIME 583.9 PRIMARY TIME 547.9 SECONDARY TIME 11.6 INSTRUCTOR TIME 0.8 EVALUATOR TIME 0.9 OTHER TIME 23.5 NIGHT 11.2 PRIMARY INST 6.9 PRIMARY SIN INST 9.0 NVG TIME 0.0 COMBAT TIME 397.5 CMBT SUPPORT TIME 0.9 COMBAT SORTIES 36 CMBT SUPPORT 9 TOTAL SORTIES 65 SSAN: psu cm? was: 1 HNAE 21 NOV 08 25 JAN 15 1978.5 1939.7 l-?h-l .. OHLDGOID FLYING HISTORY REPORT (PA) GRADE. CPT PRI ACFT: RC1355TS) MNAE N0 DATE NO DATE 0.0 INQUIRY HNAE ND DATE N0 DATE PAGE 1 6-50 API: 6 OFOA: 95 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 AS OF 01 MAY 2015 ASC: 1A ASC BASE: OFFUTT AFB MNAE 64 NOV 98 17 MAR 15 140. 125. MNAE 27 JAN 09 96 JUL 11 A3.3 oocoeewsew? . . . a . MNAE 08 SEP 08 15 APR 15 116.8 85.6 on.)an GODGDDOG PCN 5A036-F40 10 MAR 99 SN N0 no DATF CD :3 00000620003193 PAGE 1 PREPARED 01 MAT 2015 20:12 [Mishap NaVIgator] CMD: ACC WING: 0343RCNS AIRCRAFT TOTALS AIRCRAFT MOS FLT DTY CERT CODE SN DATE FIRST FLowu N0 DATE DATE LAST FLOWN N0 DATE TOTAL TIME PRIMARY TIME SECONDARY TIME INSTRUCTOR TIME EVALUATOR TIME OTHER TIME NIGHT PRIMARY INST PRIMARV SIM INST NVG TIME COMBAT TIME CMBT SUPPORT TIME COMBAT SORTIES CMBT SUPPORT SORTIES TOTAL SORTIES ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 FLYING HISTORY REPORT (PA) INQUIRY SSAN: GRADE: CPT API: 6 PRI CRW P05: 1 PR1 ACFT: RC135V CAREER TOTALS CREW PORTTION (SO PRIMARY TIME 1750.2 SECONDARY TIME 25.4 INSTRUCTOR TIME 0.0 EVALUATOR TIME 0.6 OTHER TIME 69.9 TOTAL TIME 1845.5 STUDENT TIME 72.6 OTHER US MIL TIME 9.0 FOREIGN MIL TIME 0.9 CIVILIAN TIME 9.0 COMBAT TIME 1067.4 COMBAT SUPT TIME 4.3 TOTAL SORTIES 226 COMBAT SORTLES 94 COMBAT SUP SORTIES 1 NVG TIME 9.0 DATE FIRST FLOWN 06 SEP 09 DATE LAST FLOWN 16 APR 15 GRAND TOTAL 1918.1 PAGE 2 6-5 1 OFDA: 95 AS OF DI MAY 2915 ASC: 1A BASE: OFFUTT AFB PCN SA036-F4O ASC DATE: 10 MAR 69 PAGE 2 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.3.3. 30/60/90 FLYING HISTORY REPORT PREPARED 29 MAY 2915 O9 19 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 29 MAY 2915 PCN SAO39-F29 Nav'gator] GRADE. CPT SSAR: API: 9 FAC: 3 ASC: TA DAFSC: Lennav AGE: an: Acc WING: 9343RCNSO ORGANIZATION: CREW POSITION: MNAE ASC DATE: 19 MAR 2999 CDRR RATING: SENIOR COMBA1 SYSTERS OFFICER AIRCRAFT TYPE: Rc135v SERIAL no: 94-4949 MTSHAP DATE 39 APR 2915 c-3 MISHAP AIRCRAFT PRI SEC INST EVAL OTHER TOTAL NIGHT IRS SIR INS SORT RC135V 547.9 11.9 9.9 9.9 23.5 593.9 547.9 11.2 9.9 9.9 95 LAST 39 DAYS 9.4 9.9 9.9 9.9 2 1 11.5 9.4 9.9 9.9 9.9 3 LAST 69 DAYS 9.4 9.9 9.9 9.9 2.1 11.5 9.4 9.9 9.9 9.9 3 LAST 99 DAYS 9.4 9.9 9.9 9.9 2.1 11.5 9.4 9.9 9.9 9.9 3 OTHER AIRCRAFT xr? 991 sec INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT 1839.7 2.9 0.8 8.3 35.9 1078.5 1839.7 19.1 6.9 0.9 110 LAST 39 DAYS 9LAST 69 DAYS 9LAST 99 DAYS 9.9 9.9 9.9 9.9 9.9 9.9 9.9 9.9 9.9 9.9 RCIBSS 9LAST 39 DAYS 9LAST 69 DAYS 9LAST 99 DAYS 9Rc135u 9LAST 39 DAYS 9LAST 50 DAYS 0LAST 99 DAYS TC13sw 125.5 7.7 9.9 9.9 7.5 149.7 125.5 24.8 9.9 9.9 39 LAST 39 DAYS 9LAST 69 DAYS 5LAST 99 DAYS 5PAGF 1 C952 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 20 MAY 2015 09 10 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 20 MAY 2015 PEN SAeaa-Ez0 Nav'gator] GRADE: CPT SSAN: m-w API: 6 PAC: 3 Asc: 1A DAFSC: L012R3Y AGE: CMD: ACC WING: 9343RCN50 ORGANIZATION: 0343RCN50 CREW POSITION: MNAE ASC DATE: 10 MAR 2009 CURR RATING: SENIOR COMBAT SYSTEMS OFFICER AIRCRAF1 TYPE RC135V SERIAL No: 64-4848 MISHAP DATE: 30 APR 2015 OTHER AIRCRAFT PRI SEC INST EYAL OTHER TOTAL NIGHT INS SIM INS SORT Tc13ss 37.1 3.2 0.0 0.0 3.0 43.3 37.1 0.0 0.0 0.0 9 LAST 39 DAYS 0LAST 60 DAYS LAST 90 DAYS AF37AT72 85.6 0.0 0.0 0.0 31.2 116.8 85.6 0.0 0.0 0.0 38 LAST 39 DAYS 6LAST 59 DAYS 2LAST 90 DAYS 2F37AT4S 0LAST 30 DAYS 0LAST 59 DAVS 0LAST 90 DAYS 0T943A 0LAST 30 DAYS 0LAST 69 DAYS 0LAST 90 DAYS 0PAGE 2 G-53 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 20 MAY 2615 09:16 AIRCRAFT NISHAP INVESTIGATION (PA: AS OF 20 MAY 2015 PCN SAose-Eze NAME: [MiShap NaVigatorl GRADE: CPT SSAN: API: 6 PAC: 3 ASC: 1A OAPSC: L012R3Y AGE- CMD: ACC WING: 0343RCNSO ORGANIZATION: G343RCNSO CREW POSITION: NNAE ASC DATE: 10 MAR 2009 CORR RATING: SENIOR COMBAT SYSTEMS OFFICER AIRCRAFT TYPE: Rc135v SERIAL NO: 64-4848 MISHAP DATE: 30 APR 2015 OTHER AIRCRAFT PRI SEC INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT CAREER TOTALS CREW POSITION FIRST FLIGHT PR1 SEC INST EVAL OTHER TOTAL STUDENT COMBAT CWBAT SORT LAST FLIGHT TIME SUPPORT COMBAT SYSTEMS OFFICER 66 SEP 2969 1756.2 25.4 0.0 0.0 69.9 1845.5 1750.2 72 6 1067.4 4.3 220 15 APR 2915 PAGE 3 G-54 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.3.4. INDIVIDUAL DATA SUMMARY FOR OFFICIAL USE ONLY PREPARED 01 MAY 2015 20:12 INDIVIDURL DATA SUMMARY (PA) 55 0F 01 MAY 2915 PCN 5A036-A79 INQUIRY NAME: [M'Shap Nav'gam SSAN: GRADE: (PT 040: ACC WING: 0343RCNSO UNTT: 0343RCNSO BASE: OFFUTT AFB PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: USN SECURITY CLEARANCE DATE: 09 FEB 14 SVC CAT: USAF RESTRICTED AREA BADGE NO: LAST PHYS DATE: PROFESSIONAL DUAL INDEX (POI): PHYS CODE: PROFESSIONAL DUAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: PHYSIOLOGICAL TNG DATE: STATUS PHYSIOLOGICAL DUE DATE: DATE OF BIRTH: DATE ASSIGNED JUMP STATUS: DUTY AFSC: L012R3Y EFFECTIVE DATE OF DUTY: 01 SEP 14 SHORT TOUR INDICATOR: ?Am 555p DATE RETURN FRM OVERSEAS: DEPLOYED ?Am c005: DATE OF RANK: 26 JAN 11 DEPLOYED DATE: DATE OF REDEPLOYED DATE DEP LAST DUTY STA: 30 MAY 68 . DATE ARR THIS STATION: 02 JUN as $333; $513? DATE: 20 my 14 PERSONNEL RECORD STATUS: '9 RECORDS REVIEW DUE DATE: 31 MAY 15 PROJECTED DAFSC: RECORDS REVTEV STATUS CODE: PROJECTED PAS CODE: PROJECTED DUTY PROJ DEPARTURE DATE: PROJ REPORTING DATE: PAC 3 EFFECIIVE DATE. LOCAL use CODE: I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE ACC PAGE 1 PAGE 1 G-55 PREPARED 01 MAY 2015 20:12 NAME: [Mishap Navugator] BASE: OFFUTT AFB AIRCRAFT ASSIGNMENT DATA AIRCRAFT OPLOC: CMD OF AIRCRAFT: ACFT SVC CAT: PRIMARY ACFT: FLT DUTY CERT CODE: CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA LAST MPO DATE: LAST MPO REASON: PAY STOP DATE: LAST PRODUCTIVE FLIGHT DATE: PREVIOUS PRODUCTIVE FLIGHT DATE: AVIATION SERVICE DATA AVIATION SERVICE CODE: EFFECTIVE DATE: PRIOR ASC: EFFECTIVE DATE: AERD ORDER TERM DATE: OFFICER SERVICE DATE: AVIATION SERVICE DATE: TRANSITION STATUS AVIATION POSITION INDICATOR: EFFECTIVE DATE: FLYING ACTIVITY CATEGORY: OFDA GATE OFDA GATE 15/15: OFDA GATE 26/18: OFDA TO RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 SSAN: 4" SGBP 1C USAF RC135V MNAE 18 MAY 07 A NONE INDIVIDUAL DATA SUMMARY (PA) INQUIRY AS OF 01 MAY 2915 PCN SAOBG-A7D GRADE: CPT CMD: ACC G343RCNSO UNIT: AERONAUTICAL BADGE AERONAUTICAL RATING: SENIOR COMBAI SYSTEMS OFFICER EFFECTIVE DATE: 1L APR 15 AERONAUTICAL RATING: COMBAT SYSTEMS OFFICER EFFECTIVE DATE: 11 APR 08 DUS MIL RTG DT: CURR PARA RATING: CURR PARA RATING DATE: ORIG PARA RATING: ORIG PARA RATING DATE: STATUS FORMAL COURSE DATE REFRESHER PHYSIOLOGICAL HYPOXIA TRAINING 02 DEC 11 INITIAL PHYSIOLOGICAL HYPOXIA TRAINING 22 MAY 07 Your current OFDA is 95 nonth(s). You need 1 additional nonth(s) OFDA to meet your 12 Year gate requirement to receive continuous ACIP through 18 years of aviation service and you must maintain a valid flight physical. I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE ACC PAGE 2 PAGE 2 6-56 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.3.5. INDIVIDUAL FLYING TIME SUMNIARY PREPARED 13 MAY 2015 20:07 INDIVIDUAL TIME qu, AS OF 13 MAY 2015 PCN REQUEST PERIOD FROM: 30 APR 2014 TO- 30 APR 9015 [Mishap Navigator] NAML: SSAN: GRADE: (PW PRI CREW P05: PRI AIRCRAFT: RC135V CMD: ACC WING: 0343RCNSO UNIT: 0343RCN50 ACFT OPLOC: SGBP TAIL DUTY CMB SIM M05 DATE NUMB POSN PR1 SEC INST EVAL 0TH TOTAL SRT (MB SRT NITE INS 105 NVG RES 4537477 25 JUL 14 62-6093 MNBE 462-6003 MNBE 162-6003 HNBE 102-0903 HNBE 16003 MNBE 00.0 0.0 0.0 0.0 (MB SIM AF37AT72 SUMMARY PHI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT MITE INS INS NVG AIRCRAFT0.0 0.0 0.0 0-0 SIMULATOR: 9.0 0.0 0.0 0.0 3.5 12.5 5 0.0 0.01 0.0 0.0 RPA0.0 0.0 0.0 0.0 RC135V 13 MAY 14 62-4135 MNBE 764-4841 MNBE 254.4341 MNBE 7.3 0.0 0.0 0.0 7.4 1464-4848 MNBE 10.6 0.0 0.0 0.0 0.0 1064-4848 MNBE 10.7 0.0 0.0 0.0 0.0 1063-9792 MNBE 11.3 0.0 0.0 0.0 0-0 11.3 1 1162-9792 muse 11.2 0.0 0.0 0.0 0.0 11.2 1 1163-9792 HNBE 11.8 0.0 0.0 0.0 0.0 11.8 1 1163-9792 MNBE 11.2 0.0 0.0 0.0 0-0 11-2 1 1163-9792 HNBE 11.5 0.0 0.0 0.0 0.0 11.5 1 1163-9792 MNBE 111163-9792 MNBE 11.3 0.0 0.0 0.0 0.0 11.3 1 1164-4848 NNAE 764-4840 MNAE 20.0 0.0 0.0 0.0 ACC PAGE 1 PAGE 1 G-57 PREPARED 13 MAY 2015 20:07 NAME. [Mishap Navigatorj CMD: ACC WING: B343RCNSO TAIL MDS DATE NUMB RCIBSV SUMMARY RI SE AIRCRAFT: 12 .6 0. SIMULATOR: .0 0. RPA: .0 0. RC135W 14 JUN 14 62-4132 15 JUN 14 62-4132 26 OCT 14 62-4131 27 OCT 14 62-4131 07 DEC 14 62-9792 09 DEC 14 62-4139 14 DEC 14 62-6126 17 DEC 14 b3-9792 23 DEC 14 63-9792 03 JAN 15 63-979? 09 JAN 15 62-4135 16 JAN 15 62-4138 18 JAN 15 62-4138 22 JAN 15 62-4138 25 JAN 15 62-4135 0 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL FLYING TIME SUMMARY (PA) REQUEST PERIOD FROM: 30 APR 2014 UNIT: 0343RCNSO DUTY POSN p4 aucacaz MNBE MNBE MNAE MNAE MNBE MNBE MNBE MNBE MNBE MNBE MNBE MNBE MNBE MNBE MMAE PR1 \Jl? ai?d Ch CICD oxa?ai: SEC 0 ?r?vb:o c>E>c:c:s ata?m INST EVAL 0TH TOTAL SRT 1.5 138PAGE 2 ACFT OPLOC: SGBP 0TH TOTAL SRT G-58 S-u a mSviu 6 mlv:~ (NE 79.4 0.0 Pbb?k?h?HIH GRADE: (PT AS OF 13 MAY 2015 30 APR 2015 PRI CREW P05kth D G119 CICD C31: 0.0 0.0 h?r?t? 0 GIG (3 ?353 CDID C3 GIC) FICD CJED F113 C3 (3 EDCD GIGS CICDCDID CICD CI SRT SRT 0 0 GDIDIQ ?313 ?lth GDCD GSCB13 CD (DID C3 (DID GDIH UJ CIGD RDJS C143 *4 DIED CD UWCD C) val: PCN SA036-F70 INS (3?3 CJPQ FD 6913 C3 83:3 G353 FD FICD CDC: CJID Cit: GICICD GDCD GICD SIM INS (D C) c113 Ell: CJED <5 CICD CICD CICD . . . . . . . . . . . . . . (D 6) 61:3 Ella <3 CDID can: GICD ACC NVG SIM INS 0.0 0.0 (2 GDCD 63(313 Gil: (DID 23:3 (3 C3 GICD ?3 55C) CBID CDCB C3 PAGE 2 PRI AIRCRAFT: RC13SV p<9g>z seam RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:07 INDIVIDUAL FLYING TIME SUMMARY (FA) AS OF 13 MAY 2615 REQUEST PERIOD 30 APR 2014 T0: 30 APR 2015 HE [Mishap Navigator] econ NA SSAN: CPT PRI cnew POS: p01 AIRCRAFT: nc135v CMD: ACC 0343RCNSO UNIT: 9343RCN50 ACFT TAIL DUTY cue 510 was DATE NUMB POSN PR1 sec INST EVAL 0TH TOTAL SRT cna SRT SRT NITE INS TNs ch 055 cue SIM Rc135w SUMMARY PRI sec INST EVAL 0TH TOTAL SRT :00 SRT SRT NITE INS 1N5 AIRCRAFT: 133.0 0.0 0.0 0.0 13.9 152.5 15 123.3 11 0.0 0 16.5 0.0 0.0 SIMULATOR0.0 0.0 0.0 RPA0.0 0.0 0.0 Tc135w 01 MAY 14 62-4129 MNBE 462-4127 MNBE 562-4127 MNAE 50.0 3.7 0.0 0.0 0.0 cna SIM TC135W SUMMARY PR1 SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS 1N5 AIRCRAFT: 14.7 0.0 0.0 0.0 0 0 14SIMULATORRPACMB SIM GRAND TOTALS PRI sec INST EVAL 0TH TOTAL SRT cna SRT c/s SRT NITE INS INS AIRCRAFT: 279.9 0.0 0.0 0.0 25.4 305.3 33 202.7 10 0.0 0 29.1 0.0 0.0 0 9.0 0.0 0.6 0.0 3.5 12.5 5 0.9 0.0 0.0 0 RPAACC PAGE 3 PAGE 3 6-59 @9963 Ea?a?361 RC-I35V, 64-4848. Class A, 30 April 15, AFSAS #739726 G1.3.6. INDIVIDUAL FLIGHT RECORD PREPARED 01 MAY 2015 20:12 INDIVIDUAL FLIGHT RECORD REPOKT AS OF 0] MAY 2015 PCN SA036-F70 moumv New} 5549: GRADE: CPT m1 CREW P05: PRI AIRCRAFT: RC135V c149: 49c 9199: 934390159 UNIT: 934390159 ACFT 9919c: SGBP TAI DUTY CH8 IS SIM DATE HDS DATE NUMB POSN PR1 SEC INST EVAL 0TH TOTAL SR1 CH8 SR1 SRT NITE 1N5 INS NVG RES UPDATED RC135V 91 APR 14 92-4132 MNBE 729149591 91 MAY 14 524129 14999 429149596 RC135V 13 MAY 14 62-4135 MNBE 720140514 1103514 14 JUN 14 62-4132 9199: 9.2 9.9 9.9 9.9 9.1 1229149629 9913514 15 JUN 14 92-4132 MNBE 229149926 RC135V 16 JUN 14 64-4841 220140024 RC135V 17 JUN 14 64-4841 MNBE 7.3 0.0 0.0 0-0 7-4 1420140624 AF37A172 25 JUL 14 926993 was 429149731 mm 99 512914 644949 was 19.9 9.9 9.9 9-9 9.9 1929149912 TC135W 10 SEP 14 52-4127 PNBE 520140925 RC135V 19 51:9 14 64-4849 14999 19.7 9.9 9.9 9.9 9.9 1929149924 49374172 25 5129 14 62?6993 mars 129141917 RCISSW 26 OCT 14 62-4131 MAE 620141030 909591 27 ocr 14 62-4131 MAE 529141939 49374172 21 nov 14 92?6993 MNBE 129141292 RC135W 07 DEC 14 52-9792 MNBE 11.9 0.0 0.0 0.0 0.0 11.0 1 1120141209 RC135W 09 DEC 14 6294139 MNBE 11.4 0.0 0.0 0.0 0.0 11.4 1120141211 9913591 14 99114 62-4129 14999 19.9 9.9 9.9 9.9 9.9 19.9 1 1929141214 9c135w 17 DEC 14 93-9792 mm: 11.6 9.9 9.9 9-9 9.9 11.9 1 1129141219 RCUSV 20 DEC 14 53-9792 HNBE 11.3 0.0 0.0 0.0 0.0 11.3 I 1120141221 acnsw 23 99: 14 63-9792 14999 19.9 9.9 9.9 9.9 9.9 19.9 1 1929141225 ac135v 29 99: 14 62.9792 MNBE 11.2 9.9 9.9 9.9 9-9 11.2 1 1129141229 RC135V 29 DEC 14 63-9792 MNBE 11.8 0.0 0.0 0.0 00 11.8 1 1120141230 RCISSV 01 JAN 15 53-9792 MNBE 11.2 0.0 0.0 0.0 0-0 11.2 1 1120150102 ac13sw 9314915 93-9792 MNBE 11.2 9.9 9.9 9.9 99 11.2 1 1129159193 RCUSV 05 JAN 15 63'9792 HNBE 11.5 0.0 9.0 0.0 0.0 11.5 I 1120150100 ACC PAGEI 1 CERTIFY 1941 I HAVE REVIEWED 14v 1999 AND 11 15 COMPLETE 4149 ACCURATE. 5191141945 9419 PAGE 1 6-60 RC-I35V, 64-4848, Class A, 30 April 15. AFSAS #739726 PREPARED 01 MAY 2015 20:12 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 01 MAY 2015 PCN SA036-F70 INQUIRY [Mishap Navigator] NAME: SSAN: GRADE: CP1 PR1 CREW P05: PR1 RC135V ACC WING: 0343RCNSO UNIT: 0343RCNSO ACFT OPLOC: SGBP TAIL DUTY CMB US 511'! DATE 1105 DATE NUMB POSN PRI sec INST EVAL 01? TOTAL SRT CMB 5111' US SRT NITE INS INS ch RES UPDATED 09 JAN 15 62-4135 MNBE 11.2 0.0 0.0 0.0 0-0 11.2 1 1120150109 RC135V 12 JAN 15 63-9/92 MNBE 11.1 0.0 0.0 0.0 0.0 11.1 1 1120150113 9.03511 16 JAN 15 62-4138 MNBE 10.0 0.0 0.0 0.0 0.0 10.0 1 1020150116 18 JAN 15 62-4138 MNBE 11.4 0.0 0.0 0.0 0.0 11.4 1 1120150118 RC135V 20 JAN 15 63-9792 MNBE 11.3 0.0 9.0 0.0 0.0 11.3 1 11.3 1 0.0 0 0.0 0.0 0.0 0.0 20150120 22 JAN 15 62?4138 MNBE 11.5 0.0 0.0 0.0 0.0 11.5 1 1120150123 RC135W 25 JAN 15 62-4135 MNAE 5.7 0.0 0.0 0.0 5.7 11.4 1 1120150126 AF37AT72 06 MAR 15 62-6003 MNBE 120150309 TC135W 17 MAR 15 62-4127 MNAE 50.0 20150324 RC135V 06 APR 15 64-4848 MNAE 720150407 AF37AT72 15 APR 15 62-6003 MNBE 020150420 RC1351I 16 APR 15 64.4048 MNAE 220150424 CMB SIM "05 SUMMARY PRI SEC INST EVAL 01?? TOTAL SRT SRT SRT NITE INS INS NVG AIRCRAFT: 287.1 0.0 0.0 0.0 25.4 312.5 34 202.7 18 0.0 0 29.1 0.0 0.0 0.0 SIMULATOR: 9.0 0.0 0.0 0.0 3.5 12.5 5 0.0 0 0 0.0 0.0 RPA0.0 0.0 0.0 0.0 ACC PAGE 2 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 2 G-6l RC-135 V, 64-4848. Class A. 30 April 15, AFSAS #739726 G1.3.7. INDIVIDUAL TRAINING SUMNIARY PREPARED 13 MAY 2015 19:49 NAME. [Mishap Navigator] PHYSICAL DUE DATEICATIDN PROFILE IAV IIAV (E) IE1 (E) (E) (E: (E) {El (E) (E) (E1 181 (E) (E) (E) (E1 (E) 181 (E) (E) (E) (E1 GRADE: CPT INDIVIDUAL TRAINING SUMMARY CURRENI TRAINING PERIOD SSAN: PHYSIOLOGICAL DUE DATE: 31 DEC 16 TASK NANE DUAL EVAL NOLO AAR ROVU REC BREAKAHAY EMCON 3 R02 GEAR ALT EX SIM HOLD PAT REC BMAVIAY SIM ROI SIM LND GEAR ALT EX SIM 5Y5 WW LEG SIM RIVET JOINT RAP 51" 135 CURRENCY SIM MILSTAR TOT SIM SYS NAV LEG MLSIAH AUTDIENT TOT SIM RAP PRE DEPLOY SIM SIM SIM RENDEZVOUS TOT RAP 51.] TASK ID AAel APZS anus ARIZ Aaze L025 ?559 Hrs: "ran M095 M698 M12 "617 H757 N501 RAM RAll 5069 5046 $047 5099 snae 5R59 REG bv-O Mh?p- 9 PAGE 1 AC COMP .- Var-own? G-62 REM DO 100 DATE LAST ACCOMP CREW POSITION: MNAE RECORDS REVIEW DUE DATE: 31 MAY 15 DATE IN PHASE 38 APR 15 AS OF 13 MAY 2615 PCN SAO36.T19 UNIT: 0343110150 DATE DUE 31 OCT 15 OS 1111 REST DUE H15 CODE VIVD VES ACC PAGE I RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:49 INDIVIDUAL TRAINING SUMMARY AS or 13 MAY 2015 SA036-T10 CURRENT TRAINING PERIOD NAME: [M'smp Mammy] GRADE: SSAN: CREW POSITION: MNAF UNIT: 0343chso PHYSICAL nus DATE: 17 JAN 16 PHYSIOLOGICAL DUE DATE: 31 DEC 15 RECORDS REVIEW DUE DATE: 31 MAY 15 ACE DATE LAST DATE DVR REST CU QUALIFICATION PROFILE- TASK NAME 10 RED ACCONP REM IN PHASE DATE DUE DUE PMS CODE 5R59C 18 25 JAN 15 I CH R.) (MR (E) R.) RAP SRO/lam NAV R.) (HR (El TOT 51100 12 23 16 APR 15 15 JLNN 15 1 CU NAV RJ CM (El BASIC SORTTP 5X93 CONSEC TRAINING COMSEC 0109 02 APR IA 9? APR 15 YES 61? COMSEC TRAINING CONSEC Rand GAAI GRND NAV TRAINING ANTI-HIJACK GA93 GRND NAV TRAINING CNN GAOG GRND NAV TRAINING PODHA GA26 cans NAV mums M9 DUAL GRND NAV TRAINING ACAD GAAG GRND NAV TRAINING SEPT 6593 GRND NAV TRAINING STAN EVAL TEST 5595 GRND NAV TRAINING IRC G506 GRND NAV TRAINING DELAN STUDY 5522 1 94 15 GT WU NAV TRAINING NC SERVICE (1515 GMT) NAV TRAINING FLY SAFETY TRNG 6526 GRND NAV TRAINING CERT 6558 GRND NAV TRAINING RISNO STUDY 6551 13 AUG 14 28 FEB 15 YES GRND NAV TRAINING 8016 C2 PRO 6559 GRND NAV TRAINING TEST SEC 6572 YES 61? (AND NAV TRAINING ISO PREP I502 GRND NAV TRAINING INTEL TRNG TFDS GRND NAV TRAINING AFE FAN TRNIS LL91 0 9 35 AUG 08 Acc PAGE 2 PAGE 2 6-63 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2615 19:49 INDIVIDUAL TRAINING SUMMARY AS or 13 MAY 2015 pg: 59.935419 CURRENT TRAINING PERIOD NAME: [MIShap Namator] GRADE: CPT SSAN: CREW POSITION: MNAE UNIT: 0343RCN50 PHYSICAL DUE DATE: 17 JAN 16 PHYSIOLOGICAL DUE DATE: 31 DEC 16 RECORDS DUE DATE: 31 MAY 15 Acc p541 TASK "4 DATE LAST DATE OVR 1N cu QUALIFICATION PROFILE TASK NAME ID R50 acconv REM Accorw IN PHASE DATE nus DUE PIG cone wo GT GRND mw TRAINING (NONEJ) LL03 TRAINING AGGT LL94 GANG TRAINING WACDE LLGs 29 JUL 11 GT GRND TRAINING AFE TRNG LLGG GANG TRAINING LOCAL AREA 5591 TRAINING CNBT TRNG 5502 19 MR 31 MAR 17 GT GRND TRAINING (AC TRNG 5593 GRND TRAINING WST 5595 GRND TRAINING AFRICOM Icsn 5507A 9 14 GT GRND TRAINING CENTCOM Icsn 5507c GRNG TRAINING axon Icsu 55975 I) 14 GT GRND TRAINING PRCOH 55071: 14 GT TRAINING summon ICSIJ 55075 GT GRND TRAINING SPEC SERE TRNG 5519 GRND TRAINING S-V83-A 5524 16 OCT 12 In GRNU R/N/sto Aft FIT mun L192 9 14 MAR 14 6 GI GROUND SDF FLT LINE DRIVE DMZ 6 0 JD AUG 11 31-) AUG 1? YES 0 GT GROUND 50F 50F TRNG 0528 GROUND 50F 50F TOUR C529 ACC PAGE 3 PAGE 3 64?4848, Class A, 30 April 15, AFSAS #739726 GL4. CAPT [Mishap Rave" ?1 (MR1) 01.4.1. CERTIFICATE OF AIRCREW QUALIFICATIONS lel InnEli "mm [MishaoRaven1l .uml mm] ms [cm] olxl le I mam/x I (ommndu, ?43 RS G-65 RC-I35V. 64-4848, Class A, 30 April 15, AFSAS #739726 G1.4.2. FLYING HISTORY REPORT PREPARED 01 MAY 21115 19:33 FLYING HISTORY REPORT (PA) AS OF 91 MAY 2915 PCN 5Aese-an INQUIRY NAME: [Mishap Raven 1] SSAN: nun. GRADE: ART 2 Hm I OFDA: as ASC: 1A Asc DATE: as MAR 13 cm: Acc PR1 CRW P05: 1 PR) ACFT: Rc135v UNIT10343RCMSO BASE: OFFUTT AFB AIRCRAFT TDTALs CAREER TOTALS AIRCRAFT MOS TO43ATS) CREW POSITION C50 FLT DTY CERT cooE EEAET EEAET EEAET SN SN PRIMARY TIME 1279.2 DATE FIRST FLWN DATE NO DATE SECONDARY TIME 15.5 DATE LAST FLOWN DATE N0 DATE INSTRUCTOR TIME 257.6 TDTAL TIME 1147.1 441.3 339.11 9.0 9.9 EVALUATOR TIME 27.9 PRIMARY TIME 1922.4 256.8 261.0 .9 OTHER TIME 9.1 SECONDARY TIME 9.0 6.5 3.0 9.0 9.9 TOTAL TIME 1538-0 INSTRUCTOR TIME 39.5 153.0 5m 0.6 9.9 STUDENT TIME 46.5 EVALUATOR TIME 21.1 5.9 9.0 9.9 0.9 OTHER us MIL TIME 0.0 OTHER TIME 5.0 4.1 2.9 0.0 9.6 FOREIGN MIL TIME 0.9 NIGHT 135.2 74.3 9.9 0.11 9.11 CIVILIAN TIME 9.9 PRIMARY INST 9.0 9.0 9.9 9.11 9.11 COMBAT TIME 1199.5 SIM INST 6.0 0.0 6.0 6.6 0.0 COMBAT SUPT TIME 46.3 NVG TIME 9.0 9.9 9.9 9.11 9.9 TOTAL SORTIES Isa conaAT TIME 327.5 281.9 9.0 9.9 11.9 COMBAT SORTIES 106 CPBT SUPPORT TIME 37.8 8.5 0.0 0.8 0.6 COMBAT SUP SORTIES 8 COMBAT SORTIES 77 79 8 9 0 WG TIME 0.0 CMBT SUPPORT SORTIES 2 9 DATE FIRST ELDNN 12 OCT 1 TOTAL SORTTES [24 S6 95 0 DATE LAST FLOWN 66 APR 15 GRAND TOTAL 1534.9 PAGE 1 PAGE 1 G-66 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.4.3. 30/60/90 FLYING HISTORY REPORT PREPARED 29 MAY 2915 99:21 AIRERAFT MISHAP INVESTIGATION (PA) AS OF 29 MAY 2915 PCN SA036-F20 Raven 1] GRADE: CPT SSAN: API: 2 FACT 1 ASC: 1A DAFSC: 0912939 AGE: an: Acc 9199: 93439cuso ORGANIZATION: (new POSITION: EEAET Asc DATE: 95 MAR 2913 c999 RATING: conaAT SYSTEHS OFFICER AIRCRAFT TYPE: 99135v SERIAL no. 94-9949 HISHAP APR 2915 MISHAP AIRCRAFT FRI sec INST EVAL OTHER 91991 195 519 195 SORT RC135V 1922.9 9.9 99.9 21.1 5.9 1147.1 1112.9 135.2 9.9 9.9 124 LAST 39 DAYS 9.9 9.9 5.9 7.9 9.9 14.2 9.9 9.9 9.9 9.9 2 LAST 69 DAYS 9.9 9.9 23.9 7.4 9.9 31.9 23.9 9.7 9.9 9.9 4 LAST 90 DAYS 9.9 9.9 29.5 19.9 9.9 94.1 29.5 9.1 9-9 9.9 9 OTHER AIRCRAFT 991 sec INST OTHER TOTAL NIGHT 19s 519 195 SORT RC135W 156.8 6.5 108.0 5.9 441.3 424.8 74.8 0 0 0.0 56 LAST 39 DAYS 9LAST 99 DAYS 9LAST 90 DAYS 0.0 0.0 16.2 0.0 0.0 16.2 16.2 16.2 0.0 0.0 SRC135W 261.0 3.0 64.0 0 2 0 333LAST 39 DAYS 9LAST 99 DAYS 9-9 9.9 15.9 9.9 9 9 15.9 15.9 9 9 9.9 9.9 5 LAST 90 DAYS 0.0 0.0 15.9 0.0 0 0 15.0 15.0 0.0 9.0 0.9 5 F37AT45 9LAST 39 DAYS 9LAST 60 DAYS 0LAST 99 DAYs 91943A 9LAST 30 DAYS 0LAST 69 DAYS 9LAST 99 DAYS 9PAGE 1 6-67 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 70 MAY 2015 09'7'1 AIRCRAFT MISHAP INVESTIGATION (PA) AS 0F 20 MAY 2015 PCN SAOBGJZO ASC: 1A DAFSC: 0012R3H AGE: NAM?leiShap Rave" 11 GRADE: CPT SSAN: API: 2 FAC: 1 (HO: AU. Wle: ORGANIZATION: O343RCNSO CREW POSITION: EEAET ASC DATE: 05 MAR 2913 AIRCRAFT TYPE: nc135v SERIAL no: 64-4848 MISHAP DATE: 30 APR 2015 CORR RATING: COMBAT SYSTEMS OFFICER t" OTHER AIRCRAFT SEC INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT CAREER TOTALS CREW POSITION FIRST FLIGHT PRI SEC INST EVAL OTHER TOTAL STUDENT COMBAT COMBAT SORT LAST FLIGHT TIME SUPPORT COMBAT SYSTEMS OFFICER 12 OCT 2011 1279 7 IS 5 757:6 27.9 9.1 1588.4 1536.8 46.5 1109.5 46.3 188 06 APR 2615 PAGE 2 G-68 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.4.4. INDIVIDUAL DATA SUMMARY PREPARED 01 MAY 2015 19:38 INDIVIDUAL DATA SUMMARY (PA) INQUIRY AS OF 01 MAY 2015 we t[Mishap Raven 1] BASE: OHUH SSAN: GRADE: CPT CH): ACC WING: 0343RCNSO UNIT: PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: CCA SECURITY CLEARANCE DATE: 12 FEB 14 HDR SVC CAT: USAF RESTRICTED AREA BADGE N0: LAST ans DATE: PROFESSIONAL OUAL INDEX (POI): PHYS CODE: PROFESSIONAL OUAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: PHYSIOLOGICAL TNG DATE: STATUS PHYSIOLOGICAL DUE DATE: DATE ASSIGNED JUMP STATUS: DATF OF BIRTH: DUTY AFSC: 0912R3H EFFECTIVE DATE OF DUTY: 01 NOV 14 PAS CODE: SYSTEM HANAGERENT SHORT TOUR INDICATOR: . DATE RETURN FROM OVERSEAS: SQEEOSSEEIARH SEEP DATE OF RANK: 16 AUG 12 DEPLOYED DATE OF . DATE DEP LAST DUTY STA: IO JUL 10 DATE ?3 JUL 1? RECORDS REVIEW ACC DATE: 13 MAR 13 PERSONNEL RECORD STATUS: ?9 RECORDS REVIEW DUE DATE: 31 AUG 13 DAFSC: RECORDS REYIEN STATUS CODE: PROJECTED PAS CODE: PROJECTED DUTY LOCATION: PROJ DEPARTURE DATE: PROJ REPORTING DATE: FAC EFFECTIVE DATE: LOCAL USE CODE: PHA EMAIL SENT 2/12/15 CLT I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE, DATE ACC PAGE 1 PAGE 1 6-69 ICC-135V, 64?4848, Class A, 30 April 15, AFSAS #739726 PREPARED 01 MAY 2015 19:38 DATA SUMMARY TPA) INQUIRY AS OF 01 MAY 2015 PCN SA036-A79 SSAN: GRADE: CPT CHD: ACC WING: 0343RCN50 UNIT: 9343RCNSO BASE: AFB AIRCRAFT ASSIGMENT DATA AERONAUTICAL BADGE AERONAUTICAL RATING. . SGBP COMBAT SYSTEMS OFFICER 1c EFFECTIVE DATE: 09 APR IO ACFT SVC CAT: USAF PRIMARY ACFT: RC135V FLT DUTY CERT CODE: EEAET CATEGORICAL FLYING PAY DATA LAST MPO DATE: OS ION 09 LAST MPO REASON: A NONE PAY STOP DATE: 94 JUN 21 LAST FLIGHT DATE: OR APR 15 PREVIOUS PRODUCTIVE FLIGHT DATE: 02 APR 15 ous MIL R75 D1: AVIATION SERVICE DATA CORR PARA AVIATION SERVICE CODE: 1A CURR PARA RATING DATE: EFFECTIVE DATE: 95 MAR 13 ORIG PARA RATING: PRIOR ASC: 15 ORIG PARA RATING DATF: (a JJAN 13 STATUS ORDER DATE: UN 21 OFFICER SERVICE DATE: 19 MAY 08 FORMAL DATE AVIATION SERVICE 95 JUN 99 REFRESHER PHYSIOLOGICAL HYPOXIA TRAINING 16 JUN 14 TRANSITION STATUS CODE: A INITIAL PHYSIOLOGICAL HYPOXIA TRAINING 10 JUN 09 AVIATION POSITION INDICATOR: 2 EFFECTIVE DATE: O1 NOV 14 FLYING ACTIVITY CATEGORY: 1 PRE-ACIA.OFDA: OFDA GATE 10/12: 68 OFDA GATE 15/15: OFDA GATE 20/18: DFOA TO DATE: 63 Your current OFDA is 68 month(s). You need 28 additional month(s) OFDA to meet your 12 Year gate requ1rement to receive continuous ACIP through 18 years of aviation service and you must maintain a valid flight physical. I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE ACC PAGE 2 PAGE 2 6-70 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 (11.4.5. PREPARED 13 MAY 2015 29:05 [Mishap Raven 1] CMD: ACC WING: TAIL MDS DATE NUMB RC135V 02 MAY 14 62-4132 23 JUL 14 63-9792 26 AUG 14 64-4848 10 SEP 14 64?4848 15 SEP 14 64-4848 23 SEP 14 64-4848 28 OCT 14 64-4848 20 FEB 15 64-4848 25 FEB 15 62-4131 03 MAR 15 62-4131 2} MAR 13 64-4848 92 APR 15 64-4848 06 APR 15 64-4848 RC135V SUMMARY PR1 SE AIRCRAFT: 6.6 0. 0.0 0. RPA: 0.0 0. RC135W 17 JUN 14 62-4135 18 JUN 14 62-4135 23 JUN 14 62-4135 26 JUN 14 62-4130 29 JUN 14 62-4125 29 JUN 14 62-4130 02 JUL 14 62 4130 03 JUL 14 62-4125 60?15 REQUEST PERIOD FROM: 30 APR 2014 INDIVIDUAL FLYING TIME SUMMARY (PA) UNIT: DUTY POSN IEAET IEAET IEAET IEAET MEAET EEAET IEAET EEAET IEAET IEAET IEAET EEAET INST 69.0 0.0 0.0 IEAET IEAET IEAET IEAET IEAET IEAET IEAET 00699666 EVAL 21.1 0.0 0.0 SSAN: ACFT UPLOC: SGBP U3 see 5053 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 09669006 POGEGOQG PAGE 1 SRT 96.7 13 AS 0F 13 MAY 2015 TO: 30 APR 2015 GRADE: CPT PRI caew P05: CMB TOTAL 507 (MB SRT SRT NITE 90.0.0 100.0 cma CMB SRT SRT NITE 8.5 1 0.0 0 197.2 (1-71 PCN SA036-F70 PRI AIRCRAFT: RC135V SIM INS NVG .ACC PAGE 1 5 @002 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:63 INDIVIDUAL FLYING TIME SWARY (p11) AS OF 13 MAY 2615 PCN SA936-F70 REQUEST PERIOD FROM: 30 APR 2014 TO: 30 APR 2015 SSAN: 99495- CPT 991 caew P05: 5 PR1 AIRCRAFT: RC135V (MD: ACC wrNG: 0343RCNSO UNIT: ACFT 99191: 5999 TAIL DUTY cma 915 SIM nos DATE NUMB POSN PRI sec INST EVAL 0TH TOTAL SRT cue SRT SRT NITE INS 1N5 ch RES Rc135w 97 JUL 14 92.4125 IEAET 962-4130 062-4125 IEAET 062-4130 IEAET 092-4139 19491 9.9 9.9 19.3 9.9 9.9 19.3 1 1992-4139 IEAET 94125 IEAET 962-4130 IEAET 0$41135 IEAET 093-9792 IEAET 992.4131 IEAET 94131 EEAET 962-4131 MEAET 362?4131 IEAET 092.4131 IFAET 992-4131 IEAET 992-4131 IEAET 99.9 9.9 CMB SIM 91135w SUMMARY 991 sec INST EVAL OTH TOTAL SRT cna SRT c/s SRT NITE INS INS NVG AIRCRAFT: 3.5 9.9 191.9 5.9 9.9 171.3 25 119.3 14 9.9 9 35.5 9.9 9.9 9.9 SIMULATOR0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 5Rc13su 15 MAY 14 92 9992 IEAET 962-6001 IEAET 062-6001 MEAET 352-6001 IEAET 00.0 0.0 0.0 0.0 Acc PAGE 2 PAGE 2 6-72 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 26'63 INDIV10UAL FLYING TTME SUMMARY (9A) AS OF 13 MAY 2015 PCN SA636-F79 REQUEST PERIOD FROM: 30 APR 2914 TO: 30 APR 2015 SSAN: GRADE: CPT PRI CREW 005: PRI AIRCRAFT: Rc135v CMD: ACC WING: 9343RCN50 UNIT: 0343RCN50 ACFT CPLOC: SGBP TAIL DUTY CMB SIM M05 DATE NUMB POSN PRI SEC INST EVAL OTN TOTAL SRT CMB SRT SRT NITE INS INS NVG RES SRCIBHN 07 OCT 14 62-6003 IEAET 062-6006 IEBET 062-0001 IEAET 062-6001 IEAET 002-6001 IEAET 062-6002 IEAET 062-6002 IEAET 062-6005 IEAET 062-6002 IEAET 062-6002 IEAET 00.0 0.0 0.0 0.0 (MB C/s 51M 5Rc135w SUMMARY FRI 55: INST EVAL OTM TOTAL SRT cma SRT SRT NITE INS INS ch AIRCRAFT0.0 0.0 0.0 0.0 SIMULATOR: 3.0 0.0 46.0 0.0 0 0 49.0 14 MIA 0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 CM8 SIM GRAND TOTALS PR1 sec INST EVAL 0TH TOTAL 5R1 CMB SRT SRT NITE INS INS NVG AIRCRAFT: 10.1 0.0 230.9 27.0 0.0 26854.7 0.0 0.0 0.0 SIMULATOR: 3.0 0.0 46.0 0.0 0.0 49.0 14 0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 ACC PAGE 3 PAGE 3 6-73 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.4.6. INDIVIDUAL FLIGHT RECORD PHEPARED 91 MAY 2915 19:38 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF U1 MAY ?015 PIN SAB35-F7G INQUIRY SSAU: m-u. GRADE: CPT PRI CREW P05: PRI AIRCRAFT: RC135V c140: ALC yams: 0343110150 UNIT: 034306050 ACFT OPLOC: SGBP DUTY CNS SIM DATE MOS DATE NUHB PEI SEC INST EVAL OTH TOTAL SET CHE 5R1 SKI INS INS NVG RES UPDATED RC135V 02 MAY 14 62-4132 IEAET 020140506 15 my 14 62-6002 IEAET 020140612 RC135W 17 JUN 14 62 4135 IEAET 020149629 10 JUN 14 62-4135 IEAET 020140629 was?: 23 JUN 14 62-4135 IEAET 020140626 26 JUN 14 62-4130 IEAET 020140627 Rc135w 29 JUN 14 62-4125 IEAET 00.0 0.0 0.0 0.0 20140702 803514 20 JUN 14 62-4130 IEAET 020140702 RC135W 02 JUL 14 62-4130 IEAET 020140703 RC133J 03 JUL 14 62-4125 IEAET 020140704 RC13SW 07 JUL 14 62-4125 IEAET 020140707 003514 09 JUL 14 62-4130 IEAET 020140710 RC135H 12 JUL 14 52-4125 IEAET 029143114 903514 14 JUL 14 62-4130 IEAET 020140715 1103514 17 JUL 14 62-4130 IEAET 0.0 0.0 10.3 0.0 0.0 10.3 1 1020140718 RC135N 20 JUL 14 62-4130 IEAET 920149721 RCIRSV 23 JUL 14 53-9792 IEAFT 02014072? 00394 26 JUL 14 62-4125 IEAET 020140720 RCIBSW 29 JUL 14 62-4130 IEAET 020140730 RC135W 01 AUG 14 52'4135 IEAET 020140802 RC135W 04 AUG 14 63-9792 IEAET 020140207 SRC13SW 23 AUG 14 62-6001 IEAET 020140828 RC135V 26 AUG 14 64-4848 IEAET 020149828 RCIBSV 19 14 54-4843 IEAFT 920140917 RC135V 15 SEP 14 64-4348 MEAET 620140919 RC135V 23 SEP 14 54-4848 020149925 Acc PAGE 1 1 CERTIFY THAT I HAVE REVIEVJED MY 1m AND IT 15 c014an: AND ACCURATE. SIGNAYURF one VAGE 1 G-74 RC-I 35 V, 64?4848, Class A, 30 April 15, AFSAS #739726 PREPARED 01 MAY 2015 19:38 INDIVIDUAL ELIGHT RECORD REPORT AS OF 01 MAY 2015 PCN SA036-F70 INQUIRY [MishapRaven 1] E: SSAN: GRADE: CPT PRI CREW P05: PR1 RCIBSV CMD: ACC WING: 0343RENSO UNIT: 0343RCN50 ACFT OPLDC: SGBP TAIL nun me ('15 51M DATE MDS DATE NUMB POSN PR1 SEC INST EVAL 0TH TOTAL SRT (MB 5m SRT NITE INS INS NVG RES N/s UPDATED SRC135W 26 SEP 14 62-6001 HEAET 320141016 SRCIBSW 29 SEP 14 62-5001 IEAET 020141006 9203510 07 OCT 14 62-6003 IEAFT 020141017 RC1350 26 OCT 14 62-4131 IEAET 020141030 Rc135w 27 OCT 14 62-4131 EEAET 020141030 RC135V 28 OCT 14 64-4848 IEAET 00.0 0.0 0.0 0.0 20141030 5Rc135w 19 DEC 14 62-6006 TEBET 020150103 SRCIBSW 07 JAN 15 62-6001 IEAET 020150108 SRC13SW 08 JAN 15 62-6001 IEAET 020150115 SRCIJSW 14 JAN 15 62-6001 IEAET 020150125 1103514 27 JAN 15 62-4131 MEAET 320150128 04 FEB 15 62-4131 IEAET 020150213 RC135W 06 FEB 15 62-4131 IEAET 020159210 [0213511 10 FEB 15 62-4131 IEAET 020150219 00350 13 FEB 15 62-4131 IEAET 03.8 0.0 0.0 0.0 20150219 20 FEB 15 64-4848 EEAET 020150224 RCIJSV 25 FEB 15 62-4131 IEAET 00.0 0.0 0.0 0.0 0.0 20150302 RC135V 03 MAR 15 62-4131 IEAET 020150313 06 MAR 15 62-6002 IEAET 020150310 SRCIBSW 17 MAR 15 62-6002 IEAET 020150317 SRCISSW 20 MAR 15 62-6002 IEAET 020150375 snc135w 20 MAR 15 62-6005 IEAET 020150323 RC135V 27 MAR 15 64-4848 IEAET 0.0 0.0 10.7 0.0 0.0 10.7 1 0.0 0 0.0 0 8.7 0.0 0.0 6.0 20150402 RC135V 02 APR 15 64-4848 IEAET 020150403 RC135V 06 APR 15 64-4848 EEAET 020150407 SRC13SW 24 APR 15 62-6002 IEAET 020150429 ACC PAGE 2 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 2 G-75 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 0660 PREPARED 01 MAY 2015 19:38 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 01 MAY 2015 PCN INQUIRY Raven1] SSAN: GRADE: CPT PRI P05: PRI AIRCRAFT: RC135V CMD: ACC WING: 0343RCNSO UNIT: 0343RCNSO ACFT UPLOC: SGBP CHB SIM MDS SUMMARY PR1 SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS AIRCRAFT: 10.1 0.0 230.9 27.0 0 0 268.0 30 127.0 15 0.0 0 54.7 0.0 0.0 0 SIMULATOR: 3.0 0.0 46.0 0.0 0.0 49ACC PAGE 3 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 3 CF76 RC-I 35 V, 64-4848, Class A. 30 April 15, AFSAS #739726 Gl.4.7. INDIVIDUAL TRAINING SUMNIARY PREPARED 13 MAY 2615 19:54 NAME: [Mishap Raven 1] PHYSICAL DUE DATEQUALIFICATION 5V0 (HR CHR (MR CNN CHR CHR CNN (rm (HR (PF CNN CNN PROFILE (E) (E) IE) IF) GRADE: CPT INDIVIDUAL TRAINING SUMMARY CURRENT TRAINING PERIOD ssm: mm- PHYSIOLOGICAL DUE DATE: 30 JUN 19 TASK NAME OUAL EVAL RJ TACT (CORD At? cc 1: cc 1: Tlle SIH OPP SEAT SIM RIVET JOINT RAP SIH 135 CURRENCY 51" RJ TAET CORD SIH AEP ((SAP 0M0 5m SRO PROFIIF TOT SIH TOT 51" MP my saws CA5 sno TASK ID AADI ECII ECIS MTOS ?743 H757 SOD. SROD SR29 5849 1 RED 0 PAGE 6-77 AS OF 13 MAY 2015 CREW POSITION: EEAET RECORDS REVIEW DUE DATE: 31 AUG 13 DATE LAST ACCOMP ACC DATE ova REST IN ms: one out we ms [one WIACC PAGE 1 PCN SA036-T19 UNIT: 6343RCNSO PREPARED 13 MAY 2015 19:54 NAME: [Mishap Raven 1] PHYSICAL DUE DATE94515}? GT QUALIFICATION PROFILE Ewo TRNG RJ END BL TRNG RJ END BL TRNG RJ END 8L TRNG RJ END BL TRNG GRND END TRAINING GRND EWO TRAINING GRND two TRAINING GRND END TRAINING cNNu awn TRAINING TASK NAME OPP SEAT SIM INFL SIM SIM INFL DCA 51? CA5 SIN INFL CSAR SRO TOT BASIC SORTTE RJ BL 10.3 CERT R1 EL 9 CURRENCY BL 9 CERT RJ BL IO CURRENCY RJ BL 11 CERT CRM H9 DUAL ACAD SEFT RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL TRAINING SUMMARY CURRENT TRAINING PERIOD TASK to Ease sasea sasz 5272 saso snoe SR91 SR9: SR93 5R95 sxoe sxez 6578 XBOD xa090 X8110 onea sans GA43 CA46 GSIB SSAN: PHYSIOLOGICAL DUE DATEPAGE 2 G-78 REQ ACCOHP REM AS OF 13 MAY 2015 CREW POSITION: DATE LAST ACCOMP EEAET DATE TN PHASE PCN SAOBG-TIO UNIT: RECORDS REVIEW DUE DATE: 31 AUG 13 DATE DDF ACC PAGE ACC OVR IN DUE PHS YES PREPARED 13 MAY 2015 19:54 Raven 1] PHYSICAL DUE DATEQUALIFICATION PROFILE GRND END TRAINING GRND EWO TRAINING GRND END TRAINING GRND END TRAINING an0 END TRAINING GRND END TRAINING GRND END TRAINING GRND TRAINING GRND Fwo TRAINING GRND END TRAINING GRND END TRAINING GRND END TRAINING GRND END TRAINING GRND END TRAINING GRND END TRAINING GRND END TRAINING GRND END TRAINING (BNO Ewo TRAINING GINO END TRAINING GRND END TRAINING END TRAINING GRND END TRAINING GRND END TRAINING GRND END TRAINING TASK NAME STAN EVAL TEST OPLAN srunv A/c SERVICE er SAFETY TRNG nxsuo czar RISNO STUDY 8019 (2 PRO 5/5 TEST 150 PREP INTEL TRNG AF: FAN TRNG EGRESS (NONEJ) ACDT EGRESS AFE TRNG LOCAL AREA SURV CMBT SURV TRNG TRNG HST AFRICOM (CST) csu1can (csx) eucon (car, PACOH (C51) SOUTHCOM (csr) RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL TRAINING SUMMARY CURRENT TRAINING PERIOD GRADE: CPT SSAN: PHYSIOLOGICAL DUE DATE: 30 JUN 19 TASK ID 6535 6522 6523 6526 5550 6551 6559 6572 IESS LL91 LL93 LL84 LL95 LL96 $581 $562 $503 5595 5507A 5507( 5507f SSO7P $5075 ACCOMP REG .9 PAGE 3 . I 0 6N G-79 AS OF 13 MAY 2015 CREW POSITION: DATE LAST ACCOHP EEAET DATE IN PHASE 3] DEC [5 19 JUN 15 PCN UNIT: RECORDS REVIEW DUE DATE: 31 AUG 13 DATE DUE REST PHS cons Nvo YES NO (I PAGE 3 PREPARED 13 MAY 2915 19:54 NAME [Mishap Raven 1] PHYSICAL DUE DATE: 61 AUG 16 PROFILE MSK NAME GT GRND awn TRAINING SPEC SERE TRNG GT GRND Ewu TRAINING GT GROUND 50F FLT mun: GT ROUND sor sor mm: GT GROUND sor sor mun RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 TRAINING SUMMARY AS OF 13 MAY 2015 PCN 5A036-T10 CURRENT TRAINING PERIOD SSAN: CREW POSITION: EEAET UNIT: O343RCN50 PHYSIOLOGICAL DUE DATE: 33 JUN x9 RECORDS REVIEW DUE DATE: 31 AUG 13 ACC TASK DATE LASI Dill: (NR IN PEST ID R50 ACCONP IN PHASE DATE DUE DUE VHS CODE WD 5510 552? 0 89 NOV EA32 0528 052ACC PAGE 4 PAGE 4 G-80 64?4848, Class A, 30 April 15, AFSAS #739726 G1.5. [Mishap Tactical coordinator] Gl.5.1. CERTIFICATE OF AIRCREW QUALIFICATIONS 6 Mal )lH'n SQUAIWDN. 3? RS tom-v uM thwal-?411w] um I I (MRI mks/lo (IS G-8l RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.5.2. FLYING HISTORY REPORT PREPARED 01 MAY 2915 18:46 FLYING HISTORY REPORT (PA) AS OF 01 MAY 2015 PCN SA036-F40 INQUIRY NAME: SSAN: GRADE: API: 5 FAC: 3 OFDA: 129 ASC: 2A Asc DATE: 93 OCT 13 cm: Acc PRI (RN POS: PRI ACFT: Rc135v BASE: OFFUTT AFB AIRCRAFT TOTALS CAREER AIRCRAFT 9195 ac 135mm sac135wm) ?1355(5) mew NAVIGATOR FLT DTY CERT cons EEAET EEAET IEBET PRIMARY TIME 1959.3 DATE FIRST FLWN SECONDARY TIME 0.0 DATE LAST FLONN INSTRUCTOR TINE 259.2 TOTAL TIME 999.9 1999.9 94.9 4.9 EVALUATOR TIME 27.4 PRIMARY THE 736.1 923.7 53.0 0.0 OTHER TUE 47.6 SECONDARY TIME 0.0 0.0 0.0 0.0 TOTAL TIME 1994.0 INSTRUCTOR TIME 132.2 127.9 37.9 9.9 STUDENT TIME 42.9 EVALUATOR TIME 13.! 13.6 0.0 0.0 OTIILR US MIL TIHL 0.0 OTHER TIME 9.7 34.3 4.9 4.9 FOREIGN MIL TIME 9.9 NIGHT 1.5 1.9 9.9 9.9 CIVILIAN TIME 9.9 PRIMARY INST 0.0 0.0 0.0 0.0 COMBAT TIME 855.0 PRIMARY SIM INST 9.9 9.9 9.9 9.9 COMBAT SUPT TIME 354.1 NVG TIME 9.9 9.9 9.9 9.9 TDTAL 5991195 249 COMBAT TIME 496.4 358.6 0.0 0.0 COMBAT SORTIES 76 CMBT SUPPORT TIME 192.1 192.9 9.9 9.9 COMBAT SUP 5991155 59 COMBAT 5991195 42 34 9 9 we TIRE 9.9 SUPPORT SORTIES 22 28 0 0 DATE FIRST FLOWN 13 AUG 01 TOTAL SORTTES 199 139 49 2 DATE LAST FLONN 19 FEB 15 GRAND TOTAL 2636.6 PAGE 1 PAGE 1 6-82 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.5.3. 30/60/90 FLYING HISTORY REPORT PREPARED 20 MAY 2015 09:20 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 20 MAY 2015 PCN SABSO-FZB NAME: GRADE: uc SSAN: AP): 6 PAC: 3 ASC: 20 DAFSC: 0012030 AGE: can: ALL mm: 05430050 onoamuuou: 0343ch50 (new POSITION: EEAET use we. 03 on 2013 c000 mm: smon AIRCRAFT me: seam NO: 04-4040 DATE: 30 APR 2015 AIRCRAFT mu sec EVAL omen TOTAL NIGHT 1N5 5m INS som RC13SV 736 1 0.6 132.2 13 8 8.7 890.8 868.3 1.6 0.0 0.0 100 LAST 30 DAYS 0LAS1 60 DAYS 0LAST OTHER AIRCRAFT PR1 SEC INST EVAL OTHER TOTAL NIGHT INS SIN INS SORT RC135V 923.7 0.0 127.0 13.6 34.3 1098.6 1050.7 1.0 0.0 0.0 138 LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 0SRC135W 57.0 0.0 37.0 0.0 4.0 98.0 94.0 0.0 0.0 0.0 42 LAST 30 DAYS 2LAST 60 DAYS 4LAST 90 DAYS 6RC13SS LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 0PAGE 1 6-83 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 28 MAY 2015 09:26 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 20 MAY 2015 PCN SA036-F20 NAME: GRADE: LTC SSAN: m-w API: 5 PAC: 3 ASC: 2A DAFSC: BOIZRBH AGE: CHD ACC 0343RCN50 ORGANIZATION: CREW POSITION: EEAET ASC DATE: 03 OCT 2913 CORR RATING: SENIOR NAVIGATOR AIRCRAFT RC135V SERIAL NO: 64-4848 DATE: 39 APR 2915 OTHER AIRCRAFT PET SEC INST EVAL OTHER TOTAL NIGHT 1N5 SIM INS SORT *0 CAREER TOTALS pnsmou FIRST FLIGHT PRI SEC INST EVAL OTHER TOTAL INST STUDENT COMBAT CMBAT SORT LAST FLIGHT TIME SUPPORT NAVIGATOR 13 AUG 2901 1659-8 0.0 259.2 27.4 47.6 1994.0 1919.0 42 6 855.0 3543.1 240 18 FEB 2615 PAGE 2 6-84 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.5.4. INDIVIDUAL DATA SUMJVIARY PREPARED 01 MAY 7615 18:46 INDIVIDUAL DATA SUMMARY (PA) AS OF 01 MAY 2615 PCN SA036-A70 INQUIRY NAME: ""1131 SSAN: GRADE: LTC CMD: ACC WING: 0343RCN50 UNIT: G343RCNSO BASE: OFFUTT AFB PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: DO SECURITY CLEARANCE DATE: 26 APR 13 SVC CAI: USAF RESTRICTED AREA BADGE NO: LAST PHYS DATE: PROFESSIONAL DUAL (POI). PHYS CODE: PROFESSIONAL DUAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: PHYSIOLOGICAL TNG DATE: STATUS PHYSIOLOGICAL DUE DATE: DATE ASSIGNED JUMP STATUS: DATE OF BIRTH: DUTY AFSC: 8012R3H EFFECTIVE DATE OF DUTY: 02 MAY 14 PAS CODE: SYSTEM MANAGEMENT SHORT TOUR INDICATOR: HARM 555p DATE RETURN FROM OVERSEAS: DEPLOYED HARM (ODE: DATE OF RANK: 01 JAN 15 DEPLOYED DATE: DATE OF 39 NOV 27 REDEPLOYED DATE: DATE DEP LAST DUTY STA: 96 JUN 12 SPECIAL CAT ID, DATE ARR THIS STATIOW 25 JUN 12 RECORDS ACC DATE: 27 MAR 15 RECORD 1? RECORDS REVIEW DUE DATE: 31 MAR 15 PROJECTED DAFSC: RECORDS REVIEW STATUS CODE: PROJECTED PAS PROJECTED DUTY LOCATION: PROJ DEPARTURE DATF: PRDJ REPORTING DATE: PAC 8 EFFECTIVE DATE: LOCAL USE CODE: I CERTIFY THAT I HAVE REVIEWED NY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE ACC PAGE 1 G-85 PREPARED 01 MAY 2015 18:46 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL DATA SUHMARY (PA) AS OF 01 MAY 2915 PCN SA036-A7O INQUIRY NAME: SSAN: GRADE: LTC CMD: ACC WING: UNIT: 0343RCNSO BASE: OFFUTT AFB - AIRCRAFT ASSIGNMENT DATA AERONAUTICAL BADGE AIRCRAFT oanc: SGBP AERONAUTICAI RATING: SENIOR NAVIGATOR (MD of 1C EFFECTIVE 03 NOV 07 ACFT USAF AERONAUTICAL RATING: NAVIGATOR ACFT: nc13sv EFFECTIVE DATE: 03 NOV 00 FLT DUTY CERT CODE: EEAET CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA LAST MPO DATE: 17 FEB 00 LAST MPO REASON: A NONE PAY STOP DATE: 16 FEB 18 LAST PRODUCTIVE FLIGHT DATE: 18 FEB 15 PREVIOUS PRODUCTIVE FLIGHT DATE- 16 DEC 14 ous MIL RTG Dr; AVIATION SERVICE DATA CURR PARA RATING: AVIATION SERVICE CODE: 2A PARA RATING DATE: EFFECTIVE DATE: 03 OCT 13 ORIG PARA RATING: PRIOR ASC: 25 ORIG PARA RATING DATE: EFFECTIVE DATE: 01 OCT 13 STATUS AERO ORDER TERM DATE: 16 FEB 18 OFFICER SERVICE DATE: 19 NOV 99 mm? COURSE DATE AVIATION SERVICE 17 FEB 99 REFRESHER PHYSIOLOGICAL TRAINING 14 MAR 14 TRANSITION STATUS CODE: A INITIAL PHYSIOLOGICAL HYPOXIA TRAINING 12 APR 00 AVIATION POSITION INDICATOR: 6 RANDOLPH AFB, TX 17 MAR 00 EFFECTIVE DATE: 02 MAY 14 VERTIGON, RANDOLPH AFB. TX 25 FEB 00 FLYING ACTIVITY CATEGORY: 3 NIGHT VISION DEMO, RANDOLPH AFB. TX 25 FEB on OFDA GATE 10/12: 97 OFDA GATE 15/15: 127 OFDA GATE 28/18: 129 OFDA TO DATE: 129 Your current OFDA Is 129 monlh(a). You need 15 additional nonth(s) OFDA to meet your 18 Year gate requirement to receive continuous ACIP through 25 years of aviation service and you most mazntain a valid flight physical. You have met OFDA requirements for 18 year gate to receive continuous ACIP through 22 years of aviation serVIce. I CERTIFY THAT I HAVE REVIEWED MY AND IT 15 COMPLETE AND ACCURATE. SIGNATURE DATE ACC PAGE 2 PAGE 2 G-86 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.5.5. INDIVIDUAL FLYING TIME SUMNIARY PREPARED 13 MAY 2915 19:56 1NDIVIDUAL SUMMARY (9A) AS OF 13 MAY 2315 SAOSG-F78 REQUEST PERIOD FROM: 39 APR 2014 TD: 13 MAY 2015 NAME: SSAN: m-u- GRADE: LTC can P05: 991 AIRCRAFT: RC135V (MD: ALL mm: UNIT: 0343120150 ACFI OPLOC: SGBP TAI l. DUTY CHB was one was POSN FRI 55c 1951 EVAL om TOTAL 591 (M9 591 591 ?115 ms ms ch RES RC135V 24 MAY 14 64'4841 862-4132 EEAET 954-4949 MEAET 55:1: 14 54.4941 MEAET 252-4131 If.524131 15951 394-4999 EEAET 9acnsv SUHMARY FRI sec 1951 5an om TOTAL 591 NVG AIRCRAFT: 19.8 0.0 11.5 13.3 0.0 45.1 7 9.3 1 0.0 0 0.6 0.0 9.0 0.8 smuunon9.9 9.9 9.9 9.9 RC135W 39 MAY 14 52-4125 IEAET 5049 SIM RC135W summv PRI sec INST EVAL 919 TOTAL SRT 591 9.8 8.6 0.0 0.0 smuwoa9.9 9.9 9.9 9.9 RPA9.6 0.0 0.0 0.0 sncusw 99 MAY 14 62-6002 MEAET 262-5993 962-9991 MEAFW 262-9991 MEAEN 252-6001 IEAET 062-6096 MEAET 2ACC PAGEJ 1 6-87 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:56 FLYING 7mg Sum?y (FA) AS OF 13 MAY 2015 PCN SA036-I-70 REQUEST PERIOD FROM: 39 APR 2014 TO: 13 MAY 2815 SSAN: GRADE: LTC PRI POS: PR1 AIRCRAFT: RC135V cno: ACC WING: 93439cnso UNIT: 0343RCNSO ACFT OPLOC: TAIL DUIY CNB SIM 095 DATE HUME POSN FRI sac INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG RES SRCIBSW 19 AUG 14 62-6001 MEAET 262-6006 MEAET 202-6002 MEAET 262-6006 HEAET 262-6006 MEAET 262-6006 MEAET 262-6002 MEAET 262-6006 MEAET 262-6006 MEAET 262-6002 MEAET 252-6002 MEAET 262-6002 IEAET 062-6002 MEAET 262-6006 MEAET 262-6906 MEAET 20.9 0.9 0.9 9.0 0.9 CMB SIM SRCIBSW SUMMARY PR1 SEC INST EVAL 0TH TOTAL SRT CNB SRT SRT NITE INS INS NVG AIRCRAFT0.9 9.9 9.9 9.0 SIMULATOR: 36.0 9.9 6.9 9.9 9.0 42.9 21 NIA 0.0 0.0 0.0 9.0 RPA0.0 0.0 0.0 0.0 CMB SIM GRAND TOTALS PRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG AIRCRAFT: 26.0 0.9 12.5 13.8 0.0 52.3 9 9.3 1 0.0 9 0.6 0.0 9.9 9.0 SIMULATOR: 36.0 9.9 6.0 9.0 9.0 429.0 9.0 0.0 9.0 Acc PAGE 2 PAGE 7 6-88 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.5.6. INDIVIDUAL FLIGHT RECORD PREPARED 61 MAY 2015 18:46 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 01 MAY 2015 SA035-F70 INQUIRY 11400: 5540: 00400: 110 0111 000w P05: 0 PRI AIRCRAFT: RC135V CMD: WING. 63438CNSQ UNIT: ACFT OPLDC: SGBP IAIL DUTY (MB SIM DATE MOS DATE NLMB PDSN PRI SEE INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG RES UPDATED 50013511 1310013 02-0003 1040v 020140000 591313591 09 MAY 14 62-6002 MEAET 226146715 RC135V 24 MAY 14 64~4841 IEAET 826146524 50c135w 29144114 020003 20140530 RC135W 36 MAY 14 62-4126 IEAET 66.6 0.6 6.6 0.6 20146531 RC135V 10 JUN 14 02-4132 00401 020140019 50013514 24 JUN 14 02-0001 MEAEW 220140025 SRC135W 24 JUN 14 62-6661 MEAEW 220140624 RC135V 09 JUL 14 64-4848 MEAET 520146711 50.013514 15101 14 02-0001 10407 020140717 SRC135W 65 AUG 14 62-6666 MEAET 220140819 SRC135W 19 AUG 14 62-6601 MEAET 220146905 511013511 09 50? 14 02-0000 00401 220140911 50013511 11500 14 02-0002 110401 220140925 RC135V 19 SEP 14 64-4841 HEAET 26.0 0.0 0.0 6.0 26146922 511013514 0200114 02-0000 00407 220141017 Rc135v 10 oc114 02-4131 10401 020141017 SRCIBSW 64 NOV 14 62-6066 MEAET 226141106 50.01351? 10 NOV 14 02-0000 00407 220141119 SREIBSW 03 DEC 14 62-6002 HEAET 220141265 RC135V 16 DEC 14 62-4131 IEAET 326141218 50013511 14 JAN 15 020000 00401 220150125 50013511 22 JAN 15 02-0000 00401 2201501211 11 62-6602 MEAET 20.0 6.6 6.6 6.6 20156212 RCISSV 18 FEB 15 64-4848 EEAET 026150729 511013511 00 MAR 15 02-0002 00407 220150300 ACC PAGE 1 I THAT I HAVE REVIEWED MV IFRR AND IT IS CMPLETE AND ACCURATE. SIGNATURE DATE PAGE 1 G-89 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 01 MAY 2015 18:46 1ND1V1DUAL Euch RECORD REPORT (PA) AS OF 01 MAY 2015 PCN SA036-E70 INQUIRY NAME: SSAN: mu? GRADE: PRI caew POS: PR1 AIRCRAFT: RC135V CMD: Au. wmu: U343RCNSO UNIT: 0343RCNSO ACFT OPLOC: SGBP TAIL CNS SIM DKTE PDS DATE ?0103 POSN P01 SEC INST EVAL 0m TOTAL 501 cue SRT SRT NITE 105 ms we RES UPDATED 5010350 17 MAR 15 62-6002 IEAET 020150317 900350 29 APR 15 62-5002 MEAET 220150429 (MB SIM ms SUMMARY PR1 sec INST EVAL 0TH TOTAL SRT cne SRT SRT NITE INS INS NVG AIRCRAFT- 26.0 0.0 12.5 13.0 0.0 52.3 0 0.3 1 0.0 0 0-6 0.0 0.0 0.0 SIMULATOR: 32.0 0.0 9.0 0.0 0.0 41.0 20 0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 Acc PAGE 2 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 2 6-90 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.5.7. INDIVIDUAL TRAINING SUNINIARY PREPARED 13 MAY 2915 19:51 INDIVIDUAL TRAINING SUWRY AS OF 13 MAY 2915 PCN CURRENT TRAINING PERIOD NAME: GRADE: LTC 55m: posmou: EEAET UNIT: 8343RCNSO PHYSICAL DUE DATE: ab JUL 16 PHYSIOLOGICAL DUE DATE: 31 MAR 19 RECORDS REVIEW DUE DATE: 31 MAR 16 ACC PG) TASK DATE LAST DATE OVR IN REST (D QUALIFICATION PROFILE TASK NAME to R6) actor)! ?an Accw 1" PHASE DATE DUE DUE ms cons Wu (H RJ Tc (m (E) DUAL EVATACT room an(8) sum(E) TUNE no(E) SIM OPP SEAT (E) 51" DIVE) JOINT RAP NCBB 133 H612 (one M621 RG23 51)! owl? (1105 (NR (E) SRO MFILE CHR (E) TOT 51H "(:07 51;) sums 5099 saws CHR (E) (A5 5818 (E) SR29 (HACC PAGE 1 PAGE 1 G-9 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 HAY 2615 19:51 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2615 PCN 5A036-T16 CURREN) TRAINING PERIOD GRADE: ch SSAN: mm. CREW POSITION: EEAET UNIT: PHYSICAL nus DATE: 95 JUL 16 PHYSIOLOGICAL DUE one: 31 MAR 19 RECORDS Revzew nus DATE: 31 MAR 16 ACC TASK DATE LAST DATE OVR IN REST CD QUALIFICATION PROFILE TASK NAME ID REG ACCOMP REM ACCOHP IN PHASE DATE DUE DUE 9H5 CODE wu CH EW R.) TC (E) OPP SEAT $6156 SR59 959C (E) R.) SRSSI AXIOM-(L) SIM 1m. SR89 (E) SIM INFL (HR (E) SIM INFL DCA SR91 (HR (E) SIM IMFL CA5 SR92 IE) SIM INFL (SM sass a (H an R) It CM [El 51" SRO SHQS (E) BASIC SORTTE 5X93 TRNG R1 8L 18.3 CERT 6578 R.) EH) TRNG R.) EL 9 1809 TRNG R.) 8L 9 CERT XB990 Bl. TFNG R.) BL 18 CURRENCY X318 CERT GRND two TRAINING GAOGENO TRAINING um GAGE GRND END TRAINING H9 DUAL GRND TRAINIIG ACAD EMS GRNO EHO TRAINING SEPT 5593 ACC PAGE 2 PAGE 2 6-92 PREPARED 13 MAY 2615 19:51 NAME: PHYSICAL DUE DAlt: Ob JUL 16 CD QUALIFICAT Im PROFILE GENO 6N0 TRAINING sun TRAINING END TRAINING GRND ewo TRAINING ERND Fun TRAINING GRND END TRAINING GRND two TRAINING GRND ENC TRAINING GRND ENG TRAINING GRND END TRAINING GRND END TRAINING GRND Ewe TRAINING mun Ewo TRAINING BIND END TRAINING 01M) END TRAINING GINO END TRAINING GINO END TRAINING GRND TRAINING GRND Ewo TRAINING cane EHO TRAINING caun END TRAINING caun END GRND END TRAINING GRND END TRAINING TASK NAME STAN EVAL TEST STUDY FLY SAFETY TRNG RISNO CERT RISNO STUDY 8916 (2 PRO TEST SEC 150 PREP INTEL TRNG AFB ran TRNG caness (MDNEJ) ACDT Ecarss AFE TRNG LOCAL AREA sunv (NET sunv TRNG CAC TRNG NET AFRICOM (C51) caNTcon (cs1) EUCON (C51) PACOH (CSI) SDUTHCOM RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL TRAINING SUMMARY CURRENT TRAINING PERIOD GRADE: LTC SSAN: PHYSIOLOGICAL DUE DATE: 31 NAR l9 TASK to use: 5522 5525 6526 5558 6551 0559 JED: IE6: LL01 LL03 LLat LL85 LL96 5591 5501 5593 5595 5591A 559?: 5591? SSOIS ?6 RED ACCOMF REM PAGE 3 6-93 CREW POSITION: EEAET DATE LAST ACCOHF MAY 2615 DATE PCN SA036-T16 UNIT: 9343RCNSO RECORDS REVIEW DUE DATEPHS CDDE W11 VES 0 ?9 YES PAGE 3 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:51 INDIVIDUAL SUMMARY AS or 13 my 2915 PCN sAesa-na CURRENT TRAINING PERIOD NAME: came; LTC 55m; mm CREW POSITION: EEAET UNIT: 9343Rc~so PHYSICAL DUE DATE: 06 JUL 16 PHYSIOLOGICAL DUE DATE: 51 mm 19 RECORDS REVIEW DUE DATE: 31 MAR 16 ACC TASK DATE LAST DATE OVR IN REST (D QUALIFICATION PROFILE VASK NAME 1n REG ACCORD R94 ACCOPP IN PHASE DATE DIE DUE FMS CODE WU GT GMD END TRAINING SPEC 5518 END TRAINING 5524 a 17 JUL 1? ACC PAGE 4 PAGE 4 6-94 64?4848, Class A, 30 April 15, AFSAS #739726 G1. 6. SRA [Mishap Airborne Systems (MASEI) Engineer 1] G1.6.1. CERTIFICATE OF AIRCREW QUALIFICATIONS Letter or Certi?cations uame - :FxIxix [MishapRaven? IttAEf I I I I I I IxIx G-95 V, 64?4848, Class A, 30 April 15, AFSAS #739726 I I I G-96 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.6.2. FLYING HISTORY REPORT PREPARED 01 MAY 2015 20:01 FLYING HISTORY REPORT (PA) As OF 01 MAY 2015 PCN SA036-F4B INDUIRY NAME: SSAN: GRADE: SRA API: A FAC: A OFDA: 52 ASE: AA ASC DATE: 21 JUN 11 CMD: AIA NINC: 0343RCNS PR1 P05: PRI ACFT: RC135V UNIT: 0343RCNSO BASE: OFFUTT AFB AIRCRAFT TOTALS CAREER TOTALS AIRCRAFT MDS SRC135W0) CREW POSITION RADIO OP FLT DTY CERT CODE MKAB HKAEB MKAE3 UKIN PRIMARY TIME 1696.9 DATE FIRST FLOWN DATE SECONDARY TIME 6.1 DATE LAST DATE INSTRUCTOR TIME 0.0 TOTAL TIMF 1132.3 593.4 2.5 0.0 EVALUATDR TIME 0.0 PRIMARY TIME 1112.1 584.8 2.5 0.0 OTHER TIME 22.1 SECONDARY TIME 0.7 0.0 0.0 0.0 TOTAL TIME 1725.7 INSTRUCTOR TIME 0.0 0 0 0.0 0.0 STUDENT TIME 0.0 EVALUATOR TIME 0.0 0.0 0.0 0.0 OTHER US MIL TIME 0.0 OTHER TIME 13.5 8.6 0.0 0.0 FOREIGN MIL TIME 0.0 NIGHT 95.1 129 1 0.0 0.0 CIVILIAN TIME 0.0 PRIMARY INST 0.0 0.0 0.0 0.0 COMBAT TIME 1070.6 PRIMARY SIM INST 0.0 0.0 0.0 0.0 COMBAT SUPT TIME 3.11 we TIME 0.0 0.0 0.0 0.0 TOTAL SORTIES 199 COMBAT TIME 876.4 200.2 0.0 0.0 COMBAT SORTIES 91 (NET SUPPORT TIME 4.1 4.7 0.0 0.0 COMBM SUP SORHES 3 COMBAT SORTIES 79 Is 0 0 NYC TIME 0.0 CMBT SUPPORT SORTIES 1 2 0 0 DATE FIRST 14 APR 11 TOTAL SORTIES 120 79 I 0 DATE LAST now 22 APR 15 GRAND TOTAL 17:15.7 PART: 1 PAGE 1 6-97 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.6.3. 30/60/90 FLYING HISTORY REPORT PREPARED 20 MAY 2015 09:14 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 20 MAY 2015 PCN SA036-F20 GRADE: SRA SSAN: API: A FAC: A ASC: AA DAFSC: AGF: can: ALA wLuu: ORGANIZATION: 0343RCNSO CREW POSITION: MKAEB Asc DATE: 21 JUN 2011 CURR AIRCRAFT Rc135v SERIAL N0. 04-4040 MISHAP APR 2015 nxsuAP AIRCRAFT PR1 sec INST EVAL OTHER TDTAL NlanT INS SIM INS SDRT RC235V 1112.1 0.7 0.0 0.0 13.5 1132.3 1112.1 05.1 0.0 0.0 120 LAST 30 DAYS 5LAST 60 DAYS 22.1 0.0 0.0 0.0 0.0 22.1 22.1 0.0 0.0 0.0 3 LAST 90 DAYS 39.! 0.0 0.0 0.0 0.0 39.3 39.3 9.7 8.0 0.0 3 t1- OTHER AIRCRAFT 2-- PRI SEC INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT RC133W 584-8 0.0 0.0 0.0 8.6 593.4 584.8 129.1 0.0 0.0 79 LAST 30 DAYS 9LAST 50 DAYS 40.1 0.0 0.0 0.0 3.0 43.1 40.1 21.1 0.0 0.0 6 LAST 90 DAYS 50.1 0.0 0.0 0.0 3.0 43.1 40.1 21.1 0.0 0.0 6 SRCIZSW 7LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 00.0 0.0 0.0 0.0 RC135U 0LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS PAGE 1 6-98 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 29 MAY 2015 99:14 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 29 MAY 2015 PCN SAO36-F20 NAME: GRADE: SRA SSAN: API: A A ASC: AA OAFSC: 1A351 AGE: CMD: AIA WING: 0343RCNSO ORGANIZATION: 0343RCNSO CREW POSITION: MKAEB ASC DATE: 21 JUN 2011 cuan RATING: AIRCRAFT TYPE: RC135V SERIAL no: 64-4343 MISHAP DATE: 30 APR 2015 OTHER AIRCRATT t" PRI SEC INST EVAL OTHER TOTAL NIGHT INS SIM 1N5 SORT CAREER TOTALS CREW POSITION FIRST FLIGHT PRI SEC INST EVAL OTHER TOTAL STUDENT COHBAT (MEAT SORT LAST FLIGHT SUPPORT AIRBORNE SYSTEM 1a APR 2011 1696.9 6.7 0.0 22.1 1725.7 1596.9 0.0 1070.6 8.8 199 22 APR 2615 PAGE 2 6-99 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.6.4. INDIVIDUAL DATA SUMNIARY PREPARED 61 MAY 2915 28:91 INDIVIDUAL DATA SUMMARY (PA) INQUIRY AS OF 01 MAY 2615 PCN NAME: SSAN: GRADE: SRA CMD: AIA WING: UNIT: 0343RCNSO BASE: OFFUTT AFB PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: UDM SECURITY CLEARANCE DATE: 39 JUN IO MBR CAT: USAF RESTRICTED AREA BADGE NO: LAST PHYS DATE: PROFESSIONAL OUAL INDEX (POI): PHYS CODE: PROFESSIONAL QUAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: PHYSIOLOGICAL TNG DATE: STATUS PHYSIOLOGICAL DUE DATE: DATE ASSIGNED JUMP STATUS: DATE OF BIRTH. DUTY AFSC: 1A351 EFFECTIVE DATE or DUTY: 31 JAN 13 PAS CODE: DDGUFSCH SYSTEM MANAGEMENT SHORT TOUR INDICATOR: HARM (one: 553p DATE RETURN FROM OVERSEAS: 0F RANK: DEPLOYED DAIC: DATE OF 29 MAR 16 REDEPLOYEO DATE: DATE DEF LAST DUTY STA: 62 NOV 13 SPECIAL CAT ID: PERSONNEL STATUS: 1? RECORDS REVIEW DUE DATE: 31 JAN 16 RECORDS STATUS (ODE: PROJECTED PAS CODE: PROJECTED OUTY LOCATION: PROJ DEPARTURE DATE: PROJ REPORTING DATE: PAC 8 EFFECTIVE DATE: LOCAL USE CODE: CERTIFY THAT I HAVE REVIEHED MY FRF AND TT Is COMPLETE AND ACCURATE. SIGNATURE DATE AIA PAGE 1 PAGE 1 PREPARED 01 MAY 2615 20:61 NAME: BASE: orrun AFB AIRCRAFT OPLDC: CHD OF AIRCRAFT: ACFT SVC CAT: PRIMARY ACFT: FLT DUTY CERT CODE: CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA LAST MPO DATE: LAST MPO REASON: PAY STOP DATE: LAST PRODUCTIVE FLIGHT DATE: PREVIOUS PRODUCTIVE FLIGHT DATE: AVIATION SERVICE DATA AVIATION SERVICE CODE: EFFECTIVE DATE: PRIOR ASC: EFFECTIVE DATE: AERO ORDER TERM DATE: OFFICER SERVICE DATE: AVIATION SERVICE DATE: TRANSITION STATUS CODE: AVIATION POSITION INDICATOR: EFFECTIVE DATE: FLYING ACTIVITY PRE-ACIA-OFDA: OFDA GATE 10/12: OFDA GATE 15/15: DFDA GATE 20/18: OFDA TO DATE: Your current OFDA is 52 month(s). AIRCRAFT ASSIGNMENT DATA ICC-135V, 64?4848, Class A, 30 April 15, AFSAS #739726 SSAN: mm" 1C USAF RC135V HKAEB 93 JAN 11 NONE INDIVIDUAL DATA SUMMARY (PA) INQUIRY AS OF 61 MAY 2015 PCN SAO36-A76 GRADE: SRA CMD: AIA WING: O343RCNSO UNIT: 0343RCNSO AERONAUTICAL BADGE (BASIC) AIRMAN AIRCREVMEMBER 29 OCT 11 AVIATION BADGE: EFFECTIVE DATE: OUS MIL RTG OT: CURR PARA RATING: CORR PARA RATING DATE: ORIG PARA RATING: ORIG PARA RATING DATE: STATUS FORMAL COURSE DATE You need 29 additionaL month(s) OFDA to meet your 10 Year gate requirement to receive continu0us CEFIP through 15 years of aviation service and you must maintain a valid fIight physical. I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE AIA PAGE 2 PAGE 2 (3-101 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 4015 20:06 INDIVIDUAL FLYING TINE SUMMARY (PA) A5 0* 15 MAY 2915 5A036-F79 REQUEST PERIOD FROM: 30 APR 2014 T0: 30 APR 2015 NAME: SSAN: 0" 50- GRADE: SRA PRI CREW POS: PR1 AIRCRAFT: ac135v END: AIA WTNG: UNIT: ACFT OPLOC: TAIL DUTY cna SIM N05 DATE NUMB POSN PR1 sec INST EVAL OTH TOTAL SRT cna SRT SRT NITE INS INS NVG RES RC135V 05 MAY 14 04-4046 HKAEB 964-4841 MKAEB 11.7 0.0 9.0 0.0 0.9 11.7 1 1164-4041 MKAE3 604-4841 MKAEB 10.1 0.0 0.0 0.0 0.0 10.1 1 1064-4841 MKAE3 11.5 0.0 9.0 6.9 0.9 11.5 1 1154-4345 NKAEH 11.2 0.9 9.9 0.0 9.0 11.2 1 1164-4840 NKAEB 74043 MKAE3 10.6 0.0 0.0 0.0 0.0 1064-?542 NKAEB 11.5 9.0 9.9 0.9 0.9 114040 MKAEH 904-4048 MKAE3 764-4343 902-4131 MKAEB 04943 NKAE3 764-4048 NKAE3 60.0 0.0 0.0 0.0 CNB 51M RC135V SUMHARY PR1 SEC INST FVAL 0TH TOTAL SRT CMB 5R1 SRT NTTF INS INS NVG AIRCRAFT: 139 4 0.0 0.0 0.0 0.0 139.4 15 54.2 5 0.0 0 17.2 0.0 0.0 0.0 SIMULATOR0.0 0.0 0.0 0.0 RPA0.0 0.0 9.9 0.0 0.0 RC135W 11 HAY 14 52-4139 HKAE3 19.8 0.0 0.9 0.0 0.0 19.8 1 1062?4130 NKAE3 11.4 0.0 0.9 0.0 0.0 11.4 1 1102.4130 MKAEB 11.2 0.0 0.0 0.0 0.0 11.2 1 1162-4126 MKAEB 11.5 0.0 0.0 0 0 0.0 11.5 1 1162-4139 WKAE3 10.1 0.0 0.0 0.9 0.0 19.1 1 106264126 MKAE3 11.5 0.0 9.0 0.0 0.9 11.5 1 11.5 1 9.0 9 1.9 9.9 9.0 6.0 AIA PAGE 1 PAGE 1 RC-I35V, 64-4848, Class A, 30 April 15. AFSAS #739726 PCN SA036 F70 AS OF 13 MAY 2015 INDIVIDUAL FLYING TIME SUMMARY (PA) PREPARED 13 MAY 2015 20:05 TO: 30 APR 2015 REQUEST PERIOD FROM: 30 APR 2014 PR1 AIRCRAFT: RC135V GRADE: SRA PR1 CREW POS: ACFT OPLOC: SSAN: NAME: UNIT: WING: CMD: AIA STM INS 0.0 SRT NITE CMB CNB SRT 0.0 7.1 DUTY POSN MKAEB TAIL RES NVG 0.0 INS 0.0 0TH TOTAL SRT SEC INST EVAL 0.0 PR1 7. NUMB DATE RC135H 62-4126 00000 00000 00000 00000 00000 00000 00903 00000 00000 MKAE3 HKAE3 MKAE3 MKAES 62-4132 62-4132 0.0 00000 00000 00000 0 n.nununu 00000 00000 50000 00000 00000 00000 00000 00000 00000 1 1 1.1.1 63594 56669 0 0 0.0.0. 00000 00000 00000 00003 09000 .0 0 nvnunu 00000 63594 6 6 6.0.9 33333 22222 33333 1;.1 1.11.1 44444 . .- 22222 66560 4.4444 1 1.1.1 1 T.T. T. 00000 45739 22222 000000 000000 000000 090000 000000 000000 009235 000002 000000 000000 000000 000000 000000 000000 990874 069199 000000 000000 000000 000000 000000 000000 000000 000000 333333 Mums?; 225535 33.12 2 111.111 444444 222222 666606 444444 111111 000000 357801 001122 0.0 0.0 0.0 0.0 0.0 MKAE3 62-4132 62-4132 1.6 MKAE3 00000 00000 00000 00000 000 000 0000 000 0.0 0.0 000 000 0.0 0.0 200 973 9.3 3.5 0000 0030 0.0 0000 0000 0.0 0.0 220w0 333 3 11111 44444 22222 66666 44555 11111 VC OEMWW MOM @2579 30000 000 000 000 000 000 000 100 410 000 000 000 000 000 1.:ual 4.2.13.5 9 7 MKAEB MKAEB 551 333 111 ?44 ..0 224 666 555 111 MNA 902 012 AIA PAGE 2 2 6-103 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2615 26:66 FLYING TIME SUMMARY (pA) AS OF 13 MAY 2015 PCN SA036-F70 REQUEST PERIOD FROM: 30 APR 2914 T0: 30 APR 2015 GGOZ 60.62 @3661 NAME: SSAN: GRADE: SRA PR1 CREW P05: PR1 AIRCRAFT: RC135V CMD: AIA WING: UNIT: 0343Rc~so ACFT OPLOC: TAIL DUTY CMB SIN MDS DATE nuns POSN PR1 sec INST EVAL 0TH TOTAL SRT 043 SRT 5R1 um135W SUMMARY PRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS AIRCRAFT: 259.4 0.0 0.0 0.0 3.0 262.4 34 73.6 7 0.0 0 28.5 0.0 0.0 SIMULATOR0.0 0.0 0.0 RPA62-5003 MKAES 20.0 0.0 0.0 0.0 CMB SIM SRC135W SUMMARY FRI SEC INST EVAL 0TH TOTAL SRT (MB SRT SRT NITE INS INS AIRCRAFT0.0 0.0 0.0 SIMULATOR: 2.5 0.0 0.0 9.0 [3.0 2.5 1 0.6 6.0 0.0 RPA: 6.0 0.6 0.0 0.8 8.6 9.9 9.GRAND TOTALS PRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE Ius INS 398.8 0.0 0.0 0.0 3 0 401.8 49 127.8 12 0.0 0 45.7 0.0 0.0 0. SIMULATORRPAALA PAGE 3 PAGE 3 G-104 0660 GOOD RC-135V, 64-4848, Class A, 30 April 15. AFSAS #739726 G1.6.6. INDIVIDUAL FLIGHT RECORD 900070100 01 MAY 2015 20.01 INDIVIDUAL 011001 000000 000001 (PA) 45 or 01 MAY 2015 001 54030-070 INQUIRY 01100: 5540: GRADE: SRA PRI mew POS: PR1 AIRCRAFT: Rc135v 0M1): AIA 11100: 0343110050 mm: 034300050 ACH 00101: TAIL DUTY C148 SIM DATE MOS DATE NUMB POSN PR1 SEC INST EVAL 0TH TOTAL SRT OMB SRT SET NITE INS INS NVG RES UPDATED 001350 05 MAY 14 04-4040 000103 920140505 RC135V 08 MY 14 64-4841 MKAEB 11.7 0.0 0.0 0.0 0.0 11.7 1 1120140508 0013911 11 MAY 14 02-4130 MKAE3 10.0 0.0 0.0 0.0 0.0 10.0 1 1020140512 0013510 101441714 02-4130 100403114 0.0 0.0 0.0 0.0 11.4 1 1120140510 0013514 100100 14 02-4130 010103112 0.0 0.0 0.0 0.0 11.2 1 1120140510 Rc135w 210m 14 02-4120 NKAE3 11.5 0.0 0.0 0.0 0.0 11.5 1 1120140521 0013511 23 MAY 14 02-4130 MKAE3 10.1 0.0 0.0 0.0 0 0 10.1 1 1020140523 RC135V 26 MAY 14 64-4841 HKAB 620140526 RC13SW 28 MAY 14 62-4126 MKAB 11.5 0.0 0.0 0 6 0.0 11.5 1 1120140529 acusv 311m 14 04-4041 01an 10.1 0.0 0.0 0.0 0.0 10.1 1 1020140531 Rc13sv 02 Jun 14 04-4041 muss 11.5 0.0 0.0 0.0 0.0 11.5 1 1120140003 RC135V 05 JUN 14 64-4846 MKAE3 11.2 0.0 0.0 0.0 0.9 11-2 1 1120140606 0013510 07 JUN 14 02-4120 NKAEB 720140007 RC135V 24 JUL 14 04-4040 MKAE3 720140720 RCIBSV 09 SEP 14 64-4848 MKAEB 10.6 0.0 0.0 0.0 0.0 1020140912 50013511 17 500 14 02-0003 MKAE3 220140925 11013971 07 on 14 62-4132 11an 020141204 RC13SW 150CT14 62-4132 MKAB 320141021 003517 1700114 02-4132 MKAB 920141027 ac135w 21 OCT 14 02-4132 MKAE3 920141027 11013517 22 011114 02-4132 010103 020141020 nc13sw 23 00114 157-4132 HKAE310.S 0-0 0.0 0-0 0.0 1020141020 1103511 24 00114 02-4132 MKAE3 620141204 RC135W 25 OCT )4 62-4132 MKAB 620141030 1203514! 27 OCT 14 62-4132 MKAE3 60.0 0.0 0.0 0.0 20141030 0013511 20 on 14 02-4132 MKAE3 020141104 AIA PAGE 1 I CERTIFY THAT I HAVE REVIEWED HY AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 1 G-105 PREPARED 01 MAY 2015 20:01 NAME: CMD: AIA WING: M05 DATE RC135W 29 OCT 14 RC135W 03 NOV 14 95 NOV 14 RC135W 17 NOV 14 RCIBSW 18 NOV 14 RC135W 20 NOV 14 RC135W 21 NOV 14 RC135W 26 NOV 14 RC135W 29 NOV 14 RC135W 30 NOV 14 RC135W 02 DEC 14 RC135V 10 DEC 14 RC135V 14 JAN 15 RC135V 18 FEB 15 RFIBSV 24 FEB 15 RC135W 06 MAR 15 RC135W 07 MAR 15 RC135W 09 MAR 15 RC13SW 09 MAR 15 RC135W 10 MAR 15 RC13SV 27 MAR 15 RC135V 31 MAR 15 RC135V 15 APR 15 RCIBSW 22 APR 15 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. 0343RCNSO TAIL NUMB 62-4132 62~4132 62-4132 52-4125 62-4125 62-4125 62~4125 52-4132 62-4132 62-4132 67-4132 64-4842 64?4848 64-4048 64-4848 62-4130 62'4130 62-4130 62-4135 62-4135 62-4131 64 4848 64-4848 64-4131 UNIT: 0343RCNSO DUTY POSN MKAEB MKAC3 MKAE3 MKAN3 MKAE3 MKAE3 MKAEB MKAE3 NKAE3 MKAEB MKAE3 MKAEB MKAE3 MKAE3 NKAE3 NKAEB MKAES MKAE3 MKAEB 33 mm 0100 mm MKAE3 7. MKAEB 6. HKAE3 9. a OOHlemtD . . . . . . . . .n RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 SEC h:h:&:haa:c> 96669609636609 6: INDIVIDUAL RECORD REPORT (PA) INQUIRY GRADE: ACFT OPLOC: EVAL 0TH TOTAL SRT CH3 ?3 hahaiz . - 032323 hihah:ia cwaoia 0 I I I a 43me PAGE 2 G-106 SIGNATURE AS OF 01 MAY 2015 PRI CREW P05: (IS SRT NITE 0110.0 INS PCN SA036 F70 PRI AIRCRAFT: RC135V SIM r4 2: @900 - . . . . . . . . . . . . . . DATE NVG RES UPDATED 20141104 20141105 20141112 20141117 20141119 20141124 20141124 20141202 20141201 20141201 20141203 20141216 20150115 20150220 20150224 20150316 20150317 20150317 20150317 20150317 20150331 20150402 20150417 20150428 PAGE 2 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 91 MAY 2915 29:91 INDIVIDUAL FLIGHT RECORD REPORT (PA) As 0F 91 MAY 2915 PCN SA939-F79 INQUIRY NAME. SSAN: GRADE: SRA PR1 CREW P05: PRI AIRCRAFT: RC135V cm: AIA WING: 9343Rc~so um: 934390159 OPLOC: CH8 SIM MDS SUMMARY PRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS AIRCRAFT: 398.8 9.9 9.9 9.9 3.9 491.9 49 127.3 1.2 9.9 9 45AIA PAGF 3 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT Is COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 3 G-107 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.6.7. INDIVIDUAL TRAINING SUNINIARY PREPARED 13 MAY 2015 19:51 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2015 PCN CURRENT PERIOD NAME: GRADE: SRA SSAN: m? CREW POSITION: NKAB mm: 0343RCNSO PHYSICAL out out: 13 APR 15 PHYSIOLOGICAL DUE DATE: 39 SEP 15 RECORDS REVIEW DUE DATE: 31 JAN 16 ACC P68 IASK DATE LAST DATE OVR IN REST (D MSK NAME 10 RED ACCOHP REM IN PHASE DATE DUE DUE. H15 (ODE WU CH ASE 3 RJ SORTIE ASE-3 DUAL EVAL A563 LND GEAR ALT EX L025 SORTIE SIH LND GEM ALT EA MFSE SORUE SIM R) ASL M149 SORTIF R1 ASP 3 SKIS (E) SIM RIVET JOINT RAP M686 IE, 51" 135 CURRENCY M612 (E) TOT "Tb(E) TOT SIM RAP $090 CIR IE) TOT RAP SRGG RAP 5R59 5R59C RAP SRSOR CIR (E) TOT 5X00 CPR (E) BASIC SORTIE 5X03 16.3 CERT 6578 TFWG RJ EL 9 CURRENCY X899 CERT X80 CUMENLY X516 TRNG RJ BI. 11 CURRENCY X811 TRNG RJ BI 11 CERT X3110 GRND ASE RJ TRAINING ANTI-HIJACK M03 51040 ASE RJ TRAINING CRM GAGE TRAINING M9 DUAL M43 AIA PAGE 1 PAGE 1 G-108 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:51 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2915 SAGBG-TID CURRENT TRAINING PERIOD NAME: GRADE: SRA SSAN: cnew POSITION: HKAES uun: PHYSICAL DUE DATE: 18 APR 15 PHYSIOLOGICAL DUE DATE: 30 sec 15 RECORDS REVIEW DUE DATE: 31 JAN 16 ACC Pm TASK DATE LAST DATE OVR IN REST CD OUALIFICATION PROFILE TASK NAME [0 RED REM ACCOMP IN PHASE DATE DUE DUE FMS CODE WU GRND ASE RJ TRAINING ACAD GMTGRND ASE RJ TRAINING SEPT 6593 GBND R.) TRAINING STAN EVAI TEST 5565 GRND ASE RJ TRAINING OPLAN STUDY 6522 0 9 30 AUG 12 CT CRND A55 RJ TRAINING SERVICE 6525 GRND ASE RJ TRAINING FLY SAFETY 6526 GRND 3 TRAINING TEST SEC GRND ASE RJ TRAINING ISO PREP IEOGRND ASE RJ TRAINING AFE FAN TRNG LL91 0 0 15 JUL 14 GT GRND ASE RJ TRAINING EGRESS (NONEJ) LL63 GRND ASE RJ TRAINING ACDT LL84 GRND A59 RJ TRAINING EGRESS WACDE LL05 8 El 97 JAN 11 GT GRND ASE RJ TRAINING AFF TRNG LL96 GRND ASE R3 TRAINING LIKAL AREA SURV 5501 0 0 38 MAR 11 GT GRND ASE RJ TRAINING CWT SURV TING 5502 GRND ASE RJ TRAINING CAI TRNG 5503 GRND ASE TU TRAINING W51 5505 GRND ASE RJ TRAINING AFRICON $507!! 6 0 GT GRND ASE RJ TRAINING 5501C WIND Abt NJ TRAINING (CSI) 550" 0 0 GT GHND ASE RJ TRAINING PAIOH ICSI) 0 0 GT GRND ASE RJ TRAINING SOUWCOH (CST) $5875 GRND ASE RJ TRAINING SPEC SERE TRNG 5510 GRND ASE R3 TRAINING 9 9 22 FEB 12 AIA PAGE 2 PAGE 2 G-109 PREPARED 13 MAY 2015 19:51 NAME: PHYSICAL DUE DATE: 18 APR 16 CD DUALIFIEATION PROFILE TASK NAME GT GRND ASE RJ TRAINING ALERT RESPONSE RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2015 PCN SA936-T10 CURRENT TRAINING PERIOD GRADE: SRA SSAN: CREW POSITION: MKAEB UNIT: PHYSIOLOGICAL DUE DATE. 36 SEP 15 RECORDS REVIEW DUE DATE: 31 JAN 16 ACC TASK 'u DATE LAST DATE DVR IJI REST 850 REM Accom? 1? PHASE DATE nu: nu: cooAIA PAGE 3 PAGE 3 G?llO 64?4848, Class A, 30 April 15, AFSAS #739726 G137. [Mishap Airborne MISSION Supervisor] G1.7.1. CERTIFICATE OF AIRCREW QUALIFICATIONS CI 08 - 4 .1 lulu. link to Of?RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.7.2. FLYING HISTORY REPORT PREPARED 01 MAY 2015 18:21 FLYING HISTORY REPORT (PA) AS OF 01 MAY 2015 PCN 5A036-F40 INQUIRY NAME: SSAN: GRADE: MSG APT. A TAC: A OFOA: 109 ASC: BA ASC DATE: 10 FEB 15 CMD: AFR PRI P05: 0 PR1 ACET: Rc135v UNIT: 0097INTSO BASE: OFFUTT AFB AIRCRAFT TOTALS CAREER TOTALS AIRCRAFT Ros RCISSNIS) SRCISSMIO) CREN POSITION LINGUIST FLT DTY CERT CODE EOAEM EOAEM EOAEM UOAEM EOAEL PRIMARY TIME 1926.5 DATE FIRST FLOWN SECONDARV TIME 0.0 DATE LAST FLONN INSTRUCTOR TIME 120.0 TOTAL TIME 1007.3 664.1 230.2 426.0 3.3 12.2 EVALUATOR TIME 41.7 PRIMARY TIME 009.0 045.4 205.7 400.0 3.3 10.7 mm TIME 11.7 SECONDARY TIME 0.0 0.0 0.0 0.0 0.0 0.0 TOTAL TIME 2100.7 INSTRUCTOR TIME 04.1 18.7 26.5 10.0 0.0 1.5 STUDENT TIME 0.0 EVALUATDR TIME 41.7 0.0 5.0 0.0 0.0 0.0 OTMER 05 MIL TIME 0.0 OTHER TIME 11.7 0.0 0.0 0.0 0.0 0.0 FOREIGN MIL TIME 0.0 NIGHT 26.7 6.9 0.0 10.0 1.1 0.0 CIVILIAN TIME 0.0 PRIMARY INST 0.0 0.0 0.0 0.0 0.0 0.0 CDMDAT TIME 910.9 PRIMARY SIM INST 0.0 0.0 0.0 0.0 0.0 0.0 COMBAT SUPT TIME 0.0 we TIME 0.0 0.0 0.0 0.0 0.0 0.0 TOTAL SORTIES 240 COMBAT TIME 550.0 309.4 0.0 59.5 0.0 0.0 COMBAT SORTIES 02 (MST SUPPORT TIME 0.0 0.0 0.0 0.0 0.0 0.0 COMBAT SUP SORTIES 0 COMBAT SORTIES 50 27 0 5 0 0 NVG TIME .0 CMBT SUPPORT scams 0 0 0 0 DATE FIRST FLOW 15 JLN 05 TOTAL SORTIES 110 79 94 48 1 4 DATE LAST FLONN 23 APR 15 GRAND TOTAL 2100.7 1 PAGE 1 G-112 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.7.3. 30/60/90 FLYING HISTORY REPORT PREPARED 20 HAY 2015 99:33 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 29 MAY 2015 PCN SAeas-er GRADF: MSOT A A ASC: BA DAFSC: IABTIG AGE: (MD: quu; aussnecwc ORGANIZATION: OOQIINTSQ CREW POSITION: EOAEM Asc DATE: 14 FEB 2915 CURR RATING: AIRCRAFT RC135V SERIAL no: 94-4949 MISHAP DATE. 39 APR 2915 MISHAP AIRCRAFT PR1 sec IRsr EVAL OTHER TOTAL NIGHT INS 519 1N5 son! 9:135v 869.8 9.9 94.1 41.7 11.7 1997.3 953.9 26.7 9.9 9.9 113 LAST 39 DAYS 9LAST 69 DAYS 22.8 9.9 6.8 9 9 9.9 29.6 29.6 11.7 9.9 9.9 4 LAST 99 DAYS 39.9 9 9.9 7 a 6.2 59.4 36.8 12.2 9.9 9.9 I OTHER AIRCRAFT PRI SEC INST EVAL OTHER TOTAL NIGHT INS INS SORT RCL35V 045.4 0.0 18.7 6.0 0.0 664.1 664.1 6.9 0.0 0.0 79 LAST 30 DAYS 0LAST 50 DAYS 5LAST 90 DAYS 5.5 0.0 0.0 0.0 0.0 5-5 5.5 1.4 6.0 0.8 SRCIBSW 213.7 6.0 26.5 5.0 6.3 244.7 239.7 0.0 9.0 6.6 97 LAST 30 DAYS 7LAST 69 DAYS 16.4 0.0 0.0 2.5 8.0 18.9 16.4 0.9 0.0 0.0 8 LAST 90 DAYS 18.7 0.0 0.8 2.5 8.9 21RC1355 408.0 0.0 18.0 0.0 0.0 426.0 426.0 18.0 0.0 0.0 40 LAST 30 DAYS 0LAST 60 DAYS 0DAYS 1RC13SU 3LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 0PAGE 1 (3-1.13 RC-I 35 V, 64-4848, Class A, 30 April 15. AFSAS #739726 AIRCRAFT MISHAP INVESTIGATION AS OF 26 MAY 2015 PCN SAGSB-FZG PREPARED 76 MAY 2015 99:33 API: A PAC: A ASC: BA DAFSC: 1A8716 AGE: NAME: "Vuuws? GRADE: MSGT SSAN: cno. AFR eessaEcwc 0097TNT50 anw POSITION: EOAEM ASC 14 FEB 2015 (URR RATING: AIRCRAF1 IYPE: RC135V SERIAL No: 04-4040 MISHAP DATE: 30 APR 2015 OTHER AIRCRAFT PRI SEC INST EVAL OTHER TOTAL NIGHT ms 5101 ms SORT snc135x 10.7 0.0 1.5 0.0 0.0 12.2 12.2 0.0 0 0 0.0 4 LAST 30 DAYS 0LAST 00 DAYS 0LAST 90 DAYS 0CAREER TOTALs =44 CREW POSITION FIRST FLIGHT PR1 SEC INST EVAL OTHER TOTAL STUDENT COMBAT COMBAT SORT LAST FLIGHT TIME SUPPORT AIRBORNE OPERATOR 15 100 2005 1920 0 0 120.0 41.7 11.7 2100.7 2047.3 0.0 910.9 0.0 240 23 APR 2015 PAGE 2 (3-1141 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.7.4. INDIVIDUAL DATA SUMMARY 91 MAY 2915 18:21 INDIVIDUAL DATA SUMMARY (PA) AS OF 91 MAY 2015 PCN INQUIRY NAME: SSAN: GRADE: MSG CMD: AFR WING: DOSSRECVC UNIT: 0097INTSO BASE: OFFUTT AFB PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: SECURITY CLEARANCE DATE: 19 JUL 10 SVC CAT: A=?r RESTRICTED AREA BADGE N0: LAST PHYS DATE: PROFESSIONAL DUAL INDEX PHYS CODE: PROFESSIONAL DUAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: PHYSIOLOGICAL INC DATE: Jun? STATUS PHYSIOIOCICAL DUE DATE: DATE ASSIGNED JUMP STATUS: DATE OF BIRTH: DUTY AFSC: 1A87IG EFFECTIVE DATE OF 61 APR 15 PAS CDDE: SYSTEM MANAGEMENT SHORT TOUR HARM CODE: DATE RETURN FHOM OVERSEAS: DEPLOYED HARM (ODE: DATE OF RANK: 01 MAY 12 DEPLDYED DATE: DATE OF 21 OCT 15 REDEPLOYED DATE: DEF LAST DUTY 25 94 CAT ID: ARR THIS STATI 1 22 99 RECORDS REVIEW Acc DATE: 69 SEP 14 13 RECORDS REVIEW DUE DATE: 30 JUN 15 PROJECTED PAS CODE: RECORDS REVIEW STATUS CODE. PROJECTED DUTY LOCATION: PRDJ DEPARTURE DATE: PRDJ REPORTING DATE: PAC 8 EFFECTIVE DATE: LOCAL use CODE: I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURF DATE AFR PACE 1 (3-1215 PREPARED 01 MAY 2015 18:21 NAME: AIRCRAFT OPLOC: END OF AIRCRAFT: ACFT SVC CAT: PRIMARY ACFT: FLT DUTY CERT CODE: CATEGORTCAL FLYING WAIVER: INCENTIVE PAY DATA LAST MPO DATE: LAST MPO REASON: IAD: PAY STOP DATE: LAST PRODUCTIVE FLIGHT DATE: PREVIOUS PRODUCTIVE FLIGHT DATE: AVIATION SERVICE DATA AVIATION SERVICE CODE: EFFECTIVE DATE: PRIOR ASC: EFFECTIVE DATE: AERO ORDER TERM DATE: OFFICER SERVICE DATE: AVIATION SERVICE DATE: TRANSITION STATUS CODE: AVIATION POSITION INDICATOR: EFFECTIVE DATE: FLYING ACTIVITV CATEGORY: PRE-ACIA-DFOA: OFDA GATE 10/12: OFDA GATE 15/15: OFOA GATE 20/18: OFDA TO DATE: You have met OFDA requirements I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. AIRCRAFT ASSIGNMENT DATA ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 SSAN: m?vx- SGBP 1C USAF RCIBSV EOAEM 26 NOV 13 NONE 106 109 109 for current gate. INDIVIDUAL DATA SUMMARY (PA) INQUIRY GRADE: MSG CMD: AFR AVIATION BADGE: EFFECTIVE DATE: AVIATION EFFECTIVE DATE: OUS MIL RTG DT: CURR PARA RATING: CURR PARA RATING ORIG PARA RATING: DRIG PARA RATING DATE: FORMAL COURSE REFRESHER PHYSIOLOGICAL HYPOXIA TRAINING INITIAL PHYSIOLOGICAL HYPOXIA TRAINING SIGNATURE PAGE 2 G-ll6 AS OF 01 MAY 2915 WING: OOSSRECWG AERONAUTICAL BADGE SENIOR AIRMAN AIRCREWMEMBER 22 FEB 12 (BASIC) AIRMAN AIRCREWMEMBER 21 FEB 06 STATUS DATE 19 SEP 14 09 NOV 04 DATE AFR PAGE 2 PCN SAOBG A70 UNIT: OOQTINTSO RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 (}l.7lfi PREPARED 13 MAY 2015 29:03 INDIVIDUAL TIME SUMHARV (FA) AS OF 13 MAY 2015 5A036-F70 REQUEST PERIOD FROM: 30 APR 2014 TO: 13 MAV 2015 ssnn: GnAoe- MSGT 991 995: 9 PR1 AIRCRAFT: RC135V CMD: AFR WING: aossnecwe UNIT: 999719159 ACFT 99109: 5999 TAIL DUTY CMB SIM M95 9419 NUMB POSN 991 sec 1951 EVAL 979 TDTAL 591 cna SRT 591 N919 INS INS NVG 995 RC13SS 99 MAY 14 91-2993 MOAEL 19.5 9.9 9.9 9.9 9.9 1961-2663 MOAEL [9.3 0.0 0.0 0.0 0.0 1991-2593 99491 991-2993 MOAEL 901-2663 MOAEL 491-2953 99491 91-2993 MOAEL 13.4 9.9 9.9 9.9 9.9 1392-4129 IOAEM 1CMB 51? 9c13ss SUMMARY FRI 59: INST EVAL 0TH 191A1 591 can 591 975 591 ?115 195 INS ~va AIRCRAFT: 99.3 9.9 1.9 9.9 9.9 71.3 a 9.9 9 9.9 9 11.9 9.9 9.9 9.9 SIMULATOR9.9 9.9 9.9 9.9 RPA0.0 0.6 0.0 0.0 Rc135v 97 AUG 14 92-4129 MDAEL 962-4130 MDAEL 894-4949 HDAEL 11.4 9.9 9.9 9.9 9.9 1194-4949 MOAEM 762-4130 094-4949 EDAEM 964-4949 MQAEM 664-4949 MOAEM 94848 HQAEM 10.7 0-0 0.0 0.0 0.0 1092-4131 IQAEM 9AFR PAGE 1 PAGE 1 CF117 RC-135V. 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:03 INDIVIDUAL puma 1mg gummy (9A) AS OF 13 MAY 2015 PCN SA030-F70 REQUEST PERIOD FROMI 30 APR 2914 TO: 13 2015 NAME: 3] SSAN: GRADE: MSGT PR1 CREW P05: 0 PRI AIRCRAFT: cm): Am wmu: UNIT: 0097INTSO ACFT OPLOC: SGSP TAIL DUTY (MB SIM 0405 DATE NUMB POSN PR1 SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG RES 048 SIM RC135V SUMMARY PRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NIT: 1N5 INS AIRCRAFT: 58.9 0.0 6.8 7.4 6.2 79.3 10 0.0 0 0.0 0 14.7 0.0 0.0 0 SIMULATORRPARC135W 02 OCT 14 62-4131 MOAEI. 10.8 0.0 0.0 0.0 0.0 1062-4131 MOAEM 50.0 0.0 0.0 CMB SIM RCIBSH SUMMARY PRI SEC INST EVAL 0TH TOTAL SRT CKB SR1 SRT NITE INS INS AIRCRAFT: 16.3 0.0 0.0 0.0 0.0 16.3 2 0.0 0 0.0 0 3-9 0.0 0.9 SIMULATORRPA62-0001 MOAEL 262?0001 MOAEL 202-0001 MQAEL 262-0001 MOAEL 262.0001 EOAEL 262-0001 MOAEL 202-0001 EOAEL 2.162-0001 MOAEL 262-0001 MOAEL 252-6001 MOAEL 462-0001 MOAEL 262-0001 EDAEM 20.0 0.0 0.0 0.0 AFR PAGE 2 PAGE 2 G-118 o'cnen babe RC-135V. 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 215 20:93 INDIVIDUAL FLYING TIME SUMMARY (pm AS OF 13 MAY 2615 PCN SA036-F70 REQUEST PERIOD FROM: 30 APR 2614 TO: 13 MAY 2915 SSAN: GRADE: M50T PR1 CREW Pos: 0 PR1 AIRCRAFT: RC135V cno: AFR 0100: 0055R?cwc UNIT: ACFT OPLOC: SGBP TALL DUTY an 51M Mos DATE MUMB POSN PRI sec INST EVAL 0TH TOTAL SRT CME SRT SRT NITE INS INS NVG RES SRc1zsw 18 DEC 14 62-0001 262-0001 EOAEM 262-0001 MOAEM 262-0001 MDAEM 62-0001 EOAEM 262-0001 EQAEM 262-0001 MQAEM 202-0001 EQAEM 002-0001 EOAEM 262-0001 EQAEM 262-0001 EQAEM 202-0001 EOAEM 262-0001 EOAEM 2cna 1/5 51M 5Rc1asw SUMMARY PR1 sec INST EVAL 0TH TOTAL SRT OMB SRT SRT NITE INS 1N5 NVG AIRCRAFT0.0 0.0 0.0 0.0 SIMULATOR: 57.0 0.0 0.0 2.5 0.0 59.5 25 0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 cna SIM GRAND TOTALS PR1 55c INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG AIRCRAFT: 143.5 0.0 9.0 7.4 6.2 166.9 20 0.0 0 0.0 0 29.6 0.0 0.0 0.0 SIMULATOR: 57.0 0 0 0.0 2.5 0.0 59.5 25 0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 AFR PAGE 3 PAGE 3 G-ll9 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.7.6. INDIVIDUAL FLIGHT RECORD PREPARED 01 HAY 2015 10.21 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS or 01 MAY 2015 PCN 54036-1670 INQUIRY 55411: GRADE: MSGI P01 6st P05: 0 PRI AIRCRAFT: Rc135v mo: AFR wmc: 005506ch mm: 0091111150 ACFT OPLOC: 5000 IAIL DUTY EMS 51" DATE MOS DATE NUMB POSN FRI SEC ??57 EVAL IOTAL SRT CHE SRT SR7 NITE INS INS NVG RES UPDAIED mass 06 MAY 14 61-2663 HOAEL 10.5 0.0 0.0 0.0 0.0 1020140507 RC1355 08 MAY [4 51*2563 MOAEL 19.3 9.5 0.0 6.0 0.9 1929140512 RCIBSS 10 1141/14 61-2663 HOAEL 620140521 RC1355 221141114 61-2663 ?01101 020140606 00355 03 JUN 14 61-2663 HQAEL 420140606 RC13SS 09 JUN 14 61-2663 HOAEL 420140610 15 JUN 14 61-2663 HOAEL 13.4 0.0 0.0 0.0 0.0 1320140617 SRc135w 0210114 62-0001 HOAEL 220140702 SRC135W 08 ?ll 14 67-0091 NOAEL 229140719 RCIBSV 07 4110 14 62-4126 HOAEL 920140019 SRCISSW 25 AUG 14 62-0001 MOAEL 220140025 sncusw 20 1105 14 02.0001 140451 220140020 5Rc135w 02 SEP 14 62-0001 EOAEL 220140904 RC135V 05 SEP 14 62-4130 MQAEL 020140900 mass?: 10 sep 14 620001 ?01101 220140910 SRE13SW 22 500 14 62-0001 EOAEL 220140922 SRC135W 23 SEP 14 62-0001 HOAEL 220140023 snc135w 25 SEP 14 620001 00451 220140925 00350 02 on 14 62-4131 ?0401 10.0 0.0 0.0 0.0 0.0 1020141015 11613511 07 OCT 14 64-4040 110461 11.4 0.0 0.0 0.0 0.0 1120141015 5Rc13sw 10 on 14 152-6001 110421 420141015 mass?: 24 ?av 14 620001 004121 220141124 511613514 04 05c 14 62-0001 EOAEM 220141204 10 DEC 14 62-0001 EOAEM 220141210 5Rc135w 13141115 62-0001 204620150113 Rc135v 03 FEB 15 64-4040 ?011214 7.2 0.0 0.0 0.0 1120150204 AFR PAGE 1 I CERTIFY nun I HAVE REVIEWED 1w IFRR AND IT IS COMPLETE 400 ACCURATE. SIGNATURE 041': PAGE 1 G-120 RC-135V, 64-4848, Class A, 30 April 15. AFSAS #739726 PREPARED 91 MAY 2915 19:21 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 91 MAY 2915 PCN 511939-1/9 INQUIRY SSAN: GRADE: PR1 P05: 9 AIRCRAFT: Rc135v c119: Ark 9199: 9955RECMG UNIT: 9997IMT59 ACFT 9919c: 5999 TAIL DUTY EMB SIM DATE M95 DATE NUMB POSN PR1 sec 1951 EVAL 0TH TOTAL SRT CMR SET :15 SRT MTTE 1115 195 we RES UPDATED 99 FEB 15 52-9991 MDAEM 229159299 RE13SV 10 FEB 15 52-4130 MQAEM 00.0 0.0 0.9 0.0 20150219 17 FEB 15 64-4848 EOAEM 929159219 Rt1355 23 FEB 15 52-4128 IDAEM 129159224 Rc135w 99 MAR 15 92-4131 MDAEM 529159423 sac1359 99 MAR 15 52-9991 MQAEM 229159399 SRc135w 11 MAR 15 62-9991 EQAEM 229159311 5Rc13511 12 MAR 15 52-9991 EQAEM 229159312 RC135V 16 MAR 15 64-4848 MQAEM 620150323 SRc135w 19 MAR 15 52.9991 MQAEM 229159319 Rc135v 19 MAR 15 54-4848 MDAEM 529159323 SRc13sw 23 MAR 15 62-9991 EQAEM 929159323 RC135V 27 MAR 15 64-4848 MQAEM 10.7 0.0 0.0 0.0 0.0 1020150402 06 APR 15 67-0001 FOAFM 020150406 sacusw 15 APR 15 62-0001 229159415 5Rc13sw 22 APR 15 52.9991 EQAEM 229159422 RC135V 23 APR 15 62-4131 IQAEM 020150428 c119 5114 M95 SUMARY PR1 5Ec INST EVAL 9111 mm SRT c119 5R1 us 5R1 M111. ms 195 NVG 143.5 9.9 9.9 7.4 5.2 159.9 29 9.9 9 9.9 29.9 9.9 9.9 9.9 SIMULATOR: 53.9 9.9 9.9 2.5 9.9 55.5 23 9.9 9.9 9.9 9-9 RPA9.9 9.9 9.9 9.9 AFR PAGE 2 I CERTIFY THAT I HAVE REVIEWED HY IFRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 2 6-121 RC-I35V, 64-4848, Class A. 30 April 15, AFSAS #739726 PREPARED 13 MAY 2915 20:83 NAME PHYSICAL DUE DATEWALIFKLATION PROFILE was TRNG AIS DUTY CHC tuna/cs cm mt cm cm tuna/cs cu m: nuts/rs rm (Fl (Ht CHI (E0 (Ht Mica/(s m. mt on (El cm (MC RJ/(llts In ENC (MI Mica/(S (m (E. RJ/ca/(E) CHC RJ/cB/(E) GRADE INDIVIDUAL TRAINING SUVHARY CURRENT TRAINING PERIOD SSAN: PHYSIOLOGICAL DUE 36 SEP 19 TASKNAHE LANG EVT ANS RECUR EVAL Ms SID Ms mm 0% sac/sow (Mt CONT PRO 5m RIYET JOINT 51" COBRA BALL RAP (MAT SENT SM 135 (unusual 51RAP sac/sew (swam TASK ID M24 A997 "?81 ?109 SR59 ERGO 59.60: ?61 SRGIE no a a a? CONDO-I: PAGE I. ACCONP (3h1122 AS OF 13 MAY 2615 CREW POSITION: EOAEM RECORDS REVIEW DUE DATE: 30 JUN 15 DATE LAST 23m" UNIT: ODQTINTSO Acc DATE ova IA am IN ms: DATE out DUE AFR PAGE 1 CODE IND RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:03 INDIVIDUAL SUMMARY AS OF 13 MAY 2015 PCN SA036-T16 CURRENT TRAINING PERIOD NAME: GRADE: MQGT SSAN: CREN POSITION: EOAEM UNIT: 6997INTSO PHYSICAL DUE DATE: 21 APR 16 PHYSIOLOGICAL DUE DATE: 36 SEP 19 RECORDS REVIEW DUE DATE: 30 JUN 15 ACC POM TASK DATE LAST OATE OVR IN REST CO OUALIFICATION PROFILE TASK MHE ID R50 REM ACCONP IN PHASE DATE ONE DUE ms CODE wn CN CK RJ/ca/cs CMR (E) TOT sxoe CNC CNR (E) BASIC same 5x03 RECUR EVAL A395 DUTY N542 19.3 CERT 5575 CERT x3990 OI OCT 13 CMC BL TRNE R1 BL 19 CURRENCV x318 TRNE FU BL 11 CERT mm a as JUL 1: 51' CONSEC TRAINING CORSEC CONSEC TRAINING CORSEC Read 51111 TRAINING ANTI-HUMK mas 16 51:? 16 sec: 15 CT ORNO ms TRAININO can came GRNO ms TRATNING MO OUAI canGRNO ms TRAINING AmGRNO MS TRAINING SEPT 6503 GRNO ms TRAINING STAN EVAL TEST 5555 GRNO ms TRAINING OPLAN STUDY (5522 (14 APR 14 GT GRND ms TRAININO FLY TRNG 6526 ORNO ms RISNO CERT 6556 ORNO ms TRAININO svunv 6551 GRMD ms TRAINING NICKELBACK 0555 TRAININC. csr61' GRNO ms TRAININs 8019 (2 PRO 6559 AFR PAGE 2 PAGE 2 G-123 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARE) 13 MY 2915 26:03 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2615 Put CURRENT TRAINING PBIIOD GRADE: SSAN: CREW POSITION: EOAEM UNIT: 0097INTSO PHYSICAL DUE DATE: 21 APR 16 PHYSIOLOGICAL DUE DATE: 30 SEP 19 RECORDS REVIEW DUE DATE: 3 JUN 15 ACE TASK 1. DATE LAST GATE ova IN REST cn IILIALITICATIGN PROFILE TASK NAME ID REG REM Kconp IN PHASE DATE DUE nus ms cone wn GT GRND ANS TRAINING TGST sac G512 GET: 15 No GT Gmo ms TRAINING ISO PREP IEOZ Ans TRAINING AFF rm TRNG L101 11 a 91 JUN I GT 6ND ANS TRAINING EGRESS (NONEJ) LL93 GFWD AFB TRAINING MDT LL04 GANG ms TRAINING mess 1mmGRND ANS TRAINING TRNG LL06 TRAINING LOCAI. AREA suuv 5591 a II 15 FEB as GT 6WD Ans TRAINING cm suav TRNG $502 TRAINING TANG $563 GRNII ANS TRAINING 5565 (IND M6 TRAINING ATRIOOH (L511 558M 9 51? SEND ME TRAINING CENTCOM (C51) 5597C cam: ms TRAINING sum! 5597: a I 6' GRNII ms TRAINING mo? 5597? GT GPND ms TRAINING soumton 55975 TRAINING SPEC SERE TANG 5519 GRND ms TRAINING s-vas-A 5524 93 JUL 12 GT GRND ms TRAINING ssnGRND ms TRAINING ALERT RESPONSE mas GHND UK LAND TRNG GLOBAL LMG man AFR PAGE 3 PAGE 3 64?4848, Class A, 30 April 15, AFSAS #739726 tol G1.8. smogrgg?'w (MCO) G1.8.1. CERTIFICATE OF AIRCREW QUALIFICATIONS _l to um mm :9 on?. 3-3373 n553338ag - w; m. ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.8.2. FLYING HISTORY REPORT PREPARED 01 MAY 2015 17:47 FLYING HISTORY REPORT (PA) As or 01 MAY 2015 PCN 5A035-F40 INQUIRY SSAN: Wu?- ORAOE: SRA A FAC: A 10 ASC: AA Asc DATE: 15 MAR 14 cm: AIA WING: 0055REcw PR1 P05: 0 PRI ACFT: RC13SV UNIT: 0097INTSQ BASE: OFFUTT AFB AIRERAFT TOTALS CAREER TOTALS AIRCRAH Mus caew POSITION LINGUIST FLT CERT CODE MOANL UOANL UQANL PRIMARY TIME 59.7 DATE FIRST FLOUN DATE NO DATE SECONDARY TIME 0.0 DATE LAST FLOWN DATE NO DATE INSTRUCTOR TIME 0.0 TOTAL TIME 50.7 15.9 24.2 0.0 0.0 EVALUATOR TIME 0.0 PRIMARY TIME 43.8 15.9 24.2 0.0 0.0 OTHER TIME 0.9 SECONDARY TIME 0.0 0.0 0.0 0.0 0.0 TOTAL TIME 66.6 LNSIRUCTOR TIME 0.0 0.0 0.0 0.0 0.0 STUDENT TIME 0.0 EVALUATOR TIME 0.0 0.0 0.0 0.0 0.0 OTHER us MIL TIME 0.0 OTHER TIME 6.9 0.0 0.0 0.0 0.0 FOREIGN MIL TIME 0.0 NIGHT 2.0 1.4 0.0 0.0 0.0 CIVILIAN TIME 0.0 INST 0.0 0.0 0.0 0.0 0.0 COMRAT TTMF 0.0 PRIMARY SIM INST 0.0 0.0 0.0 0.0 0.0 COMBAT SUPT TIME 0.0 NVG TIME 0.0 0.0 0.0 0.0 0.0 TOTAL SORTIES 11 COMBAT TIME 0.0 0.0 0.0 0.0 0.0 COMBAT SORTIEs 0 CMBT SUPPORT TIME 0.0 0.0 0.0 0.0 0.0 COMBAT SUP SORTIES 0 COMBAT 0 0 0 0 NVG TIME 0.0 CMBT SUPPORT SDRTIES 0 0 0 DATE FIRST FLOWN 00 res 14 TOTAL SORTIES 0 3 10 0 0 DATE LAST now 06 MAR 15 G-126 GRAND TOTAL 66 . 6 RC-I35V. 64-4848, Class A, 30 April 15, AFSAS #739726 G1.8.3. 30/60/90 FLYING HISTORY REPORT PREPARED 20 MAY 2015 09:40 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 20 MAY 2015 PCN 5A030-F20 NAME: GRADE: SRA SSAN: m-n- A FAC: A Asc: AA DAFSC: mam AGE: 010: Am lle: 0055:20ch ORGANIZATIOM: 009710050 (000 POSITION: NOANL ASC DATE: 15 MAR 2014 CURR RATING: AIRCRAFT TYPE: RC135V SERIAL NO: 64'4848 MISHAP DATE: 39 APR 2015 MISHAP AIRCRAFT sac 1051 EVAL omen TOTAL 001/1051 mom ms 510 ms soar 43.0 0.0 0.0 0.0 0.9 50.7 43.0 2.0 0.0 0.0 0 LAST 3 DAYS 0LAST 00 DAYS 0LAST 90 omrs 0OTHER AIRCRAFT FRI SEC INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT RCISSV 15.9 9.9 9.9 9.9 9.9 15.9 15.9 1.4 9.9 9.9 3 LAST 39 DAYS 9LAST 69 DAYS 5LAST 90 DAYS 5SRCI3SW 26.2 0 0.9 9.9 11 LAST 39 DAYS 2LAST 69 DAYS 7LAST 99 DAYS 11 5 6.9 0.0 0 9 0.0 11.5 11.5 0.0 9.9 9.9 RCIBSS LAST 39 DAYS 9LAST 60 DAYS LAST 90 DAYS LAST 39 DAYS 9LAST 69 DAYS 9LAST 99 DAYS 9PAGE 1 6-127 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 20 My 2915 99:49 AIRCRAFT MISHAP mvesnomon (PA) As or 20 MAY 2015 PCN SAOSG-FZO GRADE: SRA SSAN: API: A A ASC: AA 1A831H AGE: CMD: "Inn; OOSSRECNG ORGANIZATION: 0097INTSO CHEN POSITION: MOANL ASC DATE: 15 MAR 2014 cuaa RATING: AIRCRAFT TYPE. RC135V SERIAL no: 64-4848 MISHAP DATE: 30 APR 2015 u- omen ?t PRI SEC INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT CAREER TOTALS CREW POSITION FIRST FLIGHT PR1 SEC INST EVAL OTHER TOTAL STUDENT COMBAT COMBAT SORT LAST FLIGHT TIME SUPPORT AIRBORNE OPERATOR 06 FEB 2014 59.7 6.0 0.0 0.0 6.9 66.6 59.] 0.9 0.0 6.9 11 06 MAR 2015 PAGE 2 G-128 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.8.4. INDIVIDUAL DATA SUMMARY PREPARED 61 MAY 2015 17:47 INDIVIDUAL DATA SUMMARY (PA) INQUIRY AS OF 01 MAY 2015 PCN SADBG-A7G SSAN: m-u GRADE: SRA CMD: AIA WING: ODSSRECNG UNIT: OO97INTSO BASE: urruoo Ara PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: SECURITY CLEARANCE DATE: 17 AUG 11 MBR CAT: USAF RESTRICTED AREA BADGE N0: LAST PHYS DATE: PROFESSIONAL DUAL INDEX (POI): PHYS CODE: PROFESSIONAL OUAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: PHYSIOLOGICAL TNG DATE: JUNP STATUS PHYSIOLOGICAL DUE DATE: DATE ASSIGNED JUMP STATUS: DATE OF BIRTH: DUTY AFSC: EFFECTIVE DATE OF DUTY: 21 NOV 14 PAS CODE: ODOUFX1F SYSTEM MANAGEMENT SHIRT TOUR INDICATOR: HARM CODE: 568p DATE RETURN FROM OVERSEAS: DEPLOYED CODE: DATE OF RANK: 1; NOV 13 DEPLOYED DATE: DATE ARR THIS STATION: ?1 13 RECORDS REVIEW ACC DATE: 19 FEB 14 1? RECORDS REVIEN DUE DATE: 23 FEB 15 PROJECTED RECORDS REVIEN STATUS CODE: PROJECTED PAS CODE: PROJECTED DUTY LOCATION: PRDJ DEPARTURE DATE: PRGJ REPORTING DATE: FAC EFFECTIVE DATE: LOCAL USE CODE: I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. PAGE 1 SIGNATURE DATE AIA (I-ISE9 PAGE 1 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 61 MAY 7615 17:47 INDIVIDUAL DATA SUMMARY (PA) INQUIRY A5 UT 91 MAY 2015 PLN NAME: SSAN: BASE: OFFUTT AFB AIRCRAFT ASSIGNMENT DATA GRADE: SRA CMD: AIA WING: UNIT: DDQ7INTSO AERONAUTICAL BADGE AIRCRAFT OPLOC: CMD OF AIRCRAFT: 1? No RATINGS OR BADGES SELECTED ACCT CAT: USAF PRIMARY ACFT: RC135V FLT DUTY CERT CODE. CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA LAST MPD DATE: 15 Nov 13 LAST MP0 REASON: NONE PAY STOP DATE: 14 NOV 23 LAST PRODUCTTVE FLIGHT DATE: 06 MAR 15 PREVIOUS PRODUCTIVE FLIGHT DATE: 15 DEC 14 uus MIL RTG or; AVIATION SERVICE DATA CURR PARA RATING: AVIATION SERVICE CODE: AA CURR PARA RATING DATE: EFFECTIVE DATE: 15 MAR 14 ORIG PARA RATING: PRIOR ASC: Ax ORIG PARA RATING DATE: EFEECTIVERDATE: ATE 14 I233 STATUS AER DRDE ERM 14 OFFICER SERVICE DATE: FORMAL COURSE DATE AVIATION SERVICE 15 Nov 13 INITIAL PHYSIOLOGICAL HYPOXIA TRAINING IO AUG 11 TRANSITION STATUS CODE: 9 AVIATION POSITION INDICATOR: A EFFECTIVE DATE: 21 NOV 14 FLYING ACTIVITY CATEGORY: A OFDA GATE 19/12: 13 OFDA GATE 15/15; 0 OFDA GATE 26/18: 0 OFDA TO 18 Your current OFDA Is 18 month(s). You need 54 additional month(s) OFDA to meet your 10 Year gate requirement to receive conIInuous CEFIP through 15 years of aviauon service and you must maintain a valid ?ight physical. I CERTIFY WHAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE AIA PAGE 2 PAGE 2 G-l30 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 (}191115. REPARED 13 2915 INDIVIDUAL FLYING TIHE summv (FA) AS OF 13 WW 2915 ?936479 REQUEST PERIOD FROM: 30 APR 2014 TD: 13 MAY 2915 DOOZ @530 @032 SSAN: mm- GRADE: 59A 991 can: 995: PR1 AIRCRAFT: acusv cun: AIA NING: eossaccwc ACFT OPLOC: TAIL DUTY cna SIM 995 DATE 9999 POSN PR1 sec INST EVAL 0TH TOTAL SRT can SAT SRT NITE INS INS NVG 9c135v 15 MAY 14 93-9792 MOANL 764-4841 MOANL 693.9792 MOANL 59.9 9.9 9.9 9.9 :99 s19 ac135v SUMMARY 991 sec INST EVAL 0TH TOTAL SRT cna SRT SRT NITE INS INS AIRIRATT: 29.9 9.9 9.9 9.9 9.9 299.9 9.9 9.9 SIMULATOR9-9 9.9 9.9 RPA9.9 9.9 was?: 15 99c 14 52-4131 MQANL 492-4131 MOANL 51.4 9.9 9.9 9.9 cne ~51" RCIasw SUMMARY PRI 55c INST EVAL 9TH TOTAL SRT :99 SRT SRT NITE INS INS AIRCRAFT0.0 1.4 8.9 8.9 SIMULATOR92-9991 MOANL 292-9991 MOANL 392.9991 MOANL 292-9991 MOANL 292-9991 MOANL 62-9991 MOANL 262-9991 MOANL 262-9991 MOANL 292-9991 MQANL 29.9 9.9 9.9 9.9 AIA PAGE 1 PAGE I G?l3l RES @000 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 29:16 INDIVIDUAL FLYING TIME SUMMARY (pm AS OF 13 MAY 2815 SAME-F79 REQUEST PERIOD TRON: 30 APR 2014 TO: 13 MAY 2015 NAME: SSAN: m-w canoe: SRA FRI (new P05: 0 PR1 AIRCRAFT: ncusv cm: Au mus: aossREcwc mm: aeonurso ACFT UPLOC: mu. uurv cna us 51!? Has one nuns posu sec INST EVAL RES SRCISSW 06 APR 15 62-0001 MOANL 262-0001 HDANL 20.9 0.0 0.0 0.8 CMB SIM SRCIBSW SUMMARY FRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG AIRCRAFT0.0 0.0 9.0 0.0 SIMULATOR: 26.2 0.0 0.0 0.0 0.0 26.2 11 0 0 0 0 0.0 0.6 RPA0.0 0.0 0.0 0.0 CH3 SIM GRAND TOTALS PR1 SEC INST EVAL 0TH TOTAL SRT CMB SET SRT NITE INS INS NVG AIRCRAFT: 29.9 0.0 0.0 0.0 0.0 29-9 5 0.0 0 0.0 0 1.4 0.0 0.0 0.0 SIMULATOR: 26.2 0.0 0.0 0.0 0.0 26.2 11 MIA 0.9 0.0 0.9 0.0 RPA0.0 0.0 0.0 0.0 AIA PAGE 2 PAGE 2 G-l32 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.8.6. INDIVIDUAL FLIGHT RECORD PREPARED 61 MAY 2615 17:47 INDIVIDUAL FLIGHT RECORD REPORT (PA) A: 01- en MM 2015 pcu INQUIRY SSAN: m-N- GRADE: SRA PRI CREW P05: 991 AIRCRAFT: RC13SV 9149: MA WING: 995519ch UNIT: 99971NT50 ACFT OPLOC: TAIL DUTY (MB SIM DATE "05 DATE NUHB POSN PR1 SEC EVAL 07H FOTAL SKI SRT SRT NIKE INS NVG RES UPDATED 15 MAY 14 63-9792 MOANL 729149521 59(13511 99 JUL 14 92. 9991 991119 229149719 snc1asw 16 JUL 14 62-9991 HOANL 329149719 RC135V 99 AUG 14 64-4941 HOANL 629149914 59(13511 15 AUG 14 62-9991 MOANL 229149919 9c135v 93 on 14 63-9792 HOANL 529141996 51913511 17 OCT 14 62-9991 MQANI29141927 59(135w 24 Nov 14 62-9991 MQANL 229141124 RCI35W 15 DEC 14 62-4131 NQANL 429141215 SRC13SW 03 FEB 15 62~9001 MQANL 220150294 sacusw 96 FEB 15 62-9991 NQANL 229159297 5903514 93 MAR 15 62-9991 MOANL 29159393 11:13va 99 MAR 15 52-4131 NQANL 529159423 59113511 11 MAR 15 62-9991 NOANL 229159311 sac135w 96 APR 15 62-9991 MOANL 229159496 (149 5111 1195 SUMMARY PRI sec INST EVAL (119 TOTAL SRT c149 5111 591 um INS 1115 WC 4191:9491: 29.9 9.9 9.9 9.9 9.9 29.9 5 9.9 9.9 9 1.4 9.9 9.9 9.9 41911111911: 24 2 9 9 9.9 9.9 9.9 24.2 19 11/71 9.9 9.9 9.9 9.9 RPA9.9 9.9 9.9 9.9 AIA PAGE 1 I CERTIFY THAT I HAVE REVIEWED 14v 1999 AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 1 6-133 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.8.7. INDIVIDUAL TRAINING SUNINIARY PREPARED 13 MAY 2015 26:99 NAME: PHYSICAL DUE DATEDUAL I ION PROFILE CHC CNC CMC CHE CHC CHC CHE (Ulla/L5 CHE CHC ENC ED DUTY CD DUTY ((N) GRADE: SM INDIVIDUAL TRAINING SUMMARY CURRENT TRAINING PERIOD 55m: PHYSIOLOGICAI DUE DATE: 3] AUG 16 TASK NAME CK CW: CONT PRO 51H RIVET JOINT RAP 51M caanA BALL RAP SIN COMBAY SENT RAP SIM 135 CURRENCY SIM CKC SRO 51n(n[(mur TOT SIM SBWS TOT 51H RAP TOT RAP 515 an ID RAP (0 RJ RAP CBRAP CB RAP co ca RAP sue/sale CS RAP CSRAPCO cs RAD Tm BASIC SORTIE C0 REEUR EVAL C0 DUTY TASK 5060 SRHC SRSD SR66C SRSOR 5X69 5X83 A365 QIHQOPOGH can? PAGE 1 REM 3 109 100 umbbuoaawcoowwon?mocom?M G-l34 CREW POSITION: NOANL DATE LAST MIN MAY 2015 DATE IN PHASE PCN SAB36-T16 UNIT: 6397INT50 RECORDS REVIEW DUE DATE: 28 FEB 15 DAVE DUE OSHARIB AIA ACC ova REST our: PHS cane PAGE 1 PREPARED 13 MAY 2015 29:09 NAME: PHYSICAL UUI: DAIEQUALIFICA1ION PROFILE C0 DUTY C0 LAN: TRNG NJ CMC BL TENS RJ Bl. 1m; in (NC BL TRNG PJ (NC BL Tm; GRND CD TRAINING GRND co IRAINING GRND CD TFAINING 6M0 co 1M1NING GRND co mums Wu Lu "mum. 6mm co TMINING cm cn 5mm (0 MINING GRND co TRAINING GENO ?0 TRAINING GENO CD TRAINING GRND co TRAINING GRND CO TRAINING GRND "mums GRNO co TRAINING cam co TRAINING sale (0 TRAINING IASK NAME SIN co DUTY LANG EVT R.) BL 18.3 CENT CURRENCY In El. 11 CERT (RN n9 QUAL ACAD SEPT SIAM EVAL on?: may FLY SAFETV TRNG NIIKELBACN C591 TEST SEC ISO PREP GLOBAL IANG EVT AFE FM TRNG EGRESS (NONEJ) ACDT amass WACDE AFE ma RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 GRADE SRA INDIVIDUAL TRAINING SUMMRY CURRENT TRAINING PERIOD SSAN: .zt_ PHYSIOLOGICAL DUE DATE: 31 AUG 16 IASK ID FKAZ LA24 6578 X3890 X810 X3110 0006 GA4E 6563 LEGS 6522 6526 6555 6557 6572 IE92 LL01 LL63 LL04 LL05 LL96 vounuu 1; RED AccaMP REM PAGE 2 G-l35 CREW POSITION: MOANL DATE LAST Accow MAY 2915 DATE 1N PHASE 31 DEC IA 38 JUN 15 PCN SAOJB-TIG UNIT: BDWINTSO RECORDS REVIEW DUE 28 FEB 15 DATE DIE REST DUE PHS CODE UVD PAGE RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:09 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2915 PCN CURRENT TRAINING PERIOD NAME: GRADE: SRA SSAN: PHYSICAL DUE DATE: 14 FEB 16 PHYSIOLOGICAL DUE DATE: 31 AUG 16 (REV POSITION: MOANL UNIT: 6697INTSO RECORDS REVIEW DUE 28 FEB 15 ACC POM TASK DATE LAST DATE OVR IN NEST CD QUALIFICATION PROFILE TASK NAME In 350 ACCOMF R51 IN PHASE DATE OLE DUE PHS CODE WD 61' GRND CO TRAINING LOCAL SURV 5591 9 03 JAN 14 GT GRID C0 TRAINING (MOT TRNG $582 GRID (O TMINIM: (AC TRNG $503 GRND CD TRAINING 5583 TRAINING AFRICON (C51) 5507A 0 GT (0 TRAINING (CST) 5567! 19 JUN 14 GT GRID CO TRAINING BJCON (C51) SSGTE 8 GT (0 TRAINING SSO7P 9 GT GRID CO TRAINING SOUTHCOM $5075 9 9 GT GENO CO THAINING SPK SERE TRNG $518 GENO C0 TRAINING S-V83-A 5524 0 1! OCT 13 (O TRAINING ALERT RESPONSE M83 AIA PAGE 3 PAGE 3 G?l36 64?4848, Class A, 30 April 15, AFSAS #739726 Airbo G1-9- SRA 5&3; 5.1932"; 21 (MASEZ) G1.9.1. CERTIFICATE OF AIRCREW QUALIFICATIONS DME. bMu .?Ol'a M3 (S u! rI Illkal-m?. (-mmamev 94: I4: G-l37 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.9.2. FLYING HISTORY REPORT PREPARED 91 MAY 2015 29:98 FLYING HISTORY REPORT (PA) AS OF 01 MAY 2915 PCN 5A036-Fao INQUIRY NAME: GRADE: SRA API. A FAC: A OFDA: 23 ASC: AA as: DATE: 34 DEC 13 040; AIA PRI (Rw ACFT: RC135V UNIT: 6343RCNSO BASE: OFFUTT AFB AIRCRAFT TOTALS CAREER TOTALS AIRCRAFT MOS RC135WS) CREW POSITION RADIO OP FLT DTY CERT CODE MKAEZ MKAE2 PRIMARY TIME 672.0 DATE FIRST FLOWN SECONDARY TIME 0.6 DATE LAST FLOW INSTRUCTOR TIME 0.0 TOTAL TIHE 328.6 343.4 11.6 EVALUATOR TIME 0.0 PRIMARY TIME 328.6 343.4 11.6 OTHER TIME 6.6 SECONDARY TIME 6.8 6.0 6.0 TOTAL TIME 672.6 INSTRUCTOR TIME 6.9 0.0 9.0 STUDENT TIME 6.6 EVALUATOR TIME 6.9 6.0 6.6 OTHER US MIL TIME 6.0 OTHER TIME 6.6 6.0 0.0 POREIGN NIL TIRE 6.6 NIGHT 36.0 51.9 9.0 CTVTI TAN TIME 0.6 PRIMARY INST 6.8 6.8 6.6 COMBAT TIME 294.6 PRIMARY SIN INST 6.6 6.0 6.6 COMBAI SUPT TIME 6.6 NVG TIME 6.0 0.0 9.0 TOTAL SORTIES 86 CMBAT TIME 173.6 121.8 6.6 COMBAT SORTIES 27 CMBT SUPPORT TIME 0.0 6.0 6.0 COMBAT SUP SORTIES COMBAT SORTIES 16 11 9 NVG TIME 6.0 (NET SUPPORT SORTIES 6 0 6 DATE FIRST FLOW 23 SEP 13 TOTAL SORTIES 39 47 5 DATE LAST FLOWN 23 APR 15 GRAND TOTAL 672.0 PAGE 1 G-l38 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.9.3. 30/60/90 FLYING HISTORY REPORT PREPARED 20 MAY 2015 09:12 ALRCRAFT HISHAP 1NVESTIGATIDN (PA) AS OF 20 MAY 2015 PCN SA030-F20 GRADE: SRA A A ASC: AA DAFSC: 1A351 cuo: AIA NING: 6343RCNSO ORGANIZATION: 9343RCNSO (new POSITION: Asc DATE: 04 DEC 2013 cuna AIRCRAFT TYPE: RCIJSV SERIAL NO: 04-4040 MISHAP DATE: 30 APR 2013 MISHAP AIRCRAFT PR1 sac INST EVAL OTHER TOTAL NIGHT 510 INS SORI RC135V 320.0 0.0 0.0 0.0 0.0 320.0 320.0 30.0 0.0 0.0 39 LAST 30 DAYS 27.7 0.0 0.0 0.0 0.0 27.7 27.7 3.0 0 0 0.0 4 LAST 60 DAYS 37.2 0.0 0.0 0.0 0.0 37.2 37.2 12.5 0.0 0.0 5 LAST 90 DAYS 37.2 0.0 0.0 0.0 0.0 37.2 37.2 12.5 0.0 0.0 5 OTHER AIRCRAFT FRI SEC INST EVAL OTHER TOTAL NIGHT INS SIN INS SORT RCISSW 343.4 0.0 0.0 0.0 0.0 343.4 343.4 51.9 0.0 0.0 47 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 23.5 0.0 6.0 0.8 0.0 23.5 23.5 23.5 0.0 0.0 6 SRC135W 0.0 14.0 14.0 0.0 0.0 0 0 6 LAST 30 DAYS LAST 60 DAYS 0LAST 90 DAVS 6LANCER TOTALS CREW POSITION FIRST FLIGHT PRI SEC INST EVAL OTHER TOTAL STUDENT COMBAT COMBAT SORT LAST FLIGHT TIME SUPPORT AIRBORNE COMUNICATION SYSTEM 23 SEP 2013 672 672.0 0 0 294.6 6.0 86 23 APR 2015 PAGE 1 G-l39 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.9.4. INDIVIDUAL DATA SUNIMARY PREPARED 01 MAY 2015 29:98 INDIVIDUAL DATA SUMMARY (PA) AS OF 91 MAY 2015 PCN INQUIRY SSAN: GRADE: SRA CMD: AIA WING: 0343RCNSO UNIT: 9343RCNSO BASE: OFFUTT AFB PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: SECURITY CLEARANCE DATE: 29 JAN 13 SVC CAT: USAF RESTRICTED AREA BADGE N0: LAST PHYS DATE: PROFESSIONAL OUAL INDEX (POI): PHYS CODE: PROFESSIONAL DUAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL PHYS AVAIL DATE: PHYSIOLOGICAL TNG DATE: STATUS PHYSIOLOGICAL DUE DATE: DATE ASSIGNED JUMP sums: DATE OF BIRTH: DUTY AFSC: 1A351 EFFECTIVE DATE OF mm.- 20 JAN 15 PAS CODE: SYSTEM MANAGEMENT SHORT TOUR INDICATOR: ?Am CODE: SGBP DATE RETURN FROM OVERSEAS: DEPLOYEO HARM (ODE: DATE OF 10 SEP 16 . DATE DEP LASI DUTY STA: 25 MAY 13 E?gik?w??f?i?? ARR "?15 93 13 RECORDS REVIEN Acc DATE: 67 APR 15 PERSOWEL RECORD STATUS: 19 RECORDS DUE DATE: 31 MAR 16 PROJECTED RECORDS REVIEW smus CODE: PROJECTED PAS CODE: PROJECTED DUTY LOCATION: PROJ DEPARTURE DATE: PROJ REPORTING DATE: PAC 8 EFFECTIVE DATE: LOCAL USE CODE: I CERTIFY THAT I HAVE REVIEWED HY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE AIA PAGE 1 PAGE 1 G-l40 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED DI MAY 2915 20:98 INDIVIDUAL DATA SUMMARY (PA) AS or 01 2015 PCN SA036-A70 INQUIRY NAME: WASEZI SSAN: GRADE: SRA CMD: AIA WING: UNIT: 0343RCNSO BASE: OFFUTT AFB AIRCRAFT ASSIGMENT DATA AERONAUTICAL BADGE OPLOC: AVIATION BADGE: (BASIC) AIRMAN CHD 0F 1C EFFECTIVE DATE: 14 APR 14 ACFT SVC (AT: ?55? PRIMARY ACFT: RC135V FLT DUTY CERT CODE: HKAEZ CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA IAST MPO DATE: 14 JUN 13 LAST MPO REASON: NONE PAY STOP DATE: 13 JUN 23 LAST PRODUCTIVE FLIGHT DATE: 23 APR 15 PREVIOUS PRODUCTIVE FLIGHT DATEAVIATION SERVICE DATA CURR PARA AVIATION SERVICE CODE: AA CURR PARA RATING DATE: EFFECTIVE DATE: O4 DEC 13 ORIG PARA RATING.- PRIOR ASC: Ax DRTG PARA RATING DATE: me 9133 ?33 W5 OPEICER SERVICE DATE: FORMAL COURSE DATE AVIATION SERVICE DATE: 1A JUN 13 INITITAL PHYSIOLOGICAL HYPOXIA TRAINING 14 DEC 12 TRANSITION STATUS CODE: AVIATION POSITION INDICATOR: A EFFECTIVE DATE: 28 JAN 15 FLYING ACTIVITY CATEGORY: A PRE-ACIA-OFDA: OFDA GATE 19/12: 23 OFDA GATE 15/15: 0 OFDA GATE 26/18: 0 OEDA TO DATE: 23 Your current OFDA is 23 month(s). You need 49 additional monthIs) OFDA to meet your 10 Year gale requirement to rccelVe continuous CEFIP through 15 years of aviation service and you must maintain a vaTid flIght physical. I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE AIA PAGE 2 PAGE 2 (3-141 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.9.5. INDIVIDUAL FLYING TIME SUNIIVIARY PREPARED 13 MAY 2015 29:06 INDIVIDUAL FLYING VINE SUMMARY (pA) AS OF 13 MAY 2015 PCN SA036-F70 REQUEST PFRIOD FROM: 39 APR 2014 TO: 36 APR 2615 @660 SEAN: GRADE: 504 PRI cnew P05: PRI AIRCRAFT: RC135V CMD: AIR WING: 0343RCN50 UNIT: ACFT OPLOC: TAIL 0011 SIM NUS DATE NUHB PR1 SEC INST EVAL OTH TOTAL SRT (MB SRT SRT NITE 1N5 INS NVG RC135V 05 MAY 14 64-4846 MKANZ 964.4041 11.7 0.0 0.0 0 0 0.0 11.7 1 1164-4041 NKANZ 664'4841 MKANZ 10.1 0.0 0.0 0.0 0.0 10.1 1 1064-4841 11.5 0.0 0.0 0.0 0.0 11.5 1 1164-4846 11.2 0.9 0.0 0.0 0.0 11.2 1 1164-4848 MKAN2 762-4126 MKANZ 964-4841 HKANZ 662-4040 MKANZ 762-4130 MKANZ 762-4131 MKANZ 764-4048 MKANZ 664.4046 96a~4348 MKAE2 664-4848 MKAEZ 764-4848 HKAEZ 64131 MKAF2 61.0 0.0 0.0 0.0 CMB 51M RC135V SUMHARY SEC INST EVAL 0TH TOTAL SRT CMB SAT SRT NITE INS INS AIRCRAFT: 14954.2 5 0.0 0 17.5 0.0 0.0 e. SIMULATORRPAac135w 11 MAY 14 62-4130 MKANZ 10.0 0.0 0.0 0.0 0 0 104130 MKANZ 11.4 0.0 0.0 0.0 0.0 11.4 1 1162-4130 MKANZ 1111.2 1 11.2 1 0.0 0 0.0 0.0 0.0 0.0 AIA PAGE 1 a U1 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:06 FLYING TIME SUMNARY (FA) AS OF 13 MAY 2015 REQUEST PERIOD FROM: 30 APR 2014 TO: 39 APR 2015 SSAN: GRADE: SRA PRI P05: PR1 AIRCRAFT: RC135V CMD: AIA WING: 0343RCNSO UNIT: 0343RCNSO ACFT OPLOC: TAII DUTY CMB SIM MDS DATE NUMB POSN PRI I 5 EVA TH SRT CH8 SRT SRT INS RES RC135W 21 MAY 14 62-4126 MKANZ 11.5 11. 11.5 .0 23 MAY 14 62-4130 MKANZ 10.1 . . 10. 10.1 28 MAY 14 62-4126 MKANZ 11-5 11 11.5 07 JUN 14 62-4126 MKANZ 07 OCT 14 62-4132 MKANZ 15 OCT 14 62-4132 MKANZ . 17 OCT 14 62-4132 MKANZ 21 OCT 14 62-4132 MKANZ 22 OCT 14 62-4132 MKAN2 23 OCT 14 62-4132 MKANZ 1 . 24 OCT 14 62-4132 MKANZ 25 OCT 14 62-4132 MKANZ 27 OCT 14 62-4132 MKANZ 28 OCT 14 62-4132 MKANZ 29 OCT 14 67413? MKANZ 03 NOV 14 62-4132 MKANZ 05 NOV 14 62~4132 MKANZ 17 NOV 14 62-4125 MKANZ 18 NOV 14 62-4125 MKANZ 20 NOV 14 62-4125 MKANZ 21 NOV 14 62-4125 MKANZ 26 NOV 14 62-4132 MKANZ 29 NOV 14 62-4132 MKANZ 30 NOV 14 62-4132 MKANZ 02 DEC 14 62-4132 MKAN2 7.8 JAN 15 67-4131 39 JAN 15 62-4131 MKANZ 03 FEB 15 62-4131 MKANZ 04 FEB 15 62-4131 MKANZ AIA PAGE PAGE 2 G-l43 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:06 INDIVIDUAL FLYING TIME SUMMARY (FA) AS OF 13 MAY 2015 PCN REQUEST PERIOD 30 APR 2014 30 APR 2015 55AM: GRADE: SRA PR1 caew P05: PRI AIRCRAFT: Rc135v AIA WING: UNIT: ACFT UPLOC: TAIL DUTY CMB SIM HDS DATE NUMB POSN PRI sac INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG RES Rc13sw 05 FEB 15 62-4131 MKANZ 462-4131 MKANZ 36?-4131 462-4131 MKAN2 33.0 0.0 0.0 0.0 SIM Rc135w suuMARv PR1 sec INST EVAL 0TH TOTAL SRT SRT SRT NITE INS INS ~vc AIRCRAFT: 251.5 0.0 0.0 0.0 0.0 251.5 36 73.6 7 0.0 0 39.6 0.0 0.0 0.0 SIMULATOR0.0 0.0 0.0 0.0 RPA62~6061 MKANZ 62-6901 MKANZ 262-6002 MKANZ 262-6001 MKANZ 62-6001 MKAE2 62-6002 MKANZ 0.0 0.0 0.0 0.0 L/s SIM snc13sw SUMMARY PRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT ~11: INS INS uvc AIRCRAFT0.0 0.0 0.0 0.0 SIMULATOR: 14.0 0.0 0.0 0.0 0 0 14.0 6 0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 AIA PAGE 3 PAGE 3 G-l44 RCJ 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:06 1NDIV10UAL FLYING TIME SUMMARY (FA) AS OF 13 MAY 2015 SA036-F70 REQUEST PERIOD FROM: 30 APR 2014 TO: 30 APR 2015 SSAN: GRADE: SRA PR1 ?sz P05: PRI AIRCRAFT: RE135V CMD: AIA wme: 0343RCNSO UNIT: 0343000050 ACFT OPLDC: CMB SIM GRAND TOTALS PR1 SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE TNS INS AIRCRAFT: 401.3 0.0 0.0 0.0 0.0 401.3 54 127.8 12 0.0 0 57.1 0.0 0.0 0 SIMULATOR: 14.0 0.0 0.0 0.0 0.0 14.0 5 0.0 0.0 0.0 0 RPAPAGE 4 PAGE a RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.9.6. INDIVIDUAL FLIGHT RECORD PREPARED 01 MAY 2815 20:03 INDIVIDUAL FLIGNT RECORD REPORT (PA) AS OF 01 MAY 2015 PLN 1~0019v SSAN: GRADE: 5114 991 CREW POS: PRI AIRCRAFT: acusv cm: AIA WING: 9343110150 mm: 934390159 4ch 0919c: TAI DUTY CMB SIM DATE MUS DATE NLMB POSN PRI SEC INST EVAL 0TH TOTAL SRT CHE SRT SRT NITE INS INS MIG RES UPDATED RC135V 05 MAY 14 64-4846 HKANZ 920140505 RC135V 09 MAY 14 94-4941 1419192 11.7 0.9 9.0 0.9 9.9 1129140599 RC135W 11MY14 62-4139 MKAN210.8 0.0 0.9 0.6 0.0 10.3 1 1020140512 RC13SW 15 MAY 14 52-4130 11.4 0.0 3.0 0.0 0.0 11.4 1 11.4 1 0.0 0.0 9.0 8.0 9.0 20140515 191441714 92-4130 14104112112 9.o 9.9 0.9 9.9 11.2 1 1129149519 9913514 21 MAY 14 92-4129 14101112119 0.9 9.9 9.9 9.0 11.5 1 1120149521 RC135W EMAY 14 62-4130 MKANZ 10.1 9.0 0.0 0.0 0.0 10.1 1 10.1 1 9.9 0.0 0.0 3.0 9.0 20149523 RC135V 29 MAY 14 94-4941 14194112 929149529 RC135W 291m 14 92-4129 1410102115 0.9 9.0 0.9 9.9 11.5 1 1120140529 RC135V 31MY14 64-4841 10.1 0.0 0.0 0.0 0.0 10.1 1 1020140531 RC135V 92 JUN 14 94-4941 MKANZ 11.5 0.9 9.9 0.9 9.9 11.5 1 1129149903 RC135V 05191114 94-4949 11191112112 9.9 9.9 0.9 9.9 11.2 1 1120149995 RC135W 07 JUN14 52-4125 720149507 RC13SV P4 JUL 14 54-4843 HKANZ 729140723 5111:1351? 39 JUL 14 92-9991 MKANZ 229149731 57103514 31 JUL 14 92-9991 14104112 229149904 SRCESW 05101514 62-5902 HKANZ 220140819 mm 07 499 14 92-4129 mom 929149919 9113517 12 AUG 14 94-4941 20140927 SRCIBSW 20 AUG 14 52-6061 MKANZ 220140827 9c135v 02 559 14 92-4949 MKAMZ 720149995 97 OCT 14 92-4132 14mm 920141919 RC135W 150CT14 62-4132 MKANZ 320141021 RC135W 170CT14 62-4132 90.9 0.0 8.0 0.9 29141927 1103517 21 OCT 14 924132 149492 920141927 RC135W 22 OCT 14 62-4132 MKANZ 620141028 AIA 911991 I. CERTIFY THAT I HAVE REVIEWED MY TFRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 1 G-l46 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 01 MAY 215 20:08 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 01 MAY 2015 PCN SA636-F-70 INQUIRY NAME: SSAN: mm GRADE: SRA PRI 005: PR1 AIRCRAFT: Rc135v c110; AIA wmc: 03430CN50 UNIT: 0343110150 4ch OPLDC: IAIL DUTY CMB SIM DATE 1105 we 0090 001 sec INST EVAL 0TH TOTAL 511T c110 507 US SRT NITE 1N5 1N5 NVG RES N/s UPDATED RC135N 23 OCT 14 62-4132 HKANZ 10.5 0.0 0.0 0.0 0.0 1020141020 24 um 14 62-4132 MKANZ 620141204 003511 25 OCT 14 624132 010012 620141030 RCIBSW 27 OCT 14 62-4132 MKANZ 620141030 Rc135w 28 OCT 14 62-4132 NKAN2 620141104 29 0:1 14 62-4132 MKAHZ 920141104 Rc135w 03 Nov 14 62.4132 NKAN2 620141105 mm?: 05 Nov 14 62-4132 NKAN2 620141112 RC135N 17 Nov 14 62-4125 920141117 RC135W 18 Nov 14 62-4125 NKAN2 120141119 Rc135w 20 Nov 14 62-4125 920141124 21 Nov 14 62-4125 MKANZ 920141124 RC135W 26 NOV 14 52-4132 MKANZ 29.6 9.0 9.9 9.0 70141262 Rcusw 29 Nov 14 62-4132 HKANZ 120141201 Rc135w 30 Nov 14 62.4132 MKANZ 920141201 003514 02 DEC 14 62-4132 MKAN2 720141203 Rc135v 17 DEC 14 62-4130 MKANZ 120141210 RC135V 22 DEC 14 62-4131 HKANZ 720150106 RC135V 23 DEC 14 64-4040 NKAN2 620150106 Rc135w 28 JAN 15 62-4131 MKANZ 420150129 30 JAN 15 62-4131 MKANZ 420150203 11013511 03 FEB 15 62-4131 NKAN2 420150204 Rc13sw 04 FEB 15 62-4131 MKAN2 320150213 Rc135w 05 FEB 15 62-4131 MKANZ 420150213 RC135W 07 15 62-4131 MKANZ 320150210 11 FEB 15 624131 14104112 420150213 AIA PAGEZ 1 CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT Is COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 2 G-147 RC-I35V, 64-4848, Class A, 30 April 15. AFSAS #739726 PREPARED 01 MAY 2015 20:08 INDIVIDUAL FLIGHT RECORD REPORT (PM AS OF 01 MAY 2015 PCN SA036-F70 INQUIRY SSAN: GRADE: SRA PRI CREW Pos: PR1 AIRCRAFT: Rc135v CND: AIA WING: 034300150 UNIT: 034an090 ACFT OPLOC: IAJL DUIY CNS SIM DATE MOS DATE HUME PDSN SEC INST EVAL 0TH TOTAL SRT CH8 SRT SRT NIYE INS INS NVG RES UPDATED 13 FEB 15 62-4131 MKAN2 320150219 RCIBSV 10 MAR 15 54.4043 MKAEZ 920150310 Rc135v 02 APR 15 04?4048 MKAE2 620150403 RC135V 06 APR 15 64-4048 20150407 514121350 13 APR 15 62-6002 MKAN2 320150420 Rc135v 15 APR 15 54-4043 MKAEZ 020150417 RC13SV 23 APR 15 02-4131 MKAE2 020150423 CMB SIM 1405 SUMMARY PRI SEC INST EVAL DTH TDTAL 501 cm: SRT SRT NITE INS INS ch AIRCRAFT: 401.3 0.0 0.0 0.0 0.0 401.3 54 127-0 12 0.0 0 57.1 0.0 0.0 0.0 SIMULATOR: 11.0 0.0 0.0 0.0 0.0 11.0 5 0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 AIA PAGE 3 1 CERTIFY THAT I HAVE MY IPRR AND IT Is COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 3 G-l48 RC-I 35 V, 64-4848. Class A. 30 April 15, AFSAS #739726 Gl.9.7. INDIVIDUAL TRAINING SUMNIARY PREPARED 13 MAY 2015 19:50 INDIVIDUAL TRAINING SWARY AS OF 13 MAY 2015 PCN SA036-T10 CURRENT TRAINING PERIOD NAMEJMASEZI GRADE: SRA ssm; caew POSITION: MKAEZ UNIT: PHYSICAL DUE one: 15 NOV 15 PHYSIOLOGICAL DUE DATE: 31 DEL RECORDS ?mew DUE one: 31 MAR 16 ACC pg" TASK DATE LAST om: ova am to NALIFICATION PROFILE TASK 10 RED ACCORP REM ACCORD 1N WASP. DATE DIE DUE VHS (on; CH ASE 2 RJ SONTIE ASE-Z OUAI. A867 some $011115 ID ASE 2 5X14 (E) SIM RIVEI JOINT RAP (E) SIM 135 CURRENCY H612 CPR 1E) TOT SIM RAP SRIYS 5069 1E) TOT RAP SRGO SR59C CMR IE) 31CMR IE) IOT 5X99 ASE A.) (NR (ED BASIE SORTIE 9:TRNG RJ BL 10.3 CERT 5578 IRNG RJ EL 9 CURRENCY X809 TRNG RJ BL 9 CERT 363090 CURRENCY K819 TRNG NJ 11 CURRENCY X011 TRNG RJ 31 II CERT X8110 9 24 JUL 14 GT (OMSEC IRAINING (OMSEC M99 COHSEC TRAINING (OMSEC Read GAAI GINO ASE RJ TRAINING 6M3 GINO ASE RJ IRAININC (RM GAGE GINO ASE RJ TRAINING "AIA PAGE 1 PAGE 1 G?l49 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:59 INDIVIDUAL TRAINING SUMMARY As or 13 MAY 2015 PCN CURRENT TRAINING PERIOD NAME: SRA SSAN: CREW POSITION: MKAEZ 0343RCN50 PHYSICAL DUE UAIE: L5 NOV 15 PHYSIOLOGICAL DUE DATE: 31 DEC 17 RECORDS REVIEW DUE DATE: 31 MAR 16 MI p5? TASK 1 DATE LAST DATE IN REST CD QUALIFICATION PROFILE TASK NAME TD RED KEN IN PHASE DATE DUE DUE PHS EDDE NVD GT GRND Abl- RJ TRAINING ACAD GMTURND ASE TRAINING SEPT 6593 DRND ASE RJ TRAINING STAN EVA: TEST 6505 V55 GRND ASE RJ TRAINING OPLAN STUDY 6522 9 10 FEB IA GT GRND ASE n) TNAINING SERVICE 6575 GRND ASE RJ TRAINING FLY SAFETY TRNC- 6576 GRND ASE RJ TRAINING TEST SEC 6572 GRND ASF RJ TRAINING ISO PREP IEDZ GRND ASE RJ TRAINING APE FAN TANG 29 JUN 13 GT GRND ASE NJ TRAINING EGRESS (NONE): LL83 GRND ASE RJ TRAINING ACDT LL04 GRND ASE RJ TRAINING EGRESS NIACDE LL95 a 0 21 JUN 13 GT GRNO ASE RJ TRAINING AFE TRNG LL86 GRND ASE RJ TRAINING LOCAL AREA SURV 5501 0 19 JUN 13 0 GT GRND ASE RJ TRAINING CAST SURV TANG 5562 GRND ASE TRAINING CAC TANG 5501 GRND ASE RJ TRAINING NET 5505 (5an ASE RJ TRAINING AFRICOH 5587A 61 GRND ASE RJ TRAINING CENTCOH (CSI) 5507c GRND ASE RJ TRAINING EUCON (C51) SSDTE GI GRND ASE RJ TRAINING PACOH SSB7P a GI GRND ASE DJ TRAINING SOUTNCOH (CST) 55915 9 GT GRND ASE RJ TRAINING SPH SERE TRNG GRND ASE RJ TRAINING S-VRB-A 5524 6 24 MAY 13 AIA PAGE 2 PAGE 2 G-150 PREPARED 13 MAY 2015 19:50 NAME: PHYSICAL DUE DATE: CO CT 15 NOV 15 OUALIFICATION PROFILE GRND ASE RJ MINING NAHE ALERT RESPONSE RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL TRAINING SUWIARY AS OF 13 MAY 2015 PCN CURRENT TRAINING PERIOD qmw.w9_ GRADE: SRA SSAN: PHYSIOLOGICAL DUE DATE: 31 DEC 17 CREW POSITION: MKAEZ UNIT: RECORDS REVIEW DUE DATE: 31 MAR 16 ACE TASK DATE LAST OVR IN REST ID RED ACCOHP REM ACCOMP IN PHASE DATE DIIF DUE PHS CODE AIA PAGE 3 PAGE 3 6-151 G110. TSGT [Mishap Airborne Systems Engineer 3] 64?4848, Class A, 30 April 15, AFSAS #739726 (MASE3) G1.10.1. CERTIFICATE OF AIRCREW QUALIFICATIONS bMav?J?l': yleDnQN IrmaMWI INWIIAI IILanvnumlu- $13 r15 G-152 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.10.2. FLYING HISTORY REPORT PREPARED 81 MAY 2815 19:52 FLYING HISTORY REPORT AS OF 01 MAY 2615 PCN 5A036-F40 INQUIRY SSAN: Wu?. GRADE: TSG API: A TAC: A OFDA: 153 ASC: 0A Asc DATE: 10 FEB 15 CHI): AIA WIN620343RCNS PRI P05: PR1 ACFT: Rc135v UNIT: BASE: OFFUTT AFB AIRCRAFT TOTALS CAREER TOTALS AIRCRAFT mos CREW POSITION RADIO 0? FLT DTY (FRI CDDE MRANA UKIN EKA EKAEI PRIMARY TIME 2790.9 DATE FIRST FLOWN SECONDARY TIME 0.0 DATE LAST FLOWN INSTRUCTOR TIME 429.6 TOTAL TIME 163.1 04.0 24.0 2450.5 722. 7 EVALUATOR TIME 149.3 PRIMARY TIME 163.1 64.0 24.0 2017.9 545.9 OTHER TIME 30.: SECONDARY TIME 0.0 0.0 0.0 0.0 0.0 TOTAL TIME 3400.3 INSTRUCTOR TIME 0.0 0.0 0.0 301.0 127.8 STUDENT TIME 0.0 EVALUATOR TIME 0.0 0.0 0.0 127.5 21.8 OTHER US MIL TIME 0.0 OTHER TIME 0.0 0.0 0.0 3.3 27.2 FOREIGN MIL TIME 0.0 NIGHT 5.0 0.0 0.0 98.5 0.0 CIVILIAN TIME 0.0 PRIMARY INST 0.0 0.0 0.0 0.0 0.0 COMBAT TIME 356.2 PRIMARY 51M INST 0.0 0.0 0.0 0.0 0.0 COMBAT sun TIME 82.2 ch TIME 0.0 0.0 0 0 0.0 0.0 TOTAL SORTIEs 1057 COMBAT TIME 0.0 0.0 0.0 211.6 144.6 COMBAT SORTIES 102 (NET SUPPORT HME 0.0 0.0 0.0 53.3 25.9 COMBAT sup SORTIES 19 COMBAT 0 0 0 92 10 NVG TIME 0.0 CMBT SUPPORT SORTTES 0 0 0 16 3 DATE FIRST FLOMN 01 Nov 01 TOTAL SDRTIEs 23 9 0 947 78 DATE LAST FLOWN 23 APR 15 GRAND TOIAL 3400.3 PAGE 1 G-153 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.10.3. 30/60/90 FLYING HISTORY REPORT PREPARED 20 MAY 2015 09 17 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 20 MAY 2015 SA036-F29 GRADE: TSGT API: A FAC: A Asc: 9A DAFSC: 1A371 AGE: CMO: AIA WING: 03430cuso ORGANIZATION: CREN POSITION: MKAN4 Asc DATE: 18 FEB 2015 CURR RATING: AIRCRAFT TYPE: Rc135v SERIAL NO: 64-4848 HISHAP APR 2015 HISHAP AIRCRAFT PR1 sec INST EVAL OTHER NIGHI 1N5 510 INS SORT RC135V 103 1 0.0 0.0 0.0 0.0 103.1 103.1 5.0 0 0 0.0 23 LAST 30 DAYS 20.3 0.0 0.9 9.0 0 0 20.3 20.3 3.0 9.0 0.0 3 LAST 50 DAYS 49.9 0.0 9.0 9.0 9.0 48.0 48.0 3.9 9.8 6.0 7 LAST 99 DAYS 55.5 0 0.9 0.0 9.0 55.5 55.5 3.0 9.9 0.0 9 OTHER AIRCRAFT PRI SEC INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT RCISSW 64.0 0.0 0.0 0.0 0.0 04.0 50.0 0.0 0.0 9.0 9 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 0SRCIBSW 24.0 9.0 0.0 0.0 0.0 24.0 74.0 0.0 0.0 0.0 6 LAST 30 DAYS 0LAST 50 DAYS 0LAST 90 DAYS 0C037A 2017.9 0.0 301.8 127.5 3.3 2450.5 2319.7 93.5 9.0 0.0 947 LAST 36 DAYS 0LAST 60 DAYS 0LAST 99 DAYS 0RC1355 545.9 0.0 127-8 21.8 27.2 722.7 673.7 0.0 9.0 9.0 78 LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 0PAGE 1 (3-lfi4 PREPARED 26 HAY 2615 09:17 CMD: ALA wxwo: 0343RCNSO CURR RATING: SEC CREW POSITION FIRST FLIGHT PRI SEC LAST FLIGHT nM? AIRBORNE COMMUNICATION SYSTEM 01 NOV 2001 2790.9 0.0 23 APR 2015 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 AIRCRAFT MISNAP INVESTIGATION (PA) GRADE: TSGT INST INST 429.6 trt_ti SSAN: O343RCN50 AIRCRAFT TYPE: RC135V API: A OTHER AIRCRAFT EVAL CARFFR TOTALS EVAL OTHER SUPPORT 149.3 30.5 PAGE 2 OTHER CREW MKAN4 SERIAL NO: 54-4848 AS OF 29 MAY 2915 PCN DAFSC: 1A371 AGE: ASC DATE: 18 FEB 2015 MISHAP APR 2015 EAC: A ASC: BA TOTAL NIGHT INS SIM INS SORT er. TOTAL STUDENT COMBAT COMBAT SORT 3690.3 3229.5 0.0 356.2 82.2 1057 G-155 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 01 MAY 2015 19:52 INDIVIDUAL DATA SUMMARY (PA) AS OF MAY 2615 PCN SA036-A7O INQUIRY SSAN: GRADE: TSG CMD: AIA WING: 9343RCNSO UNIT: 9343RCNSO BASE: OFFUTT AFB PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: SE SECURITY CLEARANCE DATE: 10 SEP 14 SVC CAT: USAF RESTRICTED AREA BADGE No: LAST PHYS DATE: PROFESSIONAL DUAL INDEX (POI): PHYS CODE: PROFESSIONAL DUAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: . . PHYSIOLOGICAL TNG DATE: WW5 PHYSIOLOGICAL DUE DATE: DATE ASSIGNED JUMP STATUS: DATE OF BIRTH: DUTY AFSC: LA371 EFFECTIVE DATE or DUTY: 13 AUG 14 PAS c005: ooeurgcu SYSTEM MANAGEMENT SHORT TOUR INDICATOR: . DATE RETURN FROM OVERSEAS: CODE: SGBP DATE DE 12 JUN 17 DATE: DATE DEP LAST DUTY STA: 91 JAN 14 SPECIAL CAT ID: PERSONNEL RECORD 19 RECORDS REVIEW DUE DATE: 31 DEC 15 RECORDS REVIEH STATUS CODE- PROJECTED PAS CODE: PROJECTED DUTY LOCATION: PROJ DEPARTURE DATE: PROJ REPORTING DATE: FAC 8 EFFECTIVE DATE: LOCAL USE CODE: I CERTIFY TNAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE SIGNATURE DATE AIA PAGE 1 (3-1565 PAGE 1 PREPARED 91 MAY 2615 19:52 NAME BASE: OFFUTT AFB AIRCRAFT OPLOC: CMO OF AIRCRAFT: ACFT SVC CAT: PRIMARY ACFT: FLT DUTY CERT CODE: CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA LAST MPO DATE: LAST MPO REASON: PAY STOP DATE: PROOUCTIVE FLIGHT PREVIOUS PRODUCTIVE FLIGHT DATE: AVIATION SERVICE DATA AVIATION SERVICE CODE: EFFECTIVE DATE: PRIOR EFFECTIVE DATE: AERO ORDER TERM DATE: OFFICER SERVICE DATE: AVIATION SERVICE DATE: TRANSITION STATUS CODE: AVIATION POSITION INDICATOR: EFFECTIVE DATE: FLYING ACTIVITV CATEGORY: PRE-ACIA-0FDA: OFDA GATE 10/12: OFOA GATE 15/15: OFDA GATE 20/18: OFDA TO DATE: SSAN: AIRCRAFT ASSIGNMENT DATA ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 SGBP 1C USAF RC135V MKAN4 01 JAN 95 NONE 163 You have met OFDA requirements for current gate. I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. INDIVIDUAL DATA SUMWARY (PA) INQUIRY AS 0F 01 MAY 2015 PCN SAO36-A7O GRADE: TSG (MD: AIA WING: O343RCNSO O343RCNSO AERONAUTICAL BADGE AVIATION BADGE: SENIOR AIRMAN AIRCREWMEMBER EFFECTIVE DATE: 13 AUG 08 AVIATION BADGE: (BASIC) AIRMAN AIRCRENMENBER EFFECTIVE DATE: 31 MAY 02 nus NIL RTG OT: CURR PARA RATING: CURR PARA RATING DATE: DRIG PARA RATING: DRIG PARA RATING DATE: STATUS FORMAL COURSE DATE REFRESHER PHYSIOLOGICAL HVPOXIA TRAINING 17 MAR 11 INITIAL PHYSIOLOGICAL HYPOXIA TRAINING 13 JUN 01 SIGNATURE DATE AIA PAGE 2 PAGE 2 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.10.5. INDIVIDUAL FLYING TINIE SUMMARY 13 MAY 2815 10:64 INDIVIDUAL Fume TIME gummy (pA) AS OF 13 MAY 2015 PEN REQUEST PERIOD FROM: 39 APR 2014 30 APR 2015 NAME SSAN: GRADE: r507 PR1 CREW POS: PRI AIRCRAFT. RC135V CMDZ AIA WING: 0343RCN50 UNIT: 0343RCNSO ACFT OPLOC: SGBP TAIL 007v cna 510 nos DATE nuns POSN PR1 sec 1057 EVAL 010 TOTAL 501 cue SRT SRT NITE INS INS ~v0 RES RC135V 06 MAY 14 62-4139 UKIN4 662-9792 403-9792 uxru4 703-9792 MKAN4 064-4831 MKAN4 663-9792' MKAN4 604-4048 MKAN4 10.0 0.0 0.0 0.0 0.0 1064?4848 MKAN4 004-4040 MKAN4 10.7 0.0 0.0 0.0 0.0 1064-4848 MKAN4 74843 MKAN4 04040 MKAN4 064~4848 HKAN4 752-4131 MKAN4 854~4848 MKAN4 664-4848 002.4131 MKAN4 03.0 0.0 0.0 0.0 SIM RC135V SUMMARY PRI 50c 1057 EVAL 0TH TOTAL 5R7 (MB SRT 507 NITE INS INS uvc AIRCRAFT: 121.1 9.0 9.0 0.0 0.0 121.1 17 0.0 0 0.0 0 5.0 8.0 0.0 0.0 SIMULATOR0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 Rc135w 15 MAY 14 02-4135 uxIN4 00.0 0.0 0.0 0.0 AIA PAGE 1 PAGE 1 G-158 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 20:04 INDIVIDUAL FLYING TIME SUMMARY (pg) AS OF 13 MAV 2915 PCN SA036-F79 REQUEST PERIOD FROM: 30 APR 2014 T0: 36 APR 2015 SSAN: GRADE: TSGT PRI cnew 005: PRI AIRCRAFT: RC135V (MD: AIA MING: 0343Rcuso UNIT: 03430c~so ACFT OPLOC: SGBP TAIL DUTY (MB SIM NOS DATE NUMB POSN FRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS ch RES CMB SIM RC13SW SUMMARY PRI sec INST EVAL 0TH TOTAL SRT cus SRT NITE TNS INS st AIRCRAFT0.0 0.0 0.0 0.0 SIMULATOR0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 0.0 SRc135w 17 NOV 14 62-6004 UKINS 662-6004 UKINS 662*6984 362-6004 UKINS 362-6004 UKINS 362-6001 UKIN 30.0 0.0 0.0 0.0 (00 SIM SRC13SW SLMMARY PR1 SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG AIRCRAFT0.0 0.0 0.0 0.0 SIMULATOR: 24.0 0.0 0.0 0.0 0.0 24.0 6 0.0 0.0 0.0 0.0 REA0.0 0.0 0.0 0.0 CMB SIM GRAND TOTALS PRI sec INST EVAL 0TH TOTAL 501 CNB SRT SR1 NITL 1N5 INS NVG AIRCRAFT: 127.2 0.0 0.0 0.0 0.0 127.2 18 0.0 0 0.0 0 5.0 0.8 6.0 0.0 SIMULATOR: 24.0 0.0 0.0 0.0 0.0 24.0 6 0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 AIA PAGE 2 PAGE 2 G-159 RC-135V, 64-4848, Class A, 30 April 15. AFSAS #739726 G1.10.6. INDIVIDUAL FLIGHT RECORD PREPARED 01 MAY 2015 19:52 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 01 MAY 2915 PCN SAO36-F79 INQUIRY NANE: "MluSEal SSAN: GRADE: TSGT FRI CREH POS: PRI AIRCRAFT: RC13SV CMD: AIA WING: 03430CN50 UNIT: 0343RCN50 ACFT OPLOC: SGBP TAIL DUTY CNS SIM DATE MOS DATE NUHB FOSN PR1 SEC INST EVAL 0TH TOTAL SR1 CMB SRT SET NITE INS INS NVG RES UPDATED RC135V 06 MAY 14 62~4139 UKIN4 60.0 0.0 0.0 0.0 20140507 RC135N 15 MAY 14 62-4135 UKIN4 60.0 0.0 0.0 0.0 20140516 RC135V 20 MAY 14 62-9792 UKIN4 420148521 RCIBSV 29 MAY 14 63-9792 UKIN4 70.0 6.0 0.0 0.0 20140530 RC135V 14 JUL 14 63-9792 HKAN4 60.0 0.0 0.0 0.9 20140723 RC135V 15 AUG 14 54-4841 MKAN4 620140828 RCIBSV 04 SEP 14 63-9792? MKAN4 620140905 RC135V 09 SEP 14 64-4048 MKAN4 10.6 0.0 0.0 0.0 0.0 1020140912 RC135V 15 SEP 14 64-4848 MKAN4 620140919 RC135V 18 SEP 14 64-4848 MKAN4 10.7 0.0 0.0 0.0 0.0 10.7 1 0.0 0 0.0 0 0.0 0.0 0.0 0.0 20140924 QRCIBSW 17 NOV 14 62-6004 UKINS 620150112 SRC135W 19 NOV 14 62-6004 UKINS 620150109 SRCISSW 21 NOV 14 62-6004 UKINS 320150112 SRCIBSW 05 DEC 14 62 6004 UKINS 320150112 08 DEC 14 52-6004 UKINS 329150112 SRC135W 12 DEC 14 62-6001 UKIN 320150109 RC135V 18 FEB 15 64-4848 MKAN4 720150220 RC13SV 16 MAR 15 64-4848 MKAN4 620150323 RC135V 19 MAR 15 64-4848 MKAN4 60.0 0.0 0.0 0.0 20150323 RC135V 24 MAR 15 64-4848 MKAN4 720150327 RC135V 77 MAR 15 62-4131 820150331 RC135V 02 APR 15 64-4848 NKAN4 620150403 RCIBSV 15 APR 15 64?4848 MKAN4 620150417 RC13SV 23 APR 15 62-4131 PKAN4 620150428 AIA PAGE 1 I CERTIFY THAT I HAVE RLVIEWED MY 1FRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 1 G-l60 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 01 MAY 2015 19:52 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 01 MAY 2015 PCN SA036-F70 INQUIRY SSAN. GRADE: TSGT PRI CREW PRI AIRCRAFT: RC135V CMD: AIA WING: 0343RCNSO UNIT: OPLOC: SGBP (MD US SIM M05 SUVMARY PRI SEC INST EVAL 0TH TOTAL SRT SRT SRT NITE INS INS AIRCRAFT: 127.2 0.0 0.0 0.0 0.0 127SIMULATOR: 24.0 0.0 0.0 0.0 0.0 240.0 0.0 0.0 AIA PAGE 2 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. SIGNAVURE DATE PAGE 2 G-l6l . . RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.10.7. INDIVIDUAL TRAINING SUMNIARY PREPARED 13 MAY 2015 19:52 NAHE: PHYSICAL DUE DATEQUALIFICAIION PROFILE ASE 4 RJ SORTIE ASE 4 RJ SORIIE A56 4 RJ seamTRNG RJ ASE Bt TRNG RJ ASE Bl TRNG RJ ASE BL TRNG RJ ASE BL rune RJ ASE BL TRNG GRND ASE an TRAINTNG GRND ASE n1 TRAINING GRND ASE RJ TRAINING GROD ASE RJ GRHD ASE RJ TRAINING TASK NAME ASE-4 OUAL EVAL 51SIM RIVCT JOINT RAP SIM 135 TOT SIM TOT SIM RAP TOT RAP R) RAP RJ RAP CO a: RAP TOT sum/s SORTIF RJ BL 10,3 CERT RJ 8L 9 CURRENCY RJ EL 9 CERT RJ BL 10 CURRENCY RJ BL 11 CURRENCY m. 11 CERT ANTI-HUACK cm M9 OUAL ACAD SEPT INDIVIDUAL TRAINING SUMMARY CURRENT TRAINING PERIOD GRADE: TSGT wt:-:y PHYSIOLOGICAL DUE DATE: 31 MAR 16 TASK 10 A884 M156 5X16 H608 HIST 5009 SROB SXGG 5X93 6578 X399 K8890 X519 K8110 SAGE GAGE GA43 GA46 6503 REO ACCOHP PAGE 1 REM 89 89 56 56 G-162 CREW POSITION: MKAN4 DATE LAST ACCOMP MAY 2015 DATE 1N PHASE 39 APR 15 PCN SAO36 - T10 UNIT: 0343RCNSO RECORDS REVIEW DUE DATE: 31 DEC 15 DATE DUE REST DUE PHS CODE WVU mHHPAGE 1 PREPARED 13 MAY 2015 19:52 PHYSICAL DUE DATE: 82 JUN 16 CD 322333333322322 .4 GT GT GT GT GT QUALIFICATION PROFILE GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING BAND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GENO ASE RJ TRAINING GRND ASE RJ TRAINING GRNO ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRND ASE RJ TRAINING GRNO ASE RJ TRAINING GRND ASE R1 TRAINING GRND ASE RJ TRAINING TASK NAME STAN EVAL TEST OPLAN STUDY AIL SERVICE FLY SAFETY TANG 5/1 1557 sec 150 PREP AFE TANG EGRESS (NONEJ) ACDT EGRESS WIACDE AFE TRNG LOCAL AREA SURV CMBT SURV TRNG CAC TANG HST AFRICOM (C513 CENTCOM (CSI) EUCOM PACDM (C51) SOUTNLUH sen: rano S.va3-A ALERT RESPONSE RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL TRAINING SUMMARY CURRENT TRAINING PERIOD GRADE: TSGT SSAN: PHYSIOLOGICAL DUE DATE: 31 MAR 16 TASK ID 6505 6522 6525 6526 6572 [?02 LL01 LL03 LL04 LL65 LL66 S561 5582 5583 5595 SSBTA 5587C SSETE $587? 55375 5510 5524 era RED PAGE 2 G?l63 i REM CREW POSITION: MKAN4 AS OF 13 MAY 2015 PCN 5A836-T10 UNIT: RECORDS REVIEW DUE DATE: 31 DEC 15 DATE LAST ACCOMP DATE IN PHASE 2151 DATE DUE DUE PHS AIA PAGE 2 CODE WVD 64?4848, Class A, 30 April 15, AFSAS #739726 ?1.11. 1LT (MR2) G1.11.1. CERTIFICATE OF AIRCREW QUALIFICATIONS 0 Mn IUD sundown: Ml RS Lena: MILO unmmr k1, RS G-l64 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.11.2. FLYING HISTORY REPORT PREPARED 01 MAY 2015 10:50 FLYING HISTORY REPORT (PA) AS OF 01 MAY 2015 PCN SA030-F40 INQUIRY [Mi-Shep RaVe" 21 55AM: mm GRADE: API: 2 MC: 1 OFDA: 20 ASE: 1A 7151: DATF: 17 SEP 14 CHI): Acc PR1 (RN 005: PR1 ACFI: RC13sv UNIT: 0343RCNSO BASE: OFFUTT AFB AIRCRAFT TOTALS CAREER TOTALS AIRCRAFT MOS TGGIMS) (REM POSITION CSO FIT DTY CFRT CODE MEANX SN SN PRIMARY TIME 433.7 DATE FIRST FLOMN DATE NO DATE SECONDARY TIME 0.0 DATE LAST now DATE Na DATE INSTRUCTOR TIME 0.0 TOTAL TIME 140.1 293.0 79.0 0.0 0.0 EVALUATOR TIME 0.0 PRIMARY TIME 140.1 293.6 77.5 0.0 0.0 OTHER TIME 0.0 SECONDARY TIME 0.0 0.0 0.0 0.0 0.0 TOTAL TIMC 433.7 INSTRUCTOR TIME 0.0 0.0 0.0 0.0 0.0 STUDENT TIME 97.2 EVALUATOR TIME 0.0 0.0 0.0 0.0 0.0 OTHER US MIL TIME 0.0 OTHER TIME 0.0 0.0 1.5 0.0 0.0 FOREIGN MIL TIME 0.0 NIGHT 3.7 23.0 0.0 0.0 0.0 CIVTIIAN TIME 0.0 PRIMARY INST 0.0 0.0 0.0 0.0 0.0 COMBAT TIME 363.3 PRIMARY SIM INST 0.0 0.0 0.0 0.0 0.0 COMBAT SUPT TIME 0.0 NVG TIME 0.0 0.0 0.0 0.0 0.0 TOTAL SORTTES 43 COMBAT TIME 79.4 203.9 0.0 0.0 0.0 COMBAT SORTIES 33 CMBT SUPPORT TIME 0.0 0.0 0.0 0.0 0.0 COMBAT SUP SORTTES 0 COMBAT SOATIES 7 20 0 0 we TIME 0 0 CMBT SUPPORT SORTIES 0 0 0 0 0 DATE FIRST FLOMN 29 JUL 14 TOTAL SORTIES 16 27 25 0 0 DATE LAST PLONN 22 APR 15 GRAND TOTAL 530.9 PAGE 1 PAGE 1 G-l65 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 GLI 1.3. 30/60/90 FLYING HISTORY REPORT PREPARED 20 MAY 2015 09:25 AIRCRAFT MISHAF INVESTIGATION (PA) AS OF 20 MAY 2015 PCN SA036-F20 [MiShap Raven 2] TLT SSAN: API: 2 FAC- 1 ASC: 1A DArsc- 012R3H AGE: CHD: Acc WING: ORGANIZATION: CREW MEANX ASC DATE: 12 SEP 2014 CURR RATING: COMBAT SYSTEMS OFFICER AIRCRAFT RC135V SERIAL NO: 64-4848 HISMAP APR 2015 '04 MISHAP AIRCRAFT PR1 SEC INST EVAL OTHER TDTAL NIGHT INS SIM 1N5 SDNT ?(135v 140.1 0.0 0.0 0.0 0.0 140.1 140.1 3.7 0.0 0.0 ID LAST 30 DAYS LAST 60 DAYS 0LAST 90 DAYS 0OTHER AIRCRAFT PRI sec INST EVAL OTHER TDTAL NIGHT INS SIM INS SORT ACISSY 293.6 0.0 0.0 0.0 0.0 293.0 293.0 23.0 0.0 0.0 27 LAST 30 DAYS 9LAST 60 DAYS 42.6 0.0 0.0 0.0 0.0 42.5 42.6 0.1 0.0 0.0 4 LAST 90 DAYS 174.5 0.0 0.0 0.0 0.0 174.5 174.5 9.0 0.0 0.0 10 SRCIBSW 04 0.0 0.0 0 0 1.5 35.0 04.5 0.0 0.0 0 0 27 LAST 30 DAYS 8LAST 60 DAYS LAST 90 DAYS T001A 0LAST 30 DAYS 0LAST 00 DAYS 0LAST 90 DAYS 0T006A 0LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS DAGF 1 (3-1t56 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 29 MAY 2815 09:25 AIRCRAFT MISHAP INVESTIGATION (PA) AS 0F 26 MAY 2915 PCN NAME: [Mishap Raven 2] GRADE: 1LT SSAN: API: 2 FAC: 1 1A DAFSC: 012R3H AGE: can; ALL. mm; uoaamlNSO ORGANIZATION: 0343RCN50 CREW POSITION: NEMX ASC DATE: 12 SEP 2914 (URR RATING: COMBAT SYSTEMS OFFICER AIRCRAFT TYPE: Rc135v SERIAL no: 64-4843 MISHAP DATE: 39 APR 2915 OTHER AIRCRAFT PRI SEC INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT CAREER TOTALS CREW POSITION FIRST FLIGHT PRI SEC INST FVAL OTHER TOTAL STUDENT COMBAT COMBAT SORT LAST FLIGHT TIME SUPPORT COHBAT SYSTEMS OFFICER 29 JUL 2014 433.7 0 0 0.0 0.0 0.0 433.7 433.7 97.2 363.3 0.0 43 22 APR 2015 PAGE 2 G-l67 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.11.4. INDIVIDUAL DATA SUNIMARY PREPARED 31 MAY 2015 18:49 INDIVIDUAL DATA SUMMARY (PA) INQUIRY AS OF OI MAY 2015 PCN SAOBS-A7O NAME [Mishap Raven 2] BASE: OFFUTT AFB SSAN: GRADE: 1LT CMD: ACC WING: D343RCNSO UNIT: 0343RCN50 PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: SECURITY CLEARANCE DATE: 89 APR 12 M88 CAT: USAF RESTRICTED AREA BADGE N0: LAST an5 DATE: PROFESSIONAL ODAL INDEX (POI): PHYS CODE: PROFESSIONAL ODAL INDEX DATE: PHYS DUE DATE: PHYS AVAIL CODE: PHYS AVAIL DATE: PHYSIOLOGICAL TNG DATE: STATUS PHYSIOLOGICAL DUE DATE: DATE ASSIGNED JUMP DATE OF BIRTH: DUTY AFSC: 612R3H EFFECTIVE DATE OF OI APR 15 PAS CODE: SYSTEM MANAGEMENT SHORT TOUR INDICATOR: HARM CODE: 568p DATE RETURN FROM HARM CODE: DATE OF RANK: 17 14 DEPLOYED DATE OF DATE: DATE DEF LAST DUTY STA: 20 DEC 13 SPECIAL (AT ID: DATE ARR THIS 23 DEC ?3 RECORDS REVIEW ACC DATE. 10 APR 15 PERSONNEL RECORD 1? RECORDS DUE DATE: 31 JAN 15 PROJECTED W55: RECORDS REVIEW STATUS CODE: PROJECTED PAS CODE: PROJECTED DUTY LOCATION: PROJ DEPARTURE DATE: PROJ REPORTING DATE: FAC EFFECTIVE DATE: LOCAL USE CODE: I CERTIFY THAT I HAVE REVIEWED HY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE ACC G-l68 PAGE 1 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED OI MAY 2015 18:49 INDIVIDUAL DATA SUMMARY (PA) INQUIRY AS OF 01 MAY 2015 PCN SAO36-A79 NAME: [Mishap Raven 2] SSAN: GRADE: 1LT CMD: ACC WING: 6343RCN50 UNIT: 9343RCNSO BASE: OFFUTT AFB AIRCRAFT ASSIGNMENT DATA AIRCRAFT OPLDC: 553" END OF AIRCRAFT: 1C ACFT SVC CAT: USAF PRIMARY ACFT: RC135V FLT DUTY CERT CODE: HEANX CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA LAST MPO DATE: 27 NOV 12 LAST MPO REASON: A w/mu: NWE PAY STOP DATE: 26 NOV 24 LAST PRODUCTIVE FLIGHT DATE: 22 APR 15 PREVIOUS PRODUCTIVE FLIGHT DATE: 11 MAR 15 AVIATION SERVICE DATA AVIATION SERVICE CODE: 1A EFFECTIVE DATE: 12 SEP 14 PRIOR Asc: 1x EFFECTIVE DATE: 22 NOV 13 AERO ORDER TERA DATE: 26 NOV 24 OFFICER SERVICE DATE: 17 JUL 12 AVIATION SERVICE DATE: 27 NOV 12 TRANSITION STATUS CODE: A AVIATION POSITION INDICATOR: 2 EFFECTIVE DATE: OI AFR 15 FLYING ACTIVITY CATEGORY: 1 OFOA GATE 10/12: 29 OFOA GATE 15/15; OFDA GATE 20/18: 0 OFOA TO DATE: 29 AERONAUTICAL BADGE AERONAUTICAL RATING: COMBAT SYSTEMS OFFICER EFFECTIVE DATE: 22 NOV 13 OUS MIL RTG DT: CURR PARA RATING: CORR PARA RATING DATE: ORIG PARA RATING: ORIG PARA RATING DATE: STATUS FORMAL COURSE DATE INITIAL PHYSIOLOGICAL HYPOXIA TRAINING 06 DEC 12 Your current OFDA is 29 month(s). You need 6/ add1t10nal month(s) DFDA to meet your 12 Year gate requirement to receive continuous ACIP through 18 years of aviation service and you must maintain a Valid flight physical. I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE ACC PAGE 2 PAGE 2 (3-1f?9 RC-I35V, 64-4848, Class A, 30 April 15. AFSAS #739726 (}1.llufi. PREPARED 13 MAY 2015 20:00 INDIVIDUAL FLYING TIME SUMMARY (pA) A5 0P 1.1 MAY 2013 PCN 5A036-f-Iu REQUEST PERIOD FROM: 30 APR 2014 TO: 30 APR 2915 NAME: [Mishap Raven2] SSAN: mu:- GRADE: 1LT mew POS: 001 AIRCRAFT: RC135V (MD: ACC WING: UNIT: ACFT OPLOC: SGBP TAIL DUTY (MB SIM nos DATE NUHB POSN PRI sec INST EVAL 0TH TOTAL 501 (MB SRT C/s SRT NITE 1N5 INS NVG RES ?c135v 29 JUL 14 02-4126 uezuw 062-4126 UEINW 762-4139 UEINW 762-4139 UEINH 063-9792 UEINW 662?4139 UEINW 662-4130 UEINW 762-4139 UEINW 764-4848 MEANX 69792 MEANX 11.3 0.0 0.0 0.0 0.6 11.3 1 1162-9792 MEANX 11.2 0.0 0.0 0.0 0.0 11.2 1 1103-9792 MEANX 11.0 0.0 0.0 0.0 0.0 11.0 1 119792 MEANX 11.2 0.0 0.0 0.0 0.0 11.2 1 1163-9792 MEANX 11.5 0.0 0.0 0.0 0.0 11.5 1 1103-9792 11.1 0.0 0.0 0 0 0.0 11.1 1 1103-9792 MEANX 11.3 0.0 0.0 0 0 0.0 11.3 1 11.3 1 0.0 0 0.0 0.0 0.0 0.0 CMB SIM RC135V SUMMARY 001 sec INST EVAL 0TH TOTAL SRT cma SRT SRT NITE 1N5 INS NVG AIRCRAFT: 140.1 0.0 0.0 0.0 0.0 140.1 16 79SIMULATOR0.4 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 RC135W 07 DEC 14 62-9792 MEANX 11.0 0.0 0.0 0.0 0.0 11.0 1 114139 MEANX 11.4 0.0 0.0 0.0 0.0 11.4 1 1162-4126 MEANX 10.9 0.0 0.0 0.0 0.0 10.9 1 1002-4139 NhAnx 99792 MEANX 10.9 0.9 0.0 0.0 0.0 10.9 1 10.9 1 0.0 0 0.0 0.0 0.0 0.0 ACC PAGE 1 PAGE 1 (3-17C) RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2915 20:00 INDIVIDUAL FLYING TIME SUMMARY (pA) AS OF 13 MAY 2015 SAGBG-F70 REQUEST PERIOD FROM: 30 APR 2814 T0: 30 APR 2015 Rave" 2] m-u- GRADE: 1LT PR1 CREW P05: PRI AIRCRAFT: RC135V (MD: ACC WING: 034361450 UNIT: 0343chso ACFT OPLOC: SGBP TAIL DUTY STM M05 DATE NUMB 9050 001 INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE 105 1N5 NVG RES RC135W 09 JAN 15 62-4135 MEANX 11.2 0.0 0.0 0.0 0.0 11.2 1 1162-4130 MEANX 10.3 0.0 0.0 0.0 0.0 10.8 1 10JAN 62-4138 MEANX 11.4 9.9 0.0 0.0 0.3 11.4 1 1162-4138 MEANX 11.5 0.0 9-0 0.0 0.0 11.5 1 1162-4135 MEANX 11.4 0.0 0-0 0.0 0.0 11.4 1 1162-4135 MEANX 862-4139 MEANX 11.6 0.0 0.0 0.0 0.0 11.6 1 1162-4130 MEANX 11.0 0.4 0.0 0.0 0.0 11.0 1 1162-4138 MEANX 19.8 0.0 0.0 0.0 9.9 10.8 1 1963-9792 MEANX 11.1 0.0 0.0 0.0 0.0 11.1 1 1162-4135 MEANX 10.9 0.0 0.0 0.0 0.0 10.9 1 1062-4135 MEANX 10.9 0.0 0.0 0.0 0.0 10.9 1 1063-9792 MEANX 962-4135 MEANX 10.0 0.0 0.0 0.0 0.0 10.0 1 1062-4135 MEANX 10.0 0.0 0.0 0.0 0.0 10.8 1 104135 MEANX 11.7 0.0 0.0 0.0 0.0 11.7 1 1162-4139 MEANX 11.4 0.0 0.0 0.0 0.0 1162-4135 11.3 0.0 0.0 0.0 0.0 11.3 1 1162-4135 MEANX 11.0 0.0 0.0 0.0 0.0 1162-4125 MEANX 11.0 0.0 0.0 0.0 0.0 1162.4125 MEANX 10-9 0.0 0.0 0.0 0.0 1064-4131 MEANX 90.0 0.0 0.0 0.0 ACC PAGE 2 PAGE 2 G?l7l RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2915 20:00 INDIVIDUAL FLYING TIME SUMMARY (pA) AS OF 13 MAY 2015 PCN SA036-F7B REQUEST PERIOD FROM: 30 APR 2014 T0: 33 APR 2015 NAME: [Mishap Raven 2] 55AM: WM GRADE: 1LT FRI casw PDS: PHI Rcusv CMD: ACC 0100: 034300050 UNIT: 034300050 ACFT OPLOC: 5000 TAIL 00w cm: us 510 005 DATE NUMB POSN PR1 sac INST ?an om TOTAL SRT :00 SM US 5m 0m: 1N5 INS NVG RES CMB SIM RC135W SUMMARY PR1 SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG AIRCRAFT: 293.6 0.0 0.0 0.0 0.0 203.6 27 203.9 20 0.0 0 23.3 0.0 0.0 0.0 SIMULATOR0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 SRC135W 21 MAY 14 62-6002 UEINW 02 JUN 14 62-6002 UEINN 06 JUN 14 62-6902 UEINN 09 JUN 14 62-6002 UEINW 12 JUN 14 62?6002 UEINW 23 JUN 14 62-6002 UEINN 25 JUN 14 62-6002 UEINN 26 JUN 14 62-6003 UEINW 27 JUN 14 62-6002 UEINW 30 JUN 14 62~6092 UEINW 01 JUL 14 62-6002 UEINW 02 JUL '14 62-6002 UEINW 03 JUL 14 62-6002 UEIN 09 JUL 14 62-6094 UEINW 11 JUL 14 62~6002 UEINW 22 JUL 14 62-6002 UEIN 24 JUL 14 62-6902 UEINW 13 AUG 14 62-6004 UEINW 26 AUG 14 62-6002 UEINN 03 SEP 14 62-6002 UEINN 29 OCT 14 62-6001 MEANX mooamoewmmawemowomaem 990066030099069000060 GOGGSGOGOOSOGODGQQEQQ .I- '00 ?on ACC PAGE 3 PAGE 3 G?l 72 PREPARED 13 MAY 2015 20:00 [Mishap Raven 2] (MD: ALL wmn: uaasnwso TAIL NUMB 62-6001 62-6001 62-6004 62-6092 62-6002 DATE APR HDS SRCIBSW 14 14 14 15 15 SRCIBSW SUMMARY FRI AIRCRAFT: 0.0 SIMULATOR: 8 RPA: oeem @600 1.5 0.0 6RAND TOTALS AIRCRAFT: SIMULATOR: RPA: FRI 433.7 31.5 0.0 EGGH REQUEST PERIOD FROM: 30 APR 2014 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 UNIT: DUTY POSN MEANX MEANX MEANX MEANX MEANX I (9632 @692 GOO-1 gamma-c I'l'l 969!- emer- 9966631.]! ACFT OPLOC: SGBP TOTAL 433.7 83.0 0.0 PAGE SRT 43 26 0 4 INDIVIDUAL FLYING TIME SUMMARY (PA) GRADEEMS CMB 353MAY 2015 T0: 30 APR 2015 PR1 CREW POSSA036-F76 PRI AIRCRAFT: RC135V SIM INS INS NVG RES 0.0 0.0 0.0 0.0 0.0 0.9 0.0 0.0 0-0 0.0 0.0 0.0 0.0 0.0 0.0 SIM INS INS NVG 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 SIM INS 1N5 NVG 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 ALL PAGE 6 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.11.6. INDIVIDUAL FLIGHT RECORD PREPARED 01 MAY 2015 10.49 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 01 MAY 2015 PCN SAO35-F7O INQUIRY NAME: [M'Shap Rave" 2] 5540; GRADE: 111 PM mew P05: PR1 AIRCRAFT: RC135V c140: AU. 14101.: 0543110450 UNIT: 034300050 am 09100: SGBP TAIL DUTY CMB SIM DATE- MOS DATE NUMB FRI SEC INST EVAL 0TH TOTAL SET CH8 SRT SRT NITE INS INS NVG RES UPDATED snc135w 211141114 02-0002 uemw 120140710 SRCISSH 02 JUN 14 52-5002 UEIW 220140703 511013514 00 JUN 14 02-0002 001020140709 SRC135W 09 JUN 14 52-5002 UEINW 320140703 SRC135W 12 JUN 14 52-5002 UEINW 320140708 SRCIHSW 23 JUN 14 52-6002 UEINW 720140709 50013514 253014 14 62-5002 usmw 320140700 SRCISSW 25 JUN 14 52-5003 UEINW 320140709 SRCIBSW 27 JUN 14 62-6002 UEINW 320140709 5001351? BGJUN 14 52-5002 umuw 320140709 01 JUL 14 02-0002 051104 220140709 SRCIESW 023UL14 62-6002 UEINW 320140700 50013514 03 JUL 14 02-0002 new 220140710 sac135w 09 JUL 14 02-5004 new 320140724 SRCIJSN 11 JUL 14 62-5002 UEINW 420140714 sac135w 2210114 02-5002 20140724 50013514 24 JUL 14 62-6002 uemw 420140725 RC135V ZQJUL 14 62-4126 UEIW 620140730 mm 04 AUG 14 02-4120 UEINW 720140005 RC135V 03 AUG 14 024139 051101 720140014 SRCISSW 13 AUG 14 52-6004 UEINW 420140813 mm 21 AUG 14 02-4139 umw 00.0 0.0 0.0 0.0 20140025 snc135w 20 AUG 14 02-5002 051104 420140827 RC135V 28 M514 63-9792 UEINW 520140902 SRC135W 03 SEP14 52-6002 UEINW 420140904 01135v 00 521214 02-4139 051014 520140909 ACC PAGE 1 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 1 G-174 PREPARED 01 MAY 2015 18:49 Raven 2] WING: 0343Rcuso CMD: ACC MDS RC135V RC135V RC135V SRC135W SRC135W SRC135W SRCIBSW RC13SW RC135W RC135W RC13SW RC135V RC135W RCIJSV RC135V RC135V RCIBSV RC135W RC 135V RCIBSW RC135W RC135V RC135W RC135W RCIBSW RC135W 1 CERTIFY THAT I DATE HAVE REVIEWED MY IFRR AND IT IS COMPLETE AND ACCURATE. TAIL HUME 62-4130 62-4139 64-4848 62-6001 62-6001 62-6001 62-6004 62-9792 62-4139 62-4126 62-4139 63-9792 53-9792 62-9792 63-9792 63-9792 63-9792 62-4135 53-9792 62-4138 62-4138 63-9792 62-4138 62-4135 62-4135 62-4139 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 UNIT: DUTY POSN UEINW UEINW MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX MEANX HEANX MEANX v?r??r?I . I I PR1 want-wqu SEC INST A . a SSAN: INQUIRY ACFT OPLOC: SGBP EVAL - . 0TH GRADE: 1LT (MB TOTAL SRT CMB SRT 711.0 1 11.0 1 11.4 1 11.4 1 10.9 1 10.9 1 9.7 1 9.7 1 11.3 1 11.3 1 10.9 1 10.9 1 11.2 1 11.2 1 11.8 1 11.8 1 11.2 1 11.2 1 11.5 1 11.5 1 11.2 1 11.2 1 11.1 1 11.1 1 10.8 1 10.8 1 11.4 1 11.4 1 11.3 1 11.3 1 11.5 1 11.5 1 11.4 1 11.4 1 8.9 1 8.9 11.6 1 11.6 1 SIGNATURE PAGE 2 (3-175 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 01 MAY 2015 PR1 CREW POS: SRT NITE c>cua>u3<3 Eacaczia Ea?ac>c>PCN SA036-F70 PRI RC135V SIM 2 U5 DATE NVG RES UPDATED 20140915 20140917 20141030 20141106 20141104 20141202 20141125 20141209 20141211 20141214 20141217 20141221 20141225 20141228 20141230 20150102 20150108 20150109 20150113 20150116 20150118 20150120 20150123 20158126 20150129 20150131 ACC PAGE 2 DATE RC-135V, 64-4848, Class A, 30 April 15. AFSAS #739726 PREPARED 01 MAY 2015 10:49 INDIVIDUAL FLIGHT RECORD REPORT (PA) A5 0F 01 MAY 2015 PCM 5A030.P70 INQUIRY RaVen 2] SSAN: m-w- GRADE: 1LT PR1 CRER P05. PR1 AIRCRAFT: RC13sv cm.- Acc WING: 0343RCN50 UNIT: ACFT OPLOC: SGBP I DUTY CMB (2/3 51" DATE MUS DATE NUMB POSN sec 1051 EVAL 010 TOTAL SRT c140 SRT SRT NITE INS INS ch RES N/s UPDATED Ram! 02 FEB 15 62-4138 MEANX 11.0 0.0 0.0 0.0 0.0 11.0 1 1120150202 04 FEB 15 62-4138 MEANX 10.0 0.4 0.0 0.0 0.0 10.0 1 1020150204 Rc13sw 06 FEB 15 03.0792 MEANX 11.1 0.0 0.0 0.0 0.0 11.1 1 1120150206 mm?: 09 FEB 15 62-4135 MEANX 10.9 0.0 0.0 0.0 0.9 10.9 1 1020150209 11 FEB 15 02-4135 MEANX 10.0 0.0 0.0 0.0 0.0 10.9 1 1020150211 Ram: 14 FEB 15 03?9792 MEANX 920150215 17 FEB 15 02.4135 mm 10.0 0.0 0.0 0.0 0.0 10.8 1 1020150217 RC135N 20 FEB 15 62-4135 mm 10.0 0.0 0.0 0.0 0.0 10.8 1 1020150221 23 FEB 15 02?4135 11.7 0.0 0.0 0.0 0.0 11.7 1 1120150223 Rc135w 26 FEB 15 02-4139 19qu 11.4 0.0 0.0 0.0 0.0 11.4 1 1120150227 RC135W 01 MAR 15 02-4135 MEANX 11.3 0.0 0.0 0.0 0.0 11.3 1 1120150302 04 MAR 15 02-4135 11.0 0.0 0.0 0.0 0.0 11.0 1 1120150304 08 MAR 15 02-4125 MEANX 11.0 0.0 0.0 0.0 0.0 11.0 1 1120150311 Rc135w 11 MAR 15 02-4125 MEANX 10.9 0.0 0.0 0.0 0.0 10.9 1 1020150319 5RC1350 17 APR 15 62-6002 MEANX 420150421 $103511 22 APR 15 64-4131 920150420 m0 SIM 1105 SUMMARY PRI SEC INST EVAL 0TH TOTAL SRT C149 SRT C/s SRT NITE INS INS NVG AIRCRAFT: 433.7 0.0 0.0 0.0 0.0 433.7 43 303.3 33 0.9 0 27.5 0.0 0.0 0.0 SIMULATOR: 77.5 0.0 0.0 0.0 1.5 79.0 25 0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 Acc PAGE 3 I CERTIFY THAT I HAVE REVIEWED MY IFRR AND 11 Is COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 3 G-176 RC-I 35 V, 64-4848. Class A, 30 April 15, AFSAS #739726 Gl.ll.7. INDIVIDUAL TRAINING SUMMARY PREPARED 13 MAY 2015 19:57 [Mishap Raven 2] PHYSICAL DUE DATEOUALIF HON PROFILE CNN (N, 11GRADE: 1LT INDIVIDUAL TRAINING SUMMARY CURRENT TRAINING PERIOD SSAN: PHYSIOLOGICAL DUE DATE: 31 DEC 17 TASK IME DUAL EVAL RAVEN 66? CC RX CC RX SYNC TUNE SIM RIVET JOINT RAP SIM 135 CURRENCY SIM RAVEN SIN AEP (CSAR 0M0 SIN SRO PROFILE TOT SIM [01 RAP TOT MP CSAR (AS SRO RJ RAP TASK 10 M81 ECII Ec13 5(15 M112 M608 1612 M518 H529 M322 me: "'96 M114 mac ?nsz NT43 5000 sacs sae7 5818 SR29 sane SR59 IEO 9 18 r: PAGE 1 ACCOHP a 35 UU am (13000: 6) 6-177 AS OF 13 MAY 2015 CREW POSITION: MEANX RECORDS REVIEW DUE DATE: 31 JAN 16 DATE LAST ALCOHP ova REST 111 must am we our: ms (onACC PAGE 1 PCN UNIT: 0343RCN50 RC-I 35 V, 64-4848. Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:57 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2015 PCN SADBE-TID CURRENT TRAINING PERIOD NAME: [Mishap Raven 2] PHYSICAL DAlt: ?13 111:1. 15 GRADE: 1LT PHYSIOLOGICAL DUE DATE: 31 DEC 17 CREW POSITION: MEANX UNIT: D343RCN50 RECORDS REVIEW DUE DATE: 31 JAN 16 pan TASK 1: DATE LAM DAT: OVR ?It: REST co QUALIFKATIDN PROFILE TASK NAME ID R50 AccuNP REM ?(coup IN mass DATE 011E DUE PHS CODE 51159RAP 5115911 1 22 APR 15 I ca 310 11.1 R): can (m on 511(.N 2110 RJ Rx cm (N1 AI OR AIIOCA A0 51172 51H INFL ocA/suu saw 0 I (IN END 11.! ax CMR (N) 5111 INFL A 51199 a a 1 CH EWD 11.1 mt cm IN) SIN INFL DCA SR91 a a 1 CH It.) ax CMR 1N) SIM INFI (IN) SIN INFL CSRR SR93 IN) SIN INFL SRO $1195 9 I CH EWO RJ RX 01R IN) TOT 5X00 CMR INI BASIC SORTIE $1103 TRNG R.) at 10.3 CERT G578 CURRENCY X809 9 0 I CH RJ E110 BL TRNG RJ EL 9 CERT XBOQO 8 a 5 (H R1 E710 8L TRNG R.) BL 10 CURRENCY X819 TRNG RJ 81 11 CERT 118110 1 27 OCT 1? 6 GT GINO Fm TRAINING GAEB 0 12 51GRND Ewo TRAINING can M96 (GINO END TRAINING N9 DUAL (IF (END am TRAINING ACAD (61? GRND ENO TRAINING SEPT 6593 GRND Ewo TRAINING STAN TEST 5595 61' GRND Ewo TRAINING DPLAN STIDY 6522 92 MAY 14 ACC PAGE 2 PAGE 2 G?l78 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 19:5) INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2015 PCN CURRENT TRAINING PERIOD NAME: [M'Shap Rave" 21 GRADE: 1L1 SSAN: caew POSITION: MEANX mm: 9343Rc~sq PHYSICAL DUE DATE: 28 DEC 15 PHYSIOLOGICAL DUE DATE: 31 DEC 17 RECORDS REVIEW DUE DATE: 31 JAN 16 MI DAIE LAST OVR IN REST CD QUALIFICATION PROFILE TASK NAME IO RED ACCONP REM ACCOMP IN PHASE DATE DUE DUE PMS CODE W0 GI GRND ENO TRAINING All: SERVICE 6525 GRND EW TRAINING FLY SAFETY IRNG C1526 GRND two RISNO CERT 6550 GRND CWO TRAINING RISNO STIDY 6551 GRND EWO TRAINING 8018 (2 PRO 6559 GINO EWO TRAINING 5/5 TEST SEC 5572 GINO EWO TRAINING ISO PREP 1582 GRND 5W0 TRAINING INTEI TRM IEBS CRNO EVIO TRAINING AFE FAM TRNG lLf-H 6 07 MAY 1.4 5 (1T GINO EWO TRAINING (NONEJI (RM) END TRAINING ACOT LL04 GINO 5W0 TRAINING EGRESS LL95 0 32 MAY 24 GT CRND EWO TRAINING AFE TRNG LL06 GRND ENO TRAINING LOCAL AREA SURV 5591 0 96 MAY 14 6 GT (3ND EWO TRAINING CMBT SURV TRNG 5592 GRNO 5m TRAINING CAC TANG 5593 GRND EWO TRAINING WST 5595 ENG TRAINING AFRICOH (CSII 5597A 9 5T TRAINING CENTCOM 5597C GINO 5W0 TRAINING EUCOH SSQIE 9 9 5T GRND EWO TRAINING PACOM (CSI) 9 0 GT GINO 5W0 TRAINING SOUTMCOM (C51) 55975 0 0 GI CRND EHO TRAINING SPEC SERE TRNG 5510 GINO END TRAINING S-VRB-A 552? 9 21 MAR 14 Acc PAGE 3 PAGE 3 G?l79 64?4848, Class A, 30 April 15, AFSAS #739726 G1.12. [Mishap Signals, Search 8 Development] G1.12.1. CERTIFICATE OF AIRCREW QUALIFICATIONS Hi-l? H.353 r? G-180 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G1.12.2. FLYING HISTORY REPORT PREPARED 91 MAY 2015 17:42 FLYING HISTORY REPORT (PA) AS OF 01 MAY 2615 PCN SA036-F49 INQUIRY NAME: SSANcup: AIA WING-OGSSRECW PR1 DOS: 0 FRI ACFT- ncuss UNIT: 9997mm) BAst 0mm AFB AIRCRAFT TOTALS AIRCRAFT MDS FLT DTY CERT CODE DATE FIRST FLOWN DATE LAST TOTAL TIHE PRIMARY TIME SECONDARY TIME INSTRUCTOR TIME EVALUATOR TIME OTHER TIME NIGHT PRIMARY INST PRIMARY SIM INST NVG TIME COMBAT TIME CHBT SUPPORT TIME COMBAT SORTIES CMBT SUPPORT SORTIES TOTAL SORTIES T3 M0361 22 JAN 97 20 FEB 15 1553 . 1023. 0. 253. 277. \i #90009 A leW 206 MDBEI 28 DEC 96 19 AUG 14 1486.8 1086.1 0. 188. 195. 17. ?41> h1u1cbeuta WOGGOGODGOGOGOQ N0 DATE N0 DATE 0.0 GGOGDGOQGOQ cae1a>hahz?ahah>?a?zhahaka?z GOGGOQOOGQ WOQOODGOGGOQGOA UOAE 5.: PREPARED 01 MAY 2015 17:42 NAME cm): AIA WING: eessnecw AIRCRAFT TOTALS AIRCRAFT MOS FLT DTY CERT CODE DATE FIRST FLOWN DATE LAST FLOWN TOTAL TIME 51. PRIMARY TIME 45. SECONDARY TIME INSTRUCTOR TIME EVALUATDR TIME OTHER TIME NIGHT PRIMARY INST PRIMARY SIM INST TIME COMBAT TIME EMBT SUPPORT TIME COMBAT SORTIES CMBT SUPPORT SORTIES TOTAL SORTIES 993699?969 UOAE 17 JAN 91 62 FEB 31 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 FLYING HISTORY REPORT (PAT INQUIRY SSAN: GRADE: CMS API: A PRI CRW P05: 0 FRI ACFT: RCIBSS CAREER TOTALS CREW POSITION LINGUIST PRIMARY TIME 2652.8 SECONDARY TIME 0.0 INSTRUCTOR TIME 455.6 EVALUATOR TIME 485.1 OTHER TIME 17.5 TOTAL TIME 3616.4 STUDENT TIME 8.0 OTHER US MIL TIME 0.0 FOREIGN MIL TIME 0.0 CIVILIAN TIME 9.0 COMBAT TIME 1067.6 COMBAT SUPT TIME 707.8 TOTAL SORTIES 449 COMBAT SORTIES 105 COMBAT SUP SORTIES 99 NVG TIME 8.5 DATE FIRST FLONN 21 DEC 95 DATE LAST FLOWN 20 FEB 15 GRAND TOTAL 3610-4 PAGE 2 G-182 FAC: A OFDA: 233 UNIT: 9097INTSO AS OF 01 MAY 2015 PCN SAOBS - F40 ASC DATE: 22 JUN 11 BASE: OFFUTT AFB PAGE 2 PREPARED 20 MAY 2015 09:43 NAME: 040: MA cum: rumm- RCIBSV LAST 30 DAYS LAST 60 DAYS LAST 90 DAYS LAST 30 DAYS LAST 60 DAYS LAST 90 DAYS RCIBSN LAST 30 DAYS LAST 60 DAYS LAST 90 DAYS SRC135W LAST 30 DAYS LAST 60 DAYS LAST 90 DAYS SRC135V LAST 30 DAYS LAST 60 DAYS LAST 90 DAYS RC-I35V. 64-4848, Class A, 30 April 15, AFSAS #739726 Gl.12.3. 30/60/90 FLYING HISTORY REPORT AIRCRAFT MISNAP INVESTIGATION (PA) APT: A FAC: A ASC: CA ORGANIZATION: DOSIXNISQ CREW POSITION: AIRCRAFT TYPE: RC135V SERIAL N0: 64~4048 HISHAP AIRCRAFT GRADE: CNS SSAN: WING: 0055RECWG SEC INST EVAL OTHER TOTAL NIGHT INS 1023.4 9.0 253.0 277.0 0.0 1553.4 1276.4 100.0 0.0 7.2 7.2 0.0 0.0 OTHER AIRCRAFT FRI SEC INST EVAL OTHER TDTAL NIGHT INS 357.5 8.0 1.0 0.0 0.0 350.5 3580.0 0.0 0.0 0.0 0.0 0.0 0.0 0.9 0.0 0.0 0.0 0.0 0.0 0.0 1086.1 0.0 188.2 195.0 17.5 1486.8 11748.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 PAGF 1 DAFSC: 1A800 ASC DATE: 22 JUN 2011 MISHAP APR 2015 AS OF 20 MAY 2015 PCN SABBG-FZB AGE: SIM INS SORT @003 .0 .0 .0 .0 SIM INS 960 000 GQOG @6300 GOOG 060$ (DOCDCD @960 206 0 0 1 SORT camp: (9336 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 20 MAY 2015 09:43 AIRCRAFT MISHAP INVESTIGATION (PA) AS OF 20 MAY 2015 PCN SA036-F70 GRADE: CMS SSAN: A FAC: A ASC: CA DAFSC: 1A800 AGE: CMD: AJA HUDSRECHG ORGANIZATION: 0097INTSO CREW POSITION: EQBEI ASC DATE: 22 JUN 2011 CURR RATING: AIRCRAFT TYPE: RCISSV SERIAL N0: 64 4848 MISHAP DATFI30 APR 2015 OTHER AIRCRAFT FRI SEC INST EVAL OTHER TOTAL NIGHT INS SIM INS SORT RC13SU 117.4 0.0 0.0 0.0 0.0 117.4 117.4 0.0 0.0 0.0 13 LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 0C130H 23.4 0.0 12.8 6.3 0.0 42 36.2 0.0 0.0 0.0 5 LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 0EC130E 45.0 0.0 0.0 6.8 0.0 51.8 45.0 0.0 0.0 0.0 6 LAST 10 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 0SRC135X 0LAST 30 DAYS 0LAST 60 DAYS 0LAST 90 DAYS 0PA65 2 G?l84 RC4 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 PRFPARED 29 MAY 2915 was AIRCRAFT MISHAP INVESTIGATION (PA) AS 0F 29 MAY 2015 PCN NAME: GRADE: CMS SSAN: ARI: A FAC: A ASC: CA DAFSC: 1A800 AGE: AIA WING: ORGANIZATION: 9097INTSO CREW POSITION: Asc DATE: 22 JUN 2011 CURR RATING: AIRCRAFT TYPE: Ruasv SERIAL NO: 64-4848 NISRAP DATE: 30 APR 2015 OTNER AIRCRAFT PRI SEC INST EVAL 0THFR TOTAL NIGHT INS SIM INS SORT CAREER TOTALS CREW POSITION FIRST FLIGHT PR1 SET INST OTHER TOTAL STUDENT COMBAT COMBAT SORT LAST FLIGHT TIME SUPPORT AIRBORNE OPERATOR 21. UEC 1995 2652-8 (9 0 43.8 4851 17.5 3619.4 3161.8 0 lab/.6 107.8 449 20 FEB 2015 PAGE 3 G-185 ICC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 81 MAY 2315 17:42 INDIVIDUAL DATA SUMMARY (PA) AS 0F 61 MAY 2015 PCN INQUIRY . . . . NAME. SSAN. - - GRADE. CMS CMD AIA NINE. oessREch UNIT. BASE: OFFUTT AFB PERSONAL DATA DUTY PHONE: SECURITY CLEARANCE: OFFICE SYMBOL: SECURITY CLEARANCE DATE: 16 APR 14 SVC CAT. USAF RESTRICTED AREA BADGE N0: LAST PHYS DATE: PROFESSIONAL OUAL INDEX LPOI): PHYS CODE: PROFESSIONAL OUAL INDEX DATE. PHYS DUE DATE: PHYS AVATL CODF: PHYS AVAIL DATE: PHYSIOLOGICAL TNG DATE: JUMP STATUS PHYSIOLOGICAL DUE DATE: DATE OF BIRTH: DATE ASSIGNED JUHP STATUS: DUTY IABGG EFFECTIVE DATE OF DUTY: 91 SEP 14 PAS CODE: ODOUFKIF SYSTEM MANAGEMENT SHORT TOUR INDICATOR: . DATE RETURN FROM OVERSEAS: SGBP 0F 91 14 DATE: DATE OF 05 JAN 18 REDEPLOYED DATE: DATE DEP LAST DUTY STA: 26 APR 11 SPECIAL CAT m: DATE ARR THIS 01 11 RECORDS REVIEW ACC DATE. 14 JUN 13 STATUS: 1? RECORDS REVIEN DUE DATE: 39 JUN 14 PROJECTED RECORDS STATUS CODE: PROJECTED PAS CODE: PROJECTED DUTY LOCATION: PROJ DEPARTURE DATE: DATE: PAC 8 EFFECTIVE DATE: LOCAL USE CODE: PHA ERATL SENT 03/19/2015 AF 1 CERTIFY TNAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE AIA PAGE 1 PAGE 1 (E-ISCS PREPARED 01 MAY 2015 17:42 NAME: BASE: OFFUTT AFB AIRCRAFT OPLOC: CMD OF AIRCRAFT: ACFT SVC CAT: PRIMARY ACFT: FLT DUTY CERT CODE: CATEGORICAL FLYING WAIVER: INCENTIVE PAY DATA LAST NPO DATE: LAST NPO REASON: PAY STOP DATE: LAST PRODUCTIVE FLIGHT DATE: PREVIOUS PRODUCTIVE FLIGHT DATE: AVIATION SERVICE DATA AVIATION SERVICE CODE: EFFECTIVE DATE: PRIOR ASC: EFFECTIVE DATE: AERO ORDER TERM OATF: OFFICER SERVICE DATE: AVIATION SERVICE DATE: TRANSITION STATUS CODE: AVIATION POSITION INDICATOR: EFFECTIVE DATE: FLYING ACTIVITY CATEGORY: OFDA GATE 19/12: OFDA GATE 15/15: OFDA GATE 20/13: OFDA TO DATE: AIRCRAFT ASSIGNMENT DATA RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 55AM, SGBP 1C USAF RC135S 22 JUN 11 NONE 120 189 233 233 You have met OFDA requlrements for current gate. INDIVIDUAL DATA SUMMARY (PA) INQUIRY GRADE: CMS CMD: AIA WING: HOSSRECWG AERONAUTICAL BADGE CHIEF AIRMAN AIRCREWMEMBER AVIATION BADGE: EFFECTIVE DATE: AVIATION BADGE: EFFECTIVE DATE: AVIATION BADGE: EFFECTIVE DATE: OUS MIL RTG OT: CURR PARA RATING: CURR PARA RATING DATE: ORIG PARA RATING: ORIG PARA RATING DATE: STATUS FORMAL COURSE REFRESHER PHYSIOLOGICAL HYPOXIA TRAINING INITIAL PHYSIOLOGICAL HYPOXIA TRAINING I CERTIFY THAT I HAVE REVIEWED MY FRF AND IT IS COMPLETE AND ACCURATE. SIGNATURE PAGE 2 G-l87 AS OF 01 MAY 2015 PCN UNIT: OOQ7INTSD 19 SEP 11 SENIOR AIRMAN AIRCREWMEMBCR 01 JAN 01 (BASIC) AIRMAN AIRCREWMEMBER 01 DEC 96 DATE 12 JUL 11 01 NOV 95 DATE AIA PAGE 2 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2915 28:13 INDIVIDUAL FLYING IIHE SUMMARY (p4) AS OF 13 MAV 2615 PCN SAB36-F7B REQUEST PERIOD FROM: 39 APR 2614 TO: 13 MAY 2915 5549; man 99499: C145 991 can: 0 991 CMD: AIA NING: eossREch UNIT: 999719150 ACFT OPLOC: SGBP TAIL 997v cna 9/5 SIM 995 DATE NUMB POSN 991 SEC INST EVAL 979 TOTAL SRT :99 597 SRT NITE INs INS NVG RES RC135V 17 JUN 14 92-4132 90951 19.9 9.9 9.9 9.9 9.9 19.9 1 1964-4946 99461 11 1 9.9 9.9 9.9 9.9 11.1 1 1162-4125 99962.4131 M0991 594-4949 594-4949 MQBEI 7cna SIM 9c135v SUMMARY 991 SEC INST EVAL 0TH TOTAL 591 cue 591 (IS SRT NITE INS INS ch AIRCRAFT: 45.5 9.9 9.9 9.9 9.9 45.5 6 21.9 2 9.9 9 3.2 9.9 9.9 9.9 SIMULATOR974 9.9 9.9 9.9 9.9 9949.9 9.9 9.9 9.9 Rc135w 27 MAY 14 62-4125 MOBEI 119.9 11.3 1 1162-4132 99951 962-4139 MOAEI 962-4135 99991 292-4132 M0891 19.8 9.9 9.9 9.9 9.9 19.9 1 1962-4139 NOBEI 11.4 9.9 9.9 9.9 9.9 11.4 1 1192-4129 99951 19.5 9.9 9.9 9.9 9.9 19.5 1 1953-9792 MOAEI 63-9792 MOAEI 963-9792 99491 99.9 9.9 9.9 9.9 414 PAGE 1 PAGE 1 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MAY 2015 28:13 INDIVIDUAL FLYING Tm; gummy (M) AS OF 13 MAY 2615 PCN SA939.HB REQUEST PERIOD FROM: 30 APR 2014 TO: 13 MAY 2015 5599: mm- 9999:: casw P05: 9 FRI AIRCRAFT: ch55 (MD: AIA WING: GOSSRECWG UNIT: 0097INTSO ACFT OPLOC: SGBP TAIL nun (:99 us SIM MDS DATE HUME POSN PRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG RES ?99 SIM RC135W SUMMARY PRI SEC INST 0TH TOTAL SRT CH8 SRT SRT NITE INS INS NVG AIRCRAFT 54.9 9.9 9.9 9.9 17 92.4 19 92.2 6 9.9 9 9.9 9.9 9.9 9.9 SIMULATORN79 9.9 9.9 9.9 9-9 RPA0.0 0.0 0.0 0.0 59c135w 99 on 14 92-9991 99991 262-0001 ?0551 262-009] MQBEI SRCIBSW SUMMARY PRI SEC INST EVAL 0TH TOTAL SRT CH8 SRT SRT NITE INS INS NVG AIRCRAFT9.9 9.9 9.9 9.9 smuwoa9.9 9.9 9.9 9.9 RPAJ 90.0 0.0 0.0 0.6 cue SIM GRAND TOTALS PRI SEC INST EVAL 0TH TOTAL SRT CMB SRT SRT NITE INS INS NVG AIRCRAFT: 1l0.4 8.0 0.9 0.9 17.5 127.9 16 84.1 0.0 0 11.? 0.0 0.0 0.0 SIMULATOR9.9 9.9 9.9 9.9 RPA0.0 0.0 0.0 0.0 AIA PAGE 2 PAGE 2 G-189 RC-I35V, 64-4848. Class A, 30 April 15. AFSAS #739726 Gl.12.6. INDIVIDUAL FLIGHT RECORD PREPARED 01 MAY 2015 17:42 INDIVIDUAL FLIGHT RECORD REPORT (PA) AS OF 01 MAY 2015 571036-90 INQUIRY GRADE: (MS PRI CREW P05: 0 PRI AIRCRAFT: RC1355 (MD: AIA WING: 0055RECWG UNIT: 0097INTSQ ACFT OPLOC: $68? 1411 DUTY (M8 05 SIM DATE ?as 0415 nuns POSN Pm sac INST EVAL 1145 ms RES uromeo 29 APR 14 64.4841 MOAEI 11.5 0.0 0.0 0.0 0.0 11.5 1 1120140430 RCIBSW 27 MAY 14 62-4125 MOBEI 11.3 0.0 0.0 0.0 0.0 11.3 1 1120140529 RC135V 17 JUN 14 62-4132 MOBEI 10.8 0.0 0.0 0.0 0.0 10.8 1 1020140619 RCIBSW 23 JUN 14 62-4132 M0861 920140710 09 JUL 14 62-4130 MOAEI 920140710 RC135V 19 JUL 14 64-4846 MOAEI 11.1 0.0 0.0 0.0 0.0 11.1 1 1120140721 RC135H 23 JUL 14 62-4135 MOBFI 220140724 RCIBSW 29 JUL 14 62-4132 "0861 10.8 0.0 0.0 0.0 0.0 10.8 1 10.8 1 0.0 0 3.0 0.0 0.0 0.0 20140801 110350 05 AUG 14 62-4130 MOBEI 11.4 0.0 0.0 0.0 0.0 11.4 1 1120140808 Rcusw 13 AUG 14 62-4126 MOBEI 10.5 0.0 0.0 0.0 0.0 10.5 1 1020140814 RC135W 17 AUG 14 63-9792 MQAEI 00.0 20140820 18 AUG 14 63-9792 MOAEI 020140820 01:13st 19 AUG 14 63-9792 HOAEI 020140820 SRCIBSH 09 OCT 14 62-0001 M0061 220141016 RC135V 25 NOV 14 62-4125 MDBEI 520141126 5103517 10 DEC 14 62-4131 M00151 520141215 RC135V 36 JAN 15 64-4848 MOBEI 50.0 20150203 SRCIBSN 09 FEB 15 62-0001 MOBEI 220150209 RC135V 20 FEB 15 04-4848 MOBEI 720150224 511013514 27 MAR 15 62-0001 M0051 220150327 CUB 51M Mus PR1 SEC INST EVAL 010 TOTAL SRT (MB SRT SRT NITE INS INS NVG AIRCRAFT: 121.9 0.0 0.0 0.0 17.5 139.4 17 95.6 9 0.0 0 14.2 0.0 0.0 0.0 SIMULATOR0.0 0.0 0.0 0.0 RPA0.0 0.0 0.0 0.0 AIA PAGE 1 I CERTIFY THAT I HAVE REVIEWED MY IPRR AND IT IS COMPLETE AND ACCURATE. SIGNATURE DATE PAGE 1 G-l90 RC-I35V, 64-4848, Class A. 30 April 15, AFSAS #739726 G1.12.7. INDIVIDUAL TRAINING SUNIMARY PREPARED 13 MAY 2015 26:13 INDIVIDUAL TRAINING SUVMARY AS OF 13 MAY 2015 SAOJG-TIO CURRENT TRAINING PERIOD NAME GRADE: CNS SSAN: CREW POSUION: EOBEI UNIT: 00971N150 um. UMtt :1 JUL 16 PHYSIOLOGICAL DUE DATE- 31 JUL 16 RECORDS RFVIFW DUF DATF- 38 JUN 14 MC pr," TASK an: 115' one ova IN ?is? co ouAununou PROFILE TASK NAME 1150 ?cw REM 1cm IN ME 11176 out nus PHS (1106 CMC CONT PRO 11.1 m; 5111 R1161 10111! H608 a .1 27 MR 15 I (1'1 m: an: 5111 115 cumamv (111: an: 5111 (.111 can 11645 TOT 5111 sans 11151 RAP sm'vs 5099 11.1 101? an saws 51100 51159 5111: 1L) 1w co 51159: 14 A115 11 1 01 an: 11.1 wt 11? 5110111013 511591 6 21: nov 12 01 01c 11.1 10T 51169 an: ans". 501111: 51103 11.1 m: IL mu; Iu BL 19.: can 557: arr 13 I 01 n3 (Ht 111 ?1an RJ 81. 9 CERT 111090 cumv 1818 a 27 11111 (MC 111. TM 113 BL 11 CERT 113110 1 1 NOV 14 5 01 550 01m 550 new: EVAL 1399 5511 01m 5511 ow ucoa $511 ourv N643 9 3 27 15 1 61? (Mn 5511 11111111116 ANTI-HIJACK 61103 611.1111 551 "mums 551) M9 DUAL MIA PAGE 1 PAGE 1 6-191 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 PREPARED 13 MY 2015 26:13 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2615 PCN SAOBS-TIB CURRENT TRAINING PERIOD NAME: GRADE: cus ssm: "nw? (new POSITION: EOBFI UNIT: GBQTINTSD PHYSICAL DUE DATE: 31 JUL 16 PHYSIOLOGICAL DUE DATE: 31 JUL 16 RECORDS REVIEW DUE DATE: 30 JUN 14 TASK DATE IN CD PROFILE TASK ID R50 ACCOW IN PHASE DATE DUE PHS CODE GT GRW $50 TRAINING ACAD 5?GRID 550 MINING SEPT 6593 GRID SSD TRAINING STAN EVAL TEST 6595 GRID SSH TRAINING OPLAN STUDY 5522 IMINIMI FLT SAFETY TMG 6526 55? TRAINING NIEKELBACN 6555 CRUD SSD TRAINING 5/5 TEST SEC 557GRND SSD TRAINING ISO PREP GRUB 550 TRAINING AFE TRNG [151 9 61 NOV 95 61 GRND $50 TRAINING EGRESS (NONEGRND 550 TRAINING LL94 BIND 550 TRAINING ?63555 LL95 9 25 but: 93 8? GRNO 550 TRAINING AFE HOG a 18 FEB 1? 28 I153 15 YES GT Gm 559 IMININO LOCAI AREA SURV 5991 GEN 550 MINING CWT SURV TENS 5592 GRID 550 TRAININB (AL TRNG $563 GRND 55? TRAINING 5505 GRND $50 TRAINING AFRICM 9 5T GRID $50 TRAINING (C51GRND SSU TRAINING SSG7E a 9 ET GRND 550 PACOM 55077 9 9 In, GRND SSD TRAINING 55875 9 GT Gm 550 TRAINING SPEC SERE WW) 9519 51' CHM) 5?0 TRAINING S.V83-A 5524 9 9 I7 AIA use 2 PAGE 2 G-192 PREPARED 13 MAY 2015 29:13 PHYSICAL DUE DATE: 31 JUL 16 POM CD QUALIFICATION PROFILE CT GRND SSD TRAINING TASK NAME ALERT RESPONSE RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 INDIVIDUAL TRAINING SUMMARY AS OF 13 MAY 2915 PCN CURRENT TRAINING PERIOD GRADE: CH5 SSAN: PHYSIOLOGICAL DUE DATE: 31 JUL 16 CREW POSITION: EOBEI UNIT: 0697INTSO RECORDS REVIEW DUE DATE 30 JUN 14 ACC TASK VOL/ova DATE LAST DATE ova REST 11: RED ACCOMP REM IN muse one our: cue was canAIA PAGE 3 PAGE 3 6-193 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2. FLIGHT EVALUATION AND TRAINING RECORDS. G2.1. CAPT [Mishap Pilot] G2.l.l. AF FORM 85 (MP) CERTIFICATE or AIRCREW QUALIFICATION I. EXAMINEE IDENTIFICATION (L8H. Ml"de HANK SEAN DERIOD [MIshap PIlot] Cap. Apr - Sec 13 ORGANVATION AND 343 Rs. AFB. NE RC-135V IMC ll. QUALIFICATION 6R0 PHASE FLIGHT PHASE FJKAIMNATIONICHECK DATE GRADE DATE Closed Book 04 Jun 13 100 NIN INSTWOUAUMSN 22 May 13 Open Book 06 Jun 13 100 Boldface 28 May 13 EPE za May13 1 Instrument 10 Jun 13 94 WALFNWON LEVEL ADDITIONAL mm QUALIFIED UVOUAUFED DUE DATEIS) DATE TRAINING COMPLETED 1 NIA NIA EXPIRATION DATE OF OUAUFICATION CERTIFVING OFFICIAL, RANK AND SIGNATURE (Dct ?4 ORGANIZATION 1 RESTRICTIONS :1 EXCEPTIONAMY QUALIFIED COMMANDFR-DIRECTED DOWNGRAOE IEthun Commonly en Baa) (Emu In Mum: or (Emma In Common?: on Back) Ill. CERTIFICATION CHECK man NAME AND RANK ORGANIZATION 8 sIsqune on: I FLIGHT EXAMIIER 1 343 RSIDOV 11Jun13 Rewewms I. 343 RSIDO I . FINAL APPROVING OFFICER 3 3w RSIGC I 3 I CERTIFY hat I have been briefed and undetsland Ibo acIon beinalakm this date. DATE NAME GRADE OF EXAMNEE - [MIshap Pllot] Cap, I 3 343 RSIDOW AF FORM 8, 20061208 PREVIOUS EDITIONS ARE OBSOLEI t. G-l94 RC-135V, 64?4848, Class A, 30 April 15, AFSAS #739726 AF FORM 8 CONVINUATION SHEET IV. commst REMARKS: A. Mission Description. This was a No-Notlce Oopilot Quali?cation. Instrument and Mission evaluation ?own on a local tramng acrtie out of Ofiutt AFB. NE The ?ight pro?le consisted of ere-?ight. takeotf. air refueling. orbit. transition. and 'andmg. The examinee planned. briefed, accomplished. and was evaluated on the following events- mission planning, pro-flight, takeoff. departure. receiver air retooling. practice emergency separation. simulated orbit procedures. enroute descent and transition Transition consisted of precision. non?precision and VFR approach work to include landings, mlssed approach. and lunch 905. B. Discrepancies. None. C. Recommended Additional Training. None. D. Additional Comments. Commendeble. Area 2 Mission Plannmg. Outstanding EP brief to lull crew on jammed stabilizer Examinee elected to re-align expiration dates. Alert/scramble start. emergency procedUres. systems knowledge. unusual attitudes. fix to fix. holding. and tactical employment were evaluated In the RC-135 OFT on 28 May 2013 by Capt. in conjunction with the EPE. Requisiles and flight satisfy all requirements for the Copilol position on and 358M aircraft REVIEWING REMARKS: None. APPROVING OFF REMARKS: None. REVIEWS: None. AF FORM 8. 20051208 G-l95 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 one 0 CERTIFICATE or AIRCREW QUALIFICATION 12 l. eumues noeunncmou NAME ILMI. Flm. Maudie lulu-l) RANK ELIGIBILITY PERIOD [Mishap Pilot] NIA ORGANIZATION AND LOCATION ACFTICREW POSITION 338 CTS. 0mm AFB. NE RC-135V mc u. oununcnmou ,7 enouno pm: mom muse I DAVE. GRADE MSSIWICIECK DATE Closed Book 04 Apr 12 92 WW msmnuaumsre 06 Apr 12 Open Book Instrumem 20 Jan 12 100 QUALIFICATION LEVEL I ADDITIONAL TRAINING QUALIFIED UNOUALIFIED I DUE DATEIS) DATE ADDITIONAL TRAINING COMPLETED 1 MA MA mama? one o; omuncmon cemnms OFFICIAL RANK mu SIGNATURE one onwunou Sep 13 um Resmcnous axcernowu ouaunen COMMANDER-DIRECTED DOWNGRADE (Em In Commons on em I [Elm In Covmranlz on Back) (Exp-rm In Con-noun on M) m. can TYPEDW AND RANK ORGANIZATION 8 SIGNATIRE DATE 3 I I I FLIGHT EXAMINER 1 333 c1smoo :1 a 50 Am REVIEWING omcen 2 338 crszoo l: . 02 m1 IL FINAL APPROVING 3 338 I I3 05a Hay/2 DATE MAY AF 8, 20081208 PREVIOUS EDITIONS ARE WSOL: G-l96 I CERTIFY that have been busted and understand the action being taken this late NAME GRADE OF EXAMINEE [Mishap Pilot] RC-I 35 V, 64?4848, Class A, 30 April 15, AFSAS #739726 AF FORM 8 CONTINUATION SHEET N. COMHENTS REMARKS: A. Mission Description. This was an initial Copilot Qualification. instrument and Mission evaluation ?own on 9 local training sortie out at Oi?lutt AFB. NE. The ?ight pro?e consisted ot takeoff, air refueling. orbit, transition. and landing The examiner; planned. briefed. accomplished. and was evaluated on the follownng events: mission planning. prenight. takeoff, departure, receiver air ruiueling. practice emergency separation. simulated orbit procedures, enroute descent and transition Transition consisted ofe four engine non- reoision approach and planned missed approach. a four engine precision approach and touch and go landing and a four engine FR approach and touch and go landing. B. Discrepancies. 1 Ground None 2. Flight. Area t2. Departure/Climb - 0-. Dobrieled. Examines exceeded 0 airspeed tolerances for departure and climb out. Did not hinder mission accomplishment. C. Recommended Additional Training. None. 0. Additional Comments. Alert/scramble start. emergency procedures. systems knowledge, unusual attitudes. for to noiolng. and tactical employment wore evaluated in the R0435 OFT on 27 Jan 12 by in conjunction with the EPE. Requisitea and ?ight satisfy all requirements for the Co-piloi position on and airmail. FORM 8. 20061208 (REVERS G?l97 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.1.2. AF FORM 8A Temporary Flight Evnlnahou Certi?cate FLIGHT EVALUATION {we 2 I 5 WORKSHEET ?51an - [Mishap mot] GRADE. 0-3 ORGANIZATIONWTION: P08: PERIOD: as, ormrr AFB. NE MP NM GROUNDPHASE FLIGHT PHASE EXAMIGIECK DATE GRADE MISSIONICHECK DATE CLOSED OPEN :0 Mn Is 9s BOLDFACFI00 Racommeaded Addfnonnl Amen QUALIFICATION I an? QUALIFIED Rennmons DUE DATES: Non: (Eprun comments) YES 0 DATE I. . . . . . TRAINING cowme AddItIoml Trauma Actompmhed . .m of No 0 NM None Quali?cltim: COMMENTS: ?The Form 80' adue :9 338 003!? nextwodmg day. muramawm?mqm_ . IIyoumonmemd umummo Rumcuans None CERTIFICATION PRINT NAME AND GRADE ORGANIZATION I. FLIGHT EXAMINER: 33" Cm 2. orrIcnR; 33" 3. APPROVING omcm 33? ma REQUIREMENTS NOTE: ~m Pilot all apply) Dilfm (Y or N) initial (Y Immeer or N). RACK FOR NOTES) Boldface(QMuitiqucdthai . Data: 1151;?; Pubs checkzd on Cm: by Theeulsllis?esn: arm circlemmn oawc cmsso BOOK CRITIQUED awn/m3: mc CRmom-J) Signature of Flight Examiner Date 33: CIs I ALIS cn In Is OPEN BOOK BYIDATE: an: GIVEN JAWS 20Mtl5 users 55 00 FORM 8A-135P, FEB l5 55 06 FORM BA-ISSP. FEB l5 G-l98 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AREMSUB-AREA [elo- REMARKS Q- REMARKS (P) Pam Only initial Only an I168 I. QUALIFICATION . Eqrurmn?mbfim?am Mission Planning . . Cheekir'at Premiums [Crititnll NM 2 1 4. Proeednres 5 We}! (Crilieull NJA Aircrew Discipline (Critical) WA 3. Coordi'ttormn 9. Brie?ngs ll). Pre?Takeoff Takeo? JE. its} 13. Cruise'Navigation l-l. lit-Flight Cheeks 15. ATE Commtr'FF'rSt'F 18. Comm. Logs. Reports 19. Air Re?lelingv?ReueivEr (LE, 6} Descent [Enmule at Published} 25. vt-n'rratneparrem 25. taming Touch and Ge Landings 23. GuAmund [ll] Sim Eng Out Patr?Lndg 30. Eng Faieralteol'fC'on 3 I. Sim FJD Clo-Around 32. EP - Bolit?tc?e r'tC?ril'imU Nit-9t 3-3 . Systems Knowiedgr-?pomrimrs 3-1. A?er Lande 35. Paay?ilgh??eb?ef 39. Air RefuelinyTath-er l2. Li. l4. >1 J0. Cobra Ball Dairies RnerJoml Duties 12. Open Shite: Duties d3. Constant Phoenix Duties 5L Pilot's brie?ngs on mission day were outstanding. He ensured all information was briefed in detail and gave an esteellent of} engine pattern procedures In his eopilot. ll. INSTRUMENT lb. Unusual Attintdes IT. Holding 21. IER Pattern {print to FA F) 22. Precision App 13. Non-Precision App 24. Missod Approach Itl. .. Touch and (in Landing 35. Instruction-ml Abillty Instructional 33. Demonstration and Performance NR Limits Demo App to initial Buffet (I) -- JU Hap Landing {In} -- Sim 3-cng Rud. Off LM (ll -- Touch and Go Landing 55 0G FORM Brit?135?. FEB 15' NOTES: [1 Sou W. Both a. PAR. and IL8 are required if equip and facilities are available Dr traf?c ?ow pennils. lihoth aren?t available the [light oval may he completed with one precision Walt ?OW'l?l. Do not verbally evaluate the approach than wasn?t flown Unusual attitudes will. and holding may. be aeeomplished in the OFT Include reverse thrust. initial AC and diff AC evals must be accomplished lnllight waiver to All other raw-w: thrust Walls may be evaluated in die OFT CPs will be checked on permanence nfduties during Ind: and tufu=ling ops. including fuel panel. CG. and breakaway procedures. AR cheeks may be on the ground or in DPT if unable in ?ight {13} Track time should be scheduled to allow for 30 min ofenntaet DOV may establish a mint time from initial pre?euntnel In achieve required contact time- lil Inadvertent disconnects are pennissible and will not he polluted against examiner. l8} Missed approach must he initiated from on approach May be graded using rectangular pattern or circling maneuver l'l"I must perform a touch and gt: as both the pilot flying and piled not ?ying to complete this area {1]}Maj' be ?own from IFR or VFR. SEFE rnng.r direct it go around at any point in an approach or landing to evaluate procedures. May be graded during it missed approoelt Ill} Area includes and limitations are established fot orbit. 111in platform. post MR. and breakaway. Momentary deviations are acceptable du?ng re?reling {13] COS will be evaluated only on performance duties during rm]: and NR ops {l4} When auto pilot add 100 ft, Shite, and 5 degrees to all tolertmucs :15} Airspeed [elem-noes do not apply unless by A'l'C'Iteuh tints, Must net ectde placard Speeds For must meet awe 25 and 26 standards Only required if mission certified ilt tanker air retire-ling Awarding a. in any oftltesu areas will result in a (3?3 [hr the overall Instructor grade. The overall grade for the instructor portion ul?tlre evaluation will he no higher than the lowest overall grade awarded under QUMJIN STM Data uttered daze: Initials: 55 06 FORM Sit-135?. EB 15 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.l.3. AF FORM 942 RECORD OF EVALUATION NAMHLM, firs! mm. Inl?d) 33m [Mishap ACFTICREW 7:5 DATE ouwncmou ACF1ICREW ?5:5 DATE QUALFICATOON PWITION COMPLEYED LEVEL POSITIW EVALUATION COMPLEIED LEVEL ACC o1 Apt 12 no-135v mc 06Apv1? 1 Review was 23 Am 12 vac?135v mc um 10 Jun 13 INSTMIOUALIMSN AF Form 942, PREWOUS EDWIONS ARE OBSOLETE 64?4848, Class A, 30 April 15, AFSAS #739726 G2.1.4. TRAINING RECORDS TRAINING SUMMARY AND CLOSEOUT REPORT NAME I RANK CLASS NAME I RANK [Mishap Pilot] 1562 NUMBER OF DATE ENTRY DATE COMPLETE TOTAL DAYS AIRCRAFT COURSE 5 12-Nov-14 5 142 R0135 GENERAL [Mishap Pilot] has completed RC-135 AIRCRAFT COMMANDER QUALIFICATION In the ?c.1355/u/V/w and muss/w Training consisted of all ground and flight events required by AH 11-2RC-135 Vol 1. Training covered events listed In ACC Syllabus Course RC135 AIRCRAFT COMMANDER OVERALL PERFORMANCE: [MiShap excelled during Aircraft Commander Quali?cation. [MiShap Pilo? scored 98% on Computer Based Training, 99% on stan/eval exams, and 98% on Academic exams. No weaknesses were noted during training. [M'Shap earned a Cu on his flight eval. [MlShap will make an excellent addition to the 343 RS Aircraft Commander force. [M'Shap Pno? deserves consideration for early upgrade to Instructor Pilot based on his performance in IQT. TRAINING TO BE COMPLETED AT GAINING UNIT: None. ADDITIONAL COMMENTS: [MiShap Pilot] had 5 FTU instructors. Per the syllabus, aircraft commander students are allowed a maximum of 3 Instructors during Exceeding this limit requires documentation of this fact in the student's training iolder. Also, inclement weather and maintenance cancels, [MlShap exceeded the number of allotted syllabus training days. These MFRs are in his training folder. llMiShap PilOt] was recommended for his check ride by Capt an 30 Mar 15 and his check ride was givan by Capt 2 Apr 15. SIGNATURE hunt: manner: to: 338 CTS Form 46 (11 Jun 14) G-201 64?4848, Class A, 30 April 15, AFSAS #739726 TRAINING ACCOMPLISHMENT REPORT GROUND MASTER [Mishap Pilot] Records Review Clearance Egress. Non Resource Management SERE Orientation Initial Dual Formal Training Course - See TMS Printoul Warrior Course - Test Score informailon Protection itumen Relations Egress with ACDE life Training Book Examination Book Examination Ouallicalian Evalualion C2 Procedures Certi?cation Defense Survival Skills' Care' Quali?cation? -02 RC-135AC Force Protection Suicide Prevention DOD IAA v2.0 of Armed Con?ict 13Nov-14 Assault Prevention 21-Nov-14 1? Exercise of Classi?cation revel Card Holder (GTC 101 30-Jan-15 Risk - Counter-ED Awareness Ordinance Reoonnaissame and Force 2A Culture General Course MISSION 14 and Cort AC. 21-Nov-14 SERE (sv-ao-A) thnv-l 4 Alter Capture Survival Detention LeveiC PLincatlons Check Emergencies Procedures Evaluation Refresher Course and Examination 3 Rendezvots Procedures Stan Procedures Fuel Staner Stan Prevention of Safety Tra'ning training to be accomplished at gaining squadron '52 -A2 TRAINING FOLDER INSTRUCTOR PRE-EVENT REVIEW I SPECIALTY CHIEF FUGHTUNE WEEKLY REVIEW IRANING EVENT PO-2 90-4 TAO TAG TAC TAC SPECIAI TY CHIEF WEEKLY DATE 33?; CT?I=orm 45 (11 Jun 14) PO-S Fc-1 F0-2 0-4 M-1 M-2 M4 M-5 TAG TAG vii?av" G-202 35 V, 64?4848, Class A, 30 April 15, AFSAS #739726 TRAINING ACCOMPLISHMENT REPORT STUDENTS NAME I RANK wsmucrons NAME IRANK counse [M'Shap 15-02 TRAINNG PERIODS INSTRUCTORS INITIALS It EVENT DATE - 31m FLIGHT I SIMULATOR DURATION . 3.0 OVERALL GRADE 01 TRAINING LISTING dub-Lul-DJ-l-A-I ?0030061000 uuwubwuub 338 Form 45 Flight Neale: (11 Jun 14) G-203 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 TRAINING ACCOMPLISHMENT REPORT TRAINING PERIOD TRAINING EVENTITASK LISTING wee not observed or me eIementwas not perfonned. - Periorrmnoe was weak (one demon! marked will require an overall made 0! ?zero'). - Performance indicates: Iadr knowledge. - Pe?ormanoe is sate. but Indians Iimiled pro?denq. Melee: error: 0! mission or cornmlulon. - Performance ls essen?aly correct. Recognizes and curred: anon. - Penormanoe as correct elitism, mm and without MW. -Petf0rmanmre?edsehigh degreeol - Unu?mdory; unsa?sfadory ptogrea or regression - Satisfactory. progress In sa?sfadory. butrequired pro?durcy level is not achieved - Emelem; 9mm progress beyond required pro?aency levels hr weaned training period - PM adlieved the requ?red pro?ciency level [Note Student mun be graded (P) Pro?o'om to W10 11-202 Evaluation] - Nou?edivelevents not complemd tor weather. equipment maltundim. abon. cancellation. AND unable to accomplish on future some - Non-effectivdeth undie meet RPL 338 CTS Form 46 Fll?m ?at! (11 Jun 14) G-204 35 V, 64?4848, Class A, 30 April 15, AFSAS #739726 TRAINING ACCOMPLISHMENT REPORT STUDENTS NAME I RANK CLASS NAME COURSE [Mismp 15-02 ammo INSTRUCTORS INITIALS EVENT DATE FLIGHT SIMULATOR DURATION OVERALL GRADE TRAINING EVENTITASK 0059900 338 CTS Form 45 Flam Manor (H Jun I4) G-205 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 TRAINING ACCOMPLISHMENT REPORT TRAINING PERIOD TRAINING EVENTITASK LISTING TASK - Periotmamo was not obmad or me element was not perfumed. - Momma. was unsalo (one olemwt lurked will requer an mall grad. of'um'). - Puformanoo mm a lack of guilty or knowbdoo. - Performance In safe but indicates ?amed pro?cicnw. Makes Om of omission 0: com. - Performance In ?untidy comet. Recognizes and corrects anon. - Wt. wivlouthasduoon. - Performance re?ect- I Umau?adoty. musme progress 0: regressbn - Sammy; progress is satislactory. but required pro?ciency level Is not achieved - Excelbnt; 369ml progress beyond required pro?ciency Ievels for sped?od training period - Noo-offeclhelovonts not comle forwuthor. oquipmom abort uncallah?on. AND unable Io mnplish on future safe - Nme?ec?velstudent mama to meet RPL 333 CTS Fonn 45 Flighl Master (11 Jun 14) G-206 uJ?o?nuaah i I 2 3 2 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.2. CAPT [Mishap 00%? (MCP) 02.2.1. AF FORM 8s DATE COMPLETED CERTIFICATE Or AIRCREW QUALIFICATION 21 May 14 EXAMINEE IDENTIFICATION NAME (LnsI, rm. Middle mum) RANK SSAN PERIOD [Mishap Co-Pilot] Cant Fab Jul ?4 ORGANIZA AND LOCATION Posnou 343 RS AFB NE RC-135V IMC II. QUALIFICATION GROUND PHASE FLIGHT PHASE on: name one CIosed Book 19 May 14 100 INSTMIQUALIMSN 12 May 14 Open Book In May 14 98 Boldlace Inslrumenl 21 May 14 98 QUALIFICATION LEVEL ADDITIONAL TRAINING QUALIFIED UNOIJALIFIED DUE DATEIS) DATE ADDITIONAL TRAINING COMPLETED 1 EXPIRATION DATE OF QUALIFICATION SERTIFYNG OFFICIAL. RANK AND SIGNATURE DATE ORGANIZATION Oct 15 MIA RESTRICTIONS COMMAND: R-DIRECTED OOWNGRADE {Fla-m Comm: an arm; {Emma Cmnmuus on Bacu [j ?Exmm an Back] Ill. CERTIFICAHON CHECK TYPEO NAME AND RANK ORGANZATDN 8 I SIGNATURE DATE I I a EXAMINER I 238 CTSIADO a - 26 Feb 15 REVIEWING OFFICER 2 -I Col 343 RSIDO 02 FINAL APPROVING OFFICES 3 g] [Ir?u? I CERYIFY that I have been busted and understand [he adIon balm Irus dale DATE NAME AND GRADE OF EXAMINEE SIGNATURE 03Mar15 [Mshap CoP-Iotl . Ian Kc. I um- [M'Shap 00? 'Diln? AF FORM 8. 20061208 PREVIOUS EDITIONS ARE OESOLETE G-207 ICC-135V, 64-4848. Class A, 30 April 15. AFSAS #739726 AF FORM 8 CONWNUATION SHEET iV. COMMENTS REMARKS: A. Mission Deooription. The was a Recurring Copilot instrument. Quali?cation. and Mission evaluation ?own on a local training sortie out at Oliutl AFB. NE.. and the 55 CG Evaluation Profile Letter The ?ight pro?te consisted of ore-?ight. takeoff. air reiuelng. orbit. transition. and landing. The examinee planned. on?eted, accomplished. and was evaluated on the foliowmg events: mission planning. preJligtll. lakeoii. departure. receiver air refueling. practice emergency separation. simulated orbit procedures, enroute descent and transition Transition consisted ol 4 engine touch and 90. LCD 4 engine Missed approach. VF-R 4 engine touch and 90 B. Discrepancies. None. Recommended Additional Training. Nona. D. Additional Comments. Alert/scramble start. emergency procedures. systems knOWIodce. unusual attitudes. fix to holding. and tactical employment were evaluated in the Etc-135 OFT on 16 May 14 by in conjunction with the Requisitas and night satisfy all requirements for the Copllot position on Rc-tossiuNiw and 76-1 aircrelt REMARKS: None APPROVING REMARKS: None. ADDITIONAL REVIEWS Nona AF FORM 8, 20081208 (REVERSE G-208 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 DATE ETED CERTIFICATE OF AIRCREW QUALIFICATION Feb 13 l. EXAMINEE NANE (um, _MIddIe RANK SSAN ELIGIBILITY PERIOD [MIshap Co-Pllot] 1L. NIA ORGANZATDN AND LOCATION ACFTIOREW POSITION 338 CTS. 0mm AFB. NE RC-135V IMC OUAUFICATION GROUND PHASE FLIGHT FIIACE DATE mun: ussmcaecx DATF Closed Book 07 Feb 13 96 INIT 15 Feb 13 Open Book 05 Feb 13 96 BoldEc100 QUALIFICATION LEVEL Anomowu. TRAINNG QUALIFIED UNOUALIFIED DUE OATEISI DATE TRAINING COMPLETED 1 NM MA I DATE OF QUALIFICATION CERTIFYING OFFICIAL. RANK AND IISIGNATURE DATE ORGANIZATION I - RESTRICTIONS I EXCEPTIONALLY DUALIFIED COMMANOER-OIRECTED OOWNGRADE (mm In com": on Huh.- _l In Camus Im Boot) [Eng-um In Comm; an 539) CER CIIECII NAMEAND RANK 1 Human: um FLIGHT EXAMINER OFFICER 2 338 CTSIDO fair /3 FINAL APPROVING OFFICER I 338 CTSICC CERTIFY MI I have been Dnelad and uMaIsIand me achn bang taken 1m: DATE ITVPED AND GRADE 0F EXAMINEP 3 Aw I3 [Mishap Co-Pilot] ILI 1338 AF FORM 8. 20061208 PREVIOUS EDITIONS ARE OBSOLETE G-209 RC-135V, 64?4848, Class A, 30 April 15. AFSAS #739726 AF FORM 8 CONTNUATION SHEET IV. COMMTS REMARKS: A. Mission Description This was an Initial Conilot Qualification, instrument and Mission evaluation ?own on a local training sortie out oIOi'Iutt AFB. NE. The light profile consisted eitakeolt?. air refueling. orbit. transition. and landing. The examinee ptanned. briefed. accomplished. and was-evaluated on the following events: mission planning. pre?ight, takeoti. departure. receiver air refueling. practice emergency separation. simulated orbit orooedures. enroute descent and transliort Transition consisted at a right, seat 4E touch 8. no. VFR touch 8. go. and a LOC missed approach. B. Discrepancies. 1. Ground, None. 2 Flight Area 15. ATC - Debrieted. Missed multiple radio calls. slow to comply with controlling agency mstructiona. Made errors in the operation of equipment. C. Recommended Additional Training. None. 0. Additional Comments. Alert/scramble stan. emergency procedures. systems knowledge. unusual attitudes. ?x to holding. and tactical employment were evaluated in the R0136 OFT on 30 Nov 12 by in conjunction with the EPE Raqusitos and tight satisfy all requirements for the Copilot position on and T04 aircraft. REVIEWING REMARKS: None. APPROVING OFFICERS REMARKS: None. ADDITIONAL REVIEWS: None AF ?brin?n 8. 20081208 (REVERS G-210 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.2.2. AF FORM 942 RECORD OF EVALUATION NAME (Last. Firs! Middle Initiaa ssAN [Mishap Co-Pilot] ACFTICREW 7:25 DATE QUALIFICATION ACFTICREW 7:25 DATE QUALIFICATION COMPLETED LEVEL POSITION EVALUATIM COMPLETED LEVEL ACC RC-135VIMC INIT 15 Feb 13 1 Initial Review 343 RS 01 May 13 luv/3n: 1 M1 A: Form 942, 209.120. PREVIOUS aomous ARE 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.3. CAPT [Mishap Navigator] G2.3.1. AF FORM 85 (MN) DATE COMPLETED CERTIFICATE OF AIRCREW QUALIFICATION ?3 May 1? I. EXAMINEE IDENTIFICATION NAME (LBSI. FIVUL MIOUIG RANK SSAN PERIOD [Mishap Navigator] Cap! MSN Den-.13 - May 14 QUAL: NIA ORGANIZATION AND LOCATION POSITION 343 RS. 0mm AFB. NE RC-135V IMN II QUALIFICATION GROI ND PHASE mam pm: EXAMINAIIONICHECK DATE GRADE MISSIONICHECK DAIE Closed Book Open Book Instrumenl 05 May 14 98 LEVEL TRAINING 1 QUALIFIED UNQUAUFIED 'Duz DATE ADDITIONAL TRAINING I EXPIRATION DATE OF CERTIFYING OFFICIAL. RANK MU SIGNATURE DATE ORGANIZATION Oct 15 INIA REST RICTIONS Its-mam .0 Common on Sam El IONALLY QUALIFIED IEpruI In Comment: en Back) El COMMANDER-DIRECTED OOWNOMDE (Expmn Ir. Conwaan on Back) CERYIFICATION TYPED NAME AND RANK ORGANIZATION I SIGNATURE DATE FLIGHT EXAMINER 7 I 343 RSICCE VA - 15 May14 REVIEWING 343 RSIDO 16 May 14 FINAL APPROVING a 343 RSICC 19May14 I CERTIFY that Ihave been b?ofe? and undersIand Ihe Adina baIrIg taken IhIs date DATE TTYPED NAME AND GRADE 0F EXAMINEE SIGNATURE 05 .Iun 14 [Mishap Navigator] . . . . - I343 ?saw I [Mlshap NaVIgator] AF FORM 8. 20061208 PREVIOUS EOTIONS ARE OBSOLETE G-212 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 3 BDNTINUATION SHEET W. COMMENTS semesters: A. Mission Description. This was a Recurring Navigator Quali?cation and Mission evaluation ?own on a local training sortie out of D?ull AFB. NE. The flight profile Consisted of ore-flight. deparltire. air refueling. recon orbit area. transition and lending. The examines perlormecl and was evaluated on mission planning. pro-?ight. checklist procedures, general navigation, alr refueling procedures. recon orbiter-ea procedures. and transition. Discrepancies. None. G. Recommended Additional Training. None. D. Additional Comments- Commenoable. Area 3. CREW RESOURCE MANAGEMENT COORDINATION. Did a grestjoo providing backup to the pilots during critical phases oflilght. 'Commendahle. Area 23. RECONNAISSANCE ORBIT AREA PROCEEDURES Multiple timing problems were handled with no issues and perfect execution Requisites and flight satisfy all renuirements lorlhe Nevrgelor position on and Tit-1358M aircraft. REVIEWING REMARKS: None. APPROVING REMARKS: None. ADDITIONAL REVIEWS: None. AF FORM 8, 20061203 RC-135 V, 64?4848, Class A, 30 April 15, AFSAS #739726 DATE COMPLETED CERTIFICATE OF AIRCREW QUALIFICATION 13 Dec 12 I. EXAMINEE IDENTIFICATION II n1 fIm mama RANK EL.GIBILITY PERIOD [MIshap NaVIgatorORGANIZATDN AND LOCATION ACFTICREW POSITION 343 RS. AFB. NE RC-135V IMN II. QUALIFICATION GROIND PHASE FLIGHT PHASE EXAMINAYIONICHECK DATE MISSIONICHECK DATE Closed Book Open Book Instrument 05 Dec 12 94 QUALIFICATION LEVEL ADDITIONAL TRAINING QUALIFIED UNOUALIFIED DUE DATE ADDITIONAL TRAINING COMPLETED 1 MA NM EXPIRATION DATE OF QUALIFICATION CERTIFVING OFFICIAL RANK AND SIGNATLRE DATE ORGANIZATION May 1? MIA RESTRICTIONS EXCEPTIONALLY QUALIFIED COMMANDER-DIRECTED DOWNORADE (Emma Comments on Back) IEprm In Comment: on [Emlyn In Comoms on new CHECK TYPED NAMEAND RANII ORGANIZATION a i SIGNATURE DATE I FLIGHT EXAMINER .1 '1 DEUL I 343 a I: VB FINN. APPROVING OFFICER a 55 OG/cc $1 J4 A [j I CERTIFY Ir-al I nave been briefed and understand me acIIon bemg Iakeu Ims dale. DATE NAME AND GRADE OF EXAMINEE gem-mas [Mlshap NaVIgator] 0 MAR I3 WW, AF FORM 8, 20061208 FREvous EDITIONS ARE G-214 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 3 CONTINUATION IV. DMM ENTS REMARKS: IOl?futt AFB. NE. The flight pro?le consisted of ore-?ight. departure. rendezvous, navigation leg procedures. transition and landing. The exeminee performed and was evaluated on pre?ighl. checklist procedures. general navigation. rendezvous procedures. recon orbit. and transition. B. Discrepancies. None. C. Recommended Additional Training. None. D. Additional Comments. Requisites and flight satisfy all requirements tor the Navigator position on and TIC-1351 aircraft. REVIEWING None. APPROVING REMARKS: None. ADDITIONAL REVIEWS: None. iA. Mission Description. This was. a Recurring Navigator Quali?cation and Mission evaluation flown on a local training sortie out of AF FORM 3. 29061293 RC-135 V, 64?4848, Class A, 30 April 15, AFSAS #739726 DATE 00M LETED CERTIFICATE AIRCREW QUALIFICATION :9 Sep 11 I. EXAMINEE IDENTIFICATDN NAME II Fig! Inillnh RANK SSAN ELIGIBILITV PERIOD [Mishap Navngator] cm Jul Dec ,1 ORGAN2ATION AND LOCATION Acmcnew POSITION 343 RSIDOT. OffuII AFB. NE IMN memo PHASE FLIGHT PHASE DA It OW MMIONCHECK Closed Book Open Book InslrumenI 28 Sep 11 92 QUALIFICATION LEVEL ADDITIONAL TRAINING QUALIFIED UNGUALIFIEO DUE DATEIS) DATE ADDITIONAL TRAINING COMPLETED 1 NIA i NIA EXPIRATION DATE OF QUALIFICATION CERTIFYING OFFICIAL RANK AND SIGNATURE DATE ORGANIZATION Feb 13 . RESTRICTIONS EXCEPTIONALLY QUALIFIED COMMAN DER-DIRECTED DOWNGRADE . (Explain Came: on Jack) [Explm In on Dado rEprun Coma-nu on Back) cuter. TYPED NAME AND RANK ORDAIEATDN 8 SIGNATURE DATE I FLIGHT EXAMINER 1 343 Oc+ REVEWING OFFICER 2 343 RSIDO '4 at I I FINAL awnovme omcea a 343 [j 9 M, CERTIFY Ihat I have been and undmtand the action being taken Ihls date DATE NAME OF EXAMNEE sun-A?? In: [Mlshap NaVIgator] QINHII AF FORM 8, 20061208 PREVIOUS EDITIONS ARE 055mm: G-216 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 8 CONTINUATIDH SHEET IV. CDMHEHTE emulnen'e REMARKS: A. Mission Description. This was a Recurring Navigator Quali?cation evaluation ?own on a local training sortie out of other AFB. I NE. The ?ight pro?le consisted of pro-flight. departure, air re?tellng. RivetJolnt orhit procedures, transition. and landing. The Evaluatee performed and was evaluated on prefi'rght, checklist procedures. general navigation. air refueling procedures. Rivet Joint omit procedures, and transition. Ground EPE was on Unscheduled Rudder de?ection and stat: trim runaway. Flight EPE was on changing the signal ampli?er. Discrepancies. None. G. Recommended Additional Training. None. Additional Comments. Comrnenclable. Area 2. Mission Planning. Expertly replannerl the mission in an hour, then replanned again when the mission pro?le changed 15 minutes prior to engine start. Guaranteed mission success for all crew members with skillful mission planning. This evaluation satis?es all requirements for the navigator position on the and 355M. AF Fortrul a, 2ooe12rm (REVERSE RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 8. 20061208 PREVIOUS EDITIONS ARE OBSOLETE G-218 CERTII .TE OF AIRCREW QUALIFICATION DA comm? 25 Aug 10 I. EXAMINEE NAM: no Finn MIMI. mum RANK BSAN PERIOD Ishap NaVIgator LT MA ORGANIZATION AND LOCATION POSITION 343 Rs, 0mm AFB. NE RC-135V IMN QUALIFICATION snow!) PHASE FLIGHT PHASE EWNAIIONCMECK DATE 6W DATE SPOT 25 Aug 10 QUALIFICATION LEVEL AnnmoNAL DUE DATE ADDITIONAL TRAINING 1 NIA NIA EXPIRATION DATE OF OUAUFICATION OFFICIAL RANK AND SIGNATURE DATE ORGANIZATION EXCEPIIONALLY QUALIFIED DOWNGRADE El (Em-m Comments on Back) (Emma In Dammit Back) In Comma on man CERTIFICATION cage! TVPEII AND RANK ORGANIZATDN 8 I SIGNATURE DATE I II I FLIGHT EXAMINER 343 I I 29 304% [0 REVIEWING OFFICER 343 RSIDOT 2 12 3 Ham 0 FNALAPPROVING OFFICER 343 RSICC 3; DO 56? I I CERTIFY ma! I have been briefed and unamtand the action baing Iauan dale. DATE NAME GRADE OF EXAMNEE su [MIshap NaVIgator] I RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 8 SHEET W. COMMENTS EXAMIN RE MARKS: A. Mission Description. This was a NoNoiice Navigaior evaluation flown on a local training sortie out of UfiuttAFB NE. The ?ight profile consisted of pre?flihi. departure. rendezvous, navigation leg procedures. iransiilon. and landing. The evalualee performed and was evaluated on preilighl. checklist procedures. general navigation. rendezvous procedures. navigation leg procedures. and transition. Ei. Discrepancies. None. C. Recommended Additional Training. None. .D. Additional Comma-rim. None AF FORM 3, 20!}51208 RC-I35V, 64-4848. Class A, 30 April 15, AFSAS #739726 OF THE AIR FORCE 34D RECONNAISSANCE SQUADRON (ACC) FORCE BASE NEBRASKA 10 \m i 2 FOR RECORD FROMForm 8 Discrepancy 1. Additional Comments In Section IV block shnuld rend ?Requisites and Flight satisfy. all chuiremcms for the Navigator position on the RC-13SS I and TC aircra?." 3. Pin?: llu?s MFR in Section II of members FEF above affected Penn 8. 343 G-220 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 DATE CERTIFICATE OF AIRCREW QUALIFICATION ?mg? 04 May 10 I. EXAMINEE IDENTIFICATION - ?um I m? RANK 85AM ELIGIBILITY PERIOD [MIshap NaVIgator] 1LT Fewul ORGANIZATION AND LOCATION ACFTICREW Posmou 343 RS. 0mm AFB. NE RC-135V IMN ll. QUALIFICATION GROUND PHASE FLIGHT FEE EXAMNATIONICHECK DATE emu: MISSIONICHECK Closed Book 04 May 10 36 QUAL 14Apr10 Open Book Inslrumenl 04 May 10 88 QUALIFICATION LEVEL ADDITIONAL TRAINING QUALIFIED UNOUALIFIED DUE DATEISI DATE ADDITIONAL IRAINING COMPLETED 1 NIA NIA EXPIRATION DATE OF OUALIFCATDN CERTIFVING OFFICIAL RANK AND SIGNATURE DATE . ORGANIZATION Sep 1 . RESTRICTIONS - - I EXCEPTIONALLY OUALIFED DOWNGRADE l?l (am In Gunman on Back) I I (Explain Comm/II: on sea) Iemwn In Cum: on w) TYPE) NAME AND RANK ORGANIZATION 1. SIGNATURE DATE mom EXAMINER 343 RSIOSKR I II 16 u! I REVIEWING OFFICER 343 RSIDO -- FINAL APPROVING OFFICER 343 Rs/cc 3 mm) I CERTIFY um I have been Mama and unoemand Ihe awon being taken IhIs data. one MEI) NAME AND GRADE or EXAMINEE 5mm In; A [MIshap NaVIgator] 4 d' I.) I AF FORM 8, 208 PREVIOUS somons ARE OBSOLETE G-22 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 3 CONTINUATION SHEET IV. GU MMENTS REMARKS: A. Mission Description. This was a Recurring Navigator Quall?tion evaluation ?own on a local training sortie out oi G?utt AFB NE. The flight pro?le consisted of ore-flight. departure. rendezvous. navigation leg procedures. transition. and landing. The evaluate-e performed and was evaluated on preflight. checklist procedures. general navigation. rendezvous procedures. navigation leg procedures. and transition. .3. Discrepancies. None. C. Recommended Additional Training. None. D. Additional Comments. Requleltee and flight satisfy all requirements for the Navigator position on the aircraft I AF FORM 3. 20051203 (REVER 64?4848, Class A, 30 April 15, AFSAS #739726 DATE 0 PLETED CERTIFICATE or AIRCREW QUALIFICATION 04 Feb 09 I. EXAMINEE IDENTIFICATION NAME (LEM. FITSL Middle halal) RANK ELIGIBILITY PERIOD [Mishap Navigator] IIT NIA ORGANZATION AND LOCATION 333 ms. 0mm AFB. NE Rc-Iasv IMN II. QUALIFICATION GROUND PMSE FLIGHT PHASE MIMI GRADE DA I 2 Closed BOOK 24 NOV 03 100 INIT QUAL 04 Feb 09 Open BOOK Instrumenl 02 Oct 08 100 OUNJFICATION LEVEL ADDITIONAL TRAINNG QUALIFIED UNOUALIFIED ous omsIsI one ADDITIONAL COMPLETED I NIA NIA EXPIRATION DATE OF OFFICIAL. RANK AND Jul 10 ORGANZATON URE DATE RES QUALIFIED COMMANDER-DRECTED El [Exclam Common: on Back: (Emma Comments on Back) (Em-m Comments on Back) TYPED um: mu rum onemzmou menu-nae m1: FUGHT EXAMINER 338 CTSIDOF I IE FEB on] REVIEWING OFFICER APPROVING orncen 338 crs/cc a I CERTIFY Inal Ihave been named and undeIsIand the . DATE men NAME mo GRADE 0F EXAMINEE i [Mishap Navigator] If." AF FORM 8. 20061208 PREVIOUS EDITIONS ARE OBSOLETE G-223 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 8 BONTINLIATIDH IV. GDHMENTS REMARKS: A. Mission Description. This was an Initial Navigator Quali?cation evaluation flown on a local training sortie out of Offutt AFB. NE. The flight pro?le consisted of ore-flight. departure. recon orbit area procedures. rendezvous. alternate landing gear extension. transition and lending. The evaluatee performed and was evaluated on preliighl. checklist procedures. general navigation. rendezvous procedures. recon orbit area procedures. alternate landing gear extension. and transition, E. Discrepancies. None. Recommended Additional Training. None. D. Additional Comments. Requisites and ?ight satisfy all requirements for the Navigator position on and airmaft. Reviewing Officer's Remarks: Approving Of?ce r'e Remarks: AF FORM 3, RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.3.2. AF FORM 942 OF EVALUATION Fim Middle him [Mishap Navugator] ?3:5 DATE QUALFICATION acmcasw 2:5 one ounmcmou POSMON COMPLETED LEVEL POSI EVALUATION LEVEL ACC RC-135V INIT OUAL 04 Feb 09 1 Inn-at Revlon 343 Rs 05-May 09 nc-usv mm cum. 04 May ?0 1 vac-135v IMN NIN SPOT 25 Aug 10 1 RC-135V QUAL 29 Sep 11 I RC-135VIMN QUALIMSN 13 Dec12 1 Periodic Review 13 Dec 13 RC-135VIMN OUALIMSN Fovrn 942. 20061208 PREVDUS anmons ARE OBSOLETE 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.4. CAPT [Mishap Raven 1] AF FORM 85 (MR1) DATE CERTIFICATE O. AIRCREW QUALIFICATION I. EXAMINEE IDENTIFICATION NAMF IlaIl Ml?dll mun RANK SEAN ELIGIBILIIV PERIOU [MIshap Raven1] Cap, Apr - Sep 14 AND LOCATION POSII ION 343 RS. AFB. NE PIC-135V IIE II. QALIFICATION GROUND PHASE FLIGHT PHASE EXAMINATIONICHECK 0M: GRADE MSSIONICIECK DATE Closed Book Open BOOK 1? 80914 94 EPE 12 Sep 14 I QUALIFICATION LEVEL ADDITIONAL TRAINING UNOUALFIED DUE DATEI5) DATE ADDITIONAL TRAINING COMPLETED 1 NIA NM EXPIRATION DATE OF QUALIFICATION OFFICIAL. RANK AND SIGNATURE DATE ORGANIZATION Feb 18 RESTRICTIONS CI (Emma 6mm an Bum Cl OUAL IFIED {Explam HI Caninme at any COMMANDER-DIRECT ED DOWNGRAOE Exam HI Conmonn vn 8am CERTIFICATION CHECK NAME AND RANK ORGANIZATION I SIGNATURE DATE EXAMINER 1 343 RSIDOW a ?0 Feb ?5 OFFICER APPROVING OFFICER a 343RS/cc - 24Feb15 I CERTIFY Ihal I have been landed and understand Ihe ac IIon banng taken IN: daIe DATE NAME AND GRADE 0" EMMINEE 26 Feb 15 [Mlshap Raven1] 1343 RSIDOS 2am SIGNATURE [Mishap Raven1] AF FORM 8, 20061208 PREVIOUS ARE OBSOLETE G-226 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 3 SHEET W. COMMENTS REMAFEKS: I IA. Mission Description. This was a Recurring instructor Tactical Coordinator Quali?cation and l'u?ssion evaluation flown on a local training sortie out ol Oflutt AFB. NE. The flight profile consisted of pro-?ight. takeoff, air retooling. on-welcn. off-watch. and landing. The exeminee performed and was evaluated on mission planning. checklist procedures. coordination. operation. and data collection recording. instructional toms was on Bill Diff Cert B. Discrepancies. 1 GFGUHG. NONE IC. Recommended Additional Training. None. 2 Flight. Area 13 Employment - Cl- Debriefed. Radio Doe-rations in. Additional Comments. Requisites and ?ight satisfyr all requirements for the instructor TC position on aircraft. REVIEWING REMARKS: None. IAPPROVING REMARKS: None. ADDITIONAL REVIEWS: None. AF FORM 3. 20061208 (REVERE. RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.4.2. AF FORM 942 RECORD OF EVALUATION Firs! Initial) [Mishap Raven 1] 55?" ACFTICREW 72:5 mm: ouwncmou ACFTICREW "3:5 DATE ouwncmou POSITION EVALUAUON COMPLETED LEVEL POSITION COMPLETED LEVEL ACC RC-135VIME 11m QUAL 24 Jan 11 1 Innlal Review 343 RS 07 Feb 11 omumsw 19 Dec 11 1 Rc-135vme cumsu 7 9.1. ?mm mm 1mm 15 1 ir- 155V/r?; I AF Form 942. 20061208 PREVIOUS EDITIONS ARE G-228 G2.4.3. TRAINING RECORDS V, 64?4848, Class A, 30 April 15, AFSAS #739726 mums SUMMARY AND chseour REPORT 4 STUDENTS NAME I RANK CLASS NAME I RANK [Mishap Raven 1] Cam MA NUMBER OF INBTR DAT: ENTRY DAT: sonnet: TOTAL DAYS AIRCRAFT COURSE RC-1 35 Baseline RC-135VNV swo 1 25mg? 4 25?Aug'? 1 1 1 Diff Quai Baseline 11 OVERALL PERFORMANCE. WEAKNESSES. ETC. Capt completed all training requirements to be certified on Baseline 11 aircraft. Training Summary: Capt [MR1laccomplished a PGOT/Classroom training event and has completed the training program for Baseline 11 Diff Qualifacation SIGNATURE G-229 OPERATIONS OFFICER SIGNATURE V, 64?4848, Class A, 30 April 15, AFSAS #739726 G2.5- [Mishap TBCIICBI Coordinator] G2.5.1. AF FORM 85 CERTIFICATE OF AIRCREW QUALIFICATION DATE COMPLETED 22 Jan 14 I. EXAMNEE IDENTIFICATION NAME (um. rim. Middl- RANK SSAN ELIGIBILITY PERIOD mi Nov 13 - Apt 14 ORGANIZATION mo LOCATON POSITION 38 RS. AFB. NE FIG-135V (IE "4 QUAMGAJIPE GROUND PHASE FLIGHT PHASE EXAMINAIIONICMEGK DATE GRADE MISSIDNIGHECK CIosod Book Open Book QUALIFICATION LEVEL ADDITIONAL QUALIFIED UNOUALIFIED DUE DATEIS) DATE ADDITIONAL TRAINING COMPLETED I NIA EXPIRATION DATE OF QUALIFICATION CERTIFYING OFFICIAL HANK AND SIGNATURE DATE ORGANIZATION Jun 15 MA FIESIRICI IONS EXCEPTIONALLY QUALIFIED COMMANLEFI-DIRECTED DOWNGFIADE (Ema arr-mums Bark) (Ew Gammon on and) (5mm In Cam-us on Back) etigcu' TYPEO NAME AND HANK ORGANIZATION I swam: DATE EXAMINER I 38 FISIADO El . 23 Jan 14 REVIEWING OFFICER 2 38 R5100 31 Jan 1a FINAL APFROVING OFFICER 3 35 85/CERTIFY that I have been un?efad and understand the action bean Iaken this dale. DATE ITYPEDINAME AND GRADE OF EXAMINEE SIGNATURE FORM 8. 20061208 PREVIOUS EDITIONS AHE OBSOLETE. G-230 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 hF FORM 8 SHEET IV. CDM MENTS ExMIM?E?s?n?inin KS: A. Mission Description. This was a Recurring hotmoior Tactical Coordinator Quali?cation evaluation flown on a local training audio out oi Gl'lutt AFB, NE. Tho flight pro?le consisted oitokoolf. {an-watch. oil-watch, and landing. The oxaminoe po?ormod and was oraluated on mission planning. checklist coordination, equipmon?s ysiom operation. and data collection recording. Inoiruotional {onus was on signal recording. B. Discrepancies. None. I3. Flecomrnended Additional Training. None. D. Additional Comments. Commonoablo, Area 4. Emergency Procedures. Superior handling oi fumes Commondablo. Area 8. Coordination. Demonstmiod excepiional coordination during hag drag and fomoo EP. REVIEWING REMARKS: None. REMARKS: None. MDITIONAL REVIEWS: Smoke and forms EPE was verbally evaluated. Floquis'rtes and flight all requirements lot the Instructor TC position on the inc-135 VM. AF FORM 3. 20051263 (REVERSE RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.5.2. AF FORM 942 RECORD OF EVALUATION mums. 55m 73:5 DATE ACFTICREW ?6:5 DATE ouwncmou POSITION EVALUATION COMPLETED LEVEL councno LEVEL ACC Review 356 09 Jul 12 CTS RC-135V IIE RQ QUAIJMSN so Nov 12 I RC-135V ne QUALIMSN 22 Jan :4 Inmal Review 343 RS 07 Apr 14 AF Penn 20061208 PREVIOUS EDWIOPE A5 OBSOLETE 64?4848, Class A, 30 April 15, AFSAS #739726 G2.5.3. TRAINING RECORDS TRAINING ACCOMPLISHMENT AND PROGRESS REPORT NAME (Last, First) RANK NAME RANK DATE Maj 09 Jul 14 SORTIE NUMBER AIRCRAFT TYPE DURATION OVERALL GRADE FMT 5?6 Todays instruction was a guided discussion which provided an overview to mission aircraft including compartment layout and capabilities. In addition, OWS upgrades including emphasizing new functionality and how to accomplish current requirements with new increased communications capabilities, Digital SIGINT System (operator customizable settings, RAID. LAN and increased processing capabilities), and SHAWNA system. emphasizing new functionality and how to accomplish current requirements with the new system. Maj had the opportunity to setup the BL11 Operator Workstation and use the USS/Database, as well as set up and employment of the D88 and other upgrades on an FMT. SIGNATI Int: SIGNATURE G-233 G2.6. SRA G2.6.l. AF FORM 85 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 Engineer 1] [Mishap Ailbome Systems DATE COMPLETED CERTIFICATE OF AIROREW QUALIFICATION 15 Jan 15 I. EXAMINEE IDENTIFICATION me man. Hm Inman mum SSAN ELGIBILITY szoo gm Aug 14 Jan 15 ORGANIZAIIDN AND LOCATION ACF ncnew POSI now 343 RS. AFB. NE PIC-135V II. OUAUFJCATIDN GROUND mg; FLIGHT Pugs EXAMINATIDNCHECK DATE GRADE MISSIONICHECK DATE CIosed Book 06 Jan 15 96 OUALIMSN 15 Jan 15 oven Book OUALIFIOATIGI LEVEL ADDITIONAL TRAINING QUALIFIED UNOUALIFIED DUE DATE ADDITIONAL TRAINING COMPLETED NM EXPIRATION DATE OF QUALIFICATION CERTIFYING OFFICIAL. RANK AND SIGNATURE DATE ORGANIZATION Jun 16 NM Resmcnons EJICEPIIQNALLV OUALIF IED COMMANDE mmREmeo If Comma" on Ham mm? In Comments 0? Ham Ibum In common" on Emu Ill. CERTIFIQATION CHECK TYPED NAME AND RANK ORGANIZATION 8 SIGNATURE DATE II I FLIGIIT EXAMINER 1 343 [j - 15Jan 15 .4 REVIEWING OFFICER LI Cal 343 RSIDO K4 [j ?5 ?5 I HNAL APJROVINGOF- mean I a 343 RSICC - 26 Jan I5 I I CERTIFY IhaI have been DneIed and undersland Ihe awon being Iaken IhIs dale DATE ITYPED NAME AND GRADE 0F EXAMINEE SIGNATURE 27 Jan 15 I I, 34.1 AF FORM 8. 20061208 PREVIOUS EDITIONS ARE OBSOLETE RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 nF FORM a CONTINUATION SHEET IV. commems REMARKS: A. Mission Description. This was a Recurring Airborne System Engineer 3 Quali?cation and Mission evaluation ?own on an HHCI sortie out of Elliott AFB. NE. The flight pro?le consisted oi ore-Ilighi. takeoff. eir refueling. on-wetch. off-watch. and landing. The exeminee performed and was evaluated on mission planning. procedures. CRMl?crew coordination. equipment and system IimoWIodge. and maintenance and troubleshooting. B. Discrepancies. Ground. None 2. Flight. Area ?12. COMMUNICATIONS. LOSS. AND REPORTS - Debrioied. All loge. reports. media. and forms required were completed with minor omissions which did not. significantly impact the planned mission. IC. Recommended Additional Training. None. D. Additional Comments. Requielles and ?ight satisfy all requirements for the ASE 3 position or: RCI35VM aircraft. REVIEWING REMARKS: None. APPROVING REMARKS: Mene. REVIEWS: None AF FORM 8, RIDE-1 2H3 (REVERSE RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.6.2. AF FORM 942 RECORD OF EVALUATION . .. . ACFTICREW ??25 DATE QUALIFICATION ACFTICREW "0:5 DATE OUAUFIOATION POSITION EVALUATION couaneo LEVEL Posmow EVALUWON comma en LEVEL Acc IMK INIT DUAL 20 Jun 11 1 Initial Review 343 RS 06 Sep 11 RC-135V IMK omumsn 29 Aug 12 2 RC-135V IMK OUALIMSN 27 Aug 13 1 KING I AF Form 942. 200812? PREWOUS EDMONS OBSOLETE 64?4848, Class A, 30 April 15, AFSAS #739726 G2.6.3. TRAINING RECORDS TRAINING ACCOMPLISHMENT REPORT acuuvnv As: a Gull Baseline 11 10.1111 15-Jul Flight Hour- TU DURATION 10 Menu IION 21.3 100.00% ?0 3 5322-00001: 1 1o 1 .110 8822-1300044 syum out 9. Check ESBZ2rccai1nrsum3.0 3.0 UplDown and Foam?: "maven 0 0.0 1 2.0] 1 3.0 2 3.0: 3.0 ?01681122 001511151111011 Amos SleerableBeamAmy 310 3.0 'mquoncy Range 3.2.0! 1 :10 a 3.0 30 CN105 comers 3.0- 3.0 oquwandoonuomunuem Electmnic Form 45 (30 Jan 12) G-237 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 calm: and lramfar murn la teal AWG 10 wauaron'n al'lnr Shawna Int .E??r?nmnl??unb?ulanon was unsafe. a rank - or - Performad at ASE 3 Electronic Form 4513DFWIEES reg-amber: 5 madam: panama Ia mm, but required pm?ciancy larval 15 no! achlawd Frn?danl; achiwau the rewind plu?danw lava] EISHF - Non-e?mamluuen: non-pmqraasiuh twmulalfva low PLREJ NEIDTH - Nan-unwiwmwm animate!? fut mam. malfunctinn. 64?4848, Class A, 30 April 15, AFSAS #739726 PROGRESS STUDENTS NAME (Last. First) RANK NAME I RANK DATE 24 Jul 14 SUN I ll: NUMBER AIRCRAFT TYPE DURATION OVERALL GRADE RIVET JOINT M4 Baseline 11 7 0 Pro?le: 1 his was an local training some out at (mutt AFB. Mission Planning: attended the mission planning briefs as well asthe alternate gear brief. Premght: ran the pre?ight checklist with no Issues. System Boot/ lnit: ran the system boot and init with no problems. On-Wateli: ONce we were on-watch kept an on the system while we went through required tasks and We had some issues with the being unable to be controlled. and [troublesth and System Shutdown: did the system shutdown with no errors noted. Forms Debrief: wrote up the CANIOS issue in the forms and the green book Strength/Weaknesses: did pretty well on tlus night. He knew the ansWers to nearly all the questions asked with only a little help from the ETMs He was able to preform the required tasks with no di??iculty Recommendations: Dll?f. Cert. complete G-239 G2.7. MSGT G2.7.1. AF FORM 85 V, 64?4848, Class A, 30 April 15, AFSAS #739726 Supervisor] [Mishap Airbome Mission (MAMS) DATE CERTIFICAT AIRCREW QUALIFICATION 24 Jan 14 I. EXAMINEE IDENTIFICATION NAME (L882. Middle lmlIl) RANK ELIGIBILITY PERIOD M89 NM ORGANIZATION AND LOCATION ACFTICREW POSITION 97 IS. AFB. NE RC-135V IIO QUALIFICATION GROUND PHASE FLIGHT PHASE I: MMIMI IWCHECK DATF GRADE DAT Closed Book 17 Jim 14 100 R0 QUALIMSN 24 Jan 14 Open Book QUALIFICATION LEVEL ADDITIONAL TRAINING QUALIFIED DUE DATE ADDITIONAL TRAINING COMPL ETED 1 EXPIRATION DATE OF OUAI IFICATON CFPTIFYING OFFICIAI RANK AND SIGNATURE DATE ORGANIMTION Jun 15 RESTRICTIONS EXCEPTIONALLY QUALIFIED COMMANDER-DIRECTED DOWNGRADE (Exam: on Back) (51mm Gunman: on Bank) (Ewan: comm-nu un Buck) CHECK 8 1' TYPED NAME MD RANK ORGANIIATDN SIGNATURE DATE 5 i a I FLIGHT EXAMNER I 97 )2 30 Jan 14 REVIEWING OFFICER 2 97 06 Feb 14 FINAL APPROVING OFFICER 3 9r ISICC [j 07 Feb14 I CERTIFY I have been bneIod and understand the salon being Iakan this data. ON I: Iwwn mm: man name or 10 Feb 14 AF FORM 8, 20061208 PREVIOUS EDITIONS ARE (ESOLETE G-240 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM SHEET IV. COMMENTS A. Mission Description. This was a Reouali?t?alion Instructor Airborne Mission Supentisor Quali?cation evaluation ?own on a local sortie out of ?0th AFB. NE. The ?ight pro?le consisted of takoo?'. on-watoh. off-watch. and landing. The evaluateo performed and won evaluated on mi?ton planning, ohooltlist procedums. CRMlorow coordination. operation womstation utilization. communication systems. and crew management. Instructional focus was on communications: equipment. setup and usage, 3, Discrepancies. None. 13. Racormnended Additional Training. Nona. D. ?dditlonal Cour-rents. Commendahlo. Area 2. Mosinn Planning. Vary thorough and professional mission planning session. A benchmark for Dflutt training suntan. Commendable. Area 23. Tasking and Reporting. Excellent jot) explaining tasking to the crew. BTW scenario was handled well. Great job wiln crew coordination and anticipalicn of what was hapoening. Reouali?ootion was nonesoary one to loss. ofgtral'r?oation. Requisitos and flight satisfy all requirements for the Instructor AMS position on . nc-tasvtw aircraft. REVIEWING REMARKS: None. APPROVING REMARKS: None. ADDITIONAL Nona. AF FORM 8. 200812'33 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.7.2. AF FORM 942 RECORD OF EVALUATION mus First mm mm? 35." 73:5 one omncmou ACFIICREW DATE QUALIFKSATION POSITION EVALUATIW COMPLETED LEVEL MSW EVALUATION COMPLETED LEVEL ACC Inmal Review 97 IS 01 Aug 07 Etc-1357 mn? cum??EN 09 May of 1 mo Ro-1asv mo INIT ouaumsu 10 Mar 09 a Rc-135v INIT QUAUMSN 20 Mar09 1 IMO RC-135V Ilo INIT INSTR 01 Jul 10 1 RC-135V IIO 23 Nov 10 1 (QUAUMSN Rc-135v no QUALIMSN 31 May 12 1 Potiodic Review 24 Sep 12 Periodic Review 19 Feb 13 IIQ RQ QUALIMSN 24 Jan 14 1 Ponodlc Review 15 May 14 AF Form 942. 20061208 REVDUS eomous AREOQSOLETE V, 64?4848, Class A, 30 April 15, AFSAS #739726 G2.7.3. TRAINING RECORDS TRAINING SUMMARY AND CLOSEOUT REPORT RANK CLASS NAME IRANK NUMBER OF INSTR one 91th on: comma TOTAL AIRCRAFT COURSE R0135 Baseline AMS 1 1 11 um Cert Baseline 11 OVERALL PERFORMANCE, WEAKNESSES, ETC. Summary:[MAMS] accomplished and a POST event and has completed the training program for Baseline 11. has completed all lralning requirements to be certi?ed on Baseline 11 airctaft. SIGNATURE I omcsn SIGNATURE G-243 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.8. SRA (MCO) G2.8.l. AF FORM 85 DATE COMPLETED CERTIFICATE Or AIRCREW QUALIFICATION 14 Mar 14 I. EXAMINEE IDENTIFICATION NAME ILJIOI. ?rst MIddIe RANK 88AM ELIGIBILITY PERIOD A1 NM ORGANIZATION AND LOCATION ACFTICREW POSITION 338 075. OIfulI AFB. NE RC-135V IMO BROVIND PHASE FLIGHT PHASE enwmnawcnecx DATE amt.- one Closed Book 07 Mar 14 100 INIT 14 Mar 14 Open Boot QUALIFICATION LEVEL IDDITIONAL TRAINING QUALIFIED UNQUALIFIED DUE DATEISI DATE ADUTIONAL TRAINING COMPLETED 1 NIA EXPIRATION DATE OF QUALIFICATION OFFICIAL. RANK AND DATE ORBANZATION Aug 15 RESTRICTIONS EXCEPTIONALLY OUAUFIED DOWNGRADE (Emma In Cum?: on Mum Ian!? comm-m: on Back) 05mm on on anew 7 CHECK TYPE) NAME AND RANK 8 I SIGNATURE DATE i I [mam EXAMINER 1 338 . 21 Mar REVIEWING OFFICFR 338 CTSIDO 27 Mar14 FINAL APPROVING OFFICER 338 CERTIFY he! I have baen brIofed and understand Ihe acuon being Iaken Ihis date. one ITYPED NAME AND GRADE 0F EXAMINEE 31 Mar 14 MC 1 1.538 UfS/X?f?Hgm AF FORM a. 20061208 PREVIOUS EDITIONS ARE OBSOLETE. G-244 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM CONTINUATION SHEET IV. CQMMENTS REMARKS: A. Mission Description. This waa an initial Operator Quali?cation and Mission evalualicn ?own on a incal training some ml at DMAFB. NE. The ?ight pro?le consisted of takeoff. air refueling, cn-walch. of?watch. and landing. The examines performed and was cvaluaied on mission planning, chccidist procedures. CHM-brew coordination. operator utiliz a?an. graphics functions. and gcovlccalicn data. 3. Discrepancies. None. Recommended Additional Training. Nana D. Additional Comrnants. Requisites and ?ight 5311st all requirements for the CO pusi?cn on aircra?. REVIEWING REMARKS: None APPROVING REMARKS: Nona- ADDITIONAL REVIEWS: None. AF FORM 8, 2011612115 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.8.2. AF FORM 942 RECORD OF EVALUATION mama Firs! mm ma) 33m 13:5 one QUALIFICATION acmcnaw 732? one omuncmou CWLETCD lava. COMPLETED LEVEL ACC rte-135v mu omuusu 14 Mar 14 1 IMO I Imus? ns? 01 Apr Periodic Review 21 Jul 14 AF Form 9.2, 20061203 memos some? ARE 0mm: G2.9. SRA G2.9.l. AF FORM 85 [Mishap AiIbome Systems Engineer 2] RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 (MASEZ) AT .0 CERTIFICATE OF AIRCREW QUALIFICATION CW ,5 I. EXAMINEE IDENTIFICATION NAME (Last MIMIO RANK SSAN EUOIBILITY PERIOD Duc 14 - May 15 ORGANZATION AND LOCATION 343 RS. AFB. NE RC-135V IMK II. QUALIFICATION GROUND PHASE FLIGHT PHASE EXAMINATIOMCHECK DATL MISSIOMGHECK DATE Closed Book 11 Mar 15 96 OUALIMSN 08 Apr 96 Open Book QUALIFICATIOII LEVEL ADDITIONAI. TRAINING QUALIFIED UNQUALIFIED DUI: DATE ADDITIONAL TRAINING COMPLETED 1 MIA EXPIRATION DATE or QUALIFICATION CERTIFYINO OFFICIAL RANK AND SIGNATURE DATE ORGANIZATION Sep 16 RESTRICTIONS (swim In Common? on Saw Cl EXCEPTIONALLY QUALIFIED (Emmn In common on Bun COMMANDER-DIRECTED DDWNORADE (Elmo/n Comnunls an East!) II. CERTIFICATION DHEDK TYPED NAME AND RANK ORGANIZATION I SIGNATURE DATE II rLIem EXAMINER 1 I 55 OGIOGT [j 8 07 15 REVIEWING OFFICER 2 343 RSIDO 13 Apr 15 FINAL APPROVING OFFICER 3 343 RSICC 13 Apr 15 I CERTIFY that I have Deon onefed and undemand Iha ac?an being Iakcn daIe DATE NAME AND GRADE 0F EXAMINEE SIGNATURE 14 Apr 15 [an ?ammo AF FORM 8, 20061208 PREVIOUS EDITIONS ARE OBSOLETEA G-247 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 ILF FDRM BONTINUATIDN SHEET IV. COMMENTS REMARKS: A. Mission Description- This was a Recurrin Airoome System Engineer (ASE) 2 Quali?cation and Mission evaluation ?own IAW AFI 11-2RC-135V2. and the 55 GIG Evaluation Pro?le letter. The evaluation was conducted on a local sorlie ?own out of Offotl AFB. NE. The flight pro?le consisted of ore?flight. takeoff. eir refueling. on-watch. ofH-mlch. and landing. The examinee performed and was evaluated on mission planning. checklist procedunas. CRMi'crew coordination. equipmenl and system Knowledge. and mainlenance and troubleshooting. B. Discrepancies. None. 3. Recommended Additional Training. None. D. Comments. Reuuisiies and satisfy all requirements lorlhe ASE 2 position on RIC-1 ESVMF aircraft REVIEWING REMARKS: None. APPROVING REMARKS: None. ADDITIONAL REVIEWS: None. AF FORM B, 20051203 (REVERE 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 CERTII OF AIRCREW QUALIFICATION WE COMPLETED 12 Aug 14 I. EXAMINEE IDENTIFICATION NAME (Last. First. Inllil) RANK 33M ELIGIBILITY PERIOD 0 NM AND LOCATION AGFTICREW POSITON 343 Rs. AFB. NE RC-135V IMK IL QUALIFICATION FLIGHT ammnomcuecx on: cw: DATE SPOT 12 Aug 14 LEVEL ADDITIONAL TRAINING OUALIFIED UNOUALIFIED DUE DATEIS) DATE ADDITIONAI TRANING COMPLETED 1 NM NIA DATE OF QUALIFICATION CERTIFYING OFFICIAL. RANK AND SIGNATURE DATE ORGANIZATON NM NM RES TRICTIONS EXCEFIIONALLY QUALIFIED COMMANDER-DIRECTED DOWNGRADE (Elma-n In Canaan's on Back; I l?xplun Commems on Back) (Em-In I-I Commenu on Sun i CHEM TYPEO NAME AND RANK ORGANIZATION 1. SIGNATURE DATE I FLIGHT EXAMNER I 55 OSSIOST 19 N19 14 I A I REVIEWING OFFICER Va) 343 g] 19mm 14 APPROVING osncea 3 343 RSICC >CERTIFY that I have been bneleu and undersIand the sedan nemg taken this dale DATE TYPF NAMF Ann mumFORM 8. 20061 208 PREVIOUS EDITIONS ARE OBSOLETE G-249 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 3 comm ultimo? 3H an IV- COMMENTS REMARKS: A. Mission Description. This was a No-nolioe SPOT Airborne System Engineer (ASE) 2 evaluation ?own on a local some out of D?utl AFB, NE. The flight pro?le consisled of ore-night, takeoff. air refueling. onvwatch. off-watch. and landing. The examinee performed and was ailaluatod on EqUIpmeni/Publioalions. Bailey. Post?ighll'Debriof. and maintenance and troubleshooting. El. Disorepancies. 1. Ground. None 2. l-ghi. Area 55. Post IighirDeorief - 0-. Deoneled. Failed to make appropriate inputs into both the l'?ls and pass on book. Did not affect more success. IC. Recommended Additional Training. Nona El. Additional Como-rants- None REMARKS: None. None. ADDITIONAL REVIEWS: None. AF FORM E. 20951203 (R. ERSE) RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 CERTIFICATE OF AIRCREW QUALIFICATION DATE COMPLETED 03 Dec 13 I. EXAMINEE IDENTIFICATION NAM (Last. Muddlo Irina!) RANK 58AM ELIGIBILITV PER 00 A1 NIA ORGANIZATION AND LOCATION POSITION 338 CTS. 0mm AFB. NE MK II. QUALIFICATION 6&9;le PHASE FLIGHT PHASE EXAMINATIONCHECK DATE GRADE wssuomcnecx DATE Closed Book 27 Nov 13 96 IMIT QUAUMSN 03 Dec 13 Open Book QUALIFICATICN LEVEL ADDITIONAL TRAINING QUALIFIED UNOUALFIED DUE DATE ADDITIONAL TRAINNG COMPLETED 1 NIA CERTIFYING OFFICIAL. RANK AND SIGNATURE DATE EXPIRATION DATE OF ran/Aunt:an May 15 ORGANIZATION NIA CI REST RIC HONS EXCEPTIONALLY OUALIFED COMMANDER-DIRECTED DOWNGRADE AF FORM 8. 20061208 PREVIOUS EDITIONS ARE OBSOLETE. G-251 (Exam! In Comma. on um Cumulus on Buck) (Emma In Comments on Bock) CERTIFICATION cntou ME) NADAE AND RANK SIGNATURE DATE I mam EXAMNER 1 338 CTSIDOV I 30 Dac13 OFFICER 2 338 CTSIDO 02 14 FINPL APPROVING OFFICER a 333 07 Jan 14 I CERTIFY that I have bun briefed and understand he action being man this date. DATE TYFED NAME AND GRADE 0? EXAMNEE SIGNATURE 07 Jan 14 338 I RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 3 CONTINUATION SHEET IV. COMMENTS REMARKE: A. Mission Description. This Was an Initial Airborne System Engineer 2 Quali?cation and Mission evaluation flown en a local sortie I:iLit (if O?utl AFB. NE. The ?ight pro?le consisted of takeoff. Lin-watch. oft?watch. and landing; The examinee perfumed and 'was evaluated on mission planning. checklist procedures. coordination. equipment and system knowledge. and imaintenanee and troubleehooilng. B. Discrepancies. None. C. Recommended Additional Training. Mane. D. Additional Comments. Hequusilee and ?ight satisfy all requirements fur the ASE 2 position on aircraft. REVIEWING REMARKS: None. APPROVING REMARKS: None. REVIEWS: None. AF FORM 8, 2DDE1ZDB RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.9.2. AF FORM 942 RECORD OF EVALUATION (L181 Middle Inllidl acmcnew DATE QUAuncAnon ACFTICREW "6:5 out QUALIFICATION POSITION EVALUATION COMPLETED IEVEL POSITION EVALMTIW COMPLETED LEVEL ACC Rc-135v IMK mn' QUALIMSN 03 Dec 13 1 InmaI Review 14 14 RC-135V IMK NIN SPOT 12Aug 14 Goa/ms? n, AF Form 942. 20061208 PREVIOUS EDWIONS ARE OBSOLETE 64?4848, Class A, 30 April 15, AFSAS #739726 G2.9.3. TRAINING RECORDS TRAINING AND PROLJESS REPORT NAME (Last. First) RANK NAME RANK DATE 24 Jul 14 WMBER AIRCRAFT TYPE DURATION OVERALL GRADE M-1 Baseline 11 7.4 Pro?le: This was a local sortie flown out of O??un AFB. NE on AC 848. The ?ight consisted of pre?ight. system boot, system shutdowu. and post ?ight. Mission Planning: All briefs attended. Prenight: No en?ors noted coordinated with the ASE 4 to who would do each part of the checklist. System Boot lnlt: booted all the ASE 2 systems without any assistance. On-Watch: Once all the systems were up. was noti?ed of NABRE issues. He worked with the AMSIT to solve the issues. Alla troubleshoot NABRE. the: DLO had him assist with some link problems. used proper trouhlshoot techniques to narrow down the issue. A?er all systems wem we began covering the BL differences He was able to recall from memory all the dillcrences between systems. System Shutdown: No errors noted. Forms lDebriel?: made till the appropriate write-ups and dobricfcd the ground. came well preparw for the BL 1 ?ight. He used all his tesourccs to troubleshoot the systems that were having ptoblems Recommendations: has completed all the requirements for BL I I ASE 2 position. INGTDI CIRMATI _l G-2 54 64?4848, Class A, 30 April 15, AFSAS #739726 TRAINING ACCOMPLISHMENT AND PROLAESS REPORT NAME (Last, First) RANK RANK DATE 14 Jul 14 SORTIE NUMBER AIRCRAFT DURATION OVERALL GRADE G-1 Baseline 11 4.0 Pro?le: This a was an OGT on AC 848- This was the ?rst DQ event for . All ASE 2 and common academic slides were covered on I 1 Jul 14. On-Watch: followed the checklist and coordinated with the ASE 4 to bring the system up. Once everything was powered on we started going over the BLI changes. The topics covered were OWS, Maintenance. NAV TIME. LAN, Data Storage, ICS, JTIDS windows, and STE-RI. asked questions on the changes for the ASE 2 systems. Recommendations: Proceed to next event. Ih-nvu?n unmth A'l'l It?ll? G-255 64-4848, Class A, 30 April 15, AFSAS #739726 TRA.. . .NG ACCOMPLISHMENT REPL. . High! Hours 0.0 4.0 THANING LISTNG - Unwishcm- progress or moresaon Satishnory; prowess bu! uncured prol'cioncy level Is m! - PmncunL mnieved ma required prof-enemy Ievsl NEBNP - NMIeaNelstuoom non-progress!? (mmuacva km Non-aneuwe/wants no! comploIed lor wealhu. rralhamtbn. G-256 64?4848, Class A, 30 April 15, AFSAS #739726 TRAINING SUMMARY AND CLOSEOUT REPORT STUDENTS NAME I RANK CLASS NAME I RANK A10 NUMBER OF INSTR one emv DATE COMPLETE TOTAL DAYS AIRCRAFT COURSE R01 ASE 2 1 4 '1 Baseline 11 leferencc Cert (BL 11) OVERALL PERFORMANCE, WEAKNESSES, ETC. showed a strong desire to learn the new BL 11 systems He was able to use his knowledge of BL 10 to help with all the changes. has completed all required training and is certified to ?y the ASE 2 position on all Bl11 aircraft. I SPERATIONS OFFICER suenxrun: G-257 G2.10. TSGT G2.10.1. AF FORM 85 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 [Mishap Airborne Systems Engineer 3] (MASE3) TE we so CERTIFICATE OF AIRCREW QUALIFICATION 15 I. EXAMINEE NAME (Les! First, lam-I) RANK 85AM EUGIBLITY PERIOD Tsar NIA ORGANIZATION AND LOCATION POSITION 343 Rs, AFB. NE IMK QUAUFICATIQN . GROUND Pugs; mam PHASE EXAMINAYIONICHECK DATE GRADE DAIE NIN SPOT I1 Mar 15 LEVEL ADDITIONAL TRAINING uuaunm umouameu our: onus) DATE IRNNING COMPLETED 1 NIA NIA EXPIRATION DATE OF QUALIFICATION CERTIFYING OFFICIAL RANK AND SIGNATURE DATE NIA ORGANIZAIION NIA RESTRICTIONS EXCEPTIONALLV COWANDER-DIRECTED DOWNGRADE [Em-m Cam-rm on Back) (Emma In Commons: o? Bun) {5le In (roam-Mrs on Back) II. CERTIFICATION CHECK wweo um: mo RANK onemrzmou I snrmuas DATE 9 ii FLIGHT I 343 RSICAI REVIEWING OFFICER Ila] 343 30 Mar 15 I Anew-?um: 13:;ch Lt Cal 343 RSICC - 13 Apr 15 I CERTIFY than I have seen briefed and understand me scion being taken Ibis date DATE Trvpeo NAME AND GRADE 0F EXAMINEE SIGNATURE 14 Apr 15 'Sgr [m I AF FORM 8, 20061208 PREVIOUS EDITIONS ARE OBSOLETE. G-258 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM GDHTINIJITIOH SHEET Wi CDMMEN T5 REMARKS: - A. Mission Description. This was an Aimurne System Engineer (ASE) 4 Nu-Nutice Spot eUalLla?D? CUHUUCTBU 0? for 5' lanai training smile from Offui't AFB. NE. The examinee performed and was evaluated on publication usage. 15. Discrupancies. None. Recommended Additional Training. Mane. E). Additional Comments. None. REVIEWING REMARKS: None. APPROVING REMARKS: None. ADDITIONAL REVIEWS: Nnne. FORM 3, 20061an RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 DATE COMPLETED CERTIFICATE .A- AIRCREW QUALIFICATION 30 May 14 I. EXAMINEE IDENTIFICATION NAME Middla IrmlII RANK 53AM ELIGIBILITVPEFIOD 7ng ORGANIZATION AND LOCATION ACFTICREW posmm 338 CTS. AFB. NE RC-135V II. QUALIFICATION GROUND PHASE FLIGHT PHASE :xmwnowcnecn one came MIss-omcnm an: Closed Book 01 May 14 100 INIT 30 May 14 Open Book QUALIFICATION LEVEL ADDITIONAL TRAINING DUALIFIED UNOUALIHED DUE DAIEISI DATE ADDITIONAL TRAINING COMPLETED 1 MA .NIA I EXPIRATION DATE OF QUALIFICATION CERTIFYNG OFFICIAL, RANK AND SIGNATURE DATE Om 15 NIA EXCEPTIONALLV QUALIFIED (E:an cm: on Boer) RESTRICTIONS [bxpum Common on Eat? El com/mos R-DIRECTED DOWNGRIDE 15-0!? 0' Convent: on Back) CERTIFICATION CHECK we AND RANK ORGANIZATION momma: on: II EXAMINER 1 338 -- 02 Jun I4 REVIEWING OFFICER 2 338 - 10 Jun I4 FINAL APPROVING OFFICER 3 338 CTSICC 18 Jun :4 I CERTIFY that I have been brIeIod and understand the amen aeinu taken this data on: wrap NAME mo GRADE or EXAMINEE SIGNATURE 18 Jun -- 335 . AF FORM 8. 20061208 G-260 PREVIOUS EDITIONS ARE OBSOLETE RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM SHEET Ili?rr COMMENTS A. Mission Description. This was an ln'rlial Airborne System Engineer 4 Quali?cation and Mission evaluation ?own on a local sortie out oi thutt AFB. NE. The ?ight pro?le consisted of takeoff. air refueling, sin?watch, nt?walch, and lending. The examines performed and was evaluated on mission planning. checklist procedures, coordination, equipment and system knowledge. and maintenance and troublesmoting B. Discrepancies. None. in. Recommended Additional Training. None. 0. Additional Comments. Fleqmsites and ?ight satisfy all requirements tor the ASE 4 position on 35WW aircraft. REVIEWING REMARKS: None. APPROVING REMARKS: None. IADDITIDNAL REVIEWS: None IAF FORM 3, 20061208 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.10.2. AF FORM 942 RECORD OF EVALUATION NAME M. an MM. Inn/u) ACFTICREW ?3:5 one omuncmow acmcnew 78:5 DATE omuncmon DOSITION EVALUATION CWPLETED LEVEL POSITION COMPLETED LEVEL ACC RC-135V IMK INIT QUALMSN 30 May 14 1 Inmal Review 343 RS 05 Jun 14 5ch AF Form 902. 20061203 PREVIOUS EDITIONS ARE OBSOLETE RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 RECORD OF EVALUATION 33AM 73:5 DATE QUALIFICATION ?5:5 DATE mALanou POSITION comma-ran u:sz Poamou alumna? comma-ran LEVEL AMC Initial Revlow 18 Aug 05 C-37NMK INIT ounwsn 17 Dec as 1 Annuel Revlew 21 Dec 05 SPOT 05 (wins 1 0-37NMK NIN 3901' 15 Mei oa 1 Annual Review 07 Dec 06 c-ammx QUAumsn 04 May 07 1 Annual Review 04 Dec 07 cam/1K mu 03 Jul 03 1 (3-37le SPOT 09 Sep 08 1 Annual Revlew 02 Dec 08 $901 as May 09 1 C-37NIK QUAUMSN 03 Dec 09 1 Annuel Review 16 Dec 09 Annual Review 01 Dec 10 amumsn 0:1 May 11 1 Annual Review 14 Dec 11 C-37AIIK QUALIMSN 07 Jun 12 1 037nm um SPOT 10 01:1 12 1 Annual Remew 18 Dec 12 C-37AIIK 22 Nov 13 1 Annual Review 02 Dec 13 AF 912. 20051201 V, 64?4848, Class A, 30 April 15, AFSAS #739726 RECORD OF EVALUATION mus ma. was man s's'n TYPE YYPE DATE WALWICAIION TYPE TYPE OATE 0F COMB FTFD AR- 0? ETFD can? EVALUATION (um) I . EVALUATION Assigned 338 0* 06 2001 (ACC) l, I 1 I RC-13SW INrr QUAL 01 2002 (ACC) I Assegnea 45 RS 02 "av 2002 (ACC) 1 (ac-1355 INrr QUAL 16 Aw 2002 (45 RS) I I Annual Review 31 "at 2003 (45 RS) I O. 1 RC-13SS QUAL 02 Dec 2003 . (45 RS) vac-1355 mu 23 2004 (45 RS) . ml- Rc-13ss QUAL 12 Apr 2005 i (45 RS) AF FORM 942, 19961201 (EF-VZ) PREVIOUS EDITIONS ARE OBSOLETE G-264 64?4848, Class A, 30 April 15, AFSAS #739726 G2.10.3. TRAINING RECORDS WWGAGGOWLISHMENT REPORT ac-mww ASE 4 Diff can Buoan 11 Flight Hours 10.0 TD DURATION WIRING EVENTITASK 571m 55 06 Electronic Farm 45 (30 Jan 12) G-265 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 Wabsewer Bastions 55 GIG ElecIran'rc Form 45 (30 Jan 12} 64?4848, Class A, 30 April 15, AFSAS #739726 TRAINING Aeoowmsmenrmo'moegeasfnepom NAME (Last. First) RANK NAME IRANK DATE 10 Jul 14 SORTIE NUMBER AIRCRAFT TYPE DURATION OVERALL GRADE MA 8.0 3 Baseline 11 Pro?le; not changed. weakness were noted . Recommendations: Continue with training using Ground Power-On Trainers. This was a ground training academic event. All common and 4 speci?c slides were covered and additional questions were answered. This academic review is an initial introduction to the overall changes to the Baseline I aircra? and does not cover all tasking abilities or objectives that can only be taught on the aircra?. Due to the high experience level all topics were covered in a very expeditious manner as the fundamentals from Baslinc I0 have All systems were covered and a understanding ot'knowledge/theory was demonstrated to the targeted level for each subject. No SIGNATURE SIGNATURE 55 CG Form 44 G-267 64?4848, Class A, 30 April 15, AFSAS #739726 TRAIN monsoon. PLISHMENT AND PROGRESS REPORT NAME (Last, First) RANK NAME IRANK DATE 10 Sep 14 SORTIE NUMBER AIRCRAFT TYPE DURATION OVERALL GRADE M4 RIVET JOINT 10.0 8 Baseline 11 Profile: This was a HHQ some flown on 848 consisting of system pre?lght, power on and shutdown. Mission Planning: During mission planning, went over BL11 differences. Prefiight: completed preflight in a timely manor while working with the ASE 2 to complete the new combined checklist. System Boot Init: System power-on was completed in conjunction with the ASE 2. During system boot up we reVIewed some of the hardware and emergency equipment chanceslMASB] was able to tell me many of the BL11 differences from memory. On-Watch: During on watch was able to recall much of BL 11 differences while I added additional information sthis was along flight. He also showed me how to use the different AWP and RSTA windows during this time. System Shutdown: System shutdown was completed with minor deviations to the overall ASE checklist. Tool and software inventory was completed. Forms Debrief: No write ups for during this sortie. showed his growing knewledge in R1 operations. Recommendations: I recommend be PA 1 event. Continue to next training event. STUDENTS SIGNATURE SIGNATURE ll Signed I I11 Sep 14 55 06 Form 44 G-2 68 64?4848, Class A, 30 April 15, AFSAS #739726 STUDISIIXEESTAME (Last. First) RANK I NAME I RANK DATE 11 Sep 14 SORTIE NUMBER AIRCRAFT DURATION OVERALL GRADE 3.0 Baseline 11 Profile: This was a ground training academic event on aircraft 848 with and assisted run the ASE 5 preflight checklist coordinating with the ASE 2 to complete it. During we had power issue that delayed the overall system power one. We reviewed RJ system operations focusing on position, ows operations. Ian and systems setup. was able to recall much of the information discussed from last event. System Power on: assisted run the ASE 5 checklist coordinating with the ASE 2 to complete it. After the system was powered on we focused our training on software and under-glass computer operations. We covered AWP, RSTA, XMP and associated equipment Operations.[MASE3] was a good grasp of how the systems work together. is progressing well and ahead of schedule for BL11 difference training. Recommendations: Review and work on DRT, 055 and DS operations during next event. Continue with training using Ground Power-0n Trainers. STUDENTS SIGNATURE SIGNATURE IISigned I. I11 Sep 14 55 06 Form 44 G-269 64?4848, Class A, 30 April 15, AFSAS #739726 TRAINING ACCONIPUSHMENT ANo?pRooaess..ReeoRrr NAME (Last. First) RANK I NAME RANK DATE 12 Sep 14 NUMBER TYPE DURATION OVERALL GRADE RIVET JOINT M4 Baseline 11 3'0 Pro?le: poweron. BLIO and BL 11. This was a ground training academic event on aircraft 848. Recommendations: is BL 11 difference certified. Pre?ight: During preflight we arrived at the aircraft and nothing was setup, there was a miscommunication for the start times of the OGT. However once the power and air conditioning carts were hooked up, load software and run the ASE 5 checklist coordinating with another ASE 410 complete both sides of the system System Power on: System power on was uneventful with no checklist errors. During this time we reviewed 055, DRT and 05 operations. We also brought Up the DCP OWS software to see how that setup effects the 0W5 operations. is good to go with BL 11 difference training. Keep reviewing the ETMs for EL 9, was able to SIGNATURE INSTRU SIGNATURE Signed l/12 Sep14 55 06 Form 44 G-2 7O 64?4848, Class A, 30 April 15, AFSAS #739726 TRAINING SUMMARY AND CLOSEOUT REPORT m'smucmn's NAME I RANK NAME CLASS NUMBER OF INSTR DATE ENTRY DATE TOTAL DAYS 2 10-Jul-14 12-Sep-14 64 COURSE RC-135 Baseline ASE 4 11 AIRCRAFT OVERALL PERFORMANCE, WEAKNESSES, ETC. has completed all training events and has demonstrated that he has achieved proficiencv In all reeuIred events/Items. SIGNATURE OPERATIONS OFFICER SIGNATURE /l Signed 12 Sep 14 55 06 Form 46 (3-271 [Mediaseline 11 RC-135 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G111, 1LT [MiShap Raven 2] G2.ll.l. AF FORM 85 (MRZ) AT MP CERTIFICATE AIRCREW QUALIFICATION c? $582: 14 I. EXAMINEE IDENTIFICATION kaME (Last. MIMI: Inual) RANK 55AM ELGIBILITYPERIOD [Mishap Raven 2] 1.. LI MA ORGANIIATION AND ACFTICREW POSITION 338 CTS. O?ull AFB. NE RC-135V II. QUALIFICATION GROUND PNAEE DATE cm: DATE 00ch Book 04 Sop 14 96 INT QUALIMSN 11 Sup 14 Open BOOK ODALIFICATION LEVEL TRAININO OUALIFIED UNOUALIFIED DUE DATEIS) ADDITIONAL TRAINING COMPLETED I NIA NIA DATE OF QUALIFICATION CERIIFYING OFFICIAL. RANK AND SIGNATURE DATE ORGANIZATION Feb 16 I RICTIONS QUALIFIED COWANDER-OIRECVED I?tplw Come-I: on Bum (explam In Comm: 9- Bow flown Camera: on But; CERTIFICATION CHECK TYPEO NAME AND RANK a DATE FLIGHT EXAMINER 1 338 24 38914 REVIEWING 2 338 22 FINAL APPROVING OFFCER 3 338 CTSICC CERTIFY Ihal I have been bnofed and understand 1m action being Iaken dale. DATE TYPED NAME AND GRADE OF EXAMINEE . 2 14 I - 4 a: .[MIshap Raven 21:1 LI [Mlshap Raven 2] oac I aIA-r IIqu I AF FORM 8. 20061203 G-272 PREVIOUS EDITIONS ARE DBSOL ETE RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM I CONTINUATION SHEET W. COMMENTS REMARKS: I A. Mission Description. This was an Initial Raven Quali?cation and Mission evaluation flown on a local training sortie out of lefutt AFB. NE. The ?ight pro?le consisted of takeoff. air refueling. tin?Watch. off-Watch. and landing. The examines performed and was evaluated on mission planning. checklist procedures. CRMIcrew coordination. Equipmentr'systom operation. and data collection recording. B. Discrepancies. None. Recommended Additional Training. None. E. Additional Comments. Commendable. Area El. Coordination. Examiner: demonstrated well above average CHM by coordinating 3-1 communications. de?oon?icting signals and keeping the TC Informed at all times. Requisites and ?ight satisfy all requirements forthe Raven position on aircraft. .REVIEWING REMARKS: None. APPROVING REMARKS: None. ADDITIONAL REVIEWS: None. i AF FORM 3. 20061203 RC-I35V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.ll.2. AF FORM 942 RECORD OF EVALUATION Manama. Firs! mm mm 55m [Mishap Raven 2] ACFTICREW 73:5 DATE omuncmon ACFTICREW DATE auauncmou POSITION CWPLETED LEVEL POWON EVALMTION COMPLETED LEVEL ACC Rc-135v IME omwsw 11 Sep 14 1 lnilial Rawaw 303 R8 10 Cal 14 AF Fotm 942, 20061 208 PREVIOUS EDMONS ARE OBSOLETE G-274 G211.3. TRAINING RECORDS 64?4848, Class A, 30 April 15, AFSAS #739726 TRAINING SUMMARY AND CLOSEOUT REPORT STUDENTS NAME PAW CLASS Hm I RANK [Mishap Raven 2] I Lt NUMBER OF INSTR on: DATE COMPLETE TOTAL DAYS AIRCRAFT COURSE R0435 Basaline Raven DIffOual Baseline 11 Training Summary aircraft. has completed all training requirements to be certi?ed on Baseline 11 has accomplished a FMT lClaseroom training event and has completed the lraining program for Baseline 11 Di?erence Qualifallon. OVERALL PERFORMANCE, WEAKNESSES, ETC. SIGNATURE G-2 75 OPERATIONS OFFICER SIGNATURE RC-135 V, 64-4848, Class A, hap Signals, Search G2.12. 039mm" G2.12.1. AF FORM 85 30 April 15, AFSAS #739726 (MSSD) DATE COMPLETED OF AIRCREW QUALIFICATION 24 Feb 15 I. EXAMINEE IDENTIFICATION NAME (Last ?rst. Middle hilial) RANK SSAN ELIGIBILITY PERIOD Feb - 15 ORGANIZATION AND LOMTIGN Acn/cnsw Desmou 97 IS. Offull AFB. NE IIQ II. QUALIFICATIOPL 6R0 IND PHASE FLIGHT PHASE EXAMINATIONICHECK DATE GRADE MSSIONIONECK DATE Closed Book Open Book QUALIFICATION LEVEL TRAINING QUALIFIED UNOUALIFIED DUE DATE ADDITIONAL IRAINING COMPLETED 1 NIA EXPIRATION DATE OF CERTIFVING DFFCIAL. RANK AND SIGNAI URE DATE ORGANIZATION Jul 16 RESI RICIIONS EXCEPTIOMLLY OUALIFED COMMANDER-DIRECTED DOWNGRADE (Wan Comm: on Back) {Explm In Gum-nu an Buck) {Fm Cum-m: on law CERTIFICATIQN CHECK IS NAME AND RANK OMAMZATION 8 8 SIGNATURE DATE II I i mam EXAMINER REVIEWING OFFICER FINAL APPROVING OFFICER CERTIFY (rat I have been brleled and undamand the mien being tartan mIs mic. DATE rwpeo NAME AND GRADE or axmwes 03 Mar15 [mgsm AF FORM 8. 20061208 PREVDUS EDITIONS AE OBSOLETE G-2 76 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 AF FORM 5 CDNTINUATIDN SHEET W. COMMENTS REMARKS: Misslun Description. This was a Nun-Notice Signal Sarah and Development Quali?catiorl and Mission avaluallon flown IAW AF I AFI 11-2RC-135V2. and the 55 03 Evaluation Pro?le letter. focus was on the PLP panel along with how to create and modify a PRUFUSIDN assignment. B. Discrepancies. Nona. C. Recommended Additional Training. Nona. D. Additional Comments. Higher level FE was not arrailable per ABC para 3.2.4. Examinee elected 'In realign their quali?caticm dates. Raqulsitns and flight satisfy all requirements [Dr the Instructor SSD position on 1115 REE-1 aircraft. REMARKS: Nona. REMARKS: None. REWEWS: None. AF FORM 5. RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 G2.12.2. AF FORM 942 RECORD OF EVALUATION Hrs! um Initial) 33m 75:5 DATE QUALFICATION DATE QUALIFICATION POSITION COMPLETED LEVEL POSITION Ev COMETED LEVEL ACC Annual Review 15 Nov 06 RC-135V IEA SPOT 15 May 07 1 Annual Review 30 Jul 07 Annual Review 26 Jun 08 FIG-135V IIQ R0 QUALIMSN 23 Aug 11 1 Initial Review 336 01 Jun 11 CTS RC-135V IIO OUALIMSN 28 Nov 12 RC-135V QUALIMSN 08 Feb 14 1 Initial Review 97 IS 27 Oct 14 RC-135V IIO NIN QUAIJMSN 24 Feb 15 1 AF Form 942, 20061on Pasmous some?: ans 033mm V, 64?4848, Class A, 30 April 15, AFSAS #739726 NAME (Lam, Flst. Ml!le hiliol} TYPE WE 62,115. RC-135V SPOT Annual REVIEW RC-13SV QUAL Annual REVIEW RC-135V QUAL 0A1 COMPLEIED RECORD OF EVALUATION SSN LEVEL (mm DATE COMPLETED WPE AIR- CRAFT LEVEL OF (UNIT) EVALUATION 1 (97 (97 15] (97 (9715942, 20030601. V1 PREVIOUS EDITIONS ARE OBSOLETE. 6-2 79 RC-I 35 V, 64-4848, Class A, 30 April 15, AFSAS #739726 RECORD OF EVALUATION 'ww' ssu TYPE WPE I DRTE OUALIFCMION TYPE DATE MHGATION NR- OP CMLETEO LEVEL AIR- 0F COMPLETED CRAFT EVALUATION (COMMAND) EVALUATION Am Assigned 483 IS 07 13" 99 (AM) 1 RC-13SV QUAL 07 "Dr 99 (AIA) 1 INIT QUAL 26 "or 99 (AIA) . 1 RC-135V QUAL 28 Apr 99 (MA) Annual Review 07 Jan 00 (MA) 97 IS 17 00 (AIA) 1 sac-135v RQ QUAL 08 Nov 00 (NA) - - Annual Review 20 NOV ?0 (MA(AIA) ACC Annual Review 20 Nov 01 (ACC) A 1 RC-13SV INIT QUAL 04 Dec 01 (ACC) 1 VI sac-135v mn? 02 Apr 02 (ACC) 1? 1 5901 24mm! (97 15) Annual Review 20 NOV 02 (9715) Aunual Ravlew 06 Na' 03 (9715) RC-13SV QUAL 25 M9 03 (9715) Annual Review FORM 942. 19961101 (EF-V2) PREVIOUS EDITIONS ARE G-280 64?4848, Class A, 30 April 15, AFSAS #739726 G2.12.3. TRAINING RECORDS TRAININQAC .. . .. NAME (Last. First) RANK NAME RANK DATE 10 Nov 14 SORTIE NUMBER AIRCRAFT TYPE DURATION OVERALL GRADE OGT RC-135 Baseline 11 2 OVERALL PERFORMANCE, WEAKNESSES, ETC. PROFILE AND CONDITIONS: This was a BL11 difference certification completed on the OGT Tail 848. Pre-Mission Planning/Preflight: completed all BL11 academics with DiVittorio 10 Nov 2014. ?Flight/SIM: was shown and performed all required BL11 training on the OGT. He demonstrated basic knowledge of the baseline updates and was able to complete all updated system tasks. Paperwork- was shown the updated 550 web page and was instructed proper paperwork updates. CO- Performed various CO tasks to include seize, DF, Steerable beam. and map manipulation. SSD- completed standard procedures then proceeded to work on BL11 upgrade familiarization. He was able to task a D55 reciever and use both steerable beam and DF. Additionally, we covered how to patch RF to XMP for use of additional collection tools. AND showed the abililty to complete all tasks in a timely manner. He showed a sufficient understanding of the system, however could use additional BL11 practice. has completed all tasks required for a 811] difference certification, and is capable of operating all tasked BL11 functions. G-281 RC-135V, 64-4848, Class A, 30 April 15, AFSAS #739726 G3. MAINTENANCE TRAINING RECORDS No data available. G4. OTHER PERSONNEL EVALUATION AND TRAINING RECORDS. No data available G-282 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB H EGRESS, AIRCREW FLIGHT EQUIPMENT (AFE), IMPACT, AND CRASHWORTHINESS ANALYSIS H1. EGRESS ANALYSIS ........................................................................................................... 2 H2. AFE ANALYSIS ................................................................................................................... 3 H2.1. AIRCRAFT INSTALLED AFE .................................................................................... 4 H2.2. CAREER FIELD EDUCTION TRAINING PLAN RECORDS ................................ 5 H2.3. AFE CONTINUTATION TRAINING EVENTS ........................................................ 5 H2.4. AFTO FORM 46CG PREPOSITIONED LIFE SUPPORT EQUIPMENT ............ 6 H3. IMPACT ANALYSIS ........................................................................................................... 7 H4. AIRFRAME CRASHWORTHINESS ANALYSIS ........................................................... 7 H-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 H1. EGRESS ANALYSIS No data applicable. H-2 INTENTIONALLY LEFT BLANK RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 H2. AFE ANALYSIS Analysis of Aircrew Flight Equipment AFSAS Number: 739726 Mishap Aircraft (MA): 64-14848 Mishap Date: 30 April 2015 I. INTRODUCTION: The following pertains to an RC-135V aircraft assigned to the 55th Wing, Offutt Air Force Base Nebraska that was involved in a mishap involving a fire around the aft galley section of the aircraft. A thorough review of all Flight Equipment Records Management System data was accomplished. Additionally, other available computerized products to include crewmember Individual Training Summaries (ITS) and Training Business Area (TBA) training records were also reviewed. II. BACKGROUND: AFE requirements and equipment configurations are dictated by AFI 11-301v1, AFI 11-301v2, AFI 11-301v1 ACC Supplement, and associated equipment technical orders. An evaluation of the AFE recovered from the MA was accomplished to confirm that evaluated subsystems worked as designed. There were no overdue inspections, time changes, or Time Compliance Technical Orders that required accomplishment. All crewmembers on board were current on required, grounding related and AFE continuation training events. H-3 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 H2.1. AIRCRAFT INSTALLED AFE The aircraft installed AFE was located throughout the MA and each item was found to be in its proper place. The equipment was later removed from the MA, collected by the SIB and retained at an area adjacent to the main entry control point of the MA controlled area. Photographs were taken of several oxygen masks as items potentially damaged during the incident. An accurate assessment as to the condition of each item will be determined based upon a thorough review and inspection of these components by qualified AFE personnel. At this time only one Scott Model 358 mask appears to be damaged beyond repair. a. Scott Model 358 Oxygen Quick Don Smoke Mask (used). There were 35 quick don oxygen masks prepositioned aboard the MA. Based off non-privileged written statements, 21 of the 27 crewmembers indicted donning the mask upon indication of the fire and ensuing smoke in the cabin. None indicated any failures of the AFE or problems donning the mask. An electronically generated AFTO 334CG indicated the next mask inspection wasn’t due until 21 May 15, so all were current. There were three AFE technicians who completed the last inspections of the masks with all being qualified to perform the task. b. Fire Fighters Smoke Mask (used). There were two firefighter smoke masks prepositioned aboard the aircraft. Based off non-privileged written statements, only one of the 27 crewmembers indicted donning the firefighter mask, in lieu of the Scott 358 Quick Don, in an attempt to extinguish the fire. There was no mention or indication of malfunctions of the AFE or problems donning. The electronically generated AFTO 334CG indicated the next mask inspection was due 20 Jun 15. There was one AFE technician who completed the last inspection of the mask on 22 Dec 14 and was fully qualified. c. Protective Breathing Equipment (PBE) (not used). There were two PBEs prepositioned aboard the aircraft. The electronically generated AFTO 152CG indicated the next inspection was due 31 May 15. According to these records, one AFE technician was responsible for the last inspection accomplished on 2 Mar 15. Upon verification of training records, the member was qualified on this item. d. Emergency Passenger Oxygen System (EPOS) (not used). There were 30 EPOSs prepositioned aboard the aircraft. The electronically generated AFTO 152CG indicated the next inspection was due 9 Aug 15. According to these records, one AFE technician was responsible for the last inspection accomplished on 10 Feb 15. Upon verification of training records, the member was qualified on this item. e. Anti-Exposure Coverall, CWU-16/P (not used). There were 36 CWU-16/Ps prepositioned aboard the aircraft. The electronically generated AFTO 335CG indicated the next inspection was due 14 Sep 15. According to these records, there were three AFE technicians who completed the last inspection accomplished on 18 Mar 15. Upon verification of training records, all members were qualified on this item. H-4 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 f. Restraint Harness, PCU-17/P (not used). There were two PCU-17/P restraint harnesses prepositioned aboard the aircraft. The electronically generated AFTO 392CG indicated the next inspection was due 27 Jan 16. According to these records, one AFE technician was responsible for the last inspection accomplished on 27 Jan 15. Upon verification of training records, the member was qualified on this item. g. Life Preserver, LPU-10/P (not used). There were 36 LPU-10/Ps prepositioned aboard the aircraft. The electronically generated AFTO 336CG indicated the next inspection was due 18 Feb 16. According to these records, there were two AFE technicians who completed the last inspection accomplished on 18 Feb 15. Upon verification of training records, both members were qualified on this item. h. Life Raft, F-2B (not used). There were two F-2B life rafts prepositioned aboard the aircraft. The electronically generated AFTO 338CG indicated the next inspection was due 18 Dec 15. According to these records, one AFE technician was responsible for the last inspection accomplished on 18 Dec 14. Upon verification of training records, the member was qualified on this item. i. Life Raft, F-2B, Inner Kit (not used). There were two F-2B life raft inner kits prepositioned aboard the aircraft. The electronically generated AFTO 338CG indicated the next inspection was due 18 Dec 15. According to these records, one AFE technician was responsible for the last inspection accomplished on 18 Dec 14. Upon verification of training records, the member was qualified on this item. j. Life Raft, F-2B, Outer Kit (not used). There were two F-2B life raft outer kits prepositioned aboard the aircraft. The electronically generated AFTO 338CG indicated the next inspection was due 19 Dec 15. According to these records, there were two AFE technicians who completed the last inspection accomplished on 19 Dec 14. Upon verification of training records, both members are qualified on this item. H2.2. CAREER FIELD EDUCTION TRAINING PLAN RECORDS Technician Training: A thorough review of all mishap-related AFE technicians’ training records was accomplished utilizing TBA. All equipment inspections, maintenance, and continuation training provided to the crewmembers was accomplished by AFE personnel trained on the applicable equipment and training events. H2.3. AFE CONTINUTATION TRAINING EVENTS Aircrew Individual Training Summaries (ITS): A thorough review of all mishap-related crewmembers ITS records were reviewed. All items identified as grounding events per the 15 RC/OC/WC-135 Ready Aircrew Program (RAP) Tasking Memo were current for all crewmembers on board. H-5 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 H2.4. AFT 0 FORM 46CG PREPOSITIONED LIFE SUPPORT EQUIPNIENT mun-1139 Mon: WWII: Mum: m: I LIFE 3 RT I RC-1 35v 848 Equipment Type: Qty: LocallSc?Il numbers? I) insp _50_t 17 14-Sep-5613 14? Apr- 2015 EPQS. 30_ Set ID: 22 111- Apr- 2015 F28 IN 2 Sam: 3 18-Dec-2015 14- Apr- 2015 F28 2 sum: 3 19-03331?f 2015? F28 RAFT 2 8.110;: 1 1842032015 Apr- 2015 LPU-10IP 35 18-Feb-2016 __1_4r M?g?g LPU-1OIP 1 5411 ID: 5 20-Apr-2016 14- Apr- 2015 PBE 4 2 Set no: 25 31 May-2015 ?1:31:33 PCU-17IP 2 Set to: 22 Juan-201g lApr- 2015 OUICKDON 36 591 ID: 2 14. Apr- 2015 SMOKE 2 Set 10- 19 - 26311115015 Apr- 2015 L. I canny the We smut: 0119mm mo ng?rm was preposan on_ the amoral: on the date maniac!" DATE: GRADE: NAME: 28-Apr-2015 1 ?r_a . 16 be "mow?ad and sign?Id?by th- aircraft commander or oule lemma prior to dopanuro IAWAFI11-301 V2. my twin-1113.0} this {arm an on been! and in mom! serviceable copdtuon on the dams macaw by my signature _Ls REP SENATURE: 9511:: games? nun-iguma- . ~c REP. SIGNATURE: i- AFTO FORM ?606 081' ZOMICOMPUTER GENERATEJ) Page 1 at 1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 H3. IMPACT ANALYSIS No data applicable. H4. AIRFRAME CRASHWORTHINESS ANALYSIS No data applicable. H-7 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB I DEFICIENCY REPORTS I1. DEFICIENCY REPORTS (DR) ............................................................................................ 2 I1.1. DR OFF-15-0004 REFRIGERATOR ............................................................................ 2 I1.2. DR OFF-15-0005 REFRIGERATOR ............................................................................ 4 I1.3. DR OFF-15-0006 OVEN, CONVECTION ................................................................... 6 I1.4. DR OFF-15-0007 MICROWAVE OVEN, WAVEJET ............................................... 8 I1.5. DR OFF-15-0008 FAN .................................................................................................. 10 I1.6. DR OFF-15-0009 FAN .................................................................................................. 12 I1.7. DR OFF-15-0010 FAN .................................................................................................. 14 Il.8. DR OFF-15-0011 FAN ................................................................................................... 16 I-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK 1-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 I1. DEFICIENCY REPORTS (DR) I1.1. DR OFF-15-0004 REFRIGERATOR I-3 64-14848, Class A, 30 April 15, AFSAS #739726 DR form (la-inked on: 27MAY2015) REFRIGERATOR 8/1! 400- 1379 - 02 400-1373-02 AIRCRAFT MISHAP INVESTIGATION mums! lsmnols/ ISMYZ 0.1.5 24301-2015 24311142015 15MY2015 IMHO 1-3 1?4 page: 64-14848, Class A, 30 April 15, AFSAS #739726 11.2. DR REFRIGERATOR DR Form [Printed on: Mi ahap I113 are No -BEBG ITEM INVOLVED IN AN AIRCRAFT FIRE THIS DR WAS SUBMITTED 33 PART OF AN ON-GOING AIRCRAFT MISHRP INVESTIGATION, AFEAS #739?26. ITEM IS SUSPECT IN CURRENT MISHEP 1 Quality A Evaluation DPEN 400-1378-02 TIA ?ih D3-6-33T76 773624957193 URK UNK UNK Page 1 L5 64-14848, Class A, 30 April 15, AFSAS #739726 DR Form (Printed on: 27MA12015) BRIGRATOR 400 4373 - 02 400-1373-02 AIRCRAFT INVESTIGATION 739726 II ISMYZOIS 3430:3015 24m 015 15mm 015 15MY20 Page 2 1-6 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 I1.3. DR OFF-15-0006 OVEN, CONVECTION I-7 64-14848, Class A, 30 April 15, AFSAS #739726 DR ?erm (Printed on: 27MA32015) OVBH. COEVBCTION 91105-001 91145-001 HISHAP INVESTIGRTIOR 739726 II 243012015 2400L2015 15MY2015 ISMYZOIS 2 1-8 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 I1.4. DR OFF-15-0007 MICROWAVE OVEN, WAVEJET I-9 64-14848, Class A, 30 April 15, AFSAS #739726 DR Pom (Printed on: momma Om, mm u/A 400-1409-03?1. aoo-nos-oa-L AIRCRAFT mam INVESTIGATION 739726 II 2401132015 015 15m?2015 xamuoxs Page 2 1-10 64-14848, Class A, 30 April 15, AFSAS #739726 11.5. DR OFF-15-0008 FAN DR Form (Printed on: 27m1'2015) Ile No NO NO ISMAYZDIS -8383 ITEM INVOLVED IN AN AIRCRAFT FIRE THIS DR WEE SUBMITTED AS PART OF AN DH-GOING AIRCRAFT MISHAP INVESTIGATION, AFSRS #739725. ITEM IS SUSPECT IN CURRENT MISHAP 1 Quality A Evaluation OPEN 633454 EMETEK ROTRON 8287? CD34DG082 7?3524331759 UNK Page 1 64-14848, Class A, 30 April 15, AFSAS #739726 DR Porn (Printed on: 2714122015) EAN MA 03345; 033454 AIRCRAFT MISHIP INVESTIGATION 739726 II 15ME22015 ZQJUL2015 24JUL2015 15MBY2015 Page 2 1-12 64-14848, Class A, 30 April 15, AFSAS #739726 11.6. DR OFF-15-0009 FAN DR (Printed on: Mishap ACE No HO HO Ho 15HAIZG15 -388i ITEM INVOLVED IN ER AIRCRAFT FIRE THIS DR WAS SUBMITTED AS-PART 0? EN AIRCRAFT MISHAP INVESTIGATION, A3333 ITEM IS SUSPECT IN MIEHAP 1 Quality A Evaluation OPEN 033454 RGTRUN 82871 C034OOQBS 773624831769 UNK UHK UHK Page 1 1-13 64-14848, Class A, 30 April 15, AFSAS #739726 DR Form {Printed on: 27MAE2015) 238 033?54 033?s? AIRCRAFT MISHAP INVESTIGAIION 739726 11 015 24JUL2015 ZQJULQOIS 15MKY2015 ISMNY2015 page 2 1-14 64-14848, Class A, 30 April 15, AFSAS #739726 11.7. DR OFF-15-0010 FAN DR Form (Printed an: 27MAY2015) Mishap Ile MC NO NO R0 015 -3335 ITEM INVOLVED IN Mil MRCRAFT FIRE THIS DR WAS SUBMITTED AS PART OF AN AIRCRAFT M-IEHAP INVESTIGATICW. M518 #739726. ITEM IS SUSPECT IN CURRENT MISHAP 1 {mal?w A Evaluation OPEN 033454 MISTER ROTRON 3237'? (203400038 773624881759 UNK UHF. Page 1 64-14848, Class A, 30 April 15, AFSAS #739726 DR (Printed on: 27NA32015) RAN 033454 033454 AIRCRAFT "19339 INVESTIGATION 15MRY2015 2400L2015 24JUL201S 15MK22015 Page 2 1-16 64-14848, Class A, 30 April 15, AFSAS #739726 11.8. DR OFF-15-0011 FAN DR Form (Printed on: 27MAY2U15) Mishap 1/13 EEC No No No manuals -3886 ITEM INVOLVED IN AN AIRCRAFT FIRE THIS DR HAS PART MISHAP ENVESTIGATIGN, HESAS #739126. ITEM IS SUSPECT IN CURRENT MISHAP 1 Quality 3 Emulation OPEN 033454 AMETEK ROTRDN 32377 C93409051 ??3624831?69 WK UHK UNI Page 1 64-14848, Class A, 30 April 15, AFSAS #739726 DR (Printad on: 27N332015) FAN 033654 033?s; AIRCRAFT MISHAP INVESTIGATION 739726 II 1MB 01.5 2430142015 15MY2015 quge 2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB J RELEASABLE TECHNICAL REPORTS AND ENGINEERING EVALUATIONS J1. AIR FORCE RESEARCH LAB TECHNICAL REPORT AFRL/RXS 15-030A............ 2 J-1 64?14848, Class A, 30 April 15, AFSAS #739726 J1. AIR FORCE RESEARCH LAB TECHNICAL REPORT 15-030A Onbonul Fire Mishap Investigation (Failure Analysis) 27 May 2015 Evaluation Report (SA 1 02002) Report No. 15-030A AI 81 Materials Integrity Brunch I Safety Investigation Boanl Pnesident ACC 25 RC.135 V, 64?14848, Class A, 30 April 15, AFSAS #739726 15-030A EXECUTIVE SUMMARY The Materials Integrity Branch was requested to support a Safety Invest igation Board (SIB) for an RC- 135V on-board ?re (Class A Mishap). Members of the team examined the incident airera? on-site and for laboratory analysis removed both the electrical and oxygen system near the origin of the tire. The analysis found the root cause was a leaking oxygen system. caused by poor assembly practices. The ignition source could not be detennined with the available physical evidence. although multiple sources were available onboard. Recommendations include inspecting the oxygen systems on all other aircra?. reviewing refurbishment procedures with the manufacturer. and removing loose debris near electrical systems. The ?nal was to identify any other programs that have oxygen systems re?rrbished at the same site and notify them of the risk. RC.135 V, 64?14848, Class A, 30 April 15, AFSAS #739726 15-030A ACKNOWLEDGMENTS This report re?ects the of a dedicated and talented team The authors would like to recognize the following individuals' contributions to this analysis: for his assistance with on-site and in-hottse technical evaluation, and reporting of electrical components. (Materials Integrity Branch), and (University of Dayton Research Institute) for their component analysis. subject matter expertise. and sectioning assistance, and (University of Dayton Research Institute) for data records analysis. Further. the authors would like to acknowledge (University of Dayton Research Institute). :Southwest Council on Higher Education) and (Materials Integrity Branch) for disassembly, sectioning, and digging throth seven bags ot?debris. Finally, the authors would like to acknowledge (Materials Integrity Branch) for document preparation, formatting. and editing. RC.135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 AFR URXS 15-030A TABLE OF CONTENTS Page PURPOSE .. 1 BACKGROUND .. 1 FACTUAL DATA .. 1 DISCUSSION .. 6 CONCLUSIONS .. 8 RECOMMENDATIONS .. 8 FIGURES .. 10 TABLE .. 34 APPENDIX .. 37 APPENDIX A - Wire Number for Each Conductor in Large Wire Harness iv RC-135 V, 64?14848, Class A, 30 April 15, AFSAS #739726 RC-135V Onboard Fire Elisha Investigation URPOSE Determine root cause ofan RC- 135V onboard lire. BACKGROUND On 30 April 2015. an (Tail Number 64- 4848) sustained an onboard ?re in the galley section ofthe aircraft immediately before takeoff at O?iltt Air Force Base. Nebraska. All 27 of the aircrew members onboard at the time ofthe mishap safely evacuated. Other mishap information for this Class A mishap can be found in Air Force Safety Automated System (AFSAS) report 739726. The Air Force Research laboratory/Materials Integrity Branch (AFRIJRXSA) was asked to provide support for the Safety Investigation Board (SIB) in charge ol?lhc investigation. Structural and Electrical Materials Evaluation Teams provided on-site support at OlTutt AFB for evidence analysis within the mishap aircra?. A number of components from the galley area were removed from the aircraft and renamed to RXSA for detailed laboratory analysis. collected included portions of the onhoard oxygen system and portions ot'wiring harnesses. A full list ot'conrponents that RXSA collected. and a preliminary laboratory analysis plan ere detailed in a trip report (Memorandum for dated 20 May 2015) submitted to SIB. The RC-135V reportedly undergoes a signi?cant refurbishment every ?ve years at 13 Communications in Greenvillc. Texas. Factual data for the struettual and electrical analyses are broken out into individual sections for easy reference. FACTUAL ELECTRIGIL Analysis Pglorm: ed at murrAFB - Visual inspection ot?the damaged aircraft showed the tire damage was intense and wellofocuscd in a speci?c area ofthe interior near the galley. The interior area with the most severe wire damage coincided with a large hole in the fuselage. Electrical system components in the direct proximity ot?the tire damaged region were severely compromised. Portions of cables and wiring harnesses in this area completely lacked insulation and showed signs of having partially melted. These examples were eventually removed for further analysis (Rare 1). The galley contained two refrigerators. microwave oven. convection oven. lighting. and receptacles for up to four separate beverage jugs. along with the GALLEY CONTROL PANISI. (Figure 2). The electrical connections immediately behind the GALLEY CONTROL PANEL were 1 V, 64?14848, Class A, 30 April 15, AFSAS #739726 blackened due to smoke. but showed no evidence of arcing or insulation failure. The wires associated with the beverage jugs were heavily damaged. but only in the region directly under the hole in the fuselage. The wires associated with the microwave and conwction ovens were blackened due to smoke. but showed no evidence of arcing or insulation failure. The beverage jugs and light switches were all found in the off position. The BOX ASSY - GALLEYIGOHZ, CB PANEL had three circuit breakers that were open circuit (not conducting): the MICROW AVE OVEN (10A. 1 15 VAC. 400 HZ). the CONVECTION OVEN (15A. 115 VAC, 400 HZ). and the SPARE 25A breaker (Figure 3). All other circuit breakers were closed (conducting). The remains of ?ammable debris were identi?ed in the galley area. Further inspections of undamaged R01 35 aircratt showed the area behind the beverage jug receptacles collected debris. Anal sis armed a! RXSA - An 8- foot section ol?a wire hame-ss that runs along the roof of the ?iselagc above the galley was analyzed Overall. the harness showed a wide temperature gradient, with each end showing little to no heat damage (Figt_irc 4), and the middle showing severe damage. Insulation from the middle of the 8-Foot wire harness was completely removed and the conductors exhibited a bright red color. The red coloring was identi?ed as red copper oxide. which forms when copper is exposed to temperatures greater than for an extended period where oxygen is present. Numerous wires had molten copper tenninat ions (Figure 5). Cross-sectioned samples of these terminations contained voids, which are indicators of electrical arcing. samples also displayed structured grain morphology, which occurs from extended exposure to a high temperature environment (Figure 6). An analysis of the relatively undamaged ol?tlic 8-t'oot wire harness was conducted. Insulation at the ends ofa select number of wires was removed to allow visual analysis ofthc tin- plaled copper conductors. 'l?he tin plating appeared dull compared to a new wire. and there Were no visual abnormalities on the inside surface of the insulation (Figure 7). No evidence of arcing. continuous overcurrent. or degradation to the insulation was noted. Each conductor ot'the wire harness from Figure 4 was documented (Appendix B) to aid in any follow-on system analysis that may occur. A 3-foot section of a win: harness. shown in Figure 8. was analyzed. This harness is routed through the galley to power the four beverage jug cannon plugs. This harness was exposed to high temperatures, as red copper oxide was prevalent. Molten copper terminations were observed in possibly unpowered wires. Similar molten terminations Figure 9) were created by pointing a methylacetylene-propadiene propane (MAPP) gas torch at a locally-manufactured. small wire bundle. Two wire harnesses supplying power to the microwave and convection ovens within the galley were submitted for analysis. Both harnesses exhibited little damage; insulation was intact and only displayed slight discoloration in areas that would have been exposed to the tire as it was bunting (Figure 10). A 3-foot section ol?an RF coaxial cable was submitted for analysis (Figure I). The outer shield and visible inner conductor displayed no visual evidence of electrical arcing. RC-135 V, 64?14848, Class A, 30 April 15, AFSAS #739726 Finally. an undamaged aircraft showed debris near the harness that powers the four beverage cannon plugs (Figure 12). The components ot'the oxygen system are shown in the as-receiyed condition in Figure 13. The components are shown in their approximate location on board the aircraft in Figure 14. Figgre 14 also has a numbering system for the joints that will be used throughout the report. In addition to the oxygen system, the upper portion ofthe kitchen galley, varioUs galley components. several bags of debris. and exemplar components were collected at the site and analyzed. These are shown as- received in Figirc IS. The ?ttings in the oxygen system are commonly referred to as ?ttings because each ?tting has a speci?cation that begins with 'lhese ?ttings consist of four components: a male threaded end, a female nut (referred to as a B-nut). a sleeve. and a ?ared tube. A schematic ol'the system shown in 16 indicates the sealing surface is the male ?tting cone and the inside of ?ared tube. The B?nut docs not provide scaling, only clamping force. The cxaminat ion began with a visual and stereo optical examination of the components at magni?cations up to 40X. A small piece of aluminum foil was found packed behind the circuit breaker panel in the galley. There was no evidence of primary ignition on the galley or on the piece of aluminum foil. In addition. the most signi?cant hcat damage during the on-site examination was well above the galley, with a portion oi?thc oxygen tube at its center. These facts focused the investigation on the oxygen system Oxygen system visual examination revealed there was no B-nut at junction 11. The examination further revealed no evidence that the B?nut had forcibly passed mer either the tube clamp or the ?ared end. The male threaded end of the elbow ?tting that at junction It is shown in Figure 17. As seen in the ?gure. there is some discoloration on the threads. indicating the B-nut came during. but not at the beginning ot'thc ?re. This is in direct contrast to the sleeve sidc ot'junction 1. The sleeve and the ?ared end were heavily discolored; indicating the B-nut came off from that side at the beginning of the ?re. During laboratory examination of the debris. a ti'agment ot' the missing B-nut li'om junction 11 was recovered (Figure 18). Examination of the fragment with a Zeiss Sigma VP Scanning Electron Microscope (SEM) indicated large areas ot?the nut were melted. Material melting and removal is highlighted in Figure 18. urther visual examination ot?the tithing system showed the inner liner of the ?ex hose near junction 5 was destroyed. Heat damage to the tube was indicated by rumpling found using computed tomography (CT) scanning (Figure 19). Torque stripes were noted only on junctions l. 5. 6, and It). The torque stripes at junctions 5 and 6 were charred. likely from the on-board lire. Torque stripes at junctions and IQ did not show signs ofheat damage. The tee ?tting atjunction 4. 5. and 6 appeared to be a lighter color blue than all of I J-8 V, 64?14848, Class A, 30 April 15, AFSAS #739726 the other ?ttings. Finally. the B-nuts at junction 4 and on either end ofthe damaged ?ex hose between junctions 5 and 11 were all linger tight. The B?nuts on the lies hose were the only ones in the system where stainless steel nuts were attached to aluminum ?ttings. No other defects or discrepancies. outside of deposits of combustion by-products. were noted on the remainder ofthe installed oxygen system. The outer diameters of the tubes were measured using dial calipers. The ODs were consistent with 5! 16m tubing per 4071. It was noted that one ol?thc supplied exemplar nuts from the shop at Otl'utt AFB did not have any markings indicating it was an ?tting. Following optical examination, the oxygen system was pressure tested in segments using compressed nitrogen at pressures up to 300 psi and a foaming leak detectant. The damaged ?ex hose (between 5 and l) was replaced using the ?ex hose connected to junction 1. alter junction 1 had been pressure tested. Where nuts were found to be ?nger tight during initial evaluation. these locations were tested linger tight. In the case of junction ll. the nut from junction 2 was used to replace the missing B-nut. This nut was tightened only to the point it covered the blue portion ofthc threads. which corresponded to ?nger tight. The oxygen system leaked at 20 psi from junctions 4 and ll. The junction ll leak was audible at 50 psi. Following this test, the nut at junction 4 was tightened 1/10"l rotation. The nut at junction 4 still leaked at 50 psi atler the turn. All other areas ot?thc tubing system held 300 psi with no leaks detected. Following pressure testing. the tubing system was disassembled and the individual components examined. The breakaway torques were noted during disassembly and are shown in the Table. Of note. junction 4 required 50 in-lbs. for disassembly. This nut was known to be 1/10m turn past finger tight. Further. only the two nuts with non-heat damaged torque stripes had break away torques over 100 in-Ibs. Comparing tightening torque and breakaway torque in the laboratory indicated tightening torque was typically 40 in-lbs higher than breakaway. If 40 in- ol?torquc are added to the values in Table. only one of the non-torque striped nuts (junction 8) mects the installation torque requirements found in The disassembled nuts are shown in Figure 20. The outside of all nuts were in good condition and showed no damage to the blue anodized layer or tool marks. The majority ol?nuls had a loss ol? anodize layer on the inner surface that contacts the sleeve. leaving exposed metal. No evidence ot? Teflon tape was found on any ol?the threads. The cone ends of the disassembled fittings are shown in Figure 21. The cone ends. with the exception of the 4. 5. and 6 tee ?tting. show unitbrm contact and negligible exposed metal The 4. 5. and 6 tee titling cones are all heavily damaged. showing uneven wear pattems. nicks. gougcs. and large areas ot?esposed metal. The documents provided by the SIB show L3 uses speci?cations for their ?ttings. All specifications refer to AS4841A. the industry standard procurement specification of ?ttings of this type. Section 3.4. .1 ol? A states "Bare areas occurring on 37 degree cone or spherical scaling surfaces. hearing or threaded surfaces shall be cause rejection." V, 64?14848, Class A, 30 April 15, AFSAS #739726 AS4841A also states that all ?ttings must be marked with the manufacturer?s name. CAGE code or trademark. and the letters AN. MS. or NAS as applicable. A comparison ol'the 7. 8. and 9 teetee ?tting is shown in Figure 22. This ?gure clearly shows there are no letter markings on the 4. 5. and 6 lilting. AS4841A requires all blue anodized ?ttings to be fabricated from 2014 (Ah/184133) or aluminum These speci?cations indicate the ?ttings must be machined from bars or forgings. The 4, 5. and 6 tee fitting appears to have a parting line and a rough surface. both typical ol'a casting. Finally. X-Ray Fluorescence (XRF) testing ot?all ?ttings using a Niton Goldd XL31 indicated they were consistent with aluminum alloys. except for the 4. 5. and 6 ?tting. XRF results showed the 4. 5. and 6 tee ?tting was consistent with or cast high silicon aluminum alloy. Based on the trademark. the 4. 5. and 6 ?tting was manufactured by Weatherhead. Weatherhead was purchased by Eaton in 2002. 'l'elephone discussions with Eaton indicated ?ttings similar to the 4. 5. and 6 tee were last manufactured in 2003. The llared tube ends are shown in igurc 23. Examination of the flares indicates they all had a circular contact impression from the sleeve. through the. tube coating to the base metal, except the flare at junction 1 l. The discoloration on tube 1 I stopped at a circular boundary, but it. did not. penetrate the coating. Tubes 6 and I I showed signi?cant discoloration on the tube past the area covered by the sleeve. The sleeve on tube 1 did not slide freely on the tube and was le? on the assembly. The sleeves are shown after disassemny in igge 24. There was signi?cant discoloration on sleeves these. only sleeves 6 and 11 showed discoloration under the location of the B-nut. To determine the reason for the discoloration. both sleeves were cleaned using acetate replication and subsequently re-examined (Figure 25 l. The majority of the surface deposits on sleeve 6 were removed. and some ofthe copper colored area ?aked off. which is consistent with surface contamination. A large amount ol'hlack residue was removed from sleeve 1 l. revealing a dark gray area directly under the letters The fact that the replication did not remove the dark gray discoloration suggests it is likely a tenacious oxide, which indicates this area of the bushing was exposed to high heat. The cleaning ot?sleeves 6 11 revealed signi?cant pitting on one side of sleeve ll. All other sleeves were re-examined using either stereo optical or electron microscopy. While some machining defects were found. no other sleeve had similar pitting. SEM examination of sleeve ll showed the pitting had an irregular shape. intermixed with very round pits (Figure 25). Oxides were noted at the bottoms ot?some pits. The pitting on sleeve 11 indicates the damage was directional. since it was present on one side and not the other. To determine if this damage occurred to the assembly. or to the sleeve by itself. the tube at junction was cleaned using acetate replication and examined. Fitting was found more frequently on one side ol'the tube. just past the area the sleeve covered (Figgrc No pitting damage was found beneath the sleeve. Electron microscope examination of these pits show ed 5 V, 64?14848, Class A, 30 April 15, AFSAS #739726 bulbous metal structures and heavy oxidation. These artifacts are consistent with corrosion and melting. The large coaxial cable shown in Figure 1] was examined using the SEM. The discoloration on the outer surface indicates the cable was deformed after heating. Examination of the tincture surlaces showed only indications of melting. The composition and temper ol'all tubing system components were verified. As previously determined using XRF. the composition of all ?tting (including the B-nut fragment) were consistent with 23m: aluminum alloys. with the exception ot'the 4. 5. and 6 tee ?tting. Conductivity on all ?ttings. except the B-nut fragment. was measured using a Hocking AutoSigma 3000 Conductivity Meter. All oxygen system nuts measured between 42.8 and 45.] Intemational Annealed Copper Standard (IACS). 'lhis is consistent with 2024 in the T6 temper. The male ?ttings measured between 36.9 and 45.0 IACS. 'lhcse readings are consistent with 2024-16 or 2014-1?6. Hardness values for all ?ttings and nuts were over 72 IIRB, with the exception nut 4, 6. the elbow at junction tee fitting. Hardness values for these fitting ranged between 33 and 63 indicating various levels of heat damage. Similar to conductivity. the hardness of the B?nut fragment was not measured. Composition of all tubing was consistent with or aluminum using XRF. Speci?cation AMS 4071 is mquired by L3 for oxygen system tubing and states all tubing shall be fabricated from aluminum alloy 5052. It is likely a combination ol'contaminants containing silicon and the Niton Goldd XL3t's low accuracy on silicon caused the (ants series identi?cation. With these factors in mind. the tubing appeared to be consistent with aluminum alloy 5052. The shape of the tubing made conductivity or hardness measurements impractical. Finally all sleeves were identi?ed as 33's series stainless steel. According to AS4841A. the marking found on all sleeves indicates they are 304 stainless. DISCUSSION Based on the available physical evidence, the most likely sequence of events is that a small oxygen leak formed on one side of junction 1 1. The leak allowed oxygen to escape betWeen the B-nut and the sleeve. The locally rich oxygen environment allowed a ?re to ignite. Physical evidence indicates the area ofhigh heat was localized, causing damage predominantly to one side of the sleeve and tube. This area ot?high heat like ly melted the portion ol'thc nut that held it on to the sleeve. For reference. the melting range ol?Zssx alloys starts at while 5052 starts at and 304 stainless stats to melt at 25 so the B-nut would have melted ?rst. 'Ihis allowed the ?ex hose to fall away ?'om the primary oxygen line. resulting in a much larger ?re. The damaged B-nut likely l'ell o??lhe male ?tting later in the tire, with a fragment falling onto the top ol?the galley. This fragment had localized melting. which is consistent with damage on one side ot'the tube. starting at the shoulder ot'the nut. The physical evidence also indicates the most likely cause of the leaking fitting is poor assembly. Disassembly ol'thc system showed widespread low torque values. the use of improper ?ttings. re use of signi?cantly damaged ?ttings and inconsistent torque striping. While the torque at 6 J-ll V, 64?14848, Class A, 30 April 15, AFSAS #739726 not 1 I could not be measured. there is no contact scar on the ?are at this location. This indicates it had the lowest torque of all the fittings examined. The oxygen system installation document provided by L3 indicates there are a large number of gaps in their refurbishment process. All ?ttings used in the exzunined sections of oxygen system are required to be ?tting per the provided manufacturing documents. All speci?cations cite AS4841A as a requirement. The L3 inspection oi'thc ?ttings only requires a visual examination for contatnitumts (Section 3.3.7.1). Damaged fittings or bare metal are not causes for rejection in L3 documents. even though those are both rcjectable per AS 4841. The L3 document does not have an inspection for thread and is silent on the re-ttse of fittings. The provided work orders seem to indicate that tube assemblies should be locally manufactured and new ?ttings should be used during each refurbishment. but it is clear that ?ttings and tubes are being widely re-used. Finally. the 13 documents are self-contradictory. The 1.3 document requires that oxygen system tubing be fabricated using AMS 407] tubing. but the other manufacturing documents direct the workers to use AMS 4070 tubing. AMS 4070 tubing is the same material as AMS 407]. but does not undergo the same level of quality inspection. The evidence also indicates there may have been a local area of corrosion on the top of the nut that could have led to a corrosion failure. It is impossible to detemtinc if there was a corrosion failure followed by an oxygen leak. or an oxygen leak followed by high temperature corrosion. However. the preponderance of the evidence indicates the leak occurred first. likely caused by low torque. The lack of leaking on some other nuts with very low torque values indicates the difference between a leaking and non-leaking fitting is very small. It is possible the ?tting at number 1 1 did not leak alter refurbishment. but the repeated stresses induced on the ?tting due to aircraft operations caused the leak to develop over time. The laboratory experiments show a very small rotation of the fitting causes a large change in the leaking pressure. Physical evidence also indicates that problems with the oxygen system are not caused by local maintenance. The improper 4. 5. and 6 ?tting was last manufactured in 2003. The age of this improper fitting indicates it was on the aircraft when it ?as last refurbished. While there is a large number ot?titel sources on-board the RC-135. the ignition source could not be identi?ed with the available physical evidence. Based on SAE "Guide for Evaluating Combustion Hazards in Aircrall Oxygen Systems." sections 3.2 and 5.5.6. potential ignition sources include: Contamination Particle impact Heating to ignition Friction heating Compression heating Mechanical impact Vibration 1-12 RC-135 V, 64?14848, Class A, 30 April 15, AFSAS #739726 AFRURXS Electrical are Trapped volume pres'surization All of these were potential ignition sources in the current mishap. Normally. any evidence of arcing could be a clear indication of an ignition source in an oxygen- rich environment. However, a number of factors specific to this mishap preclude that conclusron: The damage caused by the lire. and the subsequent ?re?ghting e??ortis likely would have destroyed any evidence ol? an electrical power system EPS trigger mechanism if it existed. Clear evadence of electrical arcs was present within the large wire bundle. It is known that many electrical lines were powered for some period alter the tire occurred. It is liker that the higth localized ?ame removed the insulation from the wires very quickly while power was still on and the wires intlie bundle were then able to freely arc to each other. Detailed examinations of undamaged aimrali showed generally good wiring practices Were followed by the nmnul'ncturers, modi?cation centers, and maintainers. notable exception was the bcwragc jug wiring in the galley. No chat?cd wires, poor splices, or wires - all possible lire triggers - were noted on the undamaged aircraft. The route chosen for the beverage jug wiring in the galley is poor. The Wiring crosses a sharp edge created by a raised joint in the top shelf ot'the galley. behind the beverage jug connectors (Figure 8). Collected debris in this area could be a potential ?re source. if the beverage jug circuits are powered (Figure l2). . 18? Physical evidence indicates the most liker source of the ?re was a leak at junction 11. leading to local heating, followed by failure ot'the B?nut and then an uncontained oxygen leak Evidence indicates the most likely cause of the. leak was poor assembly practices in the oxygen tubing system. Poor assembly practices include use ofimproper fittings. use of damaged ?ttings. low torque values. intermittent torque striping, and self-contradictory manufacturing documents. Physical evidence could not identify the ignition source, although several well-documented ignition sources were available on the mishap aircraft. the possibility that the EPS provided the initialtriggcr mechanism for the ?re cannot be ruled out. How own: any conclusive evidence regarding the trigger mechanism was lost in the fin: and subsequent ?re?ghting actions. J-l3 V, 64?14848, Class A, 30 April 15, AFSAS #739726 15-030A J-14 V, 64?14848, Class A, 30 April 15, AFSAS #739726 FIGURES 10 J-15 64?14848, Class A, 30 April 15, AFSAS #739726 15-030A Figure . Condition of the wiring system in direct proximity of the mishap ?re, immediately after the incident. Red arrows are pointing to a damaged Wire hamess, and the yellow arrow points to a damaged coaxial RF cable removed for detailed analysis. Both examples Show a bright red color, copper oxide, which occm?s when copper is subjected to high ternperanu?es. 11 1?16 RC-I35 V, 64-14848, Class A, 30 April 15, AFSAS #739726 15-030A Figure 2. The GALLEY CONTROL PANEL on the mishap aircraft. The switches controlling the power distribution to the beverage jugs and galley light were found to be in the of? position. 12 1-17 64?14848, Class A, 30 April 15, AFSAS #739726 5-030A 0 Figure 3. The BOX ASSY HZ CB PANEL on the mishap aircra?. Red arrows indicate the circuit breakers that were found to he disengaged: MICROWAVE OVEN, CONVECF ION OVEN. and SPARE. The SPARE circuit breaker was mechanically prevented from being engagedForward Figure 4. Overall thermal gradient map of wire bundle. Zones A and show insulation still intact (less than Zones and show charred and melted insulation 2003C. - 3003C). Zones and show missing insulation 4503C). Zone shows red copper oxide and molten copper wire terminations (greater than 13 RC-135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Figme 5. Examples of molten copper wire terminations. Blue arrows point out individual wire strands and the red arrow points out a very sharp transition from the melted end to the wire strand; both are characteristics of an electrical arc. Green arrows point to wire strands melted together and yellow arrows point out gradual transitions ?'om melted end to wire strand; both are characteristics of extended exposure to high temperature. 14 J-l9 64?14848, Class A, 30 April 15, AFSAS #739726 l5-030A o" {211)2101 Figure Cram-sectioned wires with molten copper ends. The upper images are ofrhe molten ends and the lower images are of the wire a short distance back from the end. Blue arrows point to voids which indicate arcing occurred. Green arrows point out regions of struemred grain morphology, which is indicative ot'a copper exposed to high temperatures for an extended period oftirrie, 1-20 RC-135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 15-030A Figure 7. Bare conductor ?'om wire (left) on the forward end of the wire harness that displays a uniform, dull ?nish of tin plating. A dull appearance can be explained by exposure to elevated temperatures. The inner surface of removed insulation (right) shows no sign of discoloration or degradation Clean insulation indicates it did not experience prolonged temperatures above 2 16 J-21 V, 64?14848, Class A, 30 April 15, AFSAS #739726 AFRIJRXS 15-030A Figure 8. Beverage jug harness as it is routed in an exemplar aircra? (top). The red arrow indicates an unprotected spline that the wire is routed over; this is a potential cha?ng hazard over time given the high vibration environment. The incident harness (bottom) showed severe it ire damage once the wire entered the section from the top image (to right of green line). There was several molten wire terminations located within the blue circle. 17 -22 RC-135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 AFRLIRXS LONE ZDOJKS 201 5/05 I2 1 mm Figure 9. Damage created by applying a MAPP gas torch ?ame to a small wire bundle for approximately 5 minutes. This experiment proved it is possible to produce molten wire terminations without electrical arcing. . u? Figure 10. The convection oven (left) and microwave oven (right) wiring harnesses as?received Both cables showed little to no damage and slight discoloration of the insulation in areas exposed to the ?re. No evidence or electrical arcing or overcurrent was noted. 18 1-23 RC-135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Figure 11. Section ot?RF coaxial cable removed from damage site. The outer. comlgated shield was subjected to high temperatures for a prolonged period, as evidenced by the bright red coloration. There was no visual evidence arcing on the shield or inner conductor. Figure 12. Loose debris found in area behind beverage jug electrical receptacles of undamaged RC- 135V. 19 -24 RC-135K 64-14848, Class A, 30 April 15, AFSAS #739726 15-030A RH Fuselage Fill Station Flex Hose . . Ceiling Figure 13. Sections of the incident oxygen system in the as-received condition. Connections that leaked during pressure testing are highlighted with red arrows. Major scale division 1 inch 20 J-25 64?14848, Class A, 30 April 15, AFSAS #739726 5-030A Figure 1-4. Approximate location of oxygen system superimposed on image of mishap aircraft. Mishap aircraft photo submitted by the Safety Investigation Board. are numbered consisteme throughout this report. Major scale division 1 inch 1-26 V, 64?14848, Class A, 30 April 15, AFSAS #739726 *Three additional debris bags not pictured Figure 15. Components from near the galley in the ans-received condition. A piece ol'aluminum t?oil, reportedly found behind the microwave. was shipped in the top ot?the galley (not pictured). Wood colored scalc major division 1 inch Black scale divisions - liloth inch J-27 V, 64?14848, Class A, 30 April 15, AFSAS #739726 15-030A Flare Male Fitting - Sleeve Tu be Cone B-nut Placement of Loosely Finger sleeve and tube assembled tight Sleeve Tube Schematic of assembled junction Figure 16. Components of?ared ?ttings in various states ofassembly. Schematic at bottom illustrates a cross section of an assembled joint. The seal is provided by pushing the ?ared tube and cone ofthc male ?tting together. Threads do not provide any scaling. only the force required to press sealing surfaces together. to 1-28 V, 64?14848, Class A, 30 April 15, AFSAS #739726 AFRLERXS 5-030A Before disassemny After disassemny Figure 17. Close up of the elbow ?tting whose B-nut was missmg (junction 1 1). Fitting shows clear evidence that B-nut was attached while ?re deposited combustion products onto surface. Difference in colors between protected side and missing B-nut side (right) indicate that the B-nut side was exposed to some combustion products, but not as much as the unprotected body. Minor scale division 1/104h inch 24 1-29 V, 64?14848, Class A, 30 April 15, AFSAS #739726 AFRURXS Melted mate rial? highlighted in yellow . . SignalA=SE2 WD 20.8 mm File N0 2307 100w? Mag: 303x Figure 18. Missing B-nut fragment recovered fiom submitted debris bags, compared to an exemplar B?nut blue). Yellow highlighted area outlines material removal due to melting. Secondary electron image in lower portion of ?gure shows nodular formations and mud-flat cracking indicative of melting. Scale division 1/16m inch 25 J-30 64?14848, Class A, 30 April 15, AFSAS #739726 15-030A Light passing through flex hose Light does not pass through flex hose Damaged inner tube Figure 19. Flex hose between junctions 5 and I 1. Light passing through indicates inner tubing is completely destroyed near junction 5. CT imaging of ?ex hose near junction 11 shows rumpling deformation on inner tube: indicatmg exposure to heat. 76 1?31 RC-135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 15-030A 9'10 lI'Iol Q11: Figure 20. Nuts from all junctions alter disassembly. No signi?cant damage was noted, although there were bare areas on the inside ofthe nut?s bases. where the nut contacts the sleeve. Major scale division 8 1 inch 27 J-32 V, 64?14848, Class A, 30 April 15, AFSAS #739726 8 ulo'o. l?igure Cones ofmalc ?ttings after disassembly. Fitting 4, 5, and 6 had signi?cant damage to all cones and threads. This damage would be AS4841A. Major scale division - 1 inch 1-33 64?14848, Class A, 30 April 15, AFSAS #739726 Front 7/8/9 ?minimum .. - Back Figure 22. Comparison ot'the tee ?tting. The 4? 5. and6 ?tting does not have required ?tting markings? while 7. 8. and 9 does (red oval). Further, the trademark on the 4, 5. and 6 ?tting (circled in yellow) shows the ?tting ?as produced by Weatherhcad. Weatherhcad has not produced this type of ?tting since 2003. A parting line indicating the 4, 5. and 6 ?tting is a casting was found on the top ofthe tee. Major scale division 1 inch J-34 120-135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 AF 15-030A 14'2'3'4 5 6 7 8 No coating damage Circular contact at edge of contact area through coating b- - Figure 23. The ?ared tube ends after disassembly. All tubes, with the exception of tube 11, evidenced a circular contact area through the tube coating on the ?are. Sleeve #1 would not come off tube ?are All tubes ODs were consistent with 5/ 16th inch tube per AMS 4071. Tube ?ares were dimensionally consistent with AS4330. Minor scale division 1/16ti inch J-35 RC-I35V. 64-14848, Class A, 30 April 15, AFSAS #739726 AF 15-030A . - Figure 24. Sleeves alter disassembly. Sleeves 6 and are heavily discolored; the only sleeves discolored in the area are under the location of the B-nut. Major scale division 1 inch 31 1-36 V, 64?14848, Class A, 30 April 15, AFSAS #739726 AFRURXS Side 1 Side 2 SigmalA*SE 37mm Figure 25. Sleeves from junctions 6 and 11 alter cleaning with acetate replication. The junction 6 sleeve shows no pitting evidence that the discoloration is a contaminant. The junction 1 sleeve shows the discoloration is an oxide and pitting damage was found predominantly on one side. Secondary electron image of pitting in red boxed area shown at the bottom of the ?gure. 1-37 64?14848, Class A, 30 April 15, AFSAS #739726 AFRURXS 5-030A Dashed line indicates boundary of sleeve when it was on the tube 100 Mag 300 EHT =10 00 kV Signal A 552 wo 20 2 mm File N0 2393 Figure 26. Evidence of pitting on junction 1 ltube adjacent to sleeve alter cleaning by acetate replication. Similar to the sleeve, the pitting was more prevalent on one side of the tube. A secondary electron image at the bottom of the ?gure shows nodular formations, circled in red, inthe pit. The nodular formations are consistent with melting. Melting damage was localized in the pitted features. Black scale division inch 1-38 V, 64?14848, Class A, 30 April 15, AFSAS #739726 Breakaway Torque Values Found During Disassemny Table Nut Torque Number Break Awa: Torque (in-lbs) Strip130 1-39 34 15-030A RC-135 V, 64?14848, Class A, 30 April 15, AFSAS #739726 15-030A PREPARED BY Structural Materials Evaluation Team Electrical Electronic Materials Evaluation Team Materials Integrity Branch Materials Integrity Branch Systems Support Division Systems Support Division Materials and Manufacturing Directorate Materials Manufacturing Directorate Electrical Electronic Materials Evaluation Team Materials Integrity Branch Systems Support Division Materials and Manufacturing Directorate REVIEWED BY Team Lead a?mmrt? Materials Evaluation Team aterials Integrity Branch Systems Support Division Materials and Manufacturing Directorate PUBLICATION REVIEW: This report has been reviewed and approved. Branch Chief Materials Integrity Branch Systems Support Division Materials and Manufacturing Directorate 35 J-40 RC-135 V, 64?14848, Class A, 30 April 15, AFSAS #739726 Brandi Chief Team Lead Structures Team Lead Eledronic Materials Evaluations Team Lead Ai?iaives Composite 0 Failure Analysis/Accident Investigation - Structural - Electronic - Chemical 0 Consultations on - Materials/Process Speci?cations - Physical and Mechanical Metallurgy - Materials and Component Failure Analysis - Electronics and Packaging - Bonded Repair of N'Ietals/Composites - Nonmctallic Materials - Welding, Joining and Ad hesire Bonding - Electrostatic Discharge Control and Process Specs/Standards 0 Nondestructive Inspection 0 Electrostatic Discharge (ESD) Testing 0 ESD Material Quali?cations/Acceptance Testing 0 Composites Supportability 1-41 V, 64?14848, Class A, 30 April 15, AFSAS #739726 15-030A APPENDIX A Wire Number for Each Conductor in Large Wire Harness 37 1-42 64?14848, Class A, 30 April 15, AFSAS #739726 Label Wire Gauge Label Wire Gauge 1 1-284102820 20 41 Unlabeled Twiste dPair 16 2 20 42 C412 A 20 WHT C413 A 20 BLU 20 3 1-284100820 20 43 2O 4 1?284107820 20 4-4 C421-A2O 20 5 1-284106820 20 45 C416 A 20 WHT C417 A 20 BLU 20 6 1-858170822 22 46 1-623280A12 12 7 1-523272A22 22 47 l-283041A12 12 8 20 48 20 9 1-284111820 20 49 22 10 1-090013C20 20 50 C441A20 20 11 1484099820 20 51 C440A20 20 12 1-11CKIJ1A20 20 52 C422A20 20 13 1-090012C20 20 53 1-282628A20 20 14 1?090013820 20 54 C425A20 20 15 20 55 1471023416 16 16 1?284110320 20 56 C420A20 20 17 1-090012820 20 57 1-282624A20 20 18 C423-A20 20 58 C20 A18 ??-barely visible 18? 19 H426A20V 20 59 1-06248982020 20 20 1?284098820 20 60 1-623275A20 20 21 1-858322A22 22 61 C427-A20 22 1-284103820 20 62 - not visible 23 1-062460A20 20 63 1-110011A20 20 24 1-284108320 20 64 1-284105820 20 25 20 65 20 26 C438A20 20 66 20 27 1-623170A12 12 67 C426-A20 20 28 1-1851CDA20 20 68 1-623135822 C411A20 C410A20 20 31 20 71 22 32 1-623133A22 22 72 20 33 1-350010A20 20 73 20 34 C408 A 20 WHT C409 A 20 BLU 2O 74 1-623135A22 22 35 C414 A 20 WHT C415 C418 A 20 WHT C419 Unlabeled Twisted Pair 12 78 20 39 Unlabeled Twisted Pail 16 79 1-720030A16 16 40 20 80 1470301820 20 38 1-43 64?14848, Class A, 30 April 15, AFSAS #739726 Label \Mre Gauge Label Wire Gaug_e_ 81 1470302320 20 121 20 82 1470300320 20 122 13284656A20 20 83 1-185132A20 20 123 1-284657A20 20 84 1-185127A20 1-72CX195A20 20 126 1-185121A20 20 87 1-0624S7A20 20 127 1-287172A20 20 88 1-858321A22 22 128 Unlabeled 4\Mre twisted 20 89 C147AZOV 20 129 Unlabeled 4Wire twisted 16 90 C437A20 20 130 Unlabeled 4 Wire twisted 16 91 20 131 Unlabeled 2 Wire twisted pair 12 92 14701441120 20 132 Unlabeled twusted pair 12 93 C429A22 22 133 Unlabeled 2 Wire twisted pair 12 94 18 Wires that branch of! on forward bundle 95 L50820V 20 134 1-858261A22 22 96 1-284633A20 20 135 1-282654A20 20 97 1-623146A22 22 136 1-858260A22 22 98 C146A20V 20 137 1-751401A18 18 99 22 138 1-858268A22 22 100 14200241120 20 139 1-858271A22 22 101 17211131816 16 140 1-858263A22 22 102 12846421120 20 141 1-858269A22 22 103 1-471022C16 16 142 1-858270A22 22 10411-47CD74418 18 143 1-751402A18 18 105 1-470305B20 20 144 1-858270A22 22 106 1470304320 20 145 1-858266A22 22 107 1470303820 20 146 1-858277A22 22 108 1-185130A20 20 147 22 109 1-185125A20 20 148 1-858276A22 22 110 C248A20V 20: 149 1-858259A22 22 111 Unshielded 1P unreadable 150 1-858267A20 20 112 Unreadable 151 1-251083A20 20 113 22 152 1-858323A22 22 114 1-341015H20 20 153 20 115 1-470104D20 20 154 20 116 1-185120A20 20 155 1-553474A20 20 117 1-185135A20 2 156 1-55347SA20 20 118 1-283042A12 12 157 1-858264A22 22 119 1-284578A20 20 158 1-858262A22 J-44 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB K MISSION RECORDS AND DATA K1. FLIGHT PLAN AND FLIGHT ORDERS ......................................................................... 2 K1.1. DD FORM 175 ............................................................................................................... 2 K1.2. FLIGHT ORDERS ........................................................................................................ 3 K2. AIRCRAFT WEIGHT AND BALANCE ........................................................................... 5 K-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK K-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 K1. FLIGHT PLAN AND FLIGHT ORDERS K1.l. DD FORM 175 mm Yam-?mu w? SNooe 7A A 4/er w?35r; m: AND [Mishap Pilot] 4 am?- K-3 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 KLZ. FLIGHT ORDERS CREW FLIGHT (FA) AUTHORIZATION l. PREPARED DATE, 2. 3 DE RE LOCATION. 4 DESTINATION 20150429 KOFF343X15120A KOFF KOFF 5. MISSION SYMBOL AND PURPOSE 6. DEF 7 SCHEUJLED RET Taxz 20150501 00002 20150501 08002 a AERO vsu?e. ACFT Thur pi: CALL Slat RC1 35V 84 4848 PRIVACY ACT AUTHORITY 10 0.8.0 8013; 0.8.6. 3101; AND E0 9397 PRINCIPAL PURFOSE: Sauce commonl used in almanac sum memoirs it: perform ill?man 0mm lor im avail am crawls accounth for aircrew ?noan on "union mod to vallaam almraw Mac for mm I: ma?: um, madam aging may email. and ?9m pay movement; IS VOLUNYARV: SSAN is needed in meat qualifiullon for meant-billy. will documuualm. Ind pay armaments Failure lo pmvlae my men Duhmb? a ?y mu result -n a loss 01 means. quallroallom Ind pay mum 11- CREW MFORMA A a ll NM same 83M sec. mew caew mm FOR muss cur P05 P05 RES cone 3 CH5 [Misnap Pilot] cw MPAN A 0343 1 [Mishap Co-Pilot] cm MCAE MCAE 0:43 2 [Mishap Navigator] on MNAE MNAE 0343 3 [Mishap Airborne Systems Engineers? we: MW 0343 4 ssu ?m3 leaa 034:. 5 A10 a 0m 6 TSGT mum W4 8 0343 7 . MAJ EEAET 0343 a cw EEAET IEAET 343 9 1LT MEAMX MEANX a 0343 10 MAJ UEINT UEINT 0343 11 MEANX 0343 12 12? REMARKS. (Vanni/on. In Enemy o. Plloi- G- Femllo Cm member A- Aha-h Commuer 0r Pilot In Command H- IB- Mon-cumant z- c-Acung in Higher umn?callon for Evaluation Purposes. R50 1 1: Mlive Duty. R30 2 Unit Training Assamny (Inactive Duly). R36 3 Training Period (inactive Period)J R86 4 8 Civilian Technician DA 14 FA NUMBER l5. DISTRIBUTION 20150429 15-0155 is come .00 gamma checkswem Walled fol aircrew womb-rs listed below. A: a physiaal. physical enlisting physicioolal tuning. emerge-ml egress. local area survival. Asc, (A0 gnu-ave usraenn dale) Aw I A03. FCIF card. and any other 9mm events ware cleaned won- 0 current for aimw training or drum qmliflallon have appropriate remarks codes and mum is aboard for Mr smelly Rem: persona-i no: car extendao duty are sumac! to he pruvm oilha uniform code of Military tum, while Mammy this duty rem lulu-l0: Aim-ll! Commander Mm: . mamas ORIGML CREW MEMBERS: I can? in above gum-90 check! ware Manned for alarm member Bl awed- Airuaft Commnar Signal-n: l7 UHF AND LOCATION OF AUTHMIZINO ABENCY IO SGMATURE ELEMENT OF AUTHENTICAHNG 343 RECCNNAISSANCE SQUADRON AFB. NE (ACC) L'apl. USAF [Assistant Direcror oi 19. AF IMT 4327; 20031 201 (V1) ARE oasarn: RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 70 CREW INFORMATION (CONVD) B. D. 2E: 0] MC IEAET a 0343 13 MSGT EQAEA MOAEA 0097 14 1LT 0097 15 SSGT MOANL MOANL 0007 1a SRA MOANI 8 0007 ?7 MSGT EQAEM MQAEM 0097 19 MSGT MDINL MOINL 0097 19 SRA MQANL 0097 20 SRA MOANL MQANL 0097 21 SSGT MQXEL ~10st a 0097 22 CMS 50951 MOBE1 0097 23 CPT MMNI MMNI a 0097 24 5567 IOAEL IOAEL a 0097 25 SRA MQANL MQANL a 0097 26 5507 IQAED MQAED 0097 27 27507 REMARKS (Cam?d) AF IMT 4327!, 20031201 (REVEGSEXW) RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 K2. AIRCRAFT WEIGHT AND BALANCE WEIGHT AND BALANCE CLEARANCE FORM TACTICAL "m ?or; itemize 64-14848 17? om:an . nommuosr Anconasmus Er tram warm uoex "Ugh-v? .w Esmw momma? 1L m: 753 MM _n WEIGHT INDEX _La Ig on.) 1, CMFT, no. Iom'__ gleam I 1 A. 8-1 5 1250 0' 1250i - __32?44 01 32.4 2 $0 - _0 11:9. L- I 510 1 2.50 250 393. 1 580 2 500 30.3 _o3_ 0 30.3. _4 ?10 H. 1 _250, 0; 250 30.1 WW I 2 500__. .22; .960 430., 2 500 0 500 30.2 ?90 2 5.00 0 _5_00__Ji _3 .3359: 2 500 3.140 1110' 5. 15.0.0. 15.00.. 1m g? 0 33.0 1220 9 33.1 1? 1260 a o_ 33,0 A -4. ?"70"?237 6750 _sg_5_9_I_ WEIGHT ADDED 1' - - 4] amines new? . Fool lime 6.7lbs/gal Plum-d Fun-I: YAKEOFP LANDING manna RES 5816 - 3* - 08 (500) 28314 a '9 (500) 30538 0 - 2: 2:22: 2 3 ?wo 16000 0 176835 A 33.0 UPDK 0 RAMP 105000 0 - - 4 mu -1009 104000 FUEL mm 44.5 I ?1 uumnous (m 29:) 3.39? 280.835! 44.6 1 new: (3.32.14. .3225? 3225?? 32. 188% 330% :3 Tm?wgma? ML I *j gaf?mg? ?Lnaoruawem ,4 116835. 33._o PERMISSISLE cc ?7 CIL FUEL .9 33 I 18.0% 33.0% . a! ?Mm-m I i i 3311] ESTIMATED CONDITION 3?0 1 17 'Ea'nmrau LANDING co as we 21 DD FORM 385-4 TACTICAL. Computer Generated - DAPA c135 Weight and Balance Calculator 2.0, 10 Apr 2013) RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB L FACTUAL PARAMETRIC, AUDIO, AND VIDEO DATA FROM ON-BOARD RECORDERS L1. PARAMETRIC DATA ......................................................................................................... 2 L1.1. FLIGHT DATA RECORDER ....................................................................................... 2 L2. AUDIO RECORDINGS ....................................................................................................... 3 L2.1. COCKPIT VOICE RECORDER .................................................................................. 3 L3. VIDEO RECORDINGS ........................................................................................................ 4 L4. REPORTS GENERATED UTILIZING PARAMETRIC DATA .................................... 4 L-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 L1. PARAMETRIC DATA L1.1. FLIGHT DATA RECORDER The mishap aircraft was equipped with a Flight Data Recorder. The parametric data can be found in the following files. 1.1.1. FDR_RS81_Time_History_Data.xlsx 1.1.2. FDR_RS81_P_V_Data.xlsx 1.1.3. 48488AC.rdf 1.1.4. FDR_Parameter_List.xlsx 1.1.5. FDR_RS81_Documentary_Data.xlsx L-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 L2. AUDIO RECORDINGS L2.1. COCKPIT VOICE RECORDER The aircraft was equipped with a cockpit voice recorder. The audio files can be found in the following files. 2.1.1. 848_cvr_mic1.wav 2.1.2. 848_cvr_cam.wav L-3 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 L3. VIDEO RECORDINGS No data applicable. L4. REPORTS GENERATED UTILIZING PARAMETRIC DATA No data applicable. L-4 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB M DATA FROM GROUND RADAR AND OTHER SOURCES M1. MEMORANDUM FOR RECORD .................................................................................... 2 M-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 M1. MEMORANDUM FOR RECORD DEPARTMENT OF THE AIR FORCE HEADQUARTERS AIR COMBAT COMMAND JOINT BASE LANGLEY-ELISTIS VA 20 May 2'315 MEMORANDUM FOR. RECORD FROM: Safety Investigation Board SUBJECT: Tab M, Class A Mishap, 64-14848, 30 Apr 2015, AFSAS #73 9726 l. I am the Board President for the mishap convened at Of?itt Air Force Base which occurred on 30 Apr 2015. The ?nal report will include no data in Tab M: Data From Ground Radar And Other Sources. In accordance with 91?223 paragraph 6.4.2., this memorandum Serves to document the fact that there is no radar or other source data applicable to this mishap. 2. Please direct questions to me at DSN 312-969?2?76 or Commercial Colonel, USAF Safety Investigation Board President RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB N TRANSCRIPTS OF VOICE COMMUNICATIONS N1. COCKPIT VOICE RECORDING TRANSCRIPTS ......................................................... 2 N2. AIR TRAFFIC CONTROL TRANSCRIPTS .................................................................... 3 N3. COMMAND AND CONTROL TRANSCRIPTS ............................................................ 11 N4. OTHER AVAILABLE TRANSCRIPTS .......................................................................... 11 N-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 N1. COCKPIT VOICE RECORDING TRANSCRIPTS No data applicable. N-3 RC-135V. 64-14848. Class A. 30141917115. AFSAS #739726 N2. AIR TRAFFIC CONTROL TRANSCRIPTS DEPARTMENT OF THE AIR FORCE HEADQUARTERS. 551' WING (AGO) OFFUTT AIR FORCE BASE NEBRASKA 8 May 2015 Subject: SNOOP 7 Ground Emergency Recording Facility; Offutt Tower List of Facilities/Positions: Oi?futt Tower Local Control (OFF TWR LC), OFfutt Tower Gmund Control (OFF TWR Of?m Tower Watch Supervisor (OFF TWR WS). OFF Ramp Net. OFF Crash Net. Omaha Approach Control (OMA TRACON), Unknown (1 Unintelligible Transmission requency/Position: Ol?futt Tower Local Control 120.] Omaha Approach Control Shout Line. OFF Ramp Net, OFF Crash Net Date/Time: 30 23:24:15 - 30 Apr] 5 23:39:52 Time Source; Reconstruction from Digital Audio Legal Recording ?l certify this to be a true and exact transcript of the orieinal recording on ?le at this of?ce at Offutt Air Force Base? E-3 Transcription Date- 8 May 2015 1000 23:24:15 OFF LC: Snoop7l heavy, runway 12, wind calm. cleared for takeoff, caution wake turbulence heavy c135 departure. 23:24:23 Snoop7l heavy is cleared for takeoff runway 12. 23:25:23 Tower, uh. tower snoopll heavy is. uh egressing on the, uh runway, aboning the aircrati. 23 25:32 OFF TWR LC: Snoop7l heavy roger say nature of emergency, number of persons on board, and fuel remaining in pounds. 23'25236 ll-i: Snoopl i has a ?re. uh roll the. uh trucks at this time. 23:25:41 OFF TWR LC: Roger. 23 :25242 OFF TWR LC: Approach. Offutt Tower. 23:25:46 OMA Approach. 23 :25 :48 OFF TWR LC: Emergency in progress. hold the Cessna and ail my arrivals. 23:25:50 OMA TRACON: Cessna?s already on you, ship ?em back to me. 23 :25 :54 OFF TWR LC: And Snoop, cancel release on Snoop, he had a ?re. 23:25:56 LC: Victor Whiskey. 21:25:57 OMA TRACON: H. N-4 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 23:25:59 OFF TWR LC: Attention all aircraft runway operations suspended, emergency in progress, break, Cessna 3? Romeo contact Omaha approach 120.]. 23:26:09 Nil-93711: Switching to approach, 120.1. Cessna 3? Romeo. 23:26:40 UNK: Standby stations 1 and 2 for an incoming in?ight emergency. Repeat standby stations 1 and 2 for an incoming in?ight emergency. 23:27:?1 UNK: Attention in the station, attention on the net, ground emergency t'ull crash response. C135 type on Northwest section of runway. Fire reported. crew is evacuating. 23:27:25 LINK: Attention in the station, attention on the net. ground emergency full crash response. On Northwest section of runway C135 type. Fire reported on aircraft no ?rrther details. crew is evacuating. 23:27:49 UNK: Crew?s out. 23:27:51 UNK: Copy. 23 ?755 OFF TWR GC: Offutt Towor?s up on the crash net. 23 128:01 Tower, chief 2 pcnnission for myself and other ?re deparnnent vehicles to access the runway. 23 23:03 OFF TWP. GE): Chief2 Of?Jtt Tower, proceed on the runway as requested. 23:23:12 LINK: Crash out- 23:23:15 LINK: 16?s out. 23:23:13 UNK: 9?s out. 23:23 :20 PHOEN 13.5: foutt Tower, Phoenix?- 23:23:21 out. 23:23:25 OFF TWR Last calling to tower say again. 23:23:29l PHOENIXS: foutt Tower this is PhoenixS. 23:23:32 OFF TWR. GC: Phoenix?1 tower. 23:23:36 PHOENIXS: Offutt Tower this is Phoenix? requesting permission to enter runway at Juliet apron. RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 23:28:38 CHIEF2: Tower, chief 2 is the aircra? on the hammer head or on the runway? 23:23:42 DMA TRACON: Tower. approach. 23:28:44 OFF TWR LC: Tower. 23:28:45 0MP. Transition request Cessna Romeo, l-?rr. Just going to have him hold to the Southwest of Offutt. 23:28:46 CRASHB: Chiet'2 this is crash 3. The aircraft is on the runway right now. Ofihtt show crash 3 arriving on location. We got a 135 type aircraft, complete stop on The runway. Crew is regressing at this time, I got no smoke or ?re. Go ahead and establish command of this aircraft. 23:23:51 OFF TWR LC: Yea that?s ?ne1 TV'ictor Whiskey. 23:23:52 OMA TRACUN: H. 23:23:53 OFF TWR GC: Phoenix? say again, something about an aircraft on Juliet. 23:29:10 Lib-Iii: Medic?s in service. 23:29:14 LINK: Chief 2 is on the scene and will be taking command of the aircraft. 23:29:20 BASE DPS: Air?eld 3, air?eld Ops. 23:29:23 AIRFTELD 3: A OPS, Airfield 3, go ahead. 23:29:25 UNK: Chief 2 will he going over to talk to the aircrew to f'uid out what?s going on. 23 29:23 BASE OPS: Air?eld 3. Airfield Ops. he advised there's a ground emergency in progress. 23:29:32 CRASHS: Command crash 8. 1 do have smoke showing from over wing door, ulL left side of the aircraft fuselage. 23:29:35 AIRFIELD 3: Air?eld 32 A OPS copies thank you. 23 :29:54 UNK: Letis get a ladder out, or excuse me, get on the aircraft and we have a galley ?re in the hack of the aircraft under the stabilizer. 23:30:06 UNK: 16 Copies. wait hang on. 23:30: 10 CRASHS: This is crash 8, 1 got smoke also coming from a Peto tube on the aft of the ?iselage,just Forward of the tail. 23:30:19 LINK: Copy that. RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 23:30-32 UNK: Four get a ladder off the truck and get it up there. 23:30:44 AIRFIELD 3: Tower air?eld 3 request permission onto the runway from taxiway Lima. 23 30:47 OFF TWR GC: Airfield 3 proceed on runway 12 from Lima, report off. 23:30:51 AIRFIELD 3: Tower air?eld 3 proceeding on runway 12 from Lima will advise off. 23:31:12 LINK: Crash 16 and crash 4. you?re going to be ?re attack. Crash 3 you?re going to he the red team. Tanker go ahead and get tea-supply on 16 and 4. 23:31 :10 OM TRACON: Tower. approach. 23:31:19 OFF TWP. LC: Tower. 23:31 :20 OMA TRACON: Any idea how long, I?ve got Snoop 44 asking. 23:31:23 OFF TWR W5: Undetermined at this time1 the aircraft on the runway, he aborted. He has a no lire on his airplane. We don?t lorow how long it?s going to take. 23:31:28 UNK: Tanker copies. 23:31:31 LINK: Also I?ve designated the personnel safety of?cer and probability at this time. 23:31:32 DMA TRACDN: 0k. B. 23:31 :33 OFF TWR WS: Charlie Echo. 23:31:46 UNK: Dispatch go ahead and make noti?cation to the tower. I want the air?eld shutdown at this time. Make notification of aircraft ?re. 23:31:57 OFF TWR GC: Tower copies all thank you. 23:32:01 LINK: Command, 11 we?ll get tanker 10. 23:32:03 WK: 16, command entering with 4. 23:32.19 LINK: Crash 3 go ahead and chock the aircraft, if you can. 23:32:29 UNK: We have an electrical ?re here 23:32:32 UNK: I copy 23:32:38 LINK: Copy, make sure you take a 1:11-11r chem extinguisher to with you, if? you haste one handy. RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 23:32:44 LINK: 23:32:43 LINK: Copy that. 23:33:11 ANKER 10: Command. tanker 10, we?re going to resupply crash 16 and crash 3. Those are the ones with the hand lines ?Jll. 23:33:19 LINK: Copy that, that?ll be ?ne, break. dispatch, command I?ll need medics here. We have personnel that have had smoke exposure. 23:33:30 UNK: Copy. how copy medic 23 :33:34 UNK: Copy coming out of the gate. 23:33:39 LINK: We?re going to need multiple medics because they?re saying that almost all personnel had smoke exposure. There 27' personnel on the aircraft. 23:33:49 LINK: 11 West gate please. 23:33:51 UNK: Copy all. 23:33:54 LINK: 16, command you got ?ames showing out ofthe tail. 23:34:00 LINK: 23:34:05 LINK: Let?s go get a hand line on the outside set ready to attack it. 23:34:12 LINK: We have ?ames showing through the skin of the aircraft. 23:34:16 LINK: Copy are we getting ?re. ., or we getting foam on the ?re on the interior guys? 23:34:13? LINK: Do you see this? 23:34:26 LINK: 16, are you on foam? 23 34:29 LINK: Af?rmative. 23 :34131 LINK: Copy crash 4 some down a little bit with a turret. come down with turret just a little hit, some down with your turret. 23:34:43 UNK: Four to your left a hair. 23:34:47 LINK: You?re right on it 4. 23:34:50 LINK: Command. 11?s on the runway. RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 23:34:54 UNK: Straight stream on that 4- 23:34:59 UN K: Command, can we reposition 4 to the back end. 23:35:04: LINK: Copy. crash 4 reposition. 16 take over with the turret on the ?re. 23:35:14 UNK: Command 1 1'5 read},? for assignment when you have one for us. 23:35:19 Copy bunker out. Come on up here and get ready to man the hand line. It looks like they?re getting her knocked out right now. 23:35:23 WK: 23:35:38 UNK: 11, give me a 35 foot ladder and get ready to go ahead and ladder that back of the aircraft. I don?t know it?tltey?re able to get to the ?re area or not. You may have to take a hand line up there. 23:35:49 Copy you Want that in the rear personnel door? 23:35:54 UNK: I want that back by the stabilizer, rear stabilizer. 23:35:59 UNK: 11 copies. 2336132 UNK: Control medical. 23:36:11) NK: We?ve just got the two ot?us, and we?re running ALS and need multiple medics. copy? 23:36:15 LINK: [need ventilation now. inside the aircraft. 23:36:24 UNK: Fire attack repeat. 23:36:41] UNK: Fire attack repeat. 23:37:08 MEIZM: Med 4 to control. did you copy? We're gonna need more medics, uh, ALE if you need ?etn. 23:37:23 COMMAND: Dispatch, command I'm gonna go to trip 1 with you. I?m gonna leave the fire crews on ?re main, break. crash 4 round up another sets of chocks, and put them on the back of the aircraft at this time. 23:37:40 FIRE ATTACK: Command, fine attack. Request a ventilation fan for the inside ofthe aircraft. I need engine 9 with power. 23:33:03 UNK: 16. 4 come down about 3 feet. RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 23:33:09 UNK: 23:38:13 LINK: 9 1,1?ve got engine 11 crew bringing a Ventilation fan up to the wing. 23 53:25 CRASHS: Interior, crash 8. Do you guys have a change ofoondition in there, are we making arr}r headway on this? 23:38:33 LINK: 23:38:37? PHOENIXS: Offutt tower, Phoenix 5. 33:38:40 OFF TWR GC: Phoenix 5, tower- 23:38:42 UNK: No cop).r interior, re advise chief. 23:33:43 PHOENDCS: 49 we?re almost there, Offutt tower phoenix 5. 23:38:48 UNK: 23 53:52 OFF TWR GC: Phoenix 5 O??utt tower. 23 38:56 PHOENJXS Yes ma?am this is phoenix 5 requesting permission to enter at Lima to the aircraft on runway. 23 39:03 OFF TWP. GC: Phoenix 5 proceed on runway 12 from Lima. 23 .3930? PHOENIXE: Roger, will advise when off. 23:39:20 Tower, air?eld 4. 23:39:35 OFF TWR GC: Air?eld 4, tower. 23:39:39 AIRFIELD4: Tower, air?eld 4 request permission to go onto runwayr from taxiway Lime. 23:39:34 OFF GC: Air?eld 4 proceed on runway 30 From Lima report off. 23:39:40 AIRFIELD4: Tower air?eld 4 proceeding onto runway from taxiway Lima, will report when off. 23:39:44 UNK: 1 are you setting that ladder up there for the top of the aircraft? 23:39:52 UNK: We need additional manpower. RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 END OF TRANSCRIPT RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 N3. COMMAND AND CONTROL TRANSCRIPTS No data available. N4. OTHER AVAILABLE TRANSCRIPTS No data available. N-12 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB O ANY ADDITIONAL SUBSTANTIATING DATA AND REPORTS O1. DOCUMENTS OR RECORDS REVIEWED BY THE SIB ............................................ 2 O2. AEROSPACE INFORMATION REPORT 825-13 ........................................................... 4 O3. BIG SAFARI PROGRAM MEMORANDUM OF AGREEMENT ............................... 35 O4. FIRE DEPARTMENT INCIDENT REPORT ................................................................. 54 O-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 O1. DOCUMENTS OR RECORDS REVIEWED BY THE SIB 3-3.RC-135.............................Tactical Doctrine, Combat Aircraft Fundamentals – RC135 (11 Jan 13) 55 CES/CEF AAR .................After Action Report/Lessons Learned RC-135 Aircraft Fire (30 Apr 15) 55 OG Form 25 ......................55 OG Mission Planning/Briefing Certificate AFI 10-203 .............................Duty Limiting Conditions (20 Nov 14) AFI 11-2RC-135V3 ...............RC/OC/WC/TC-135 Operations Procedures (22 Apr 10) AFI 11-202V1 ACCSUP .......Flying Operations – Aircrew Training (22 Nov 10) AFI 11-202V3 ACCSUP1 .....General Flight Rules, Air Combat Command Supplement (28 Nov 12) AFI 11-301V1 ........................Flying Operations – Aircrew Flight Equipment (AFE) Program (2 May 14) AFI 11-301V2 ........................Flying Operations – Management and Configuration Requirements for Aircrew Flight Equipment (AFE) (30 Mar 15) AFI 32-2001 ...........................Fire Emergency Services (FES) Program (27 Feb 14) AFI 48-123 .............................Medical Examinations and Standards (31 Oct 14) AFI 48-149 .............................Flight and Operational Medicine Program AIR 825-13 ............................Aerospace Information Report – Guide for Evaluating Combustion Hazards in Aircraft Oxygen Systems (1 Jan 03) AFMAN 24-204 .....................Preparing Hazardous Materials for Military Air Shipments (3 Dec 12) Checklist ................................RC-135V/W ASE5 Mission Crew Checklist, Baseline 11, Change 2 (6 Feb 15) Medical Reference .................Air Force Waiver Guide (5 Mar 15) Medical Reference .................Medical Standards Directory (6 Oct 14) Medical Reference .................Official Aircrew OTC Medication List (9 Jan 14) Medical Reference .................Official Aircrew Prescribed Medication List (15 Mar 15) T.O. 00-105E-9 ......................Aerospace Emergency Rescue and Mishap Response Information (Emergency Services) (1 Apr 15) T.O. 1C-135-2-2-2 .................Ground Handling, Servicing, and Airframe, RC-135V (15 Mar 15) T.O. 1C-135-2-3-1 ................Environmental Control Systems, USAF Aircraft Models KC-135R/T (15 Mar 15) T.O. 1C-135-2-3-2 .................Environmental Control Systems, USAF Aircraft Models RC-135V (6 Feb 15) T.O. 1C-135-2-10-1 ...............Electrical Systems, USAF Aircraft Models OC/NC/RC/TC/WC-135 (1 Mar 15) T.O. 1C-135-6WC-1 ..............Preflight/Postflight/Hourly Post-Flight Inspection Workcards – USAF Model All 135 Aircraft (9 Jan 15) T.O. 1C-135-6WC-7 ..............Hourly Inspection Workcards – USAF Model All 135 Aircraft (15 Nov 14) T.O. 1C-135(RC)-1 ................Flight Manual Reference Data (1 Apr 14) T.O. 1C-135(RC)(I)-1 ............Flight Manual Inflight Data (1 Apr 14) O-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 T.O. 13B1-3-4 ........................Illustrated Parts Breakdown – Whirlwind Oven (1 Feb 65) T.O. 13B2-7-1 ........................Overhaul Instructions and Parts List – Aircraft Skygalley (18 Aug 90) T.O. 13B5-5-2 ........................Intermediate and Overhaul Instructions – Electrical Refrigerator (15 May 13) T.O. 15X-1-1 .........................Oxygen Equipment (1 Apr 15) T.O. 15X-1-102 ......................General Care and Cleaning of Oxygen Gauges and Oxygen Device Related Test Equipment (31 Jul 12) T.O. 15X2-2-5-13 ..................Overhaul Instructions – 25-Liter Liquid Oxygen Converter (15 Jun 05) T.O. 15X6-4-3-3 ....................Overhaul – Demand-Pressure Breathing Oxygen Regulator Assembly (1 Apr 10) T.O. 35E22-3-4-42 .................Maintenance Instructions – Purging Kit, LOX Converter (15 Dec 04) T.O. 35E22-3-4-43 .................Overhaul Instructions – Purging Kit, LOX Converter (1 May 14) T.O. 35E22-3-4-44 .................Illustrated Parts Breakdown – Purging Kit, LOX Converter (1 Sep 05) T.O. 42E1-1-1 ........................Aviation Hose and Tube Manual (1 Jul 13) SGOW OI 44-03 ....................Mental Health (MH) and Alcohol and Drug Abuse Prevention and Treatment (ADAPT) Records Management O-3 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 O2. AEROSPACE INFORMATION REPORT 825-13 O-4 RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE TABLE OF CONTENTS I tu'arrll'i urnir" arena. tI\- Ill': .rnlr' - I .TI new!? n-?l ru- in! 1. SCOPE ..4 1.1 Purpose ..4 2. REFERENCES ..4 2.1 Applicable Documents ..4 2-1-1 SAE Publications ..5 2.1.2 ASTM Publications ..5 2.1.3 Other Applicable References ..5 2.2 De?nitions ..5 3. BACKGROUND ..6 3.1 What Factors Cause Fires ..6 3.2 Causes of Fires and Explosions ..S 3.3 Selection of Metals for Use in Pressurized Oxygen Equipment ..11 3.3.1 Metal Choices in Oxygen System Designs ..11 3.3.2 Selection of Non Metals for Use in Pressurized Oxygen Equipment ..12 3.3.3 Critical Locations for Risk of Combustion in Oxygen Equipment ..13 4. THE PROCESS TO REDUCE 4.1 The Issues in Oxygen Equipment Development ..13 4.2 Oxygen Systems Operations and Maintenance -.15 4.3 Application of the Hazard Analysis Process ..16 5. HOW TO DO AN OXYGEN SYSTEM HAZARD ANALYSIS 5.1 Resources and Program Issues to Consider to Perform in the Process 5.2 Hazard Analysis Overview 5.3 Hazard Analysis Steps ..19 5.4 Contamination Assessment ..21 5.5 Detailed Oxygen Hazard Analysis Procedures ..22 5.5.1 Oxygen Application and Inyestigation Scope ..22 5.5.2 Oxygen Hazard Analysis Team ..22 5.5.3 Component and System Information -23 5.5.4 Worst-Case Operating Conditions ..24 5.5.5 Material Flammability 5.5.6 Ignition Mechanisms ..25 5.5.7 Secondary Effects Analysis ..26 5.5.3 Reaction Effects Assessment ..25 5.5.5 Recommendations and Conclusions ..26 5.6 Evaluation of Results and Actions Taken I I .ns I Nun?J ?0510' 7?5 :4 0?5 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE TABLE OF CONTENTS (Continued) 6. AN EXAMPLE NOTES 7".1 Key A EXAMPLE OF A HAZARD ANALYSIS ON A NEW DESIGN FOR A PRESSURE-BREATHING REGULATOR ON A HIGH-PRESSURE (2000 PSIG) CYLINDER .29 -3- RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE AIR325I1 3 1. SCOPE: This guide is intended to promote safe designs. operations and maintenance on aircraft and ground support oxygen systems. This is also a summary ofsome Work by the ASTM 4 Committee related to oxygen ?re investigations and design concerns to reduce the risk of an oxygen ?re. There have been many recent technological advances and additional test data is available for evaluating and controlling combustion hazards in oxygen equipment Standards that use this new information are rapidly evolving. A guide is needed to assist organizations and persons not completely familiar with this process to provide oxygen systems with minimum risks of combustion- This guide does not necessarily address all the detailed issues and provide all data that will be needed. For a complete analysis. supplemental publications need to be consulted. This guide does discuss the basics oi oxygen systems fire hazards. The hazard analysis process is disoussad and a simple example to explain this process. Also. this guide does not address the overall system safety issues normally evaluated in aircraft programs. This guide does provide some important background and observations about combuotion in oxygen systems. Infon'nalion is given describing how to accomplish a hazard analysis. Furthermore, background is provided to explain critical locations in oxygen systems that need to be evaluated and other locations that do not require hazard analysis. It is important to note that any effort that requires a comprehensive and effective hazard analysis should Use the complete information in the documents referenced herein. in general. the need for a hazard analysis applies primarily to gaseous oxygen equipment at SCI psi and higher pressures. LOX equipment does have hazards concerns as well and is usually treated similarly to GOX equipment at 500 psi. It should be noted that there are other phenomena associated with LOX equipment that must be considered. An example is that LOX can combine with hydrocarbons to form a gel. which explodes under impact. 0n the other hand. since LOX is a very cold liquid ittends to quench most possible ignition sources that could cause promoted ignition. When examining oxygen equipment at lower pressures the primary concern is the increased ignition and fire concern with combuatible non?metals. 1.1 Purpose: This document is intended to provide a guide for minimizing the risk of combustion hazards associated with the design. installation. and maintenance of aircraft oxygen systems. This guide also discusses a process of planning and organizing a project assisting someone who wishes to evaluate an oxygen system{s) such that combustion risks are minimized. The use of this guide and supporting documentation in part or whole is entirely elective. 2. REFERENCES: 2.1 Applicable Documents: The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue in effect on the date of the purchase order. In the event of conflict between the text of this document and references cited herein. the text of this document takes precedence. Nothing in this document, however. supersedes applicable laws and regulations unless a specific exemption has been obtained. at; unnl- 1 um I. arc-eon .e any,? a r-j [Ir-1m Fug": JF-r-??urz? 0?7 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE 13 2.1.1 2.1.2 2.2 SAE Publications: Available from SAE. 400 Commonwealth Drivo. VIJarrendale. PA 15096-0001. Bibliography of References Pertaining to the Effects of Oxygen on Ignition and Combustion of Materials Oxygen System and Component Cleaning and Packaging AIR4DT1 Lubricants for Oxygen Use ASTM Publications: Available from ASTM. 100 Barr Harbor Drive. West Conshohocken. PA 19428?2959. ASTM 2863 Standard Test Method for Measuring the Minimum Oxygen Concentration to Support Candle-Like Combustion of Plastics (Oxygen Index) ASTM 63 Guide for Evaluating Nonmetallic Materials for Oxygen Service ASTM 88 Guide for Designing Systems for Oxygen Service ASTM 93 Practice for Cleaning Methods for Material and Equipment Used in Oxygen- Enriched Environments ASTM 94 Guide for Evaluating Metals for Oxygen Service ASTM 123 Standard Guide for the Control of Hazards and Risks in Oxygen Systems Other Applicable References: Dees. J., and R. F. Poe. Test Plan: Guide For Oxygen Hazards Analyses on Components and Systems. NASA Johnson Space Center. White Sands Test Facility. Las Cruces. NM July ?.1993 Bamford. L. B.. and M. A. Rucker. Guide for Oxygen Component Quali?cation Tests. TP-WSTF- T12. NASA Johnson Space Center. White Sands Test Facility. Las Cruces. NM 1992 De?nitions: CRES: Corrosion REsistant Stainless Steel Component: On any oxygen equipment item such as a regulator the components are subgroups of function equipment that make up the whole item. For example. the servicing or fill valve. the pressure relief valve. the pressure gauge. the outlet flow regulating device. and the supply vessel. Flammable: Possible to burn. combustible. capable of being ignited. Stress Risers: Elements that cause increased stress or a tendency to increase the risk of ignition and combustion. Thermal compensator: Special device in a mechanical design carrying a gas such as oxygen that absorbs heat energy and carry away the heat energy from mechanical parts which are at risk of ignition. The temperature is more rapidly conducted away to the ambient to keep the oxygen temperature inside the tubing minimized. The device can also shut down oxygen flow if a maximum limit is reached. -5- - ll l' Tn FNJIE 0?8 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE 3. BACKGROUND: 3.1 What Factors Cause Fires: Oxygen system fires and explosions are a result of numerous factors that are complex in their interaction and not easily understood. This guide will assist someone not familiarwith these phenomena to better understand and analyze any oxygen system hazards. It is always best that an expert be consulted who has years of background with oxygen systems combustion issues when it is important to minimize these risks. Any person thinking about investigating these issues to reduce risks must dispense with all biases concerning what is known about normal ?res in the earth's atmosphere. which is approximately 21% oxygen, "38% nitrogen and 1% inert gasos at 1531.3 kF?a psi) at sea level. Fires and fire hazards are most often conceptualized in an environment that is found at ground level. An increasa in the partial pressure of oxygen increases the potential for combustion in terms of both initiation and severity Combustion in oxygen with increased pressure will occur more readily and spread more rapidty. Most persons are not famitiarwith oxygen fed fires and therefore more information is provided herein to explain how this phenomenon is different. Normal ?res at ground level occur in a low concentration of oxygen with a relatively low pressure. The partial pressure of oxygen at sea level is 21.2? kPa (308? psi) which is determined by 0.21 kPa 101.3 kF'a psi}. There is 21% oxygen in the ea rth?s atmosphere at all altitude levels. The magnitude of the oxygen pressure can be thought of as a stress riser. Figure 1 shows a comparison of stress risers in low and high-pressure oxygen equipment as compared to the partial pressure of oxygen in air at sea level. A stress riser is also any of a number of key parameters that have been found to make ignition more likely. Stress risers in oxygen systems include: pressure oxygen concentration other included gases temperature phase (liquid versus gaseous oxygen} mechanical failure higher oxygen velocities time and age A thorough discussion of stress risers is avaifable In ASTM 123?95 i mini-1 um. I I-wmnl or. I- ix-F I I r-rFmF- I'm .. I In nellelt- --I Hummers-I arm-u: In- Tune . 0?9 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE - sno? sou?r" 400?? anu? eon - Magnitude of Stress Riser 100-". 21.27 ItPa 101 era 3 445 era 13 {3.1 PSI) (500 (2 non PSI) Pressure of Oxygen FIGURE 1 Oxygen Pressure Stress Riser Comparisons for Low and High Pressure Oxygen Equipment 3.1 {Continuedy Dalton's Law states that the total pressure of a mixture of gases is equal to the sum of the partial pressures of each gas in the mixture. In the earth?s atmosphere the following relationship describes the gas pressures. Total Pressure at Sea Level Partial Pressure Oxygen Partial Pressure Nitrogen Partial Pressure Inert Gases Any combustion in an oxygen system occurs at an increased oxygen partial pressure and usually 100% oxygen. There will also be the additional pressure used in the supply and dispensing equipment. Normal supply equipment used in aircraft oxygen systems is typically 12.400 to 14,820 ltPa to 2151!] psig). Experience and test data show that combustion in pressurized oxygen equipment occur very rapidly and with much violence. Such ?res are thought of as explosions by the observerr but high-speed ?lm shows that these so called explosions are actually oxygen fed ?res. Technically speaking, explosions are really detonations. Metal ?res are the most violent and should be the greatest cause for concern to an oxygen systems designer. Cowgth SAE Intumlrmul by HE. ulnar Iii-Jame am ?ne :os Limiter-In Made!- lr: :rnllavtlmiiu namely-newt llama-i helium-13 hut I31 Hus-Ii: DRE: 2! 0?10 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE 3,1 (Continued): What are the chains of events that lead to combustion in oxygen equipment and any equipment that is nearby? It is helpful to think of a "?re and explosion triangle-" See Figure 2. Cine side of the triangle is the oxygenr another side is the fuel and the other side is the ignition mechanism. Take away any side of the triangle and the combustion (?re and explosion) can not occur. The problem is that one cannot take away any side of the triangle with oxygen equipment Bring Legs of Triangle Together Results in Fire or Explosion FUEL IGNITION SOURCES combustibles are Numerous Factors to Consider - Non Metals - Metals I Risk Assessment - Contamination Needed OXYGEN 100% Pressurized Oxygen Available versus 21% in Normal Air at 101.3 kPa FIGURE 2 Fire and EXplosion Triangle The oxygen is always present as it is stored and dispensed. The fuel source is always present. as the container for oxygen and the dispensing equipment are metals and nonmetals, which can all combust in 100% oxygen. For example. the equipment will consist of pressurized cylinders. regulators, tubing and ?ttings that are all made of metals and nonmetals. All of these materials can combust with 100% pressurized oxygen- Emmi! ElEInlalI?Jcnn I?m-mien bu H5 ulnar men-I: on Me L??w?da?l u-r-FI undr- Ibuan If: lend-mama! mun-arson.- p-rII-utdmuu.? FE rim Result: can 21 MDT RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE AIR325I13 3.1 {Continued}: The ignition side ofthe triangle is a more difficult issue to understand. It can be explained that it is a function of a number of factors that are always present to some degree in oxygen equipment. Experience shows us that the risk of ignition from all factors should be assessed and kept as low as possible. The risk must be kept within acceptable limits. An oxygen technical expert should be consulted to determine the level of risk. Ignition can come from a number of sources. More details are provided herein to explain this, For example. moving metal particles can cause ignition. As oxygen gas is supplied from a higher pressure to a lower pressure location and the gas encounters a restriction such as a ?ll valve, a temperature rise is associated with the compression of oxygen in this looation. This occurs when ?lling pressure vessels or cylinders on the aircraft. The compression occurs at the ?rst restriction to ?ow usually at the fill valve on the aircraft. Temperature rises are also associated with restrictions on other valves such as the presoure regulator or reduoer on the aircraft pressure vessel. Experience with servicing oxygen cylinders and the resulting fires have shown that this is a likely cause of ?res in much oxygen equipment occurring more frequently than is considered acceptable. Contamination. which is readily combuetible. may be inadvertently introduced into the system. it risk assessment is advised to determine what may be done to minimize hazards associated with ignition. 3.2 Causes of Fires and Explosions: The primary causes of oxygen systems tire and explosions that may be considered are' - Improper design and manufacturing. - Improper materials both metals and nonmetals Used in equipment and assembly. - Examples of non-metals are soft goods used for seals. seats and diaphragms; lubricants; anti- seize compounds; and anti corrosion treatments. - Improper cleanliness methods and lack of adequate verification of cleanliness. - Improper operational procedures. Improper or poor maintenance methods and procedures. See ASTM 125-95 and ASTM 88 for information on primary causes of oxygen fires and explosions. SAE gives a listing of references concerning the effects of oxygen on ignition and combustion of materials. mini-1 um. I I-wmnl or. I- ir-F -: r-rFmF- .. I In Islloli- . n? in mm ITI- .IE [a I I 0?12 RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE 3.2 (Continued). As the number of stress n'sers associated with iven oxygen system increases. the risk of a ?re andil or explosion becomes greater. There will always be some degree of risk involved! Our goal should be to keep these risks as low as possible or within acceptable limits. One method to understand or visualize this is to remember each cause of combustion has a level of risk (stress riser) associated with it. Usually as all these causes are put into the equation. they become additive in nature. The extent to which these causes are additive is not an exact science. Each cause can have a different weight and associated level. Even more perplexing is that the ignition potential is not usually repeatable. For example, a series of tests accomplished under the same conditions does not provide repeatable results. This illustrates the need to run a number of test points at any given condition to determine the relevance of the data. In addition. to further confound the issue the severity of the combustion {?re and explosion) is not repeatable. It helps to keep these issues in mind when examining the risks for combustion per the illustration in Figure 3, FACTORS THAT INCREASE RISK LEVEL - HIGH oxveEN FUEL SOURCES FRESSURE -. l, MEDIUM - They are Additive LOW - Each can have a Different Weight - Ignition Potential is Not Repeatable - Severity of Fire and Explosion is Not Repeatable FIGURE 3 - How Fuel Oxygen Pressure and Ignition Sources Contribute to the Risk of a Fire and Explosion 1.3 Canary" :lE Intam?crln I?m-Inlet: by mi 5-5.6 Lice-wrench?! hFl?N??LG?m?lal?i J-r-I'i-wlli Ill-I-m H: "tympani! Ina-naming lien-nan: Its-In I-E NH that: ?ltl??'in In It.? Mm 0?13 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE AIR325H3 3.3 Selection of Metals for use in Pressurized Oxygen Equipment: Metal is a fuel that may be consumed and ignited in a tire. The fuel is one leg of the triangle and the ignition source is another. The principle recognized sources of metal ignition are: Most studied and understood - Contamination - Particle impact - Heating to ignition - Friction ignition - Compression heating - Kindling chain reaction Least studied and understood 4 Mechanical impact - Chatter - Resonance - Crack propagation Electrical spark - Puncture - Trapped volume pressurization For a detailed discussion of these sources of metal ignition refer to ASTM 128-95 and ASTM 94. 3.3.1 Metal Choices in Oxygen Systems Designs: There are several methods whereby metals are ranked according to their susceptibility to ignite. Some of these are from a kindling chain reaction in pressurized oxygen gas. from particle impact, from mechanical impact and from friction rubbing. Past test data shows that metals high in nickel or copper are the most resistant from ignition by any method! Metals that have iron or aluminum are the least resistant to ignition by any method. Past test data that looks at metals commonly used in oxygen equipment designs shows that aluminum is the most suaceptible to ignition. Not only is aluminum much more easily ignited. but it also sustains combustion with the greatest release of energy. Testing has also shown that even metal alloys with even a small content of aluminum are easily ignited. Refer to ASTM documents referenced above for a detailed discossion. Aiuminurn and aluminum alloys should be used with great caution in any oxygen system design. Aluminum should not be used in locations considered especially sUsceptibIe to ignition. For example. the ?ller valve port on high?pressure supply equipment is particularly susceptible. as this is a location of compression heating and high velocity with possible particle impact. mini-1 um. I i-wmnl or. I- ii-F I r-rFq'n' 2 I'm .. In nell?lt- -.I al'r'lut II- ellie I I II- -II 111" null: 0?14 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE AIR325I13 3.3.1 (Continued): There is a generally accepted misconception by designers that parts made of steel and stainless steel are very safe for use in gaseous oxygen systems. Actually. steel ranks only a little above aluminum for susceptibility to combust. Steel i5. however?1 a rugged material that does not shred or give off particles as easily as other softer metals. Steel has a longer life than other metals. An example about the misconception of steel is that brass valves were commoniy used for years on gaseous oxygen servicing carts. Because brass is soft. the life on the release valves Was short and it was decided to use steel release valves to increase the useful life. The incidents of an oxygen fed ?re atthese valves increased dramatically. Thus although steel was more rugged, it also led to more oxygen fed fires. Steel mUst be Used as carefully as aluminum in critical locations in an oxygen system design. Titanium easily ignites in the presence of high concentrations of oxygen and should not be used on any oxygen system. 3.3.2 Selection of Non-Metals for Use in Pressurized Oxygen Equipment: It is surprising to discover how many non-metals are used in oxygen equipment and are considered necessary to use for properly functioning oxygen equipment. This is primarily seen in equipment such as regulators. valves and pressure reducers. In selecting and using non-metals in oxygen systems. the following principles should be considered and used. - Oxygen compatibility is a function of the pressure level. - This is especially critical above 3445.5 kPa psi). - First. examine the oxygen index rating (refer to ASTM 2863) - Best choice is high index. - Second. examine the auto ignition temperature (AIT) when in oxygen gas. - The AIT should be above any expected temperature with factor of safety. Third. consider the heat release from combUstion. - Heat release should be as low as possible. - The non-metal must satisfy other performance and environmental extremes as Well. Refer to ASTM 123?95 and ASTM 63 for information on selection of non?metals to minimize oxygen ?res and explosions. Lubricants, anti-seize compounds and thread locking substances may be needed to design a proper piece of oxygen equipment. SAE A1R4071 also provides information to assist in this selection of lubricants- Lunar-II: at; uiInI- 1 um I mourn-ii..- Ir. i' l'u-i llrI revs-u." All u. The, .u Ir- [lLr' 'nr Fug": ii I 0?15 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE AIR325I13 3.3.3 Critical Locations for Risk of Combustion in Oxygen Equipment: For any oxygen system it is important to look for potential hazards where the risk of a ?re might be the greatest or not within acceptable limits. These critical or questionable areas of the oxygen system should be examined in depth. Previous inVestigations on aircraft oxygen equipment have shown design ?aws improper materials and contamination as potential combustion hazards. It is not advisable to hang on to that old rule of thumb that is has been used successfully in the past so it is good enough now. Whether a new or modi?ed aircraft. fire hazards concerns with oxygen equipment should be examined. New technology is available and aircraft systems are becoming a larger investment. Additionally. many new aircraft have large crew and passenger included and safety of these oxygen systems cannot be dyer-emphasized. Invastigations have shown these hazards are universal problems with oxygen equipment. The highest risks are usually associated with high-pressure and liquid oxygen equipment. Figure 4 is an example of some typical hazards that may be discovered on a high-pressure regulator or reduoer. The possible intent of placing the filter into the inlet of the pressure vessel is to keep contamination out of it- What was overlooked though. is that even though this traps particles on servicing keeping them from the supply container. on initiating supply the particles are swept into the supply equipment. This can cause malfunctions from clogging the components. More critical though is that high-speed metal particles can impact components and become an ignition source. A better location for this ?lter might be at the inlet of the filler valve to preclude contamination into the system at all. These filters could also introduce new hazards to the servicing equipment. Sintered bronze is considered the safest filter to use in high?pressure critical locations on transferring oxygen supply. This illustrates how a proper hazard analysis must look at the proposed system operation and piece parts and minimize all hazards. 4. THE PROCESS TO REDUCE HAZARDS: 4.1 The issues in Oxygen Equipment Development: Initially. the concern is that the equipment may have design or materials problems. In other words, the design and materials may contribute to ignition in an oxygen environment. Later. the concern is that proper precautions are taken to minimize oxygen equipment hazards and contamination by procedure. The design approach and materials selections have usually been based on the aircraft ma nufacturer?s and associated vendor's historical experience. For example. should the oxygen components such as valves. regulators. and plumbing already be used on an existing aircraft oxygen system that would often have been considered sufficient justi?cation to continue its use on another oxygen system without questioning potential hazards. Also. there is a strong desire to minimize costs and manufacturing fabrication problems. These goals are not necessarily consistent with the design of a safe. non-hazardous oxygen system. It is recommended that an expert be consulted on any proposed oxygen system whether it has been used in the pastor is a new design Much information and knowledge that is now available was not available in the past. 'Iflnl- 1 um I mlrlu-mu- or. 1M il. rvart'.F.u I'u-r .. In rcpt-u." r: ur-j. Fu-m Th. 0?16 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE Example of Potential Hagards to Avoid in Oxygen Desig? Electric Pressure Relief Ac?viation i=3 - Potential for - Fa nicie Impact Cylinder Outflow - Compression Heating - Particle Impact Pressurized Oxygen Supply - 2100 PSIG Servicing inlet Elastomeric Seat could Ignite Typical Examples of Problems that Contribute - Oxygen into Reguiator to Ignition Sources are Involved not Filtered - Filmer Traps Contamination on Servicing and Releases It into the Oxygen System on Supply I Sharp Edges. Burrs and Metal Feathers I Compression Heating on Servicing and Operation - Improper Materials [not Oxygen Compatiblei - Electrical Hazard from Gauging and Sensors FIGURE 4 An Example Illustrating Some Possible Hazards and Ignition Sources to be Avoided on Pressure Reducer or the Regulator Assembly for a High Pressure Cylinder 4.1 (Continued): It is prudent that when assessing which designs may be used in an oxygen system, that a hazard analysis and contamination assessment be considered and accomplished when considered necessary. A quick examination of the oxygen systems by an expert familiar with oxygen systems combustion will provide insight about how to best approach this. Another good reason to evaluate the use of previously designed oxygen equipment components is that it may be used in a system that is different. 1:203:13" I?m-mien bv H5 uncrv all-v: FAE null-In Mull-I If: 'QFl?-?uabll Jl'rl?n'll'run' limo-n: NW l-E liu I). Neale Dilt?m'n ILL: El MDT 0?17 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 13 4.2 Oxygen Systems Operations and Maintenance: improper operations can contribute to oxygen systems tires and explosions. It is difficult to point out speci?c methods of minimizing these types of hazards. as they are speci?c to the design under consideration. One well?known operational problem that contributed to fires in the past Was manual or automatic valves which when opened too quickly would cause a rapid increase of heat at the dead end of the dispensing equipment from adiabatic compression. Designers have since developed valves that minimize this problem. but there are still many valves in the market. which open too quickly. These valves usually cost less, so there is a tendency for some oxygen equipment designers to Use these valves. This can be veri?ed by surveys conduoted on the valves used on oxygen equipment and experience with ?res caused by these valves. Oxygen safety training and the use of procedural checklists are important tools to lteep accidents to a minimum. Additionally. if proper contamination control measures are not taken for servicing oxygen equipment. contamination may be a prevalent problem. Contamination is not only a combuetion (fire and explosion) hazard. but it may also prevent or degrade proper oxygen equipment operation. It has also been found that the servicing of pressurized oxygen equipment frequently contributes to accidents from the accumulation of contamination. Metal particles tend to shred from valves when in Use and get into the oxygen stream. Contamination is a prevalent problem at ?ttings that are connected and disconnected if the proper care is not exercised. Additionally, past practice has shown the value in installing end caps to protect open oxygen system tubing and components like regulators and valves capping any open ports to prevent entry of contamination. This could initiate a ?re or cause a component malfunction from clogging small ori?ces or blocking proper ?ow because valves and levers stick or malfunction. ASTM 93 and SAE provide information to assist in property cleaning contamination from oxygen equipment. In the assembly of oxygen components. taking measures to prevent metal can minimize contamination. Inspection after the assembly of each component may reveal metal particles that can be removed before proceeding with the next step of the assembly. These inspections are done on samplerfs} whereby the item is disassembled after the intended assembly for manufacturing. The sample item is checked for contamination caused by the proposed assembty. If contamination is found. then design andior procedural changes may be needed to reduce contamination and the associated risks for fires- Several prevalent problems that always seem to be encountered are mentioned here. lCine is screwing softer metal components such as aluminum or brass into harder metal components or vise versa can cause metal feathers and particles that can get into the oxygen stream. This problem is most prevalentwith pipe-type threads. Often lubricants. anti?seize compounds. and Teflon tape are used in assembly of oxygen components to minimize these problems. Careful assembly is required to ensure that excess material (is. lubricants. anti- seize compounds and Teflon tape) does not squeeze into the oxygen stream. This metal and non- metal contamination as discussed above can cause a kindling chain reaction as they can easily ignite when in the oxygen stream. i Lunar-II: new. I In Iowa?. 1 at m- .I-I -15- 'r - Udall-flier: -. A II. II . ru- ul'r :nt 7n}; r: in 0?18 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE 1 3 4.3 Application of the Hazard Analysis Process: The designer of aircraft oxygen system components should specify that a hazard analyses be performed on the oxygen system and components. This is as important as is the environmental testing to ensure a safe and eifective oxygen system design. Additionally. a contamination investigation could be conducted later on in flight test evaluation and operations if problems are suspected. This could be accomplished as a separate effort to examine problems. A clean oxygen system in the operational environment will assist to reduce ?re hazards. To ensure that the analyses and contamination investigation are competent. appropriate information must be available- ltwould be pertinent that the potential sUppliers provide information needed such as the configuration, the intended operationis). the materials used for components and any non-metal used including lubricants. anti corrosion (anti?seize) compounds and any thread lock compounds. This complete information is essential for a complete hazard analysis- A "quick look" preliminary hazard analysis could be provided. This will assist in an early evaluation for a safe and effective oxygen system design and may be another criterion involved in the selection of the vendor. A more detailed hazard analysis and contamination investigation could be provided later. Areasthat need examination are system problems that contribute to higher risks, materials compatibility issues, and proper component design. This investigation should examine this equipment at the system and component level (piece part level] and consider the hazards from an oxygen systems operation and maintenance viewpoint. Drawings and a detaited listing of materials used in the design are essential for a proper evaluation. Past experience has shown that Issues concerning oxygen system and equipment hazards are not generally well known or understood. Therefore it is recommended that an oxygen systems technical expert familiar with oxygen systems combustion issues be consulted when examining potential ?re hazards and contamination concerns. Supplemental information and guidance besides that customary with past practices may be necessary for review by oxygen technical ex pert(s). ohm-1 um. I ur- ir-F I: In Iguan- - -.I .?liruu: II- I II- _m flint-fluff [a - 0?19 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE AIR825I13 5. HOW TO DO AN OXYGEN SYSTEM HAZARD ANALYSIS: 5.1 Resources and Program Issues to Consider to Perform in the Process: Ensure that the technical department andior the independent organization or person that does the hazard analyses and contamination investigation furnishes the necessary personnel, funds, facilities, material supplies and data to perform hazard analysis and contamination assessment during an oxygen system development program or project. All phases of the development apply and are: - De?ne requirements - Conceptualization Design and development - Final design and prom-typing - Equipment quali?cation testing and man-rating - Production - Deployment and operations 5.2 Hazard Analyses Overview; The actual sleepy-step hazard analysis process is explained in ASTM 63. Each piece of oxygen equipment is broken down into components or stages. Team of experts assesses the potential for ignition by each mechanism. This should include the oxygen combustion experts, the oxygen system designer and the technical experts from the organization purchasing or using the oxygen equipment. A level of risk is assigned to each stage for each possible ignition mechanism. Notes are taken for each important issue agreed Upon or disputed. The oxygen system designer could choose to change the design to that with less rislds) or a test could be conduoted to assess the risk. The system and equipment design1 materials and operation of the components should be examined in complete detail. It is essential that actual hardware and associated drawings including materials lists be made available. The oar ygen system designer may provide hardware and information to the organization or person, which does the hazard analysis. Also, so that materials compatibility issues may be examined, all appropriate parts and materials need to be identi?ed. Often potential oxygen equipment vendors have proprietary andlor patent rights on this hardware. It may be necessary to take appropriate safeuards to ensure that all organizations involved in the hazard analysis protect the rights of the suppliers of this equipment. mini-1 um. I ur- ii-F - TE-iIll-Hv'a'll I'm .. I In Isrlon- --I arm-u: In- True I . n? u- ITI- .IE t'a I I 0?20 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE Hazard Analysis (HA) Contamination Assessment (CA) Process De?ne Requirements Conoeptuelization Design 3: Development 1" .E I- .i'l 1 if Include HA Use ASTM 3. Contact Experts 8: CA In SAE Guides to 3. Consider Purchase Minimize Need for Agreement Problems Testing Final Design at Prototyping Equipment Qualification 8? Testing r' I - Inspect a . Equipment for . Evidence of Re?ne Design 3.1 I Problems 7 A Flight Testing Production Deployment 5. Operations - r? Use CA lo Revisit Results Sale D?slgn of Validate HA of HA a GA Oxygen Systern 8: Re?ne where for any Design Problems Required Changes Fletnsil HA 3. CA FIGURE 5 - How the Hazard Analysis and Contamination Assessment Might be Involved in an Oxygen System Project 5.2 {Continued}: The purpose of obtaining this equipment hardware is that tear down inspections and evaluation of the component designs is essential for a proper analysis. Fabrication and assembly problems may be discovered that are not necessarily design related. It is not expected that this equipment will be destroyed or consumed in the investigation. After the investigation. the equipment may be returned to the source for cleaning and reassembly. The purpose of this analysis is to identify any potential hazards in a qualitative manner. Any hazards identi?ed should be explained in sufficient detail so that the primary aircraft designer may determine any necessary changes, Recommendations provided could include options for consideration of design. fabrication. assembly andfor operational changes. 613ml! :"lE In?nan Fowler: by HE uneven-am: ?it Me Lice-wreath! cur?Ft Ill-Iv-I "tycoons" Ila-Ill FE I: Hes-ll: E?ltl?m II MDT 0?21 RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 SEE 13 5.3 Hazard Analysis Steps: A hazard analysis of an oxygen component or system is desired. Figure 6 shows the steps that are needed to do this. The oxygen equipment application and the scope of the inVestigation should be determined first. and a team should then be assembled to conduct the analysis. information on the components and the worst-case operating conditions need to be collected. Drawings that show all components of the equipment under consideration and a materials list are essential. Usually, a fire will not occur in an environment unless the materials of the component are ?ammable and a credible ignition mechanism is present. The ?ammability of the material is first reviewed to determine if any ?re hazards exist under the worst-case operating conditions. For example. if oxygen were flowing into a dead?ended section of the system, the materials in this section would be subjected to the effects of compression heating. If the material is flammable, then the possible ignition mechanisms are surveyed to determine which are credible. If data for the particular ignition mechanism and the materialts) under consideration are not available. appropriate materials tests may be needed. These tests are useful to determine the oxygen ?re risk. Another option would be to change the materialis) to something for which test data is already available. Finaily. the secondary and reaction effects are evaluated to determine what effect an ignition and possible combustion would have on the system and the aircraft. To use an oxygen hazard analysis as a tool, it needs to be properly documented from the beginning. Figure 7 shows an oxygen hazard analysis chart. This chart contains the component designation which indicates the materials of construction including soft goods, the possible ignition mechanisms, the probability of each ignition mechanism. and results of the secondary effects analysis and the reaction effects assessment. The documentation also includes any recommendations or limitations that the oxygen hazard anaiysis team decides is important, including recommendations offurther testing if needed, stipulations of use, and any additional safety precautions. If component tests are required. these tests may be performed according to the ?Guide for Oxygen Component Quali?cation Tests (Bamford and Rucker 1992)." 10 mini-1 um I I-mel l-r ill-I unir nelloli- --I arm-u: u- :me I . n? It.? t'a 0?22 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE De?ne Oxygen Equipment Application and Scope of investigation . Compile Detailed Information 0'93'1'15 On Components Hazards Analysis Team . Configurations - Technical Speci?cations - Operational Procedure Operational Conditions Determine Realistic Worst-Case Operating conditions Determine if Materials . Consul! Promoted Combustion and are Flammable Oxygen index Databases i Perform Materiaik Tests, ?lF if Necossary Determine if Ignition ?g?gu? M?jr?a . m? MBChamsms are Present Various ignition Mechanisms -l Ferfonn Motorist. Con?guration, Determine the Likelihood of Secondary ignition Hazards and Component Tests. ii if Necessary 1 Perform a Reaction Report Oxygen Hazards Analysis Effects Assessment Results and Recommendations I Perform Materials, Con?guration, and Component Tests. If Necessary .. FIGURE 6 - Steps InonVed in an Oxygen Hazard Analysis I:qu :lE Inlunllmo in H5 un?t" Anal-e: mi 546 uc-a-I-rrn?dmi la la- Inl? l-r: top-MM luau-arcane arm-Cur: mun." Ilsa-nu noln PS It!- Healu In [a Mm 0?23 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE ?s??g?isE? tag a I 5 Reactime Ft Assumable ComponnrlA a A He'll-brawl C=Crilical cot-momma 3 a a a 2 WWI: Component: I) f} A GmnertD 4 2 A iIio_r- ?=lnpossibie Wale 1=Hermta mm - =l'ibfutharanatysis 3=Poesible matted 4=Frobabte FIGURE 7 Oxygen Hazard Analysis Chart 5.4 Contamination Assessment: A contamination assessment is a possible follow-on to a hazard analysis. Components of the aircraft oxygen system being evaluated could be examined after a relatively brief period of ?ight operations. Delays in an initial operational evaluation has the potential to result in increased dif?culties and costs associated with any design andi?or procedural changes that are found necessary. if a hazard analysis andi'or contamination are part of an aircraft oxygen system program process. it is desirable not to wait too long to complete the task or it probably will be more dif?cult and costly to make any necessary design andfor procedural changes. On the other hand to do a proper contamination assessment. it is desirable to wait some amount of time so that a contamination buildup will be found that is representative of possible contamination that could occur on the operational aircraft later on. An effective contamination assessment is only possible if the oxygen system components are taken from the aircraft and examined in a proper laboratory facility. It is also desirable to examine tubing and components on the aircraft oxygen system that are not removed. if excessive contamination is found on equipment left on the aircraft. it will be important to clean the oxygen system tubing before installing any clean replacement parts. If flight operations must continue. spare parts need to be made available and used to replace the components that have been removed. C293th I?m-mien bl H5 5A6 Liana-Fain! .I-r-I'i lint?I If: EQFIMQDN In?uential-u lion-Ira: I-E Dir. l?t Heal! OLE: El Mb'l 0?24 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE AIR325I13 5.4 (Continued): For proper shipment. these components should be properly packaged so that no contamination other than that. which may already be within the equipment while installed on the aircraft. be introduced. The equipment should also be disassembled in a properly clean environment and examined for contamination. Appropriate documentation and photographs can be used to record any contamination identi?ed. Visual examinations may be enhanced by various techniques such as magni?cation. white and black lighting to discriminate hydrocarbon or halogen type contamination from other types. A nonvolatile residue analysis may also be accomplished which includes a particle size and weight distribution count on each component. An assessment of the contamination found could then be provided which identifies the level of problem andior hazard. if any. Refer to SAE for additional Information on oxygen equipment cleaning and packaging. It may be found that proper measures are needed to control contamination during operations. For example. it may be necessary to add ?lters to the aircraft or ground support equipment. Other equipment or procedural changes may also be needed to keep the oxygen system from excessive contamination. 5.5 Detailed Oxygen Hazard Analysis Procedures: 5.5.1 Oxygen Application and Investigation Scope; The oxygen application and investigation scope may first be determined to provide the basis for choosing the oxygen hazard analysis team and for conducting the analysis. Components are examined individualiy and also as a part of an oxygen system. It may not be necessary to examine all components individuallyr but almost always a system analysis is desirable. 5.5.2 Oxygen Hazard Analysis Team: When an Oxygen Hazard Analysis Team is assembled, individual areas of expertise shouid be examined. The team should include. as a minimum. personnel with expertise in the following areas with emphasis on oxygen systems background: - Mechanical design - Metals ignition and combustion - Nonmetals ignition and combustion - Componenttesting Other personnel may also be included into the team with expertise in the following areas: - Electrical design - Cryogenic fluids Materials - Chemistry 'Ir?lrll'5l 31-: I I. ?luv sir-1.? I. we?? f-fF-?Fu I'm .. I In .1- cr-Hrvn'r "mom-wen arm-0?25 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 AIR325I13 5.5.3 Component and System Information: Information on each component in the system is needed including materials of construction, which includes soft goods and lubricants. A drawing showing the cross-sectional view of each component. particularly fluid ?ow paths and the location of the soft goods is needed for a system fluid schematic. The cross-section of a component is used to locate and identify all the soft goods. if the cross?sectional view of a component is poor quality or unclear. a disassembled component complete with soft goods is sometimes useful. All materials of construction need to be identified. The flow path along with all oxygen-wetted materials must be determined. The next step in the analysis is that the team should divide each item under consideration into manageable units' construction referred to as components. A component is a subset of the item. for example the pressure relief. the pressure gauging, the oxygen fill port. the outlet flow pressure regulating mechanism, and the supply vessel- The outlet that sends supply to the crew or passengers for breathing gas is the next component which leads to other parts of the oxygen system. Each component is examined. one at a time and Usually it is best to startwith the sequential flow of the oxygen. In other words start with the oxygen fill port. go the supply vessel and so on to the later stages of the item under consideration. In the following Figure note that components A, B. and give examples of generic components under consideration. In looking at Component A, for example, the chart is best ?lled out from left to right. Is Component A meal ?ammable or nonflammable'? Are soft goods under consideration? Each ignition mechanism can be looked at one at a time to determine how likely they are to occur. Note that footnotes should be added explaining the rationale for the rating given and the concerns and secondary effects. This will ensure that in the future should anyone examine the results of the hazard analysis it will be possible to follow the decisions of the team and see why the design Was acceptable for an oxygen hazards standpoint or why changes were needed. If design changes are made. it Is desired to again visit the same hazard analysis and determine if the design is now satisfactory. Note that footnotes should be added explaining the rationale for the rating given and the concerns and secondary effects. In examining the following table one can look to see any higher risk components are included in the design being looked at. The following includes a list of some common high-risk components: urn-m ,1 in: -. .. r-rFmF-u .. Nu.--l I In new-m- .7- ur oer-"n nor-nu- u- r. rIr-"nr ITI"3-1 0?26 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE TABLE 1 (Lyman Mutt Pmbulrht 'lH'Ht'lith?hl lgm'rlrm .H'i?i?t'mm't?mt Bat! l-"nivc Particulate generation (particle impact) and quick-opening ladiattntic compression) Rafitgf Vrt'ft't' Chatlcring (mechanical impact or frictional Itcntiltal Globe Van's oven ti-Itcn Fully open (partich impact) Ba?a??t' when fully open Lparticlc impact} Flair Hare Susceptible to adiabatic compression when dead?coded Ragui'amr Mechanical impact and high velocities generated {particle impact} Chock valve (?hattcring (mechanical impact and frictional heating] Fitter Pneumatic impact on the ?lter element and possible particle impact if poorly located within the system Fittings Particulate introduccd into the system during assembly 1 particlc impact) Soft Goods on in gas strcam (pncumatic impact. mechanical impact. and particle impact 5.5.3 {Continued}: Most ignition mechanisms for the above components can be eliminated or minimized by proper material selection. system design andlor operating constraints. 5.5.4 Worst-Casa- Oparating Conditions: The worst-casts operating conditions that the component may undergo are now determined. This information is used to evaluate the materials of construction for resistance to ignition and combustion and includes maximum use pressures. temperatures. and flow rates. Pressures and temperatures are important because material ?ammability is often a function of these two parameters- Flow rates are important because they affect the particle impact and adiabatic compression ignition mechanisms. 5.5.5 Material Flammability: The materials are evaluated to determine if they are ?ammable at the worst-case operating conditions. A large material ?ammability database is available in ASTM references that contain ?ammability data from previous and ongoing tests of both metals and polymers (soft goods). If information on a material for the worst-case operating conditions cannot be located in the database, tests may be conducted to obtain this information. The oxygen hazard analysis chart is updated with the results, using lnon?ammabla) or (?ammable). If the materials of a component are determined nonflammabla. the ignition mechanisms need not be analyzed for that component. Canary" :"lE Intum?crln Poi-mien but He mi 56.6 Lice-unspoilt?! J-r-I'i "h lint?- If: zertoduaml Jt'l'l?ndt'?llc' OTIIMMUIMI lion-nan: I-E Ill-l bi that: In: El.? 0?27 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 5.5.5 5.5.6.1 5.5.5.2 5.5.5.3 5.5.6.4 5.5.6.5 Ignition Mechanisms: The next step is to perform an ignition mechanism survey. Nine ignition mechanisms are evaluated for each component found to have ?ammable materials. Frictional heating Adiabatic compressron (pneumatic impact) or compression heating Mechanical impact Particle impact Resonance Mechanicai stress or vibration Static discharge Electrical arc Chemical reaction Each ignition mechanism is evaluated to determine if it exists in the component and that the likelihood it will cauae an ignition. The results of the analysis for each ignition mechanism are documented on the oxygen hazard analysis chart. Rating for the ignition mechanisms are: (impossible) (remote) (unlikely) (possible). (probable) Frictional Heating: Parts of a component or system can rub against each othet with enough force andior velocity to raise any one part to its ignition temperature at the given oxygen pressure and concentration. Examples: Rotating or oscillating equipment and chattering reiiet valves. adiabatic Compression: A quantity of any gas can generate a considerable amount of heat it" rapidly compressed. This happens when a gas is quickly released through a hose to a dead end or flow restriction. Low veiocity release of gas will minimize the heat buildup. Also, thermal compensators. which reduce flow on a heat rise. can minimize the heat buildup. This heat can readily ignite polymers orflammable contaminants. Exampie: A valve or ?exible hose with a polymer liner in a dead-ended high-pressure oxygen manifold. Mechanical Impact: An object with a relatively large mass or momentum striking a material can cause mechanical deformation and expose fresh surfaces. Example: A poppet of a solenoid- operated vaive impacting the polymer seat. Particle Impact: Combustible particles impinging on materials at velocities greater than 50 meters per second in an oxygen-enriched environment can cause ignition. Example: High- velocity particles from a contaminated hose or tubing are swept along with the oxygen gas at high speeds striking a valve. Mechanical Stress or Vibration: Materials that are poor heat conductors such as piastics can reach their ignilion temperatures when stressed or vibrated. Example: Unanchored joints or seats that protrude inside ?ow areas of oxygen service. (awful-at; mini-1 ui'. inn new)?. - ui II- I u- -25- 10F I n. fva?'J' ll "u-i . [Ir-1m . 0?28 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE 5.5.6.3 5.5.6.7 5.5.6.8 5.5.6.9 5.5.9 Static Discharge: Discharges of static electricity can produce high temperatures. sometimes high enough to cause a material to reach its ignition temperature. Example: The accumulation of electrostatic charges created by the friction of dry oxygen ?owing over nonmetals- Liquid oxygen creates static electricity when flowing and acts as an electrical conductor causing ?reballs or high voltage discharges. Proper grounding is essential. Electric Arc: Electric arcs can provide the energy to ignite materials in the presence of oxygen. Example: An insulated electrical heater short-circuiting and arcing through its sheath to the oxygen gas or liquid. The tubing wall of the oxygen gas is penetrated and escaping oxygen gas reacts with the metal tubing and the burning material outside to intensity 3 ?re. Chemical Reaction: A chemical reaction can produce suf?cient heat to ignite materials in the presence of oxygen. Example: A chemical process like chemical oxygen generators that generates elevated temperatures. Resonance: Acoustic oscillations within resonant cavities can cause a rapid gas temperature rise. The rise is more rapid and achieves higher values when particles are present. Ignition can result if the heat generated is not rapidly dissipated. Example: Gas flow into a tee and out of a branch port so that the remaining closed port forms a resonant chamber. This is not always easily determined without sophisticated analysis or testing. Secondary Effects Analysis: After the ignition mechanisms have been surveyed, the secondary effects are analyzed. This analysis address the effects of failures that are not ignition?related. but may create an ignition hazard in a nearby component. such as an external leak caused by normal seal wear. The leaking oxygen could build up and allow an ignition by the static discharge ignition mechanism in some nearby component. Ratings for the secondary effects analysis are (further analysis of affected components necessary) and - (no further analysis needed). Reaction Effects Assessment: Finally. a reaction effects assessment is performed and documented. This is an assessment ofthe effect if a component fails or is ignited and useful for making judgments on the safe use of a component. The reaction effects assessment would then help determine if the component may be used safely. The ratings are A (negligible, no loss of equipment or life), (marginal, equipment is damagedr but no lives are lost), (critical. loss of test data and damage to equipment. but no loss of life). and (catastrophic, loss of equipment and life). Recommendations and Conclusions: The lead activity for the haZard analysis should document the recommendations and conclusions. A record of the review is desirable because it may need to be referenced numerous times through later design or procedural changes. Such information will also greatly assist a later accident investigation that needs to be conducted. Since so much effort and resources have been expended to do a thorough hazard analysis, it is good to have this information available to the team and other management persons not involved in the investigation. i mini-1 um I In Iowa?. r: in -26- 1r?F .. "u-r I: now-Tqu -- 0?29 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE 13 5.6 Evaluation of Results and Actions Taken: information generated in the hazard analysis is consolidated into a meaningful format and next presented to senior engineering andror management within the organization. which manages the equipment under review. The next step is to develop a risk assessment versus cost to determine what changes in design. means of controlling the hazard andfor procedures are considered desirable. Since the hazard of combustion with oxygen equipment cannot be eliminated. it is desired to determine the level of risk that will be acceptable. I may also be a good idea to coordinate with the customer to determine whether they can accept some of the risks of combustion- Having the BUstomer involved from the beginning of the process is good so they might have visibility into the risks and trade-off. Also. the use and installation of the oxygen equipment under consideration is something to consider. lfit is used on a passenger aircraft it might be more desirable to expend resources to getting the risk as low as possible. it the equipment is mounted on the ground and there is no risk to the safety of persons. then some risks may be accepted more readily 5. AN EXAMPLE: See Appendix A. An oxygen component used to reduce pressure on bailout bottle (used when bailing out of the aircraft) was examined in a past effort. The pressure reducer was mounted on a 50 cubic inch steel 1800 psig cylinder. The functional block diagram shown in Figure 8 is actually only about 2 inches long. The internal detail is not shown because this is a generic example, but the materials of the included components are mentioned. as this is necessary for a proper hazard analysis. Information that includes the internal detail is essential for a proper hazard analysis- So that the view may be errpanded for clarity. the cylinder has been left off the bottom of the figure. NOTES: Key Words: Oxygen fires. oxygen explosions. oxygen guide. metal fire. contaminationI oxygen contamination. fire triangle, ignition in oxygen. aircraft oxygen systems um. I ur- ix-F anm?u I'm .. I In --I arm-u: In- True 0?30 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE Manual Cuntrul Tyne 1 le Sleeve CREE Spring CHES Type 303 Piston 2021! Aluminum Silconc Imprennted Hard Anodized Dacron Fabric Monel Mechanism is neig Nitronlr: at 50D psig Sleeve Vespel Seal MS 19min CRES 44m: Ball Silicone [II-Fling gm" Pressure Gage Eie-Cu Element Brass Seal lur Gage Housing is 53 CREE Ball Helical Bourdon Tube ones ir-r PH Silcone O-Fling Seal Spring 1111850 tn 2259 p339 Monel Housing I Hillside Threads in Cylinder Using Teflon Tape aw Thread Worst Case Conditions are Cumpnund Assumed lor Cylinder Pressure 2251] psig and Maximum ?apper Temperature Irurn Haximurn nnr'rSiplmn Ambient and Compression Heating Tube Temperature Flise NOTE: Fill Valve and Pressure Hellel Value in Other View Mounted on Housing FIGURE 8 - Functional Block Diagram ofa Pressure Reducer NOTE In an actual hazard analysis a detailed drawing is essential to an understanding of the potential hazards and analysis of the contribution of included materials. PREPARED UNDER THE JURISDICTION OF SAE COMMITTEE AIRCRAFT OXYGEN EQUIPMENT Coagrurt Inlemnumu l?nl?ll?l bi- H5 un?t." all-u- ni FAE uee-u-rn?re-u u-u-Iv null-- If: mundane" Horn-n: Ire-n l-E i I'm Real: lb [2 :l Mini 0?31 RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE APPENDIX A EXAMPLE OF A HAZARD ANALYSIS ACCOMPLISHED ON A NEW DESIGN FOR A REGULATOR ON A {2000 CYLINDER The first step is to divide this equipment under oonsideration into functional components, in this case the components are the regulator for supply. pressure gauge, fill valve {not shown in the ?gure) and pressure relief valve (not shown in the figure}. Since the new design ?ll valve was used and had been looked at in another hazard analysis. it is not included in this example. Additionally, the pressure relief valve was looked at in another analysis. The main concern with the pressure relief valve is that it may chatter or have an elastomeric or soft good that is impacted by pneumatic force or particle in motion. start a ?re and then cause a kindling chain reaction to ignite the metalFill valve 1 a 0 Lb Supply Vessel Passaqu Gauge 0 El 0 [l Pressure Rollefvalve [Gu?etFlowFtegulalm FIGURE A1 RISK LEGEND: Flammable Non-Flammable 4 Highly Probable 3 Probable 2 Unlikely ?l Remote 0 Almost Impossible NOTE: Unless otherwise noted Hazards are based on 100% oxygen. 29 13mm" Inlanmmn bu Hiull?rlumsm 5A6 Licnw?d'mthMi?iLD??EEl?tEI ?b?El H: 'eFIo-?oaon Inna-wrung OTIIMMUIMI Item-a: I-E Hut I1 E?ltl?mm El MDT 0?32 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 AIR325I13 NOTES: a. Fill valve is a new design with Monel and valve seat out of direct oxygen flow. It is possible to start a ?re. but not likely. b. The valve seat used to prevent leaking is an elastomeric and can burn and cause a kindling chain reaction. The design con?guration will minimize this to a great extent. c. The supply vessel is a steel cylinder with an anttsiphon tube. Steel can burn, but based on past experience it has been shown this rarely happens. The anti-siphon tube is inserted into the tube to prevent combustible metal particles or moisture entering the outlet flow-regulating component. Spring is most ?ammable metal in high?pressure side. This is true becauae the spring has a large surface area in comparison to the amount of material. Any other non-metals such as the silicone O- ring seal would be a combustion concern. The best design would keep any of the surfaces of the silicone out of the oxygen?Wetted area. a. 1D-micron ?lter. anti-siphon tube. oblique angles, polymer target reduces likelihood of particle ignition. negligible particle generation, deburred parts minimized particle generation. The I rating means to avoid assembly-generated contaminants by lubricating threads sparingly with Krytoir prior to assembly. f. A temperature in excess of 500 is possible from pneumatic impact {compression heating} in the diaphragm area that is within the pressure reducing region orthe largest block on Figure 8. Since silicone Auto Ignition (NT) is 450 its ignition is a probability. Note that Vespel SP-21 ignites at 2500 psi in pneumatic impact (compression heating} testing. The probability of pneUmatic impact causing ignition from a temperature rise is remote because of low pressurization rate. Q. At 1050 psi the mechanical impact ignition threshold for silicone diaphragm is 10 ft?lb. This Is muoh higher than what the toggle valverspring combination can prodUce so this ignition concern is considered remote fora rating of 1. h. Friction loads extremely small. The valve is very stable so a rating of is given. j. A risk rating of 2 is given due to issues concerning the control of thread compound. This is used to keep assembly together during vibration and handling. If excess thread compound gets into areas that see oxygen service a risk rating of 3 or 4 would apply. There should be assurance that the assembly process will be inspected and controlled to agreed upon procedures. Also upon disassemny and rebuilding, the ports will be cleaned again. it. Ensure that Krytox and RTV are used sparingly and excess is not allowed into the areas of oxygen service in side the valve- "new Il'Jh-l l-r ill-I In ull': II. . ?er?t'J? \l "In 'v-v-Ir. In Iowa?. 1 j: urn-nun} u- gh? r: In ii" 0?33 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SAE AIR325I13 RECOMMENDATIONS (pertain to this example only): 1. Determine Auto Ignition Temperature (NT) of RT?lir thread sealant used and of a potential alternate sealant. Some experts disagree with choice of as an alternate material to use in this application. Test data is needed for Giyplal so it may be compared with RTV for its AIT. The manufacturer chose RTU because it is considered safer to use than but substantiating data is not available. We should recall that this item has a long histor?,r for 30 1years as pressure reducer on bailout bottle for parachute bailing out at altitudes of 35.000 feet and lower. In fact the materials have been changed from that item for this hazard analysis so it should be even safer. 31. In nelrau. - unrnl- 1 um I I 0?34 64?14848, Class A, 30 April 15, AFSAS #739726 03. BIG SAFARI PROGRAM MEMORANDUM OF AGREEMENT . I - 4" 1?61,- ?33 - fl .3.- Memorandum of Agreement In support of the Big Safari Program Between Defense Contract Management Agency Aircraft Integrated Maintenance Operations - Greenville TX And 645? Aeronautical Systems Group 9 May 2011 umer 01 Contracting Commander 645?" Aeronautical Systems Group DCMA AIMO GREENVILLE TX 64?14848, Class A, 30 April 15, AFSAS #739726 Reviewed and Concurred by: . Colonel. USAF Commander 845'? Aeronautical Systems Group Commander 845" Automatics! Systems Squadron Lt Col Commander 661? Actonauucal Syomno Squadron 0-36 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 1. PURPOSE: This agreement de?nes the roles and establishes the relationship between the ?45th Aeronautical Systems Group (645 inclusive of 551? and 645'" Aeronautical Systems Squadron herein after collectiver referred to as the PM) {Program Management Office) and the Defense Contract Management Agency Aircraft Integrated Maintenance Operations Greenvilie TX. hereinaitr referred to as the CMD (Contract Management Of?ce). The PMO and CMO shall work in a collaborative effort to support the success of the Big Safari Program at L-3 Communications integrated Systems tL-?fiS} in Greenville and Waco. Texas. This agreement identi?es the current Program manager's desired outcomes and expectations. It is recognized that these outcomes and expectations are subject to change. This agreement will be modified to malts those changes as they occur. 2. TEAM APPROACH: An integrated team approach betwraen the PMO and Civil: will be utilized for managing contractor performance. This integrated team approach will maximize the use of limited resources. reduce dupiicative efforts. and streamline management processes. Of paramount importance to effective government contract management is open communication between PMD and CMD functional speciaiists. and (IMO personnel shall keep each other fully informed of matters discussed with the contractor. Findings from surveillance activities and other contract performance reviews will be coordinated between appropriate team members. Direct communication behveen the Phil] and (IMO is authorized and encouraged. 3. DCMA PERFORMANCE MEASURES: The following performance commitments are agreed upon to track and rate DCMA performance in support of this MUA. Just as Customer Outcomes change. the measures of DCMA success will change as well. As changes to outcomes Occur. the following measures will be changed accordingly. The perfom'ience commitment in the agreement may only be updated or changed at the direction of or concurrence by the Program Management Office. DGMA vi; 7 . -. a - teats-nay concerns} -. 1'99?? ?Ff'm'smd?? 'i ?at? Cuetomer Outcome: ContractAdministretion supports program. Greater than 95% of all contract closeouts will be within FAR mandate. meant-nests. . . Yellow: or - 95% of all contract Mummy Actuals closaouts within FAR mandate Greater than 95% of all cancelling T?reeha orchestrations} funds will be eliminated by 30 Set: of .srnii?st?ea. . . . . each Fiscal Year Yellow: 8? to 93% of all cancelling funds iimineted. 30 339 ZDXX Iv. Establish Forward Pricing Rate . Agreement and monitor actual costs on a basis. . Eastithrce?onth 3.4: - a: -- Yellow: FPRA is established and actual Copy of Contractors rate review report to DCMA may be provided to Program Office costs vary more than 3% for one to M0 months in - at three months 0?37 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 4. APPENDICES: Aggendix A: PMO Resnonsibilities mum): B: 5Mde 0: Appendix D: Appendix E: Annendix F2. Appendix 5: Customer Dutcarnes Listing Cause and Effect An??g DGMA Strateqies and Functions Communication and Reporting CMO P1510 Contract Administration Functions ICASI Points at Contact 0?38 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 APPENDIX A: PHD 1. Plan. conduct. and report on all AESG. 6&5?1 and ?ight and ground station test programs. 2. Provide operational support. Programmed Depot Maintenance (POM). acceptance and test flight operations. and associated United States Air Force Quality Assurance (DA). 3. Perform the key process and program speci?c contract administration functions outlined in FAR Subpart 42.302 and DFARS. Subpart 242.302. which have not been delegated to the CMD in Appendix to this agreement- 4. Provide Program Manager (PM) interface during depot operations. 5. Perform on-site technical program management. 6. Provide technical advice to the and DMD. as required. T. Provide on?slte technical support to pricing for ?eld pricing reviews of contractor proposals as required by FAR 15.4. Request for review of proposals may he initiated and coordinated by the Procurement Contracting Of?cer (PCO). Administrative IDor'ltractirrg Officer or the Defense Contract Audit Agency (DEM). 3. Perform technical functions associated with over and above activities. 9. Accomplish product quality assurance (GA) for assigned programs. Inspection of servicesisupplies will be performed at the contractor's facilities in and Waco. TX. 10. Perform Safety of Flight (SDF) and Aviation Critical Safety item (CSI) inspections. ii. Manage Product Quality De?ciency Reporting (PQDR) and Material Review Board (MRBJ programs. 12. Provide production surveillance and status reporting. including timely reporting of potential and actual slippage in contract delivery schedules. 13. Perform engineering surveillance of contractor design. development. production. engineering changes. subcontractor perfonnance and data. and configuration control. Review engineering change proposals. waivers. and deViations for proper classi?cation. Report to P60 and ACO any inadequacies noted in speci?cations. 14. Perform logistics support service surveillance. 15. PMO will allow opportunities for select unit members to attend Government Flight Representative (GFR) andior Government Ground Representative (GGR) training. DDMA Greenville in coordination with 645 may designate alternate DCMA GFRs and or alternate GGRs as desired. The primary and alternate GFRs will coordinate on all matters related to the conduct of ground and flight operations as required by the contract, the DMD. and service guidance- The primary and alternate GER will coordinate on all matters related to contractor ground operations. 16- Squadron personnel will ccmmunicateicoordinate with the DGMA GFR on mishaps immediately by telephone with follow-up via email message. Screen. redistribute and dispose of Fit items in the contractor's inventory. 0?39 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 APPENDIX B: CUSTOMER OUTCOMES LISTING The following Customer Desired Outcomes were voiced by customer. The metrics and standards in this appendix represent how the customer measures successful accomplishment of their desired outcomes. customer Du cemei Contract ?dminietration su'o program. Timelyr contract closeouts. No overege contracts Prevent funds cancellation. Zero cancelled funds 3U September EDXX Forward Pricing Rate Agreement In Place TBD 0?40 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 APPENUIX C: CAUSE AND EFFECT ANALYSIS. The costumer has indicated that the Agency goals for contract closeout and cancelling funds are the same for the Big Safari Program. Historically the DCMA business support team has far exceeded this goal and the DCMA business team will strive to continue to do so. No cause and effect analysis was required for these performance commitments. A Forward Pricing Rate Agreement ls important to efficient and effective contract administration for the PCB and ACE). it has been dif?cult to establish an FRPA over the last year due to unresolved issues. An increased emphasis will be placed by DCMA to achieve resolution of ongoing issues in order to establish and maintain an agreement. 0?41 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 APPENDIX E: COMMUNICATION AND REPORTING 1. Pragram Status Reports are clue an or before the 10?? calendar day of each month. The reparts will contain an executive summary of the health uf the: program with special emphasis on red or yellow areas and DCMA's carrective actions with respect thereto. 0?42 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 APPENDIX F: Chill) 3- PHD Contract Administration Functions FAR 42.302?Contract Administration Functions FMD CMO Delegations Comments at Conditions The contracting of?cer normally delegates the following contract administration functions to a Clle. The contracting officer may retain any of these functions, except those in paragraphs (9). and (11) of this section. unless the cognizant Federal agency (FAR 2.1 01) has designated the contracting of?cer to perform these functions. (1) Review the contractor?s compensation structure. Review the contractor's insurance plans. Conduct postraward orientation conferences. (4) Review and evaluate contractor's proposals under FAR 15.4 and, when negotiation will be accomplished by the contracting of?cer. furnish comments and recommendations to that officer. Technical Evaluation will be conducted by the PMO as supplemented by the DCMA in accordance with FAR 1 5.404-1 Negotiate forward pricing rate agreements. (FAR 1 (6) Negotiate advance agreements applicable to treatment of costs under contracts currently assigned for administration. 31 .1 Determine the of costs suspended or disapproved as required {see Subpart 42.8). direct the suspension or disapproval of costs when there is reason to believe they should be suspended or disapproved, approve final vouchers. Issue Notices of Intent to Disailow or not Recognize Costs (FAR 42.8) Establish final indirect cost rates and billing rates for those contractors meeting the criteria for contracting officer determination in Sub-part 42.1 (10) Attempt to resolve issues in controversy. using ADP. procedures when appropriate (FAR Suopart 33.2); prepare ?ndings of fact and issue decisions under the Disputes clause on matters in which the administrative contracting of?cer has the authority to take de?nitive action. (11] In connection with Cost Accounting Standards (FAR 30.601 and 48 GFR Chapter 99 (FAR Appendix?- (ii Determine the adequacy of the contractor's disclosure statements; 0?43 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 FAR 42.302?Contract Administration Func?ons PMCI CHO Delegations Comments 5. Conditions {ii} Determine whether disclosure statements are in compliance with Cost Accounting Standards and Part 31; Determine contractor's compliance with Cost Accounting Standards and disciosure statements. if applicabie; and (iv) Negotiate price adjustments and execute suppiemental agreements under the Cost Accounting Standards clauses at 52230-2, 52.23045, 52230?4, 52230?5. and 52230?6. (12} Review and approve or disapprove the contractor's requests for payments under the progress payments or performance-based payments clauses. (13] Make payments on assigned contracts when prescribed in agency acquisition regulations. {14) Manage special bank accounts. {15} Ensure timely noti?cation by the contractor of any anticipated overrun or under run of the estimated cost under cost?reimbursement contracts. (16) Monitor the contractor?s financial condition and advise the contracting officer when it jeopardizes contract performance. {17) Analyze quarterly limitation on payments statements and recover overpayments from the contractor. (18) issue tax exemption forms. (19} Ensure processing and execution of duty-free entry certificates. (20) For classi?ed contracts. administer those portions of the applicable industrial security program deiegated to the CMD. Subpart 4.4} LEAD The PMO is responsible for providing oversight and guidance in accordance with the DD 254 contained in each contractiorder. (21} Issue work requests under maintenance. overhaul, and modification contracts. LEAD (22) Negotiate prices and execute supplemental agreements for spare parts and other items selected through provisioning procedures when prescribed by agency acquisition regulations. (23) Negotiate and execute contractual documents for settlement of partial and comptete contract terminations for convenience. except as otherwise prescribed by Part 49. 0?44 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 FAR diam?Contract Administration Functions PMCI CMO Delegations Comments at Conditions (24) Negotiate and execute contractual documents settling cancellation charges under multiyear contracts (25) Process and execute novation and change of name agreements under Support 42.12. (26) Perform property administration. (FAR Part 45} LEAD DCMA will perform property administration for all government assets not in the PMO managed supply accounts. Approve contractor acquisition or fabrication of special test equipment under the clause at 52245-13. Special Test Equipment. XLEAU PMD will review requirements and make recommendations to DCMA prior to approvalfdisapproval. For Big Safari contracts only. (28} Perform necessary screening. redistribution, and disposal of contractor inventory. LEAD PMO 1will review all surplus lists prior to DCMA directing disposition. For Big Safari contracts only. (29} Issue contract modifications requiring the contractor to provide packing, crating. and handling services on excess Government property. When the A80 determines it to be in the Government's interests, the services may be secured from a contractor other than the centractor in possession of the property. in facilities contracts Evaluate the contractor's requests for facilities and for changes to existing facilities and provide appropriate recommendations to the contracting of?cer. (ii) Ensure required screening of facility items before acquisition by the contractor. Approve use of facilities on a noninterference basis in accordance with the clause at 52245-9. Use and Charges. {ivi Ensure payment by the contractor of any rental due. Ensure reporting of items no longer needed for Government production. (31) Perform production support. surveiliance. and status reporting. including timely reporting of potential and actual slippages in contract delivery schedules. PMO will be responsible for the integration and prioritization of scheduies across all Big Safari orders. (32} Perform ore-award surveys. [see Suopart 9.1} 0?45 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 FAR 42.3D2?Contract Administration Functions PHD CMD Delegations Comments Bi Conditions {33} Advise and assist contractors regarding their priorities and allocations responsibilities and assists contracting of?cers in processing requests for special assistance and for priority ratings for privately owned capital equipment. LEAD PM) will assist in advising the contractor on priorities for Big Safari contracts. (34} Monitor contractor indUstrial relations matters under the contract; apprise the contracting officer and if designated by the agency. the cognizant labor relations advisor. of actual or potential labor disputes; and coordinate the removal of urgently required material from the strikebound contractor?s plant upon instruction from. and authorization of. the contracting officer. (35) Perform traffic management services, including issuance and control of Government bills of Iading and other transportation documents. {36) Review the adequacy of the contractor's traffic operations. 737) Review and evaluate preservation, packaging and packing. LEAD F'lle will review and evaluate all preservation, packaging. and packing requirements for properly managed by the PMD (PX) supply accounts. (33) Ensure contractor compliance with contractual quality assurance requirements. Part 46} LEAD PMD will perform inspection and acceptance of all supplies and services. ?3!le will perform key process surveillance in accordance with DLAD 5000.4, Contract Management. For Big Safari contracts only. (39} Ensure contractor compliance with contractual safety requirements. LEAD PMD and will ensure day-to-day compliance. will provide inputs to the primary (4U) Perform engineering surveillance to assess compliance with contractual terms for schedule. cost and technical performance in the areas of designr development and production. (41} Evaluate for adequacy and perform surveillance ot contractor engineering efforts and management systems that relate to design, development. production. engineering changes, subcontractors, tests. management of engineering resources. reliability and maintainability. data control systems, con?guration management and independent research and development. PMO retained function. 0?46 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 FAR Administration Func?ons PMO EMU Delegations Comments 8: Conditions [42) Review and evaluate for technical adequacy the contractor's logistic support, maintenance and modification programs. PMO retained function, (43) Report to the contracting of?ce an},t inadequacies noted in speci?cations. PMO retained function. (44) Perform engineering analyses of contractor cost proposals. PMO retained function. (45] Review and analyze contractor- proposed engineering and design studies and submit comments and recommendations to the contracting office as required. PMD retained function. (46) Review engineering change proposals for proper classi?cation. and when required. for need. technical adequacy of design, pruducibilily, and impact on quality. reliability. schedule and cost: submit comments to the contracting officer. PMO retained function. (47) Assist in evaluating and make recommendations for acceptance or rejection of waivers and deviations. PMO retained function. (43) Evaluate and monitor the contractor?s procedures for complying with procedures regarding restrictive markings on data. {49} Monitor the contractor?s value engineering program. (50) Review and approve or disapprove. and maintain Surveillance of the contractor's purchasing system. (FAR Part 44} (51) Consent to placement of subcontracts. (52} Review, evaluate and approve plant or division-wide small. small disadvantaged and womenrowned small business master subcontracting plans. (53) Obtain the contractor's currently approved company? or division-wide plans for small, small disadvantaged and womenewned small business subcontracting for its commercial products, or, if there is no curren?y approved plan. assist the contracting of?cer in evaluating the plans for those products. 0?47 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 FAR 42.302?Contract Administration Functions FMO CMO Delegations Comments 8: Conditions {54) Assist the contracting of?cer, upon request, in evaluating an offeror's proposal small disadvantaged and women-owned small business subcontracting plans, including documentation of compliance with similar plans under prior contracts. (55} By periodic surveillance. ensure the contractor?s compliance with small. small disadvantaged and women?owned small business subcontracting plans and any labor surplus area contractual requirements; maintain documentation of the contractor's performance under compliance with these plans and requirements; and provide advice and assistance to the firms involved as appropriate. (5E) Maintain surveillance of flight operations. LEAD DCMA GFR will work with each Squadrons commander and alternate GFRs. Assign and perform supporting contract administration. (58) Ensure timely submission of required reports. (59] Issue administrative changes. correcting errors or omissions in typing. contractor address. facility or activity code, remittance address. computations which do not require additional contract funds. and other such changes. (FAR Subpart 43.101} (60} Cause release of shipments from contractor's plants according to the shipping instructions. When applicable. the order of assigned priority shall be followed; shipments within the same priority shall be determined by date of the instruction. {at} Obtain contractor proposals for any contract price adiustments resulting from amended shipping instructions. Review all amended shipping instructions on a periodic. consolidated basis to ensure that adjustments are timely made. Except when the ACID has settlement authority. the ACE) shall forward the proposal to the contracting of?cer for contract modi?cation. The ACO shall not delay shipments pending completion and formalization of negotiations of revised shipping instructions. 0?48 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 FAR 42.302?Contract Administration Functions PMD GMD Delegations Comments Conditions (62] Negotiate andtor execute supplemental agreements. as required, matting changes in packaging subcontractors or contract shipping costs. (63) Cancel unilateral purchase orders when notified of non?acceptance by the contractor. The CAO shall notify the contracting o?icer when the purchase order is cancelled. (64] Negotiate and execute onestime supplemental agreements providing for the extension of contract delivery schedules up to 9D days on contracts with an assigned Criticalin Designator of 42.1 1:15). Notification that the contractor delivery schedule is being extended shall be provided to the contracting office. Subsequent extensions on anyr individual contract shall be authorized only upon concurrence of the contracting office. {55} Accomplish administrative closeout procedures. 4304-5} Determine that the contractor has a drug-free workplace program and drug- free awareness program. (see Subpart 23.5} Support the program. product and project offices regarding program reviews, program status. program performance and actual or anticipated program problems. XLEAD DCMA will provide support on key process surveillance. (68) Monitor the contractor's environmental practices for adverse impact on contract performance or contract cost, and for compliance with environmental requiI'Ements speci?ed In the contract. AGO responsibilities include- Requesting environmental technical assistance, if needed; (ii) Monitoring contractor compliance with specifications requiring the use of environmentally preferable products. energy-ef?cient products, and materials or delivery of end products with specified recovered material content. This must occur as part of the quality assUrance procedures set forth in Part 46; and 0?49 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 FAR 42.302?Contract Administration PMD CMD Delegations Comments 8. Functions Conditions As required in the contract, ensuring that the contractor complies with the reporting requirements relating to recovered material content utilized in contract performance. (see Subpart 23.4) {69} Administer commercial ?nancing provisions and monitor contractor security to determine ensure its continued adequacy to cover outstanding payments, when on-sile review is required. Deooligate excess funds after ?nal it price determination. The CMO shall perform the following functions only when and to the extent speci?cally authorized by the contracting office: Negotiate or negotiate and execute it supplemental agreements incorporating contractor proposals resulting from change orders issued under the Changes clause. Before completing negotiations, coordinate any delivery schedule change with the contracting of?ce. (2) Negotiate prices and execute priced exhibits for unpriced orders issued by the contracting of?cer under basic ordering agreements- Negotiate or negotiate and execute supplemental agreements changing LEAD contract delivery schedules. (4) Negotiate or negotiate and execute supplemental agreements providing for the deobligation of unexpended dollar balances considered excess to known contract requirements. Issue amended shipping instructions and. when necessary, negotiate and execute supplemental agreements incorporating contractor proposals resulting from these instructions. Negotiate changes to interim billing gripes. Negotiate and de?nitize adjustments to contract prices resulting from exercise of an economic price adjustment clause. [see Subpart 16.2) (3) Issue change orders and negotiate and execute resulting supplemental agreements under contracts for ship construction, conversion and repair. 0?50 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 FAR 42.3?2?Contract Administration Functions PMO CMD Delegations Comments 8. Conditions Execute supplemental agreements 0n ?rm-?xed priced supply contracts to reduce required contract line item quantities and deohligate excess funds when notified by the contractor of an lnconsequentisl delivery shortage. and it is determined that such action is in the best interests of the Government, notwithstanding the default provisions of the contract. Such action will be taken only upon the written request of the contractor and. in no event. shall the total downward contract price adjustment resulting from an inconsequential delivery shortage exceed $250?t} or 5 percent of the contract price, whichever is less. (10} Execute supplemental agreements to permit a change in place of inspection at origin speci?ed in firm-fixed-price supply contracts awarded to non-manufacturers as deemed necessary to protect the Government's interest. {11) Prepare evaluations of contractor performance in accordance with Subpal?t 42.1 5. Any additional contract administration functions not listed in and or not otherwise delegated, remain the responsibility of the centracling office. 0?51 V, 64-14848, Class A, 30 April 15, AFSAS #739726 APPENDIX 6: POINTS OF CONTACT CONTRACT MANAGEMENT OFFICE (CMO) GREENVILLE. TX Commander Lt Col 5 Deputy Commander Business Team Leader GREENVILLE. TX DACO ACOIPI CA Intern CA - Intern p1- GFR GGR WACO, TX ACOISPI PT Primary GFR PROGRAM MANAGEMENT OFFICE (PMO) 645?" AERONAUTICAL SYSTEMS GROUP DAYTON, OH Commander Commander Chief Compass Call Program 0-52 RC.135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 645m AERONAUTICAL SYSTEMS SQUADRON GREENVILLE. TX Commander Deputy Commander Logistics Operations Product Assurance Branch Chle! Plans Management Branch Chief Jill 5613' AERONAUTIGAL SYSTEMS SQUADRON WACO. TX commander Contracts - 0-53 RC4 35 V, 64?14848, Class A, 30 April 15, AFSAS #739726 04. FIRE DEPARTMENT INCIDENT REPORT USAF Fire and Emergency Response Noti?cation System ACC F7022 Offutt AFB Date: 4/30/2015 Incident 3 2] I Location Active Runway Was the Incident On Base? Yes Occupancy Aircraft Operations Distance From Base (miles) Aerospace Type/Model Number Responding Fire?ghters 25 Time of Incident l8:27 Air Force Loss or Damage: Termination Time 23:39 Non Air Force Loss or Damage: $0.00 Total Run Time 5; [2 Air Force FD Equipment $0.00 Initial On-Seene Time 18:20 Total Lon or Damage: 32.000.000.00 Structual WMD .. - . ARFF 1:1 Wildland [Satellites [names Medical Mutual Aid Civilian Fire?ghters 0 0 [j HazMat Privatized Housing Military Fire?ghters 0 0 0m? Non DOD Fire?ghters 0 0 Non Firefighters 0 4 Was the EOC Activated? Yes Did this incident generate an OPREP-3 report? Ya this incident meet the 32-2001 reporting criteria? Yes Equipment Used ARFF suucturul equipment, tanker, foam trailer, air packs. sawmill. K?l 2, thermal imaging camera Probable Cause The cause IS unknown at this time. The tire was located ID the galley area of the aircraft that contained microwaves and refrigeration units. There is also a ventilation fan motor in the vicinity of the ?re area Incident Summary Fire department crews responded to Runway 30 for report of a tire on an 35 altered. The crew had shut down and evacuated the aircraft prior to our arrival. The tire was in the galley area of the aircratt. the left rear area in the aircra?. The ?re burnt a large portion of the galley area and hreached the fuselage shave the galley area. Interior crews contained the ?re to the galley area and crews on the outside utilized 8 PB roof turret to immediately extinguish the tire coming through the fuselage. Fire was contained to the galley area with Signi?cant smoke and water/foam damage to the rear of the aircra?. A?er the aircratt was moved from the active runway to the parking area where the investigation will occur. light smoke was observed coming from the tire area. it was determined that the smoke was coming from smoldering vent insulation in the burnt area. The ?re area was more thoroughly overhauled to insure no wignition. A standby truck is in place at the aircrall. The OtTutt aircraft accident investigation board visited the aircraft while on the active runway and the alert photographer toolt photos. The aircraft is impounded and under SF 8 guard at this time. 4 aircrew members wore taken to a local hospital for signs of smoke inhalation They are now ?ne. Nu ?re?ghter/EMS injuries. A more in depth report will be submitted as required. Cost estimates of damage are very preliminary and are likely to be much higher. Mission impact The R0135 Aircra? is out of commission. Cognilant Of?cial and Telephone Number Fire Chief 0-54 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB P DAMAGE SUMMARIES P1. ENVIRONMENTAL CLEAN-UP COSTS ......................................................................... 2 P2. NON-DOD PROPERTY DAMAGE COSTS...................................................................... 2 P3. ITEMIZED DOD PROPERTY DAMAGE COSTS .......................................................... 3 P-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK P-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 P1. ENVIRONMENTAL CLEAN-UP COSTS No data applicable. P2. NON-DOD PROPERTY DAMAGE COSTS There were damages to non-DOD property for this mishap. P-3 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 P3. ITEMIZED DOD PROPERTY DAMAGE COSTS The “Group A” item covers all the damaged mission equipment cost. The “Group B” item covers all the non-mission equipment/aircraft furnishing cost to include fuselage and structure repairs. Depot (contractor) labor costs are included in the total cost of the damage assessments in Groups A and B. Part # / NSN SOURCE UNIT EXCHANGE COST QTY 1 STRUCTURE RC-135V 2 Group A (Msn Equip) N/A Contractor $17,065,058.00 N/A $17,065,058.00 UNKNOWN DEPOT 3 Group B (Acft Equip) N/A Contractor $45,241,576.00 N/A $45,241,576.00 UNKNOWN DEPOT 4 Oxygen Mask 1660-01-424-4124 FEDLOG $1,767.73 1 TOTAL COST FIELD/DEPOT LABOR HRS LEVEL REPAIR OBJECT 1 $1,767.73 1 FIELD 5 Refrigerator 400-1378-02 Contractor $47,011.00 2 $94,022.00 1 DEPOT 6 Convection Oven 91107-064 Contractor $19,136 1 $19,136.00 1 DEPOT 7 Microwave 400-1409-03-L Contractor $19,234 1 $19,234.00 1 DEPOT 8 Fan JM000006-052 Contractor $1,725 4 $6,900.00 1 DEPOT $48 $240.00 5 FIELD Mishap Total Cost $62,447,933.73 Labor P-4 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB Q AIB TRANSFER DOCUMENTS Q1. AIB TRANSMITTAL LETTER ......................................................................................... 2 Q2. ATTACHMENT 1: LIST OF WITNESSES ...................................................................... 5 Q3. ATTACHMENT 2: 24-HOUR CLASS A PRELIMINARY MESSAGE ........................ 8 Q4. ATTACHMENT 3: FILE INVENTORY ......................................................................... 11 Q-1 V, 64?14848, Class A, 30 April 15, AFSAS #739726 Q1. AIB TRAN SMITTAL LETTER DEPARTMENT OF THE AIR FORCE HEADQUARTERS AIR COMBAT COMMAND LANGLEY AIR FORCE BASE, VIRGINIA 3 June 2015 MEMORANDUM FOR ACCIDENT INVESTIGATION BOARD PRESIDENT FROM: President, Safety Investigation Board SUBJECT: Inventory and Witness List, Class A Mishap, SN 64-14848, 30 April 2015 l. The following items are released to the Accident Investigation Board: A. Pan 1 (Tabs A through S) of the Formal Safety Report of subject mishap are released both via physical copies and via the shared drive Aircraft 64-14848 (Bennie Davis MXFacility D4 at 0mm AFB) Mishap Aircrew's aircrew ?ight equipment (Bennie Davis MX Facility D4 at Offutt B. C. D. AFB) Mishap aimrew?s ?ying records Aircraft parts sent for analysis 1. NOMAUJN 9. Sample from on top of exemplar 02 (POCLarge RF cable (POC: . Coffee pot galley cable harness (POC: . 02 line 1 0 RH 02 system (PDC: . 02 line 2 - 02 on galley (POC: . Convection oven cable (POC: . Microwave oven and panel cable (POC: Long cable hamess labeled FWD AFT (POC: Research Lab (AFRL), DSN AFRL. DSN AFRL. AFRL, DSN AFRL, DSN AFRL. DSN . AFRL, DSN .AirForce Galley light lens (POC: AFRL, DSN AFRL, DSN Burned box ?'om compartment above microwave (POC: AFRL, DSN Galley mount bolts (POC: Top component cardboard (POC: Top compartment cardboard and wiring (POC: AFRL, DSN AFRL. DSN AFRL, DSN Top tight compartment -cardboard (POCL DSN Q-2 R0135 V, 64?14848, Class A, 30 April 15, AFSAS #739726 DEPARTMENT OF THE AIR FORCE HEADQUARTERS AIR COMBAT COMMAND LANGLEY AIR FORCE BASE, VIRGINIA 15. Exemplar - nuts and bushings (POC: AFRL, DSN 16. Debris ??om ?oor at time 1240 (POC: AF RL, DSN l7. Debris from over the galley (POC: AFRL, DSN 18. Debris from galley counter (POC1. AFRL, DSN 19. Top of galley (POC: DSN 20. Bottom of galley (POC: AFRL, DSN 21. Refrigerator 1 (FCC: 645 22. Refrigerator 2 (POC: 645 23. Oven, Convection (POC: . 645 24. Microwave Oven, Wavelet (POC: . 645 25. Fan 1' (FCC: 645 26. Fan 2 (FCC: 645 27. Fan 3 (POC: 645 28. Fan 4 (FCC: . 645 F. Classi?ed aircraft pans I. Cockpit Voice Recorder (POC: 55 DSN G. Aerospace Ground Equipment released back to the 55 W0 1. Gas Turbine Generator? GTOS (POC: Lt Col DSN 2. Generator - DC26 (POC: Lt Col DSN 3. Diesel Generator D063 (FCC: Lt Col DSN 4. Air Conditioner - DA51 (TOC: DSN 5. Diesel Generator D025 (POC: DSN 6. Air Conditioning Cart - DA37 (POC: DSN 1. Lox Cart- (POC: s. Hydraulic Cart - mos (POC: . Nitrogen Can- HC03 (POC: DSN DSN DSNI H. List of Witnesses (Attachment 1) 1. 24?Hour Class A Preliminary Message (Attachment 2) Q-3 V, 64?14848, Class A, 30 April 15, AFSAS #739726 DEPARTMENT OF THE AIR FORCE HEADQUARTERS AIR COMBAT COMMAND LANGLEY AIR FORCE BASE, I. All non-privileged material. both hard and digital, documented on the ?le inventory (Attachment 3) 2. "Ihe mishap aircraft has already begun disassemny and cleaning both to determine the extent of the damage and associated costs as well as to prevent further corrosion to the aircraft from the tire suppressant chemicals. All other items removed from the aircraft not mentioned above are still located inthe cordoned area adjacent to the aircra?. 3. Please reply by endorsement below that you are in receipt of these items and take responsibility for their final disposition. Col, USAF President, Safety Investigation Board Ind, Interim Handover Point of Contact T0: President Safety Investigation Board Acknowledge receipt and responsibility for the above listed items. TSgt, USAF Interim Handover Point of Contact Accident Investigation Board Q-4 64?14848, Class A, 30 April 15, AFSAS #739726 Q2. ATTACHMENT 1: LIST OF WITNESSES .. - . 4H, may. a??mm twal'lhtervlwo?? Mai-mama Materials and 26_May_15 L3 Processes Engineer . 55 A1 Crew Chief 30-Apr-15 Assistant Chief of 68-10 Training (Fire?ghter) 13-May-15 55 - - Airborne Systems 30-Apr-15, 1-May-15, [Mishap Aimome Svstems Enoineer 21 srA Engineer 2 1 1-May-15, 18-May-15 343 Flightline Expediter 22-May-15 55 Maj Tactical Coordinator 30-Apr-15, 1-May-15 343 Rave" ?1 Capt Tactical Coordinator 30-Apr?15, 11-May-15 343 A10 Air Traf?c Controller 1-May-15 55 [Mishap Fire?ghter 1] Fire?ghter 30-Apr-15, 13-May-15 55 (SS-07 - - Airborne Systems [Mishap Airborne Systems Emineef Engineer 343 CTR Quality Control 26-May-15 L3 EW Technician 30-Apr-15 55 Airborne Systems A10 Engineer 1 30-Apr-15 343 . 55 A1 Crew Chief 30-Apr?1 5 A1 Maintainer 30-Apr-15, 13-May-15 55 Airborne Analyst 30-Apr?1 5 97 . 55 Crew Chief 30-Apr-15 lnforrnation 1st Lt Integration Of?cer 30-Apr-15 97 [Mishap Capt Co-Pilot 30-Apr-15 343 . 55 Crew Chief 30-Apr-15 AMXS IMXAB A - A Airborne Systems 30-Apr-15, 1-May-15, [Mishap Airborne Svstems Enoineer 3 Engineer 4 1 1-May?15, 18-May-15 343 . 55 Crew Chief 30-Apr-15 Q-5 64?14848, Class A, 30 April 15, AFSAS #739726 . 55 Crew Chief 30-Apr-15, 22-May-15 AMXS IMXAB A Operator 30-Apr?1 5 97 Operator 30-Apr-15 97 55 Engine Troop 30-Apr-15 Capt Supervisor of Flying 1-May?15 38 [Mishap Airbome Mission mason 30-Apr-15 97 [Mishap Mechanic] CTR Aircraft Mechanic 26-May-15 L3 Operator 30?Apr?1 5 97 1Lt Raven 30-Apr?15 343 Operator 30-Apr-15, 1-May-15 97 - - . 30-Apr-15, 12-May-15, [Mishap 0mm Operator 15_May_15 97 Operator 30-Apr-15 97 . 55 Crew Chief 30-Apr-15, 26-Apr-15 [M?S'lap Slgna'S' Seam? Signals, Search 30-Apr-15, 1-May-15, W?3?mm? Development 1 1-May-15 97 Production 55 Superintendent 3O'Apr'15? 13'May'15 [Mmap ?re?ght? 21 68-07 Fire?ghter 30-Apr-15, 13-May-15 55 Maj Raven 30-Apr-15 343 lnfonnation Capt Integration Of?cer 30-Apr?15, 11-May?1 5 55 [M'shap Rave" 21 1 Lt Raven 30-Apr-15, 1 1-May-15 343 Operator 30-Apr?1 5 97 . Mental Health Flight Maj Commander 27-May-15 55 MDG Tami" Tactical Coordinator 30-Apr-15, 9-May-15 343 RS oordlnatorl A1C Air Traf?c Controller 1-May?15 55 Operator 30-Apr-15 97 64?14848, Class A, 30 April 15, AFSAS #739726 55 Engine Troop 30-Apr?1 5 Data Link Operator 30?Apr?1 5 97 [M?Shap PM . 30-Apr-15, 1-May-15, Capt 11_May_15 343 Production 55 Superintendent 30'Apr'15 [Mishap NaV?gam?l Capt Navigator 30-Apr-15 55 . 55 Crew Chlef 30-Apr-15 AMXS IMXAB A Airborne Systems I'nsmomme Engineer 5 19-May-15 338 Svstems Enalneer] Instructor RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 Q3. ATTACHMENT 2: 24-HOUR CLASS A PRELIMINARY MESSAGE Message Release Date: 01 MAY 2015 2103(Z) Classification: Unclassified From: 1 Airborne Command Control Squadron (1 ACCS) Subject: Preliminary: Class A, 30 APR 2015, Aviation, Aircraft Flight, Aircraft/RC-135V, Offutt AFB, AFSAS Report # 739726 1. General Information: 1.1. AFSAS Report Number: 739726 1.2. Convening Authority: Air Combat Command 1.3. Accounting MAJCOM, DRU or FOA: Air Combat Command 1.4. Accounting NAF: Twenty-Fifth Air Force 1.5. Accounting Wing: 55 Wing 1.6. Accounting Base: Offutt AFB 1.7. Mishap Duty Status: On-Duty 2. Mishap Date/Time: 2.1. Mishap Date, Local: 30 APR 2015 2.2. Mishap Time, Local: 1827 3. Mishap Location: 3.1. Mishap Country: United States (USA) 3.2. Mishap State: Nebraska 3.3. Nearest Base: Offutt AFB 3.4. Latitude: 41 07.673 N 3.5. Longitude: 095 55.349 W 4. Narrative: 4.1. Narrative: During the initial takeoff roll of a local training sortie, a fire developed in the reconnaissance area of an RC-135V. The crew aborted and egressed without injury. An ISB was convened on 30 Apr 15 and is currently collecting data and preserving evidence. 5. Personnel Information: Person Number: 1 5.1.1. Gender: Male 5.1.2. Age: Q-8 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 5.1.3. Grade: O3 5.1.4. Employment Status: 5.1.4.1. Tier 1: US Military and Coast Guard 5.1.4.2. Tier 2: USAF Regular 5.1.5. Assigned MAJCOM: Air Combat Command 5.1.6. Assigned Numbered Air Force: Twenty-Fifth Air Force 5.1.7. Assigned Wing: 55 Wing 5.1.8. Assigned Group: 55 Operations Group 5.1.9. Assigned Squadron: 343 Reconnaissance Squadron 5.1.10. Assigned Base: Offutt AFB 6. Objects Information: Object Number: 1 6.1.1. Object Type 6.1.1.1. Tier 1: Aircraft 6.1.1.2. Tier 2: RC-135V 6.1.2. Unique Object Identifiers: 6.1.2.1. Tail Number: 64-004848 6.1.3. Damage Description: Repairable 6.1.4. Owning Service: Air Force 6.1.5. Owning MAJCOM: Air Combat Command 6.1.6. Owning Numbered Air Force: Twenty-Fifth Air Force 6.1.7. Owning Wing: 55 Wing 6.1.8. Owning Base: Offutt AFB 7. Interim Safety Board Personnel: Position: Investigating Officer 7.1.1. Name: 7.1.2. Grade: O4 7.1.3. Organization: 1 ACCS/SE 7.1.4 Phone(s): 7.1.4.1. DSN: 7.1.4.2. Commercial USA: 7.1.4.3. International: 7.1.5. Email: 8. Releasing Official: 8.1. Name: 8.2. Grade: O4 8.3. Organization: 1 ACCS/SE Q-9 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 8.4. Email: 8.5. Phone(s): 8.5.1. DSN: 8.5.2. Commercial USA: Q-10 RC-135 V. 64?14848, Class A, 30 April 15, AFSAS #739726 Q4. ATTACHNIENT 3: FILE INVENTORY RC-135. 64-4848. Class A. 30 Mar 2015. AFSAS #739726 188 Letter 1 HARM Checkout Checklist Fire Personnel Accident USAF Fire and Emergency Response Burnt Aerosol Can Fire Protection Branch Fire Department After FOD Found walk Event 4 Report/ Learned (3 Pages) STATEMENT - Co-Pilot 3 - 4 TSgt? Airborne Systems Engineer 4 (3x Hard Hard/Digital Hard/Digital Capt - Lt Col - Tactical Coordinator - - 1st Lt - Information - Airbome Systems Engineer Airborne Systems Engineer 1 (3 Pages) 1Lt - Raven 1Lt- Raven - Chief - Q-ll 15 1 1 9-May-1 5 5 15 1 15 12-May-15 15 1-Jun-15 Share Drive Box Share Drive 8 I Share Drive I Box 6 Share Drive Box Share Drive 6 lShare 6 6 6 I Share Drive I Share Drive 6 I Share Drive 64?14848, Class A, 30 April 15, AFSAS #739726 R0135. 644848. Class A. 30 Mar 2015. AFSAS #739726 - Box Share Drive 6 Share 8 Share Drive 6 - 6 A1 - Controller Drive - Air Traf?c - Box 6 Hard/Digital 10 - Assistant of Training (Hrefightar) (1 13-May-15 6 I Share 1 5 - 1 15 Drive Maj - Mental Health Flight Commander(1 6 [Share - Control 15 CTR - Mechanic 15 6 I CTR - and Processes Enginaer? Pages) 15 I Form 244 Record 14 Debrief Form 11 Data - 90 Tool Mx Member SURFs QQOCDOIOICD icial hats at a) MX Member Trainina Recons 11 Binder Pulled Forms Total Sets Environmental Environmental Q-12 RC-135 V. 64?14848, Class A, 30 April 15, AFSAS #739726 RC-135. 64-4848. Class A. 30 Mar 2015, AFSAS #739726 Form 7110 MOC Health Risk Assessment from Bio Turbine Fuel 4 Fluid interior Photos Photos Photos Photos Photos 1st Fire Photos 1st Fire Photos Post 2nd Fire Exterior Photos Post 2nd 848 Initial Removal 848 Interior 11 15 107 Photos Video 4 \?deos Fire Station \?deo Before Removal Photos 5 Photos 13 Photos Photos Photos 4 1' Pictures 192 Records IMT 4327a - Crew Form 175 Plan 1 135 Worksheet 1 Form 365-4 Tactical 06 Section 1 CG 06 Section 2a Simulator Detail 8. 90 RS Aircrew Hour Max 1 13 13 1-Jun-15 1 1 1-dun-15 Documents 19 Photos 30 Photos Authorization 4 and Balance 1 Q-l3 Share Drive 7 Drive Drive Drive Drive Drive Drive Drive Share Drive Box 7 Share Drive \l?d Drive Drive Drive Drive Drive Drive V, 64?14848, Class A, 30 April 15, AFSAS #739726 R0135, 64 4848, Class A, 30 Mar 2016, AFSAS #739726 97 IS Aircrew Individual Traintn 30-Apr~15 14 Aircrew SURFs 15 (27 Total) of Certi?cations Crew Hand Notes Jet Visitor 1 ?1 Data VE 1 items Crew Brief Flight Eval Folders {27 Total) 30-Apr45 (27 Total) 30-Apr-1 5 (27 Total) rainina 30-Apr-15 Located at551h ISS 9 tor Reasons Crew Checklists -15 Box 2 Tech Orders (Flight Manual lnflight Data, Flight Manual Reference Data, Misc Pubs, 1C-1 Black Binder IFG (so-Pilots In binder Ops Documents (27 Total) RJ Pdntout Medical - HIPA 72H 70 Histories (27 Sets) - Airborne Q-l4 V, 64?14848, Class A, 30 April 15, AFSAS #739726 RC-135, 64-4848. Class A. 30 Mar 2016, AFSAS #739726 Taoiicai Coordinator - Tactical Coordinator - Airborne A10 - Airborne Airborne is! Lt - Information I - Co-Pilot - Airborne Mai - - Airborne 1Lt Raven - . S- - - Search - Raven - Information I 1Lt - Raven Lt Col . Tactical Coordinate.r A - Data Link 'Capt- Navigator Maintainers 72H 70 histories (1 4 Total) (4 Total) Post Mishap Treatment Notes Toxicotv Reports (41 Total) AGREEMENTS and SIB Arrived 19 Workers 9?May-15 ?Jun-15 5 2-Jun-15 2-Jun-15 2-.Iun-1 2-Jun-1 Request From AIB Medical Of?cer Provide Upon Request From AIB Medical Of?cer 7 I Drive Box 7 I Share 7 I Share Drive 7 Drive 7 I Share dee 7 I Share Drive 7/ Drive RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 RIB-1351 64-4348. Class A. 30 Mar 2515, AFSAS #739726 Tab 1 an 2-Jun-15 Box 7' a" Share Share Drive ab 2?JunvShare Drive ital at: 2-Jun?15 Drive ital ab 22-Jun-15 Box 1" Tab 1 I Share Drive ab 2-Jun-15 7! Drive Tab Y2 5 Box Share Drive RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB R RELEASABLE WITNESS TESTIMONY R1. CAPT [Mishap Pilot] (MP) .......................................................................... 4 R1.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ........................... 4 R1.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 ............................ 8 R1.3. SIB NON-PRIVILEGED INTERVIEW – 11 MAY 15 ............................................ 14 R2. CAPT [Mishap Co-Pilot] (MCP).................................................................................. 26 R2.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ......................... 26 R2.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 .......................... 29 R3. CAPT [Mishap Navigator] (MN) .......................................................................................... 35 R3.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ......................... 35 R3.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 .......................... 38 R4. CAPT [Mishap Raven 1] (MR1) .................................................................................. 44 R4.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ......................... 44 R4.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 .......................... 48 R4.3. SIB NON-PRIVILEGED INTERVIEW – 11 MAY 15 ............................................ 54 R5. LT COL [MishapTactical Coordinator] (MTC) ............................................................................. 70 R5.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ......................... 70 R5.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 .......................... 74 R5.3. SIB NON-PRIVILEGED INTERVIEW – 9 MAY 15 .............................................. 80 R6. SRA [Mishap Airborne Systems Engineer 1] (MASE1) .......................................................................... 97 R6.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ......................... 97 R6.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 ........................ 101 R6.3. SIB NON-PRIVILEGED INTERVIEW – 11 MAY 15 .......................................... 107 R7. MSGT [Mishap Airborne Mission Supervisor] (MAMS)....................................................................... 117 R7.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ....................... 117 R7.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 ........................ 120 R8. SRA [Mishap Cryptologic Operator] (MCO) ...................................................................................... 126 R8.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ....................... 126 R8.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 ........................ 132 R8.3. SIB NON-PRIVILEGED INTERVIEW – 12 MAY 15 .......................................... 138 Airborne Systems R9. SRA [Mishap Engineer 2] (MASE2).................................................................................... 148 R-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 R9.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ....................... 148 R9.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 ........................ 151 R9.3. SIB NON-PRIVILEGED INTERVIEW – 11 MAY 15 .......................................... 157 R9.4. SIB NON-PRIVILEGED INTERVIEW – 18 MAY 15 .......................................... 171 Airborne Systems R10. TSGT [Mishap Engineer 3] (MASE3) ............................................................................. 175 R10.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ..................... 175 R10.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 ...................... 178 R10.3. SIB NON-PRIVILEGED INTERVIEW – 11 MAY 15 ........................................ 184 R10.4. SIB NON-PRIVILEGED INTERVIEW – 18 MAY 15 ........................................ 200 R11. 1LT [Mishap Raven 2] (MR2) .......................................................................... 204 R11.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ..................... 204 R11.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 ...................... 207 R11.3. SIB NON-PRIVILEGED INTERVIEW – 11 MAY 15 ........................................ 213 Signals, Search & R12. CMSGT [Mishap Development] (MSSD) .................................................................... 221 R12.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ..................... 221 R12.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 ...................... 224 R12.3. SIB NON-PRIVILEGED INTERVIEW – 11 MAY 15 ........................................ 230 R13. MSGT [Production Superintendent] (MMX) ..................................................................... 241 R13.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ..................... 241 R13.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY – 30 APR 15 ...................... 245 R13.3. SIB NON-PRIVILEGED INTERVIEW – 13 MAY 15 ........................................ 251 R14. GS-07 [Mishap Firefighter 1] (MFF1) .................................................................. 259 R14.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ..................... 259 R14.2. SIB NON-PRIVILEGED INTERVIEW – 13 MAY 15 ........................................ 262 R15. GS-07 [Mishap Firefighter 2] (MFF2) .................................................................................. 268 R15.1. ISB NON-PRIVILEGED WITNESS STATEMENT – 30 APR 15 ..................... 268 R15.2. SIB NON-PRIVILEGED INTERVIEW – 13 MAY 15 ........................................ 271 Airborne Systems R16. SRA [Instructor Engineer] (IASE) .................................................................................. 277 R16.1. SIB NON-PRIVILEGED INTERVIEW – 19 MAY 15 ........................................ 277 R17. MR. [Mishap Mechanic] (MM) ..................................................................................... 286 R17.1. SIB NON-PRIVILEGED INTERVIEW – 26 MAY 15 ........................................ 286 R18. MR. [Quality Control Manager] ............................................................................................ 300 R-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 R18.1. SIB NON-PRIVILEGED INTERVIEW – 26 MAY 15 ........................................ 300 R19. [Materials & Processes Engineer] ............................................................................................................. 313 R19.1. SIB NON-PRIVILEGED INTERVIEW – 26 MAY 15 ........................................ 313 R20. MAJ [Mental Health Flight Commander] ...................................................................................... 323 R20.1. SIB NON-PRIVILEGED INTERVIEW – 27 MAY 15 ........................................ 323 R-3 64-14848, Class A, 30 Apri115, AFSAS #739726 R1. CAPT [Mishap Pilot] (MP) R1.1. ISB NON-PRIVILEGED WI INESS STATENIENT 30 APR 15 Page I of 2 nit-Privileged Witness Statement 301191315 main l. I, [Misnap 0 3 ES, have been advised by (Name, Grade, Organization, of Witness) (Manic ofluma'gator) a safety investigator ofthe mishap that occurred on Sii?gtl? involving 355 8 (Data) (Equipment SM a This investigation is being conducted under the provisions of 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as wimess in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Mshap Pilot] (9 3/65 till? Name (Last, mm, M) 31m! Rank/Grade l? V, 64-14848, Class A, 30 April 15, AFSAS #739726 Page I of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of AF I 91-204 901er for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand 1 am being interviewed as a witness in a safety investigation and I achiowiedge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation ot'this mishap and may be released to the public pmsuant to a Freedom of Information Act request. [Mishap Pilot] WITNESS STATEMENT 0F: 45-3/0: p?i Name (Last. First, MI) and Rank/Grade Pdo?f "Ll- Reference attached document for witness account of event. This document is being entered for accounting purposes and for witness 's acknowledgement being theform they Should have received for completion of a written statement. The member?s chain of command will only review the ?nal mishap report if acquired through appropriate safety channels 91-204 para 3. 4. 5 . V, 64-14848, Class A, 30 April 15, AFSAS #739726 NON-PRIVILEGED WITNESS STATEMENT Date of the mishap Crew position (as applicable) 'l imc you begun [Mishap Pilot] 1. l. have been ?lmed by ~_Mmm )i the following. ?nor a. This investigation is being conducted under the provisions of 91-204 solcly for the purpose of mishap within the United States Air Force and to determine all timer? relating to the mishap in order to prevent recumnce. understand I am being intemewed as a witness in a mishap investigation and acknowledge that a promise ufcon?dcnuality has not been extended to me. b. This witness statement may be released to the public pursuant to a Freedom of Information Act request. it. lite chain will review the ?nal mishap repon. Provide an account of ?rst-hand ohsurvatiotts of what happened. a description of prevailing conditions, circumstances, and aswciated event: (use reverse [or continuation). r4355?? plwg? Dim? :27 m. is? wt; on, oxiewciw oi?, in in, ELEV suweria Exams; UARRWR. Maw] MAS ml WM: mskwiiy Magi/vii 0AA by kw I it. ?Gr i730L were, Oink?) N?r SW vo?v HM worker). Owi' or kacat?Md 40 (IN 51 44% 61-st ieuiM-xixlp. 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V, 64-14848, Class A, 30 April 15, AFSAS #739726 in? a? ?4,1 Jr. by ?awed u?vk u? ?\whl wig}. 1 KM oL-Jx 3m won; Rxw-Hou? ?10me we ?now Wd?t?r) +0 Shaka? 01 WK m; Lug Vb co:ng ganoCth' v0 Wu? 4m shr?f 93w? :Lb *0 3x33? 3?5 CALL m; Um? aims: OkaK? Mg '11; I *0 96A *1 ewiuw; uH?k an?. The, *2 0.32% ?rw von wovA4 Bo?H/d 6/ beer L2 62. (am) ptiorto-mishapzDate 5.0 ?qf? lot/p (gauche, - 12.0 1/4? awake" 23A a.ng Pg Z. drag}; )1 at 7,0 J/ef+ ?rt/f eureka/W R-79 64-14848, Class A, 30 April 15, AFSAS #739726 R5.3. SIB INTERVIEW 9 MAY 15 Page I of2 Non-Privileged Witness Statement ?1 Mg )5 (Datehave been advised by __[Invesugaung Of?ce? (Name, Grade, Organization, of Witness) (Name of Investigator) a safety inVestigator of the mishap that occurred on 30 A, is invoMng (Date) (Equipment 3M 3. This investigation is being conducted under the provisions 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I imderstandl am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishnp and may be released to the public pursuant to a Freedom of Information Act request. [Mishap Tactical Coordinator] A ,1 Name (Lmt, First, MI) and Rank/Grade 7?4 we lap/gfmal? A Tul- Signature R-80 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 Tactical SIB Interview of Lt Col [Mishap Coordinator] Role: Tactical Coordinator 343rd Reconnaissance Squadron Interviewers: (President) (Investigating Officer) (Medical Member) (Pilot Member) (Maintenance Member) (Aircrew Flight Equipment Member) (Recorder) (AFSEC Representative) Date: 9 May 15 [Investigating Officer] [Mishap Tactical Coordinator] : OK, um, good morning everybody this is a non-privileged interview with Lt Col being conducted on 9 May 2015 at 0900 local by [Investigating Officer] for the safety investigation board convened for the recent mishap. We’re investigating the mishap involving an RC-135V that occurred on 30 April 15. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of confidentiality is not being extended to you. Your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has NOT been extended? [Mishap Tactical Coordinator] : I do. [Investigating Officer] : Um, and for the record, would everyone present introduce yourself by stating your name, rank and affiliation with the board, starting with the witness? [Mishap Tactical Coordinator] Tactical : Um, [Mishap Coordinator] , Lieutenant Colonel, I was the Tactical Coordinator on, on that sortie. [Investigating Officer] : OK, um, [Investiga ing Officer] [Pilot Member] : Captain [Maintenance Member] [AFEM] , I’m the uh Investigating Officer. , Pilot Member. : Lieutenant Colonel , Maintenance Member. : Senior Master Seargent , Aircrew Flight Equipment Member. [President] [Medical Member] [AFEM] [Recorder] : Colonel [President] : Captain , Board President. , Medical Member. : Chief Master Seargent : And Captain , AFSEC rep. , Recorder. R-81 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Investigating Officer] : OK, so, just ask you a couple of questions sir and then uh, seeing as how you are the first interview um, and everybody is still trying to build a picture, uh, after, after you and I get done talking I’d like to open it up um in case anybody else has any questions for ya. [Mishap Tactical Coordinator] : OK [Investigating Officer] : So, uh, first things first we’ve read your uh statement um, and uh it seems like a very compressed uh, event. [Mishap Tactical Coordinator] [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] : I would say so. : But if you could just take me through it one more time. : Starting from the chocks? Or from… : Um, if you want starting from the chocks but [Mishap Tactical Coordinator] : Well cause I, yeah I’ll start there because it was a little non-standard. Um, we normally start 3, 4, 1, 2, and we got 3, 4, 1 started and then 2 um, it was not starting so they had to pin open um, the starter valve? I dunno [Investigating Officer] : Manual Start [Mishap Tactical Coordinator] Yeah and then pinned it, and then started and then and then we taxied. So that was a little bit non standard from normal. Got out to the end of the runway, everything was fine, we were eventually, we had to wait a little bit because there were some aircraft in the pattern and then we eventually got clearance and then um pushed them up. Um, I don’t know how fast we were going, I think it was about 50 to 70 knots, S1was in the 130s so we had a little bit of time but then I heard over interphone, private and call Fire Fire Fire Fire. Multiple people, multiple positions all at the same time. So… [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] : OK, and where were you sitting sir? : So I was sitting in position 23, its where the Tactical Coordinator sits right here. : OK, and there is a bulkhead here. : There it is. : But you’re able to look back. [Mishap Tactical Coordinator] : I can I can lean back, if the if the seats all the way back and I can lean back I can see all the way down. [Investigating Officer] : OK [Mishap Tactical Coordinator] : Because you can see from here you can basically see all the way down, which is what happened and soon as I, soon as I heard fire fire fire I leaned back and I see it. You know the seats all the way back, I’m leaning back and I can white smoke and fire curling up over, kind of like the bulkhead. R-82 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Investigating Officer] : So you can s… [Mishap Tactical Coordinator] : It’s right around the microwave area. There’s a fridge, microwave and it was just fire was curling up over [Investigating Officer] [Mishap Tactical Coordinator] : OK : This, the microwave on the same path as the as the fuselage and bulk area [Investigating Officer] : So if you’re, so if you’re looking back at the galley. OK and its on the right side of the airplane. Microwave is kind of here right? [Mishap Tactical Coordinator] [Investigating Officer] [Mishap Tactical Coordinator] : Uh huh. : Refrigerator is down here. : Uh, I think the fridge…microwave is right on top of the fridge but… [Investigating Officer] : Yep, you’re right. So, but I’m just saying your kind of looking at that bulk head that’s in front of the galley. Um… [Mishap Tactical Coordinator] [Investigating Officer] : So I can see… : You can kind of… [Mishap Tactical Coordinator] : So if, if you’re, were stacking on top of each other, microwave on top of the fridge, I can see fire curling up like this. Just on the aircraft itself. Just up. Up and over. [Investigating Officer] : The fuselage, OK. [Mishap Tactical Coordinator] : Yep, up and over the microwave. And I can see white smoke billowing and coming forward. [Investigating Officer] : Yes sir, OK. Uh [Mishap Tactical Coordinator] : And it was big enough flames I could see them from. They were, you know, yellowish orange flames, you know typical fire color. [Investigating Officer] : OK. Um, and then what else? [Mishap Tactical Coordinator] OK, so, you know fire fire fire, I see it at the same time pilots are pulling it back to stop because we are short of S1, um, to stop on the runway. I go on oxygen, um my two ravens go on oxygen and then once we get to a stop we start the egress out the front so everybody is going straight out to the front. Uh, Raven 1 grabs, or um I’m sorry, Captain [Mishap Raven 1] Nav 2 comes back grabs the chocks and the ladder gives them to the Navigator, they put them down and they start the egress. [Investigating Officer] [Mishap Tactical Coordinator] : OK : At that point. R-83 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] : Did, um, sorry to interrupt if you had more… : Go for it. : OK, um, was there any command to go on oxygen or was everybody sort of just doing it. [Mishap Tactical Coordinator] [Investigating Officer] : Its, its part of our checklist. : Standard. [Mishap Tactical Coordinator] : If there’s a fire, I mean if, you guys have our checklist by the way but, um, first thing is 100% oxygen. [Investigating Officer] : OK. [Mishap Tactical Coordinator] : So were all…lots of folks are on oxygen. Uh, all my guys were because I was up there, up front, and I could see them. But, um, obviously folks while they’re egressing they’re not on oxygen but. [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] : Yes sir, um and then as far as the egress through the forward uh, hatch. : Crew entry chute. : Is that standard? [Mishap Tactical Coordinator] : Crew entry chute? Yes, egress is through the crew entry chute. Um, if it was an abandon it would be any, any door, hatch or whatever but. [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] [Mishap Tactical Coordinator] : Nobody, nobody went out another exit. : No. We did open the over wing hatch just to get some ventilation. : OK. : Because the smoke was getting pretty thick and it seemed to provide some relief. [Investigating Officer] : Gotcha um, from the time you came off oxygen and starting moving forward, was it sort of a log jam with like people kind of exposed to smoke and all that for, did it seem like… [Mishap Tactical Coordinator] [Investigating Officer] : There were some folks… It’s tough to tell time and… : Temporal distortion yeah. [Mishap Tactical Coordinator] : In that kind of situation. It seemed like a couple few minutes from the time we started egress until we finished but with 27 souls on board it takes a little bit of time to get down the ladder and um, out the front. But I was on oxygen until everybody was up to the, to the line, to the bulkhead, and then I came off and went down. I don’t know, maybe off oxygen for less than 30 seconds. [Investigating Officer] : OK. R-84 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Tactical Coordinator] [Investigating Officer] : But that’s not the case for the folks that were in the back. : Gotcha. [Mishap Tactical Coordinator] : Because unless they can get up out of their seat and go forward um, unless they are taking an EPOS with them, which nobody had. [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] [Mishap Tactical Coordinator] : They’ve got to wait. : Yeah. EPOSs everywhere, they just didn’t, they just left the aircraft. : OK. : So I would say it was a few minutes before um, we finished the entire egress. [Investigating Officer] OK um, the last question I have for you sir is um, we’re considering sort of uh, bringing a mission crew member on board with the SIB, to to help us with uh, sort of just the understand of what was going on in the back of the airplane. If you were going to make a recommendation for what type of crewmember we would do. [Mishap Tactical Coordinator] : OK, if you, if you want to know basically what everybody back here does um, an AMS is going to be who you’d want to talk to. Um, they’ll give you every, everybody that’s doing, they’ll know exactly what everybody’s doing, what they’re- what they’re supposed to be doing. Um, if you get an ASE, an A S E, that’s what I would also, um, recommend. They’re going to tell you what the four ASEs are doing and what, what their responsibilities were. [Investigating Officer] : OK uh, actually I had one more question sorry. Um, the galley, just out of curiosity, is it normal that the galley is powered on prior to takeoff or on ground ops? Who owns, who kind of owns that? [Mishap Tactical Coordinator] [Investigating Officer] : Like power? Like lights? : Like main galley power. [Mishap Tactical Coordinator] : It’s normal. We have, a lot of times we have, depending on the temperature, we’ll have our full systems up, or most of our systems up on the ground. [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] [Mishap Tactical Coordinator] : OK. : But my station was up, I was working on it when, when this all happened. : Got it sir. : So it’s not abnormal at all. [Investigating Officer] : OK, that’s all I got. [President] : Do you have um, I’ve got a question for ya [Mishap Tactical Coordinator] : Yes sir. R-85 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [President] : Kind of alluding to what his, who owns, who, who manages like the galley area back there. Is it, is it, you guys don’t have an engineer of you have, does the AMS, who, who like makes sure everything in the back is up and operating before, as part of preflight. [Mishap Tactical Coordinator] [President] : Uh, that would be the ASEs. : OK. [Mishap Tactical Coordinator] : And we have four of them, and two of them were actually in the back sitting in these, in these positions here. [President] : OK, um, another thing I know you’re, you’re far in the front of the aircraft. Um, did you ever smell anything before you heard fire? Did you notice anything? [Mishap Tactical Coordinator] [President] [Mishap Tactical Coordinator] [President] : I did not. No, I did not. I had no indication until I heard fire. : OK, and you said you just saw it curling over the top. : Correct. : Ok, um, alright I don’t have anything left. [Pilot Member] : Uh, sir I just have a couple questions that go all the way back to the brief the day before. Uh, and I’m not quite sure exactly what the standard duties are in the 343rd but uh, I’m curious as far as uh what the Nav briefs egress uh, did they know that uh, [MR1] would be sitting in NAV2 that day or is it just… [Mishap Tactical Coordinator] : They briefed it um, that, I believe they briefed that was going to sit AUX and NAV2 was going to be [MR1] because the discussion was what about the jump seat. Um, and and the discussion was well the, this particular pilot team doesn’t particularly care for folks sitting in the jump so they prefer to sit NAV2 and AUX, so that’s where two of our three extra Ravens sat. [Pilot Member] [Mishap Tactical Coordinator] [Pilot Member] : Alright, cool, so they were brought in, they were brought in on the : That was during our normal crew brief. : Right, that discussion of where they are going to sit. [Mishap Tactical Coordinator] : Typically the Raven 1, this position, will give the, will get the chocks and the, and the ladder but [MR1] was closer so he… [Pilot Member] [Mishap Tactical Coordinator] [Pilot Member] : [MR1] was there? : Yeah : Awesome. Uh, what is uh, a last man out identified out in the crew brief the day prior. [Mishap Tactical Coordinator] : It is. It was part of the briefing. As the TC, I’m the jumpmaster in the back in the event of an egress so I wait on the AMS to tap me on the shoulder in which case I saw him walk R-86 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 by, asked him like four times are you the last man, it was confirmed. And then I told the pilot I’m the last man, and then we egressed, and then counted souls. [Pilot Member] [Mishap Tactical Coordinator] [Pilot Member] : Alright, so the pilot was still there when… : Correct. : …you went down and… [Mishap Tactical Coordinator] : That’s, and that’s part of the briefing is um, I, when I do the briefing, its um, I’m the jumpmaster in back and in case of an emergency in the event of an egre, egress (inaudible) an AMS tap me on the shoulder letting me know he’s the last one out of the recon compartment and then I’ll tap the AC and let him know that I’m the last man and then he follows me down, which is exactly what we did. [Pilot Member] : Perfect, good. [Investigating Officer] : Um, anybody got any other questions? [President] : I have one after you’re done, so go ahead. [Medical Member] : Um, have you ever experienced a fire or any other similar types of situation on this aircraft? [Mishap Tactical Coordinator] : It’s not uncommon to get smoke and fumes. Um, it’s the first time I’ve seen a fire in an electrical system in 15 years I’ve been flying it. [Medical Member] : OK [Mishap Tactical Coordinator] : But it’s really not uncommon to do smoke and fumes throughout and then I don’t know, it’s pretty, I would say fairly common. If I’m going to see an EP on the plane, its going to be smoke and fumes. [Medical Member] [Mishap Tactical Coordinator] [Medical Member] [Mishap Tactical Coordinator] : OK : But they don’t typically lead to fires based on my experience. : Alright, did this look like a typical fire, or was there anything weird? : Well I’ve never seen a typical RJ fire. This is typical to me now cause this is the only one. [Medical Member] : Well how about, like is it, does it look like a typical burning fire that uh, you know… [Mishap Tactical Coordinator] : Yes. Yeah, it didn’t strike me as anything, it didn’t look a different color. The only thing that maybe struck me as a little odd was the smoke was all white. [Medical Member] : OK R-87 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Tactical Coordinator] : Typically, I don’t know, I would associate a little different darker colored smoke with a fire, but it was all white. [Medical Member] : OK [Mishap Tactical Coordinator] [Medical Member] : White, kind of grayish white. : Thank you. [Investigating Officer] : And then, I’m sorry, after you egressed the airplane I would imagine you had a moment to kind of look at the airplane before the fire department got there and started hosing it down. [Mishap Tactical Coordinator] [Investigating Officer] : Yes. : Uh, what did you observe from the outside. [Mishap Tactical Coordinator] : OK, so after we all lined up in the grass and did our headcount um, you could clearly see um, the aircraft you could see um, I’m not, I’m not sure right away but I know at some point while we were waiting you could see um, flames coming up out of the fuselage. And, and white smoke coming up. [Investigating Officer] : OK [Mishap Tactical Coordinator] : As well. It was just aft an on the side of the WGS dome. With the dome on top of the aircraft. (Inaudible) [AFEM] : Um, sir in your statement you identified that you donned your um, quick don mask. [Mishap Tactical Coordinator] : Yes [AFEM] : Prior to, or once you noticed that there was a fire. Did you have any trouble getting it on, or? [Mishap Tactical Coordinator] : Nope, it’s right by my, my knee. Just pull it up, put it on. It’s preflighted and ready to go. Oxygen was already on per the checklist, so it was just put it on as soon as you open it activates oxygen flow and it was, it was good to go. [AFEM] [Mishap Tactical Coordinator] : Um, do you recall um, your last LL06 AFE training when you… : Is that the, which one is LL06? [AFEM] : That’s the just, Aircrew Flight Equipment training, it’s an annual event. [Mishap Tactical Coordinator] : Um, I think I did it in the last two months cause I just rehacked almost everything for my… [Investigating Officer] : Prior to departure R-88 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [AFEM] [Mishap Tactical Coordinator] : So just these last couple of months : Yeah. [AFEM] : OK, so we would just need to probably try to, did you get a 1522 from the AFE guys I assume [Mishap Tactical Coordinator] : Yes [AFEM] [Mishap Tactical Coordinator] [Investigating Officer] : To take back from, to your squadron? : Yes : We’ll run that down. [AFEM] [Mishap Tactical Coordinator] : Yeah we’ll just have to run it down so. It just wasn’t in your record sir. : Well if you pull a, an ARMS pull I’m sure it will show all the dates. [AFEM] : Yeah the, the last, the one that’s in there now, the ITS has uh, like a April 13 date for the last… [Mishap Tactical Coordinator] : Is LL06 a one year one? [AFEM] [Mishap Tactical Coordinator] [Investigating Officer] : Well that’s not right. Are you sure you pulled me? Cause theres more than one . So… : Imagine that. [Mishap Tactical Coordinator] [Investigating Officer] : Yes sir. : I get his emails, he gets mine. : Copy, did you have any other… [AFEM] : No sir, that’s all I have, thank you. [Maintenance Member] : I do have a question. Did you notice anything different about the operation of the LOX system? [Mishap Tactical Coordinator] : No, our preflight was normal. The gauges were all normal, everything was functioning normally, but I didn’t check the, I mean I didn’t check the amount that we had um, after or during the, the incident so. [President] : Anything else? [Maintenance Member] [President] : No sir. : Did um, did maintenance, I know there was an engine problem early on you mentioned. [Mishap Tactical Coordinator] : Correct R-89 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [President] [Mishap Tactical Coordinator] : Um, did maintenance come on board at all? Did they come in the aft area? : They did, um so, before we pinned it, they came up and they just stayed in the flight deck [President] : OK [Mishap Tactical Coordinator] : And you know, they tried, we tried to start to start it the normal way um, a couple more times. Didn’t work. And then decided to go… [President] [Mishap Tactical Coordinator] : But no actions in the aft part of the aircraft : Correct Correct [President] : Alright. Did you notice anybody, uh, doing any firefighting activities or attempting to do firefighting activities? [Mishap Tactical Coordinator] [MR2] : Um, I did not personally see it and I know we had some discussions. Uh, , is uh one of the Ravens who was sitting in the back because we didn’t have enough seats up front, and he discussed how he tried to reach for the bottle but he had his oxygen mask on and couldn’t actually get it. But, by the time, I mean we stopped and everybody got out so, it, nobody else that I know of had made any attempt to do it. [President] : OK, is there um, is there any procedure that you’re aware of ah, that you would shut off oxygen, or that anybody would shut off oxygen as part of an egress or an emergency? [Mishap Tactical Coordinator] [President] [Mishap Tactical Coordinator] [President] : No, not that I’m aware of. : Nothing? : No : OK, um, do you even… [Mishap Tactical Coordinator] Fire. Our checklist says oxygen on 100% so we would, wouldn’t even cross our mind, at least not mine to turn off our oxygen. [President] [Mishap Tactical Coordinator] [President] : Do you know where oxygen shutoff valves are? : I don’t. No. : OK [Mishap Tactical Coordinator] : I understand there’s probably, well I do know that there’s some, there’s one I believe the shutoff switch in the hell hole because I was around when the fire marshal and maintenance were talking about going in there and shutting it off because maybe that was fueling the fire but that’s all conjecture as far as… I’ve never seen it. [President] : OK R-90 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Investigating Officer] : Sir, you mentioned you had some discussions with the crew probably afterwards. Um, did, did you, did anybody ever seem to have a more detailed description of that fire? That, you know if you were going to direct us at somebody else to interview. [Mishap Tactical Coordinator] : Uh, well definitely [MR2] [Investigating Officer] : OK [President] : Was he the closest one to the fire? [Mishap Tactical Coordinator] : Um, he sits, I would, if he was sitting in row four… [Pilot Member] : Row four outboard so, he was physically the closest one to the fire. [Mishap Tactical Coordinator] : Yes, [MR2] would be one. I would also say Chief [MSSD] . Um, cause he’s sitting right across in one of the QRC seats, OP 16. Right here. So he’s got, although he’s, he’s got his back to it, but I’m sure he was turned around and stuff as soon as he saw the smoke and fire. [President] : And they are all facing aft? Normally? [Mishap Tactical Coordinator] : These seats all face aft. Um, these two seats, they face this way normally but I think for takeoff they turn them and face them aft as well. So, these guys probably have good, good view. This one does. [President] : OK [Mishap Tactical Coordinator] : Anybody in these, these seats here would have direct view of it because they are all facing aft. [President] : OK. Any other specific questions to the incident anyone can think of? Chief? [AFSEC Rep] : No sir. [Investigating Officer] Any reason to believe that anybody was out of their seat messing with any electrical equipment back there? [Mishap Tactical Coordinator] : No. As part of our um, as part of our checklist it’s um, if I had my checklist I could show you but, there’s a step in there where I, where I call back on private and I ask, um the, the AMS, or I ask everybody on private you know for, for um, ready for takeoff. And then they all report to the AMS, AMS reports to me, Ready for takeoff so… [Investigating Officer] : OK, OK. [Mishap Tactical Coordinator] : That call is made, that their ready for takeoff when everybody is seated. And then I get, I go up to the pilots and let them know we’re ready for takeoff. [President] : OK [Investigating Officer] : You good with that sir? R-91 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [President] : I’m good. Only, only, after we’re done with that I would like to, if you could just run us through, um, from the, pretty much from the pilots back what you understand about the crew positions and what they are in general terms because not everybody is an RJ, ah, type here. [Mishap Tactical Coordinator] [President] [Mishap Tactical Coordinator] : OK : At the un-class level. : OK [President] : When you’re ready. [Investigating Officer] : You want to make that part of the ah… [President] : Yes. [Investigating Officer] : OK [President] : Yep, go ahead. [Investigating Officer] : OK sir. So, so if, just a, for a layman who’s looking at this airplane. [Mishap Tactical Coordinator] [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] : OK : Ah, in, in basic, ah, terms. : OK. You guys already have the front. : Yep. [Mishap Tactical Coordinator] : Pilot, Nav, Co-pilot. Um, normally the Nav 2 and AUX seats are, aren’t, they’re not used. You don’t need them, um, but we had extra EWOs because, um, Major was giving me a, my eval and [MR1] was instructing, um, Major who was getting requal’d. So, um, after the bulkhead you have Raven 1, Raven 2 and TC. These two guys have the same equipment. And they split duties but, um… [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] : They work for you? : They work for me. They handle all the ELINT um, : Threat warning stuff. [Mishap Tactical Coordinator] : So they’ll, they’ll collect whatever’s in the environment, put it on datalinks. Um, go out on voice and tell people what’s going on. Um, I manage them. I also manage um, a Rivet Joint off board communications. Um, the back end will do some of that as well but we just have, we have separate duties so… [Investigating Officer] : OK [Mishap Tactical Coordinator] : Uh, these two pieces here are two of our ACEs, our A S Es, Airborne Systems Engineers. They got, ah, 3 sits here and ASE 1 sits, sits there. Theres four ACEs, they all have R-92 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 different duties described in our, in our T.Os. But, um, these guys will sit here. Um, these are maintenance racks. OK. We got five, I’m sorry, yeah five, OP 5, OP2, um, and then the AMS. So your, um, 5 is going to be your DLO. He’s going to do your data link ops. Your OP 2 is your radio guy, so he’ll do, he’ll load the crypto and he’ll do the radios. Um, OP1 is AMS. He is the, um, Airborne Mission Supervisor. Um, he is in charge of all of the, um, ops in the back. [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] : OK. So these guys are kind of like a comm section? Right, like… : Data links and comms. : OK [Mishap Tactical Coordinator] : Um, AMS is going to be in charge of everybody in back. Um, as far as their collection, what they’re doing, focusing their collection, talking off board and, and QC-ing all their work. So he’s more like the TC equivalent, but for the ops. [Investigating Officer] : OK [Mishap Tactical Coordinator] : And the AMS and I will work together to put the jet in the right place, um, and, and manage the fight that way. OK, after them, you basically have got your, um, there’s an IIO in here somewhere. I don’t see him labeled. It was . OK, right next to the AMS. IIO, Information Integration Officer and they’ve got a bunch of different chat rooms. Internet relay chat. Um, so they’re discussing with off board part players what, what kind of stuff is going on. [Investigating Officer] : OK [Mishap Tactical Coordinator] : Um, after them you’ve got all the OPs, your, your linguists. Um, these are just crew rest seats. And here you got your QRCs and um, special sigs folks. So Quick Reaction Capabilities and Special Signals Development, SSDs. [Investigating Officer] : OK [Mishap Tactical Coordinator] : So, it’s just, special equipment. But they all, all these folks still work for, ah, the AMS. Um, the ASEs, um, they, well where we going, sitting over here but they can really sit pretty much wherever, over here. And between the four ASEs, they handle all the mission equipment for, um, both the EWOs and the, and the COMINT section. [Investigating Officer] [Mishap Tactical Coordinator] [President] : Yes sir. : So… : Keep them, keep the equipment up and operational. [Mishap Tactical Coordinator] They’ll bring it up and they’ll fix what they can in flight and they’ll try to, um, and they’ll, so they bring in, they bring in the software to start the mission. Um, and they bring everything up. They fix everything that we need, um, and then they, after the flight they’ll put them all back in the boxes, inventory all the classified and, and bring it back to the ISS for, um, briefs. R-93 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Investigating Officer] : OK. Do you want more than that sir? [President] : No, I think that’s good. I, I just have two kind of quick questions. Number one, you guys are obviously a SCIF once the doors are closed and everything is up, right? [Mishap Tactical Coordinator] : We’re supposed to be, I’m trying to think of when it, when it actually is considered a SCIF. I think if you talk to the security folks they’ll tell you as soon as your equipment is on board it’s a SCIF. Um, but… [Investigating Officer] : I think we’re driving to the same point. [President] : Yeah. [Investigating Officer] : CVR stuff. [President] : Yeah. [Mishap Tactical Coordinator] : The CVR is actually located up here. Um… [President] : Would you guys have, without going into it, would you guys have discussed classified. This is just for us, uh, would you have discussed classified, uh, at the Secret or higher level? Um, before you, before takeoff? [Mishap Tactical Coordinator] [President] [Mishap Tactical Coordinator] : Oh, yes. Yes sir. : On board. : Yes sir. [President] : OK [Investigating Officer] : So people are kind of pre planning what they are going to do and talking about the mission. [Mishap Tactical Coordinator] Of course. If there’s no maintainers back there, um, not, not our Airborne Systems Engineers, but no maintainers. [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] : OK Yeah, we’ll, we’ll discuss classified. : OK [Mishap Tactical Coordinator] : And um, matter of fact I mean, I believe there was a binder open on AMS station, or next to, or not open, but out, of Classified. So after the whole thing was, after we had egressed, after they had put out the fire, um, I had kept about six or seven folks back who knew where all the Classified was so we could go grab the Classified before they towed it and we never saw the jet again. So, so they were able to do the, the accountability of all the Classified. So there was never… [Investigating Officer] : Yeah, gotcha. R-94 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [President] [Mishap Tactical Coordinator] : OK : Any loss of data that way. [President] : And I have kind of one other question. Do you guys do any comms checks on the radio on the ground [Mishap Tactical Coordinator] : We do. We do sir. I do a U9 check over a couple of different frequencies. I check back in with, um, HOOVR ops. And as, and as we do a secure check as well. So, we did that. We did it with the OP2 prior to the sortie. [President] [Mishap Tactical Coordinator] [President] : What radio do you use for that? : I use, it’s ah UHF9. It’s a little radio panel I have to the right of my station. : OK [Mishap Tactical Coordinator] : But the, the um, OP2 plugs in the freqs and loads all the crypto and we do our, we do our radio checks, secure and unsecure checks, on the ground. [Investigating Officer] [Mishap Tactical Coordinator] [Investigating Officer] : Do you guys use UHF3 at all? : We do U3, 5, uh, U3, 5, 9, we have tons of radios. : Who uses 3? Do you, or… [Mishap Tactical Coordinator] : Well so they, they um OP2s going to load all the radios and all the frequencies and then all the jet can use, can plug into whatever radio they want. Our intercom panel is, um, pretty nice that way. I can plug into whatever radio I want to use. But the frequencies are already programmed for me [President] : OK [Investigating Officer] : And from a CRM standpoint, as far as the egress was concerned, did, did you feel like it was fairly standard and orderly? Or, um, you know were people kind of confused with what to do. [Mishap Tactical Coordinator] : No. I actually thought it went very well. Everybody, there wasn’t, I mean you see fire, you see billowing smoke, you’d think the panic would set in, but I didn’t see that at all. And I’m looking at everybody’s face coming forward. They all seemed OK, were getting off the jet. [Investigating Officer] : Just, just another day. [Mishap Tactical Coordinator] : Its business as usual. I mean, there was a sense of urgency, but there wasn’t a, um my life more important that yours, I’m going to push you out of the way to get off the jet type of mentality. I didn’t see that at all. [Investigating Officer] [Mishap Tactical Coordinator] : OK. : It seemed very orderly and… and controlled. R-95 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [President] : Alright. Anybody else have any questions? Chief? [Investigating Officer] : OK we can knock it off. Right, so uh, if no one has any further questions we’ll conclude, we’ll conclude this interview now. Anything else you’d like to add sir? OK. So, I’d like to remind you again that you were not offered a promise of confidentiality, and that your statement is NOT protected and will be released upon any follow-on investigation of this mishap, like at the AIB or anything like that, and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony and any information shared with you today regarding this mishap to avoid the possible spread of incomplete or counter-productive information until we have adjourned the board. Notify the board immediately if you become aware of a possible release of information. And thanks for your time. [Mishap Tactical Coordinator] : OK R-96 V, 64-14848, Class A, 30 April 15, AFSAS #739726 R6. SRA ?me We? WW ?1 (MASE 1) R6.l. ISB NON-PRIVILEGED WITNESS STATEMENT 30 APR 15 Page 1 of2 Non-Privileged Witness Statement 7*0 (Date) 1 I. have been advised by (Name. Grade. Organization. of Witness) (Name of Investigator) a safety investigator of the mishap that occurred on "Sc 1X55- [5 involving c? d. 1 57% "3 (Date) (Equipment SN) a This investigation is being conducted under the provisions of AH 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand 1 am being interviewed as a witness in a safety investigation and! acknowledge that a promise of con?dentiality has NOT been extended to me ha. My witness statements written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request Name (Last, First, MI) and Rank/Grade Duty Title, 1 R-97 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Page 1 of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of AFI 91-204 301er for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand lam being interviewed as a witness in a safety investigation and acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. WITNESS STATEMENT OF: Name (Last, ?First, MD and Rank/Grade [Reference attached document for witness account of event. This document is being entered for accounting purposes andfor witness ?s acknowledgement of this being theform they should have received for of a written statement. The member ?3 chain of command will only review the ?nal mishap report If acquired through appropriate safety channels 91-204 para 3. 4. R-98 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 STATEMENT Date of thc? mishap rail '5 L) . Crew position (as applicable} 32 . Tim: you began duty MASE1 . . lit-Li. gig have been adwsedby of the following: ?mn WI Oriana-um humilplar a. This investigation is being conducted under the provisions of 9] -2l)4 solely for the purpose at" mishap prevention within the. United States AirForce and to detenninc all faclom relating to the. mishap in order to prevent mutirrence? understand I am being interviewed as a witness in a mishap invtigation and I acknowledge that a promise ofcon?dcnliality has notbce? I, 1, extended to me. This witness statement may be released In the: public pursuant to a Infun?natinn Act rnquesll c. 11}: chain ofcommand will review the final mishap report. Provide an account of ?rst-hand observations of what happened, description of prevailing cunditimts, circumstances. and associated event-5 (use raverse for continuation). Gum") l't?i'W. riggh?: at? NIL Wk bm?l?st 1.. MM ct Call Mr? tint ,thleml? (WELL Raw-:1 NW1- She?d? lnM?La?ex (timiwicm?c. will" :3 MM an Bio Ntmiq? was A) ?if 1C Hie. Plant 1.1 m?l- ii? O?qcaul'. ?will? PW. ?x Wits Gun-Tm.) [gt-t wharf.th 5% Hi [1:56.15 Eel?mmj (in. mid.sz mu Mimi LL lilbw ?ii?wlR. lc?i?mi M3 Lilian-n ain't mt Bally! whale-L allot-? with bill!? flit??1 Elihu"! Emmi ll? 34' ?"13 Wat It?? ism/lat thristlu hibiwhhmi! Kmart? ?if. Emu its"? um? Tim $154th in Bil-u. think tit?) QM. ?hi: lulu-?9 aam?mj lighter} imii? gluesffil-zn ?i?titmL Hut. 50.? E34153. {mgr Iiwk?iLE?N.1 i?awa {I'll-i ankle. WLME laugh-c with limit End. 'l-cLAhlm. 3m at} ?at ?at-pig. haul cmi aid-Ha Maidad' Emmi? 3th CHM Earl-n1 Mm} amt-??3 M41, Nt'miv-? (M fiu Wrim 94km?; 'l?lNL biw. deC?l-E PM hi agmh?y are :1 all-M? HIP ?Si-t lT 5m [DirethrOfopera?ons] intuition-it m1 diam ?M's {twig (imam. lei-Max I ?mm [is ?inth pm {Lieu dill mhitiil tum'mSm. 4.1.: lure, i ilmitu hilt/ling 3th? qilt it vi" New Data?Ull?iLl?Ei ?The. alumna statement is true to the host of my knuwladge and belief." Sign: RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 inwj?cf gimmick. magma? ?64133 #9 731?, I Titan; but) HEW Ma} 1* Cali Wk wm??c Lat?ialdomn 1mg? ?195% ?Swimkj E?utrosna? re Vat-(sari {1:13(lbw Lind?3 . ?rm. i Wise. a??n?nmw??bw?ighig? aritht?z?g: '13 ??b?gl gg- 15 Q?rtw(:Ms 2 444g wtu'lift?k' mi}, u. 9ch . mail? 919w (mews? La?mwh?m_ I, . wed. Out Mm am. 2:?it Hiya? ?(139165mm? #1 J?m?s. an ms?me 25f Elli. with Gaul It?l?h Wm R0135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 R6.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY 30 APR 15 72 HOUR AND 7 DAY HISTORY This investigation is being conducted under the provisions or AFI 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence This form is being administered by an Investigator lrom the Interim Safety Board or Safety Investigation Board (SIB). The statement you provide Will either be privileged or non-privileged applicable AFI 91-204 guidelines, NON-PRIVILEGED I understand I am being intewiewed as a witness in a safety investigation and lacknowledge that a promise of con?dentiality has not been extended to me. My witness statements may be utiIIZed for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. This non-privileged 72 hour and 7 day histOry form will be placed in Tab when complete. PRIVILEGED I understand i am providing statement(s) for a safety investigation and I acknowledge that a promise oi confidentiality has been extended to the by In veeb?g?r?ng Of?cer or Board President This privileged 72 hour and 7 day history form will be placed in Tab When complete. This 72 hour and 7 day history form Is one of many tools the mishap investigator may use to help determine the cause of this mishap. Your participation is both critical and appreciated and may help prevent future mishaps. Please answer these questions to the best of your ability when you are not rushed or distracted Be as speci?c and detailed as possible. All answers address events prior to the mishap and recovery events today?s Date: m?p Statement Completed By: (print) ER (signature) [Medical Member] ise or SIB Investigator Administering This Form: (print) R-lOl 64-14848, Class A, 30 Apri115, AFSAS #739726 Acrosmce Medicine Flight HISTORY REPORT Please list the daily activities you did during the last 72 hours. Provide the times of the events as well as the activity in the chronological order. If you cannot remember the exact time of the event, provide the closest proximate time you can remember. DAY I (72 HOURS PAST) t; ?55 3 WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times d?dmyzu get up? When you woke up, how rested did you feel?) TIME ARRIVED AT WORK: C'7oo BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) (\an MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) Lg; it?d/Miler, hut rm LUNCH: (What time did you have lunch? List all food and consumed) AFTERNOON Ag HITIES: (List all the things you did, all food and drinks Consumed) Nick TIME DEPARTED WORK: 0 DINNER: (What time did you have dinner? List all f0 and drinks consumed) 213?? Meier j??mHs' EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) Mm Led H). TIME you WENT TO SLEEP: 1329c; ALCOHOL CONSUMPTION: (List all types, amount, and times consumed) fig/u MEDICATIONS: (List all medications take. prescription and over the counter, dose and time consumed) pct/K DAY 2 (48 HOURS NAME (LAST, R-102 V, 64-14848, Class A, 30 April 15, AFSAS #739726 7 UP TIME: (What lime $1530.. wake up? How many hmuI's did you sleep? How many times ?Iid you get up? When you woke up. how rested did you feel?) WORK: 3 C) BREAKFAST: {What time dida you have brcakfasl? List all food and drinks consumed) lyan Wink MORNING ACTIVITIES: (List. all the things you did, all food and drinks consumed) memo, sham news} LUNCH: (What time did you have lunch? List all food and drinks consumed) Ham Smimh New bait? AFTERNOON all the things you did, all food and drinks consumed) PWIlman?a?. w? I TIME DEPARTEI) WORK: [6 3 C) (What lime did v_ou have dinner? List all food and drinks consumed) MED 59kg EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) (:wm 3mm No Lou-Vim cak Mb, TIME YOU WENT TO SLEEP: 27,082 CONSUMPTION: (List all types. amount, and times consumed) if? (List all medications take. prescription and over the counter, dose and lime consumed) NAME (LAST. FIRST): R-103 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 4 995.0 ?3 IV) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many tim?did you get up? When you woke up, how rested did you feel?) we,? Mu raged m. co BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) A MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) 0.2mm Mm . no A LUNCH: (What time did you have lunch? List all food and drinks consumed) 'nm 5min :Jm) Mow He? AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) Mass!? piano? ?(gm 1 ctr-2 DINNER: (What timc did you have dinner? List all food and drinks consumed) ?5pugiuH-i' {Ll}th EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) Md 7 dimer of wen/lei TIME you WENT TO SLEEP: gimd. up 93 L46 3mm 3 ALCOHOL CONSUMPTION: (List all types. amount. und times consumed) 'Yl?Mt. (List all medications take, prescription and over the counter, dose and time consumed) A on; NAME (LAST. .55? N: R-104 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 4 (TODAY) 1300 N: WAKE UP TIME: (What time did you wake up? How many did you sleep? How many times digl you get up? When you woke up. how rested did you feel?) ?hVQIQanv-s ?Lu ct TIME ARRIVED AT WORK: 5? l?i BREAKFAST: (Whit time did you have breakfast? List all foodgnd drin consumed) )Mlv. th?cl??n W?i? S?mw?benq ?We MORNING ACTIVITIES: (Listsall the things you did, all food and drinks consumed) lee LUNCH: (What time did you have lunch? List all food and drinks consumed) ?ll MOM AFTERNOON ACTIVITIES: (Llst all the things you did, all food and drinks consumed) ?bde 8: load WORK: DINNER: (What time did you have dinner? List all food and drinks consumed) Nu A. I pr EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) ULBHQ A I?Mg?k Misha?) u. TIME YOU WENT TO SLEEP: ALCOHOL CONSUMPTION: (List all types, amount. and times consumed) 910M Not MEDICATIONS: (List all medications take, prescription and over the counter, dose and time consumed) A) ARRIVAL TIME AT SQUADRON (If different than above): BRIEF TIME: (F) 3 0 5112? TIME: TAKE OFF TIME: TIME: 1'3 L?s NAME (LAST. . _ssAN;__ R-105 V, 64-14848, Class A, 30 April 15, AFSAS #739726 23 JULY 2001 257 7 KDAY HISTORY FOR AERIAL VEHICLE MISHAPIPHYSIOLOGICAL INCIDENT 7 The 14? day lustory la less detailed than the 72-hour history. Please note any signi?cant life events that have aimed ?it-3 past two weelm (example salaried forpromotion, death in family, Work, FLYING, mam'agc dllIi- ty, metal dt?iculty, vacation/leave, illness, eta). Include Ca?eine, Mods. Alcohol and Tobacco. exercise and FULL NAME I RANK Qll? Mishap day: Dale ?59 l5 1 day prior to mishap: Date Z?lkc {We ?30 NS 2 days prior to mishap: Dual?) 3 0 Ms leiJ? SWAP 3 days prior to mishnp: Date 25' {1mg (35 Slam? 4 days prior to mishap: Datum." 5 days prior to mishap: Baum nma 6 Aer Maw-?5 023mm Eqbt?m L4. (MM 7 w) 7day5pdorton1ishap:Datc 1} . /bna BM: R-106 64-14848, Class A, 30 April 15, AFSAS #739726 R6.3. SIB INTERVIEW 11 MAY 15 Page 1 of 2 Non-Privileged Witness Statement Mints; (Date) I have been advised by EH3 Emil?- Wanna, Grade, Organization, of Witness) (Name of Investigator) a safety investigator of the mishap that occurred on Sl?? involving g; '{Jn'fg 5; 572 (Date) (Equipment SM 3. This investigation is being conducted under the provisions of 91 -204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I underde am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. 94 Name (List, First. MI) and Rank/Grade R-107 V, 64-14848, Class A, 30 April 15, AFSAS #739726 74. Aircraft Diagrams VI 00-59mm i, a - - - - STATEN =15 d_ {wk/\ng U'r' GALLEY uvaronv R-108 ADDITIONAL anew men 1?012 ?s eff/l 1-19 Mar/5' 64-14848, Class A, 30 April 15, AFSAS #739726 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of SrA Role: [MASE1] Airborne Systems Engineer 3 343rd Reconnaissance Squadron Interviewers: (President) (Pilot Member) Date: 11 May 15 [Pilot Member] [MASE1] : This is a non-privilege interview with being conducted on 11 [Pilot Member] May 2015 by for the safety investigation board convened for the recent mishap. We’re investigating this mishap involving a RC-135V tail 64848 that occurred on 30 April 2015. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent reoccurrence. A promise of confidentiality is not being extended to you. Your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information act request. Do you understand that a promise of confidential- confidentiality has not been extended to you? [MASE1] : Yes sir. [Pilot Member] : For the record, would everyone present introduce yourself by stating your name, rank, and affiliation with the board starting with the witness. [MASE1] [President] : Uhm, the witness Senior Airman : Ah [Pilot Member] : Captain [Pilot Member] [MASE1] [MASE1] . , board president. , pilot member. : How are you doing today? : Alright, Sir. [Pilot Member] : Good (chuckles). Say, uh if you could, just start with uh the events that happened as you saw them. [MASE1] : Okay. Uhm, so we had just released brakes, uhm, we were at the top of the runway and we were about to take off, at least we thought. Uhm, and maybe a few seconds after we had actually released, I want to say we...I don’t, I don’t actually remember exactly the speeds ‘cause I have the NDD monitor uhm right there but it was literally maybe three or four seconds uhm down the runway and I heard someone say ‘Fire, fire, fire’ over call. Uhm, and after one person said it, then there was a lot of noise, uhm, over the uhm, the interphone system a lot of people calling ‘Fire, fire, fire’ and saying ‘get on oxygen’ all of those things. Uhm, and I was sitting at position 14 which is the left portion of the maintenance station right there. So I’ll just mark that on the piece of paper right there. [President] : Put a line out here so we can… there ya go. R-110 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE1] : Thank you. Uhm, so I was sitting at position 14, I have the ability even though the process of records was right behind me, to turn around uhm and kind of look back there uh to see what was going on. I- at the point that I heard ‘Fire, fire, fire’ I didn’t hear where it was. That wasn’t said initially. Uhm, so I kind of began looking around to make sure that it wasn’t like right in front of me, right in the raven compartment. And when I realized that it wasn’t, as I was looking up towards the flight deck and didn’t see anything, then I heard somebody say ‘At the galley’ uhm over some net, I don’t know exactly which one. And so when I turned around uh by this time the- the plane is slowing at this point uhm hadn’t come to a complete stop yet, so I was still in my seat. Uhm, and I had turned around and I looked and I saw maybe, honestly it- it’s hard to describe other than like a blowtorch, like flame- thrower style uhm fire flame uhm and it was sort of shooting out- it was about arm’s length and it appeared to be coming uh from the top of the galley area and honestly it looked like it was coming from uhm [Pilot Member] : Can you draw it out? [MASE1] : Yeah. Sort of, uh if I’m sitting, probably somewhere- right here. I don’t know if you can that so it was just coming, uh, [President] : Straight across towards the lavatory? [MASE1] : Yes. Like, just blowing out just like that. And it could have been higher, uhm higher up, I mean this is a general area obviously. It could have been higher up uhm but that’s where it appeared for me. [Pilot Member] : And you’re about halfway down the aircraft, so... [MASE1] : Right; uhm and at this point obviously everybody is seated because we’re about to takeoff. So everything is clear so I have like a direct line of vision from where I’m sitting to this flame that’s shooting out, ya know bright orange and red uhm and it was… yeah about- it looked about an arm’s length, ya know from my shoulder to my fingertips shooting out from the galley across to the uhm lavatory. Uhm… so at that point I felt the- the sort of final jerk of uhm pulling to a complete stop. I got out uhm and I was also getting oxygen on uh to make sure that I wasn’t ya know getting any kind of smoke, uh having any kind of smoke issues. And I was, at this point there aren’t- there wasn’t any smoke. I could still see the flames, but there wasn’t any smoke at all. Like, it was just the flame shooting out. Uhm, and so I was listening in and I told the ACE1, which was A1C, Airman First Class, , uh to get on interphone and kind of be the one relay as our training, ya know for our training goes. Uhm, and I was turning off all the fans to make sure that any smoke or anything feeding that wasn’t blowing around back there so I turned off all of my fans uhm which are located right here. Uhm, [President] : Right on the console next to you? [MASE1] : Right on the console, yes. Uh it’s a fan control…panel. Uhm, so I turned off all of those. And then, and this is also while I’m still on oxygen and I’m listening uh to see uh what those guys are doing back there if I need to go back there and- and help them uhm, per our [MASE3] training. So I see uhm and [MASE2] get up and they’re starting to get the firefighters masks and get those different things on. Uhm, and they were kind of sitting in their seats sort of itching and waiting to get up to fight the flame uhm or fight the fire uh until the jet R-111 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 got to a complete stop. So when it stopped I was getting up and doing all of that while they were grabbing for the firefighters mask, and that’s when I begin to see the white smoke start to come. I don’t know if it was uhm something just finally caught on fire as opposed to blowing out the flames from whatever. But, I begin to see the uh the just white-greyish smoke and it....within seconds it filled that entire area. Uhm, and this is all happening very very fast obviously. Uhm, so I’m waiting and I’m contemplating unhooking my oxygen uhm so that I can hook up to a bottle and run back there and help them and at this point I’m still thinking uh firefighter, sort of as opposed to a ground emergency. Uhm, and at that point where I was reaching for the cord I remember hearing someone say over interphone ‘Egress’; I believe it was the pilot say ‘Egress’. So when he said ‘Egress’ I tapped uhm the ACE1 on the shoulder, told him to get out of the jet. I unhooked, took everything off uhm and I took one last look. I remember taking one last look at the aft and at that point everything back there was full of white smoke. So you couldn’t- I could barely make out the orange-ness of the flames still shooting out, but it was still [MASE2] shooting. Uhm, and I could barely see uhm…uhm… I believe it was getting thethe mask on and all of that stuff. He was still like fiddling with it and I could barely like see their outlines, but it was pretty much like a-a grey wall of not even like fog but it was like big puffy white smoke…just grey wall, you couldn’t see anything after probably position 12; this is where my line of vision kind of stopped…right here. Uhm so I’ll put there ‘No longer visible’. But Ieverything back there was just completely whited-out. Uhm, so I turned uh back to head towards the crew-entry shoot uhm and at this point, ya know the- the other ravens and the-the NAVs were waving at us like ‘come on, let’s go’. So I actually ended up being the first one off of the jet uhm so I got down there, kind of more slid than stepped, down the uh (laughs) ladder and then hightailed it uh 45 degrees off the pilots’ side of the aircraft. Uhm, the first person I remember seeing after me- and this is maybe after uhm a good… 50 to 100 feet away from the aircraft ‘cause I was moving pretty fast (chuckles). Uhm the first person I saw after me was uhm the 343rd DO uh Major . And he- we got on the grass. He directed me to get over on the grass. And after that I started to see more people, and I thought it would be more people like streamlining right after me, but there was a serious pause between me and Major and then another serious pause between him and the next person before they started flooding off regularly. Uh and eventually we got over there. Uhm, we kind of sat and watched while the plane was just burning really, uh there- nobody was- the responding vehicles weren’t out there immediately. Uhm, so we were sitting there just kind of waiting; it wasn’t a-a long-very long time… I don’t remember exactly how much time passed before they got out there. Uhm, but we all- we accounted for everybody; we lined up in two lines like the NAV, [Mishap Navigator] , instructed us to. Uh he got a good headcount and we were just kind of talking making sure everybody was okay- making sure nobody was like wheezing or about to collapse from smoke inhalation or all that stuff. Uhm, ya know and some people were obviously red from either the sweat or the heat or the smoke; and then the responding vehicles got there and we just kind of sat and watched while everything unfolded. They hosed the jet God knows how many times. Uhm, I remember seeing uh the smoke coming from the tail. Uhm and then[President] : From the tail from where it was like burning through, or? [MASE1] : Yes, from the tail where it was burning through. Uhm, and I remember seeing the flames burn through the top. And that was before the uhm firefighters actually went over there and did, uhm whatever they were doing. Uhm, I don’t know what actually they did once they put R-112 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 a ladder at the top of the thing; if they were just spraying it, or whatever they were doing. But, I remember the flames just kind of breaking through and at that point it wasn’t grey smoke anymore, it was black. So, Uhm… and we just kind of sat there uhm and that’s pretty much- I mean do you want me to continue on to everything else that happened after that fact? [President] [MASE1] [President] [MASE1] : No, I think we’ve got that piece. : Okay. : Uh…okay so you told us where you thought it was coming from. : Mhm. [President] : Uhm, uhh you told us where you were sitting. I’m- so I have a question uh on one of the written things you mentioned; was the ECP temperature. Can you kind of describe that to us a little bit more? [MASE1] : Right, so right here at my console uhm 14....I’ll put a thing right here… we have uhm the upper and lower monitor....so the upper monitor.... uhm typically what I would do on-on a day like yesterday- or not yesterday, on a day like that day uhm it was super-hot, uhm and we had a late takeoff so the sun was just kind of out had been ya know- the jet just kind of baking. What usually happens is the jet will usually get heat-soaked, and so we have to end up coldsoaking it uh; when we arrived at the jet that particular day they had air hooked up like usual standard, but it wasn’t…cold. It was blowing out like lukewarm, basically ambient air. Uhm, I talked to the ground maintainers and they got it to blow out some cold air, but it was fairly late in the game so the jet wasn’t as cold as I would have personally would have liked it being the ACE3 Uhm, and uh I guess the expert on the cooling system. So what we made a point of doing uh was if-if it’s a situation like that, I usually won’t do it in the winter ‘cause it’s not a factor, but as it begins to warm up uh for takeoff, uhm and not just take off but basically after my pre-flight is finished, I’ll have ECP, which is our environmental control processor, uhm I’ll have that up on 2nd or the upper monitor and I’ll just kind of monitor temps to see if things are gonna be heating up or cooling down depending on delays and all of those other different types of things. Uh, so I will have that up to monitor the temperatures until we takeoff and get that uh left or right pack on and start to cool the system down. So what I noticed in that particular situation was… I mean though it was warm uhm there weren’t any extreme temperatures. The one thing I can say is there was a uh temperature reading of like 5200 degrees Fahrenheit, right; and that’s not abnormal for ECP…it’s not.... optimal obviously because it means it’s probably- it usually means it’s just a faulty sensor uhm because we don’t usually get it- temperatures of ya know in the thousands of degrees uhm and it wasn’t just in that one place, it was in multiple places. So, where as you would think.... okay if it-if it’s an actual situation then on an IMP.... that’s what we call it uhm I forget what it stands for, but it’s an I-M-P that’s what it’s called, an IMP. There’s.... I don’t know… more than 15- approximately 15 or more sensors on that IMP. And, on that particular IMP it will have sensors here, here, here, here, and here; and they will be reporting the temperature readings back to the processor. So, when we had that 5200 da-degree reading it was saying that it was 5200 degrees where I was sitting, which I knew for a fact was untrue. It also said it was- there were some places in the raven compartment and like maybe one or two other places like on the jet; none of which were back here uhm so, and then there were others that were completely blanked out. So, what I ended up having to do was I closed the EDIS program, that’s R-113 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 the environmental program that runs on the computer, uhm and re-opened it just to see if that would work[President] : Like a restart? [MASE1] : Yeah, just basically a reset. And it did. uhm the temperatures went back to their standard 85 degrees. Uhm, the highest temperature I saw, even at takeoff was about 87-88. And that’s based on these-these processors and then on my pack reading uh there is also a uhm the uh pack control panel is also right where I’m sitting- right on the panel- uh the highest reading I have for that was 90. And because of what my checklist says in terms of uh it not being advised not to operate equipment above 90 degrees ambient temperature, we held off on system power; which I am now very thankful of. Uhm, but we said okay, ya know I let the AMS and TC know hey we’re going to hold up on system power up because we’ve been sitting here.... I don’t think we delayed for anything, actually we did.... engine start, uhm so we had a longer engine start than normal, so I said hey we’re gonna wait on system power up until we get in the air and we get the pack because it’s super-hot. Uhm, but on....what I found strange was on ECP when I was looking in this area.... and I typically pay attention to the area across, sort of across and a little bit aft from the galley, right here. [President] : Okay. [MASE1] : It’s called the uhm aft right-hand rack...(writing)right-hand rack.... When I was looking there, I paid close attention to the back because those are 60 hertz converters back there and they heat up super quick. And if they heat up, that pretty much screws everything on the jet that takes 60 hertz, most of our processors and systems equipment takes 60 hertz. So, I paid special attention to this area, and this area was somewhere in the mid-to-high 80’s…degrees Fahrenheit. Uhm, so I didn’t notice anything hot back there, and of course ya know if I was looking back there- if there was anything hot I would- it would have caught my attention ya know if something was red across from the aft right-hand rack but I remember paying special attention to that because of how hot it was and[President] : did you physically go back there, or is it from the console? [MASE1] : No, just from- right just from the monitor; what I can see from my console. Uhm, and so yeah the- like I said the hottest temperatures back there were in the high 80’s- nothing alarming, nothing weird. So it was kind of weird that we would have that kind of situation, you know with the fire and everything and I wasn’t seeing anything. And I still had it up even when we had takeoff, I didn’t notice any- ya know red-blinking lights or anything else like that. Everything was green or yellow. Which usually means it’s in good issues or its- its starting to approach that warning area but it’s still, ya know maybe ten to fifteen degrees away from a critical limit. So... (sigh) yeah. [Pilot Member] [MASE1] [Pilot Member] : Okay. Uh I really just have one last question. : Yes sir. : At any point in time was the left over wing hatch opened? R-114 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE1] : It was, but I didn’t see it until after- It wasn’t open when I was there, when I was on the jet. [Pilot Member] : Okay. [MASE1] : Uhm, at the entire time that I’m sitting there uhm everybody was kind of sitting while we were handling the fire. At that point like I said, I was the first one off the jet… I didn’t notice that the left over wing was open until after I was on the grass, and then I noticed that... oh the left over wing is open, somebody must have pulled the hatchet. Uhm so that’s something that happened either while I was going- getting off the jet, or after I was off the jet and I didn’t actually see it happen. But, it was not open when I was on the jet. [President] : Okay. I just have one last question. Do you a uh oxygen pre-check before you takeoff[MASE1] : Yes- [President] : Do you remember-was there anything, any anomalies or anything? Do you remember the pressures or anything on there? [MASE1] : Nope, the pressure was right around uhm 325-350, like it’s supposed to be. Uhm I did my oxygen checks uhm and they were uneventful uh I mean everything checked fine, there wasn’t like any open flow issues or any mask issues or anything thing like that. For all intents and purposes everything was normal up until that... there weren’t any like weird indications or anything like that. [Pilot Member] [President] : I’m sorry, were you done sir? : Yep. [Pilot Member] : I lied, I did have one more question- Uh when you said you turned off the fans after you saw the fire, is that a procedure anywhere, or is that just an airmanship thing that you were doing? [MASE1] : It’s a little bit of both. Uhm I would have to look in my checklist for the emergency procedures. Uhm it’s typically something we do for smoke and fumes, though. It’s not really relative to the fire scenario. Uhm but we’re also trained ya know whatever you feel is best in that particular situation you can pull from a different EP checklist or EP procedure if you feel like it’s going to help in this one. So, it’s typically for smoke and fumes to help us locate the fumes we’ll turn that fans off so that if the- the fume is coming from somewhere here, it’s not being blown somewhere up here so that we can isolate it. Uhm, so I mean in the particular situation it’s not a matter of hunting for the smoke or fume source to see if something is on fire or where it is... we knew something was on fire. Uhm, but it’s just something I did so that the smoke wouldn’t blow around. Uhm and so that if, not to my knowledge there are no fans uhm that least that I can control in this galley area, none. But if it was something where ya know a fan was right here, or over here, and was feeding that[President] : Just after the- Are there any right after the galley, or- R-115 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE1] : Yes, there is a fan. I believe aft left hand rack fan, which is here... there is a fan there. So I wanted to make sure that in any situation, any scenario that there is nothing blowing air onto that flame. So, I just hit manual off on all of my, uhm on all of my little buttons up there to-to knock it out. [Pilot Member] [President] : Okay. Very good. That’s all I have, sir. : Okay, I’m good. [Pilot Member] [MASE1] : I’ll uh read this last statement. : Yes sir. [Pilot Member] : If no one has any further questions we will now conclude this interview. I would like to remind you again that you are not offered a promise of confidentiality and that your statement is not protected and it will be released to any follow-on investigation of this mishap, and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony with- and any information shared with you today regarding this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [MASE1] : Awesome. Thank you. R-116 V, 64?14848, Class A, 30 April 15, AFSAS #739726 R7. [Mishap Airborne Mission Supervisor] I 1? R7.1. ISB NON-PRIVILEGED WITNESS STATENIENT 30 APR 15 NON-PRIVILEGED WITNESS STATEMENT gamut (Datehave been advised by (Mime, Grade, organizalion, of Witness) (Name a safety investigator of the mishap that occurred on 752 involving i - (a (Date) (Equipment SN) a. This investigation is being conducted under the provisions of AFI 9 -204 solely for the purpose of mishap prevention within the United States Air Force and to detennine all factors relating to the mishap in order to prevent I understand I am being mtervicwcd as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. it. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Mix i? Name (?rst, Firs], M1) and Rank/Grade Hm at! hm" Till? Signature R-117 64-14848, Class A, 30 April 15, AFSAS #739726 Page 1 of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of AF I 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I underst I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) maybe used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. . WITNESS STATEMENT or: 5 Name (Last. First. MI) and Rank/Grade I Signature [Reference attached document for witness account of event. This document is being entered for accounting purposes and for witness ?s acknowledgement of this being the form they should have received for completion of a written statement. The member ?s chain of command will onIy review the ?nal mishap report if acquired through appropriate safety channels 14 W91-204 para R-118 RC-135 V, 64?14848, Class A, 30 April 15, AFSAS #739726 NON-PRIVILEGED WITNESS STATEMENT Date of the Crew position (as applicable) Time you began duty! 3 . l. I. i 310% have been advised by, of the following: ?un- Can a. This investigation is being conducted under the provisions ofAFl 91-204 eeler for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand [111 being interviewed as a witness in mishap investigation and I acknowledge that a promise of con?dentiality has not been attended to me. b. This witness statement may be released to the public pursuant to a Freedom of Information Act request a. The chatn of commit! will review the ?nal mishap report. Provide An account of ?rst-hand observations of what happened. description of preventing commons. circumstances. and associated events (use reverse for continuationRam} Mu (W up: j, dotRum Will/M mus-Q mm)? AM it nae/z MAJ Mime?will 5W9 4 l? arr A 30 Wt ext/Hm lo Kacey/Jar [05'MSWM it Maltala? min-M Gown/vi (mow-Mt} PS 5044,, 3 oh? thew)qu Lluwo ?Ml. FDA, Sim}, H4 an.) {aim NBC- V'llvl allin Av jib-bu kl?; 4v 3,0 mm.th slut he mg wt ?leQm/l {94?5""32 helm A (Mute Em A MW am, J: Law-l4? Awaits ?u ?(at [If/Midi), ?The above statement is true to the beSt of my knowledge and belief." Signed Date? R-119 64-14848, Class A, 30 April 15, AFSAS #739726 R7.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY 30 APR 15 72 HOUR AND 7 DAY HISTORY This investigation is being conducted under the provisions of AH 91?204 solely for the purpose oi mishap prevenbon within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence This iomi is being administered by an investigator lrom the Interim Safety Board or Satety investigation Board (SIB). The statement you provide will either be privileged or non-privileged applicable AFI 91-204 guidelines. NON-PRIVILEGED i understand I am being interviewed as a witness in a safety anestlgetion and i acknowledge that a promise of con?dentiality has not been extended to me. My witness statements may be utilized for any valid purpose and be released to any subsequent investigation or this mishap and may be released to the public pursuant to a Freedom of in?ammation Act request. This non-privileged 72 hour and 7 day history form Will be placed in Tab when complete. PRIVILEGED I understand i am providing statement(s) for a safety investigation and acknowledge that a promise of confidentiality has been extended to me by Investigating Other or Board President This privileged 72 hour and 7 day history form will be placed in Tab when complete. This 72 hour and 7 day history form is one of many tools the mishap investigator may use to help determine the cause of this mishap. Your participation is both critical and appreciated and may help prevent ruture mishaps. Please answer these questions to the best of your ability when you are not rushed or distracted. Be as speci?c and detailed as possible. All answers address events prior to the mishap and recovery events. Today?s Date: 3019?! ?if Statement Completed By: (print) I i (signature) [Medical Member] ise or SIB investigator Administering This Form: (print) _1 R-120 64-14848, Class A, 30 Apri115, AFSAS #739726 Aerospace Medicine Flight HISTORY REPORT Please list the daily activities you did during the last 72 hours. Provide the times of the events as well as the activity in the chronological order. If you cannot remember the exact time of the event, provide the closest proximate time you can remember. DAY ?72 HOURS PAST) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up, how rested did you feel?) 0300 TIME ARRIVED AT WORK: (37,20 (What time did you have breakfast? List all food and drinks consumed) 05W Ibwaloi ociwtsl /n2 (no; oi (cirq MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) (CHILI. We! LUNCH: (What time did you have lunch? List all food and drinks consumed) ?2u0 Mic! - bi Qetw AFTERNOON (List all the things you did, all food and drinks consumed) L) (A lei TIME DEPARTED WORK: DINNER: {What time did you have dinner? List all food and drinks consumed) ha} (fut-L Lieu i bni IL a! EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) 1 0( WI TIME you WENT TO SLEEP: 07330 ALCOHOL CONSUMPTION: (List all types,2tmount, and times consumed) 5% (List all medications take, prescription and over the counter, dose and time consumed) 7) 0M DAY 2 48 HOURS PAST [Medical Member] NAME (LAST. rmsr):_ ssm; R-121 V, 64-14848, Class A, 30 April 15, AFSAS #739726 WAKE UP (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up, how rested did you feel?) 0 7 TIME 5131035: (31* C00 BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) ?rsk// bit", UdHc// DZ (-4) (Ah MORNING ACTIVITIES: (List all the things you did, all food and 9333121 (I) W?wi 03? - INCH: (What time did you have lunch? List all food and drinks consumed) noow'oL data: ?t (I AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) OJ mint! TIME DEPARTED WORK: ?0?50 (What time did you have dinner? List all food and drinks consumed) die M1 ulwt ?to EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) To -1 m, Rwy, (M +051.)er a l?lfu 5?qu TIMI-L vou WENT TO SLEEP: 3,130 A LC OHOL CONSUMPTION: (List all types. amount, and times consumed) r? MEDICATIONS: (List all medications take, prescription and over the counter, dose and time consumed) [Medical Member] NAMF SEMN: R-122 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 3 (24 HOURS PAST) WAKE UP (What time did you wake up? How many hours did you sleep? How A- many times did you get up? When you woke up, how rested did you feel?) 05w /(ar (hi i TIME ARRIVED AT WORK: 09520 BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) oo?wtni MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) kit??- Pu- A l/vai?ha. g} (ta/7 pr; WM (What time did you have lunch? List all food and drinks consumed) [4 AELEBEQQE AQTIEI HES: (List all the things you did. all food and drinks consumed) ("ow-nook; wk. NM 155. TIME DEPARTED WORK: I 709 DINNER: (What timc did you have dinner? List all food drinks consu cd) 30 {Cmtk 0; ?Leaf EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) A L11 Lw (Nu (if! (241? 5 TIME YOU T0 SLEEP: 55%) (>600 ALCOHOL in all types. amount, and times consumed)M? i 1w.? (Pk er?r 0 5L9 \r'k (List all medications take, prescription and over the counter, dose and lime consumed) [Medical Member] MM (LAST, FIRST): SSAN: R-123 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 4 (TODAY) WAKE UP TIME: (What time did you wake up? How many hours did you~slee How many times did you get up? When you woke up. how rested did you feel?) 0 01/3 TIME ARRIVED AT WORK: 30 BREAKFAST: (What time did you have break ast? List all food and drinks consumed) ?bLqu? .2 (qus 0 [u MORNING ACTIVITIES: (List all the things you did. all food and drinks consumed) HSHJ mu, (What time did you have lunch? List all ?ood and drinks consumed) . mu, 0 Car in?ll-0 owl ?Jr at) AFTERNOON ACTIVITIES: (List all the things you did. all food and drinks mangled) {lad-1 fur yolk. had a 5mmth \cteJ OIL-L (D My TIME DEPARTED WORK: DINNER: (What time did youh?c dinner? List all food and drinks consumed) EVENING ACTIVITIES: (List all the things you did. all food drinks consumed) Ll 0" mung. a. You.? in?, o. (1105 6-th wiw??ut (Ml Crag)? TIME vou WENT TO SLEEP: if ALCOHOL CONSUMPTION: (List all types, amount. and times consumed) MEDICATIQNS: (List all medications take. prescription and over the counter, dose and time consumed) ARRIVAL TIME AT SQUADRON (If different than above): BRIEF TIME: 1530 M996LAKE OBFTIME: nu MISIIAPTIME: W) \r [MedicalMember] NAME (LAST. #55531, R-124 V, 64-14848, Class A, 30 April 15, AFSAS #739726 23 JULY 2001 257 7 DAY HISTORY FOR AERIAL VEHICLE INCIDENT 7 The 14 day lustory is less detailed than the 72-hour hismxy. Please note any signi?cant lira events that law oocuned ovgr past two weeks (enmple selected for promotion, death in family, work, FLYING. man-ingc dim- EMty, dif?culty, vacation/leave, illness, em). Include Caffeine, Mcds, Alcohol and Tobacco, unwise and cuts 8 cpl. [Medical Member] FULL RANKM ssm_ 3 as ldaypriortomishap:Date2p193( 2 daySp?ortomishap: N5 3daysp?ortomishapzDatc?L; ?1 3W 4dly59?orton?shapsz?_; '5kaqu ?57 v5 115 5L4 Ac} A 5W4 uh. 254%! vidw'wo? 'ow swL. mm "Mallow? 7dayspriortumishapzDatc . WI r. 6 days prior to mishap: Date R-125 RC-135V. 64-14848, Class A, 30 April 15, AFSAS #739726 R8. SRA [Mishap Operator] (MCO) R8.l. ISB NON-PRIVILEGED Wl INESS STATEMENT - 30 APR 15 Page 1 of2 Non-Privileged Witness Statement MLIS [Mishap Operator] 7 (pm) 1. 1, have been advised by (Name, Grade, Organization, of Witness) (Name of Investigator) a satay investigator of the mishap that occurred on lip; IS involving V, g, 4- ?1595 (Date) (Equipment ?1 SN) a This investigation is being conducted mder the provisions of AH 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. [Mishap Operator] I 174/3 4 Name (last, First, MD and Rank/Grade A CLA L0 Dutv 1mg Srgnature R?l26 64-14848, Class A, 30 April 15, AFSAS #739726 Page 1 of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation: is being conducted under the provisions of AH 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recun'ce. I understand I am being interviewed as a witness in a safety investigation and acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request [Mishap Operator] WITNESS STATEMENT 01?: 54 Name (Last, First, MD and Rank/Grade [Reference attached document for witness account of event. This document is being entered for accounting purposes and for witness ?s acknowledgement of this being the form they should have received for completion of a written statement. The member ?9 chain of command will only review the ?nal mishap report if acquired through appropriate safety channels 91-204 para 3. R-l27 64-14848, Class A, 30 April 15, AFSAS #739726 NON-PRIVILEGED WITNESS STATEMENT Date of themishap 30 i . Crew position (as applicable) lg a) . Time you Vegan duty . [Mishap 1 i. "0363?"! have been advised by ofthe following: Odo an. a n. This investigation is being conducted under the provisions of 91 204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. Innderstandl am being interviewed as a witness in a mishap investigation and I acknowledge that a promise of con?dentiality has not been extended to me. This witness statement may be released to the public pursuant to a Freedom oflnformation Act request. c. The chain of command will review the ?nal mishap report. Provide an account of ?rst-hand observations of what happened, a description of conditions, circumstances, and associated event: (use reverse for continuation). ad Dun?? ??e?re difCUf?J?iorJ OVQR i462. ch 0? PA Jyve/ W6 Demand NW Dowaa?ouJ'. 0N miter waej?i?f-?B?tfea victim at Bath not Bur gar ON 393? M3 Row 0X WNW mef Lame. UPON 57?an up Hang,\ Wot-l" wl?i'h 5+o?i+3 ngiNQ, KIAAB if i" be more wlilw 03 MM WVQ of 7Lth N03 \thihi 59K Nice 3; 50% ON tom-loo i9~ AFT wrik Cile \Ji?Qw 0F eumtfiixi"? AFT OF- TNiiUJt/vg Po)? The MT 0F (/I?ew MT. A5 be,ng Utaeiim?m Fan Toti?zxiFF ?hair [outs 59ml)? ?no, in few BHWT Orwgi FIRM (NRA COME \lp Ffam 7M, in? i . 0 RC twirl/3 m; 77? ?The above statement is true to the best of my knowle ge and belief.? Signed _4 Date. 0 A RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 R. T0 ?Wat R?qtii??w LY My?c?aNg? 55mg CW WCWM 100542}: mul'm?, 7mm 5W New; MN 08 510W 7L9 QR *0 ?t ?C&f ?w .fcrwavea ?thg a <3 w?pmr =09: (N 1m pprmeg 61 06 Man? 16 907* 5? [aon my ox MM ow; MW 3&0 EMWB Loom-mg Ema}: AW m) Li WW ma Max:325? $3 Jwb?an Ara: mm, cow +0 ox, eer'r cuff {of (M Up H, rm. +0 um, Prawn Qamwx AM 5mm WM. Imam} 1: mm} +0 5&2 NW eta/m Ema E?b @ww Fw??w Q?fxoxw NM Ba?fm 510w [Mg ur bowm Wig MW Mr?? EMT 0% Wag 1 mm Wow-t 030 This, me, 50% 095' RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 Wm? RQ 1% rm? 0053? ML {Yew we(?qu is NAM. thwme {3mm -- AWE 70th mm) if? Up $655 WQ Ge? 5 perm ?mm; AND <35 jkw? MW DOWN a? 13* JEN, f?m?li? NY ON We, W1 ?rm/m. A5 INN Jaw WQ (ALUKJT 30 961 MW at} oW?r mm} WW ?fa Prim TM ?Lfofat CW 7L0 ?Wk 0N We. ?3 1?14 Mmko (N 199% WW). a. Two 1w ER Wm 58M @425 OTFFRUWQ wa-Ng? MW MW 50m Wm RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 Max at?? a? of MUMM ?n ?g Ty 1W??u+3??e5L6 Afmuw 3L0 63623? 6 Jw?'rm, Mam?! GEE mm 0; 95: We: 0deva WPQ Wm prr?w ow} Wm 1E3 To gamma; mm (mm, WW AFRR bq?ng} w& Up FHW MJJ +J?e4j JDNK wt .3qu my MW gjJmolm, Swim} jg fawn?? h? fawg yum" TN 'W?osgec}; AW Armw New} QIWVCUHQ a) HN 70 DE}fo 64-14848, Class A, 30 April 15, AFSAS #739726 R82. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY 30 APR 15 72 HOUR AND 7 DAY HISTORY This investigation iS being conducted under the provrsions of AFI 91 -204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to recurrence. This term is being administered by an investigator from the interim Safety Board (ISB) or Safety Investigation Board (SIB). The statement y0u provide Will either be privileged or non-privileged applicable AFI 91-204 guidelines. a) NON-PRIVILEGED i understand i am being interviewed as a witness in a safely invastigation and i acknowledge that a promise. of confidentiality has not been extended to me. My witness statements may be utilized for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of information Act request. This non-privileged 72 hour and 7 day history form will be placed in Tab when complete. PRIVILEGED i understand i am providing statementls) for a safety investigation and acknowledge that a promise of confidentiality has been extended to me by Investigating Of?cer or Board President This privileged 72 hour and 7 day history form Will be placed in Tab when complete This 72 hour and 7 day history lorm is one of many tools the mishap investigator may use to help determine the use of this mishap. Your participation is both critical and appreciated and may help prevent future mishaps. Please answer these questions to the best oi your ability when you are not rushed or distracted Be as specific and detailed as possible All answers address events prior to the mishap and recovery events. today?s Date: 3 0" [Mishap Operator] Statement Completed 8y: (print) (Signature) ise or sie investigator Administering This Form: (prim) lap}: R-132 64-14848, Class A, 30 April 15, AFSAS #739726 Aerospace Medicine Flight HISTORY REPORT Please list the daily activities you did during the last 72 hours. Provide the times of the events as well as the activity in the chronological order. If you cannot remember the exact time of the event, provide the closest proximate time you can remember. DAY I (72 HOURS PAST) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up. how rested did you feel?) egos TIME ARRIVED AT \9 700 1 BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) w/ Hall/6%} 4' CiN?wxo MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) ?01 alien/w} f0 WorK LUNCH: (What time did you have lunch? List all food and drinks consumed) 00/ u?R (Elms woodcle AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) Work, Cf??ij TIME DEPARTED WORK: DINEEB: (What time did you have dinner? List all food and drinks consumed) H00 5019 w/ ?IvMo?ioU ?g mm EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) I Mn 5 Re? TIME YOU WENT . F0 9L EP :1 a 30 ALCOHOL CONSUMPTION: (List all types, amount, and times consumed) Non/? (List all medications take. prescription and over the counter, dost- and time consumed) Al DAY 2 (48 HOURS PAST) [Mishap 098mm] FIRST): R-133 V, 64-14848, Class A, 30 April 15, AFSAS #739726 WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did yOu get up? When you woke up. how rested did you feel?) a 6 00 )6 TIME ARRIVED AT WORK: 07 50 Mel) BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) 0630 all MORNING ACTIVITIES: (List all the things you did. all food and drinks consumad) FT Work owmri LUNCH: (What time did you have lunch? List all food and drinks consumed) so Twice?) Mano 6 vech AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) MORQ, CBTE DE TFI) /70 DINNER: (What time did you have dinner? List all food and drinks consumed) {(700 fox/0 fembff EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) Welfva TIMF. YOU WENT TO SLEEP: 00 ALCOHOL CONSUMPTION: (List all types, amount, and times consumed) Nan/?8 (List all medications take, prescription and over the counter. dose and time consumed) fl/g/VQ [Mishap Operator] NAME (LAST. FIRST): R-134 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 3 (24 HOURS PAST) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up, how rested did you feel?) 30) 7 (I I TIME ARRIVED AT WORK: 07? 0 BREAKEAST: (What time did you have breakfast? List all food and drinks consumed) 0600 animal MORNING ACTIVITIES: (List all the things you did, all food and drinks consumcd) //00 )ero? LUNCH: (What time did you have lunch? List all food and drinks consumedWink AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) Nil/W Not/why TIME DEPARTED WORK: DINNER: (What time did you have dinner? List all food and drinks consumed) 90" Gar/(Z EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) WT 00% Iowa, (coda TIME YOU WENT TO SLEEP: a ALCQHOL I ISLE: (List all types, amount, and times consumed) NOW (List all medications take, prescription and over the counter. dose and time consumed) [Mishap Operator] NAMEHAST, FIRST): R-135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 4 (TODAY) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times ditl you get up? When you woke up. how rested did you feet?) 0700 o" /500 Wm (What time did you have breakfast? List all food and drinks consumed) ?700 1/7ka MORNING ACTIVITIES: (List all the things you did. all food and drinks consumed) Brows? LUNCH: (What t'me did you have lunch? List all food and drinks consume 1/30 AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) Go To 797 TIME DEPARTED WORK: ARRIVED AT WORK: DINNER: (What time did you have dinner? List all food and drinks consumed) EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) MU GOTO Bellow. ?ow Filekf? Mal) TIMEVOUWENTTOSLEEP: ALCOHOL CONSUMPTION: (List all types, amount, and times consumed) Name MEDICATIONS: (List all medications take. prescription and over the counter. dose and Gwen Weatmt mt (Aim :15 Motrin! ls/s (5/5 STEP TIME: {6?50 TAKE OFF [9 as :3 [Mishap Opetator] NAME (LAST. FIRST): R-136 64-14848, Class A, 30 Apri115, AFSAS #739726 AFPAMBLZII 23 JULY 2001 257 7 XDAY HISTORY FOR AERIAL VEHICLE MISHAPIPHYSIOLOGICAL INCIDENT 7 [he 14? day luston In less detailed than the 72-hour histozy. Please note any signi?cant life events that have occurred over the past two (example selected for promotion, death in family, work, FLYING, marriage dial- :213; Sienna] chmculty, mutton/leave, illness, etc.). Include Calfeine, Meds, Alcohol and Tobacco, exercise and [Mishap Opetator] FULL NAME 4 SSAN am New) FHOK 7?s WORK Wow 5/9190 ?7ka CWW AN 2daysprionomishnp:Datew5: wokkj jiggle 7M5 3 days priortomishep: Daxegz?t ls Nolk/ Show 6 M5 l9 5MP ?gm 5 days prior to mishap: 0mm: 5?49} ?1 a days prior to mishap: DateM: MM 5m 9 7NU 7deys priortomishupzbutc m: . 7W R-137 64-14848, Class A, 30 April 15, AFSAS #739726 R8.3. SIB NON-PRIVILEGED INTERVIEW 12 MAY 15 Page 1 of 2 on-Privileged Witness Statement IVA (Date) [Mishap Operator] I, I have been advised by (Mime, Grade, Organization, of Witness) Warn: of Investigator) a safety investigator ofthe mishap that occurred on 3'0 apr 13? involving KC '1 (E - ?gs (Date) (Equipment SM n. This investigation is being conducted under the provisions of AFI 91 -204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. [Mishap Operator) Name (lat,va MI) and Rank/brad: A qua- R-138 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Omai Aircraft Diagrams AFTNAVIBATUR STATION Mm? mew main 1-19 R-139 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of SrA Role: [Mishap Tactical Coordinator] Cryptologic Operator 97th Intelligence Squadron Interviewers: (Board President) (Pilot Member) Date: 12 May 15 [Pilot Member] [MCO] : This is a non-privilege interview with , Senior Airman, being conducted on 12 May 2015 at 0900 local by Captain [Pilot Member] for the safety investigation board for the recent mishap. We’re investigating the mishap involving a RC-135V that occurred on 30 April 2015. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent reoccurrence. A promise of confidentiality is not being extended to you. Your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [MCO] : Yes. [Pilot Member] : For the record, would everyone present introduce yourself by stating your name, rank, and affiliation with the board starting with the witness. [MCO] : [President] : [Pilot Member] [MCO] [MCO] , Senior Airman. Witness. , Board President. : , Pilot Member. , how are you doing today? : Good, how are you? [Pilot Member] Good. So if you wouldn’t mind just starting us off talking us through the mission as you see it. [MCO] [Pilot Member] [President] [MCO] : Ah what, okay, so uh. : And uh, nothing secret. : Yeah, keep the classified out. : Absolutely. [President] : If you need to discuss something classified just let us know and we’ll probably grab a different one. [MCO] : So mission planning was pretty straight forward. We were for uh, we were going to do exercise Emerald Warrior and we discussed a lot of stuff about that and about what it was. It was a night flight so that was a little different. Uhm definitely threw off some sleep there but uh for all the mission planning, the front end and like the nose and tail end briefing everything seemed like pretty standard, like nothing was crazy; nothing was different. But they did note that there was like a- a, something with a pack on the jet that we were getting; so I guess there are two packs in the back and one in the front. The one in the front was for like the pilots and stuff so like in the event of an emergency like they have their own isolated system. R-141 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [President] [MCO] [President] : Where is the pack on this? I don’t know. I don’t know where the packs are. : Okay. Oh, okay. [MCO] : But I know that there’s two in the back, and we need one for all the ops, and then one for the system to keep it from getting too hot. And I guess we had an issue with one of them and I asked what that meant from the ASEs and that’s- they said ‘it’s not working, like but it’s not totally broken. It’s just kind of like off’ it’s not going to produce as much; like if it was an air conditioner it’s not going to produce as much cooling as you necessarily want it to, it’s just a little less. So they said ‘we can go without it, we’ll just dress warm up there and uh we can keep the one that does work well for the system and the pilots are good to go.’ It seemed like it would be fine. I was also told that like if we tested on the ground we wouldn’t- it would be like a grounding item, but we don’t have to test it on the ground and that was our way of getting around it so that we could still take off and do the mission. I don’t know how to really say anything because I don’t know anything about the pack, I just know that was an issues that was like- going into it that as the only thing that I remember as an issue. Uhm on flight day we all showed upeveryone was there. Uh we got- the front end went and then we waited at the 97th- and then the bus came for us after a while and we all went. We did all- it’s actually kind of funny because I fought over uh position 12 with a couple other ops; that’s kind of ironic. But, uhm[President] : Where’s position 12? [MCO] : Position 12 is the aft-most before you get into crew rest- so it’s right here… I was sitting there, then uh we did all of our AUX checks and our preflight; everything was good. And most of us in the back, we just- were kind of waiting to see what happens; uh the starting engines and the taxiing and the taking off finally. So they pulled the stand so we put all of our gloves on. We just sat and waited, most of us just listened to comms waiting for stuff. We do- we run our checklist ya know everyone calling in and all that. And then uh- when they were starting engines, there was an issue with engine two. They had to get their jet guy, I don’t know that that means, but they couldn’t get it to start the normal way so they had to come plug something into it to like manually force it to start. Uh that took a little bit, so there was a little bit of a delay there. And then uhm finally, we taxied out and we waited. When we finally got cleared to take off, and then I was sitting facing aft, we all face aft all the ops do, uh at least in this like row right here when we go to take off. And I was actually peaking over the seats in crew rest ‘cause we were arguing over- among the ops, not arguing but we were just discussing like: which way were we facing; which direction we were taking off from the runway ‘cause we don’t know, ‘cause we were just trying to like see out the window and figure it out for ourselves. Of course all I could see is like the grass and uh they started uh running the engines up, and ya know we starting to accelerating and you can feel it obviously. And like I was just looking around and then there was like out of nowhere there was a fire; there wasn’t like any noise associated with it that I noticed uhm course I had headsets on so ya know but, ya know it dampens a lot of noise. The flame was like, it was like a bright orange with like some light purple in it, kind of looking flame. And it was well over a foot long. It was coming out of the top; there’s like the metal paneling that makes this up here on the galley, it was coming from behind it. It wasn’t…oh this isn’t very useful (noise of a pen)…and it was kind of forced to curve up because of the roof of the jet. [President] : Try a pencil, it might work better on there. R-142 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MCO] [President] : So what I saw was like this, it was kind of forced to curve out ya know. I couldn’t: Definitely from behind? [MCO] : Definitely from behind. I couldn’t- I couldn’t see the base of the flame at all, that’s why I’m pretty sure it’s coming from behind it. It wasn’t like coming out from the sides or anything like that. It was only coming out from the top. Of course it got a lot worse; it started hitting these wires and they started melting or whatever and at this point I had called it out already uhm and of course everyone was making the call. It was kind of funny ‘cause we allafter the first person calls, it turns out everyone decides to call like; but uhm it was really quick what happened. Luckily you could feel the brakes go on, so we were- we got through to the pilot. But uh like no joke I turned to put my OX on- put my mask on ya know get everything working, and by the time I turned back around like it had filled with like white smoke. Like if I were going to like draw it… so there’s two people sitting on 15 and 16, and there were two ASEs back here in crew rest, and basically like this smoke cloud and already like filled this up; like I could barely see them, and I was closest to them other than them themselves. It was like pure white, there was no black to it at all, ya know just kind of filled it all up. And uh the first thing that AMS said was to get everyone out of AFT as in the people in crew rest, and only some of them were on headsets ‘cause the ASEs had to take their headsets off because they were trying to put the firefighter stuff on ‘cause that’s- that’s their go-to job in the event of a fire back there. And then uh I’m trying to remember- I wrote it down… so they told us to get out of AFT and puteveryone get on ox especially. And then he had- he wanted us to get up and then he kind of like gave a little more motivation, like ‘okay we’re going to get up and we’re leaving now’ like we’re going; and he did that all over the comms. And I guess the Chief kind of pushed the four guys, I mean included himself, the four out of the back and I waited to make sure they were coming out behind me before we started going on. There was a little bit of like a delay ‘cause we kind of waited for a second for the people in front of us to move. And since the smoke was like ya know still moving up, I was still sitting there with my oxygen. I didn’t want to go off oxygen until I was I was going to start getting out of where the smoke was. So once we started moving we allwe all got up to the front probably where like the TC compartment is, so basically like up past this point, we were all waiting up here and then there was kind of like some bottle-necking waiting to go down the- the ladder, because you can only go down the ladder so fast. And so we just waited to go down the ladder and everyone got out. And then as soon as we got off the- off the jet we just went all straight this way ya know to the grass off to the side of the flight line like we’re supposed to do; we all met up with the NAV and we counted everyone, and everyone was there. Now was that- by then I mean I think when I got out of the jet I was probably like the middle person to get out; I wasn’t the first and I wasn’t the last. There was already one uh fire truck there- the smaller one, or the one that doesn’t have huge wheels anyway. That was it; we kind of just waited and watched. Uh as we were watching- I mean knew there was smoke, and the firefighters started, after we got out- they put a ladder up on the wing and went in to check it out. And uh while we were sitting there watching the jet that we just ya know we just evacuated from, the fire started poking through the side and the smoke started coming through, and there was a little bit of black smoke then and it poked through the roof. And then the firefighters saw it and just like put like three hoses on it with foam and water and whatever trying to take care of it. But, it just kept burning. I don’t know, I know the oxygen line is like right there with the- the blue metal. Also- our ox tanks are underneath of there for the whole ox system, so I don’t know. Someone said that the fuel lines for engine two run through there too which is concerning ‘cause R-143 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 engine two was what was having problems. So it was kind of- I don’t know what actually happened but that’s all I got as far as details. [President] : Okay. So when you said the flames were coming from behind this galley piece up here, were they- how would you describe the flames; would you describe them as like uh like on your like small licking flames, or was it more like a torch or a flare? [MCO] : It was more like a torch. Like it seemed like it was fueled by like a gas. Like if uh think like a flamethrower, as soon as you let the fuel out and the flame is going; it looked like it was burning off of something, like pushing out ya know. It didn’t look like ‘oh, I just set this log on fire’ and it’s just casually burning, it was like actively burning. Like- I guess like a flamethrower would be the closest thing. [President] : Which direction was- obviously it’s coming up, but which direction… did it look any direction to you, or? [MCO] : Uh it looked…very vertical, to me. And it seemed like it was going up, and then just being pushed out as it hit the- the roof of the jet. I mean, the roof of the jet is curved, so it looked like it was going to the side, but it- the base of the flame like I had looked at it the- the lowest part seemed like it was going straight up, to me. And then it was being forced to curve as it hit the roof. [President] : Alright. [Pilot Member] : Yeah uh, so you saw the fire, then smoke. You saw the ASEs start to fight the fire; did you try and help fight the fire as well from your position? [MCO] : No, I didn’t. Uhm I did make the call first, but uh they were already getting all the equipment and everything and I felt like one more body back there like 5 instead of 4 wouldn’t be very helpful considering it’s already covered in smoke, its already on fire; they already have enough hands to carry every piece of equipment that is back there that they would have used and they could have- gotten to it all quicker than I could. I could have tried to grab, but it’s not here, but if like if you were in crew rest or from where I’m sitting- right there is a panel, where there is another fire extinguisher… sometimes I think I could have grabbed that but I don’t know if it would have been any help ‘cause by the time they started fighting the fire, we decided to evacuate the jet anyway. [President] : Okay. Uhm, alright. Anything about the galley did you- did you use it, did you notice anything about the galley; anything abnormal? [MCO] : No. No, I didn’t notice it at all. Uhm when we were on the bus ya know going between getting labs done and all that other stuff, one of the ASEs said that they’re never deviating from the checklist again, because they said they turned the refrigerators on uhm which is a normal thing for them to do, but they said usually you don’t- you turn things on in a particular order if you go by the checklist, and the refrigerators are like one of the last things or like a note or something. But they just turned them on at the beginning, for whatever reason. I don’t know if they had food or whatever to throw in there. But that’s the only thing that I know about the galley that anyone had done. [Pilot Member] : Do you know when they normally would have turned them on; would it had been after takeoff or before takeoff? R-144 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MCO] : I don’t know when they would. Uhm I think it might be part of their preflight stuff uh, I know that that they also- I mean a lot of people are mentioning concerns that like when they go through the baselines and they update the jet, they don’t update like the microwave and the fridges in the back, so all of their cables are really old and a lot people say that a lot of those are like really frayed in the back. And I don’t know if that’s true, ‘cause I never look back there but I know there’s people that say that. [Pilot Member] [MCO] [Pilot Member] : Do you uh use the lavatory, obviously? : I didn’t on this flight; I do sometimes, yeah. : So where do you guys keep your toilet paper, if it’s not in the sink in the lavatory? [MCO] : I guess I’ve seen it up in here before. That’s the only place that I know it to be. Usually, sometimes they stack it on the sink because the sink sometimes doesn’t work…ever. [President] : So you see right here where those water bottles would normally plug in, or are you talking about the back piece right here; the back uh cabinet? [MCO] [Pilot Member] [MCO] : I’m not sure. Probably, I don’t know. : Above the galley somewhere in one of those compartments. : Yeah. [Pilot Member] : How about uh….just curious, how long do you think it took from the time someone said ‘fire’ to everyone getting off of the airplane and egressing; if you had replayed in your mind? [MCO] [Pilot Member] : You mean everyone getting off the jet, or everyone starting the egress? : Uh how about from fire call to egress to everyone getting off the jet. [MCO] : I would say, uh. Starting from getting on my oxygen mask.. I would say I called, and they everyone else called and from the point the fire started to the time that it filled with smoke and we were told to abandon basically, I would say there was probably like 45 seconds there, max; maybe less than that, but around that. It seemed like the flame burned for like 15 to 20 seconds before it started producing a ton of smoke from hitting the wires or whatever it was burning. Uhm which is odd ‘cause it, I don’t know, it kind of burned clean and then- until it started burning other things, and then it like started producing a ton of smoke. So I would say 45 seconds, and then I would say it probably took us like two minutes or so, once we like got up to the front and were kind of bottle-necked it took us a couple of minutes to like actually get everyone off the jet. [Pilot Member] : And you mentioned a small firefighting vehicle, was that there as soon as you guys got off the jet, or was there…what was the first response you saw? [MCO] : So the first response I saw was the- it was like a, all I remember is that it was yellow and not red. [Pilot Member] : Okay, a yellow truck? [MCO] : Yeah, it was small- yeah it had like a small arm, but not one of the huge extendable arms. It was just like one on the top facing forward. So I mean, the front of this vehicle was R-145 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 facing the jet, they were like nose-to-nose. Uhm I don’t think they knew that- well maybe they knew that the fire was in the AFT but they were just sending people in, they weren’t like at AFT shooting at AFT at that point. But then all the other people came probably like- or all the other vehicles came probably 20-30 seconds later, and after that all the vehicles just kind of flooded in one at a time after that. I think that…yeah. [Pilot Member] : Cool. How do you feel? [MCO] : Lucky. I feel like if we- there’s some pilots who when we make calls like ‘oh there’s fumes in the back’ or ‘oh there’s fire in the back’ or whatever ya know a lot of the times it’s like electrical equipment, which is like ‘oh it, it fizzled out or something’ So sometimes they don’t take it as- well I shouldn’t say they don’t take it seriously, but they don’t think that it’s like ‘oh no, the jets like on fire,’ they think like ‘oh like one of the pieces of equipment is like not working.’ So I know that sometimes like deployed or whatever pilots will be like ‘oh, we’re going to take off anyway, we’re already at like S1’ or whatever… if we had taken off with this, I mean it was just too fast; like I don’t think we could have really fought it because…by the time they got the mask on, the mask was full of smoke anyway- to fight ya know, the firefighters mask to fight the fire. So it was kind of like- we would have been sitting here with this fire doing whatever it wanted, and maybe ya know trying to spray it, but it seemed too fueled for us to really like effectively fight it. If it was just like a piece of hardware or something that was like on fire on top it would be easy, but since there was so much fueling it I guess; I feel like even our fire extinguishers wouldn’t have been effective because it would have just pushed all of theeverything out and just lit itself on fire again anyway. But if we took off- I mean, I don’t know how fast we could have emergency landed I mean- I know it’s quick but a few more minutes stuck on the jet not even able to start egressing would have ya know made it a lot different. So I feel really lucky that we didn’t take off, honestly. I’m also really glad that like no one got seriously injured. I had to go to the hospital along with like the four others that were in the back for like smoke inhalation, but as far as I know we’re all better now. None of us got burned, or injured, or anything like that. [President] [MCO] [President] [Pilot Member] [MCO] [Pilot Member] [MCO] [Pilot Member] [MCO] : Chest feels okay, ya know? : Yeah. : Okay, good. : Awesome. : Yeah. : Alright, that’s all we have unless you have anything else? : No, that’s it. : Alright, then we’ll conclude. : Alright, thank you. [Pilot Member] : If no one has any further questions, we will now conclude this interview. I would like to remind you again that you were not offered a promise of confidentiality and that your statement is not protected and will be released to any follow-on investigation of this mishap and may be releasable to the public subject to the Freedom of Information act. We request that you refrain from discussing your testimony and any information shared with you today regarding to R-146 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. R-147 64?14848, Class A, 30 April 15, AFSAS #739726 [Mishap Airborne Systems R9. Engineer 2] R9.l. ISB NON-PRIVILEGED WI INESS STATENIENT 30 APR 15 Page I of 2 Non-Privileged Witness Statement ?3 a Ale, [Mishap Airborne Systems Engineer 2] (Date) 1 5 316% have been advised by (Name. Grade. Organization. of Witness) Wanna of Investigator) a safety investigator of the mishap that occurred on ?r involving EK- DC bl (Date) (Equipment SN) This investigation is being conducted under the provisions 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I i am being interviewed as a witness in a safety investigation and] acknowledge that a promise of con?dentiality has NOT been extended to me. be My witness statements (Written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request [Mishap Airborne Systems Engineer 2] Name (Last, First. MI) and [tank/Grade {is We. Signature R-148 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Page I of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of AF I 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. [Mishap Aimome Systems Engineer 2] WITNESS STATEMENT OF: Name (Last, First, MI) and innit/Grade 456'; Signature [Reference attached documentfor witness account of event. This document is being entered?r accounting purposes and for witness is acknowledgement of this being the form they should have received for completion of a written statement. The member?s chain of command will only review the?nal mishap report if acquired through appropriate safety channels L4 W91 ?204 para R-149 64?14848, Class A, 30 April 15, AFSAS #739726 WITNESS STATEMENT Date of the 3? . Crew position (as applicable) Time you began duty [Mtshap Aitbome - 5 . . I. _S_Y_5tem5 Exam? 2] m" have been ndmed by oflhc followmg. Tlus is being conducted under the provisions of 91-204 solely for the purpose of mishap prevention within the United Stats. Air Force and to dctemtine all factors relattnz to the mishap in order to prevent recurrence. I understand I am being interwewed as a witness in a mtshap investtgation and that a promise nfconftdenttality has not been extended to me. D, This Wtutcss statement may be ralcamd to th: public pursuant to a Freedom of Information Act request The chain of command will ?nal mishap rqaon. a. Provide an account of ?rst-hand observations or what happened, a description of coudluona, ctrcumunncu. and associated events (use reverse for continuation). al?? Car/f 4. (raw Mcmber IQI/eol :01. .7 hand 4.14 9/27"? ?g'f aim bra/Vt fuww- 7?9 WV mask 6?47 5mlz< Cue) so 3'64. 49 I ah" I Ant} icc a. fodf MI but .414 n4 6 I14. 'f?m {oz?(lka af?x Met47* Kauf- :4 ages Cowl?1.7? darn-w. hum/71- laws \We hall ml awn-1 WW CW AM, X1) ?lu/V? 0w W, AFE all ?mu. cum Wt 6w? 441/8 wt 4,90 4.201?? 2? [?inch MqIn-?( ?9.199. ?ay? AL bit?, Sum-c 47M w?cn ?The abovc statement is true to the best of my and bclief." Sig: Dale. 3? R0135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 R9.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY 30 APR 15 72 HOUR AND 7 DAY HISTORY this Investigation is being conducted under the provisions of AH 91-204 solely for the pUrpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. This term is being administered by an investigator from the Interim Safety Board (ISB) or Safety Investigation Board (SIB). The statement you provide either be privrleged or non-pnvileged IAW applicable AFI 91-204 guidelines. in NON-PRIVILEGED I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of confidentiality has not been extended to me. My witness statements may be utilized for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of information Act request This non-privileged 72 hour and 7 day histOry form Will be placed In Tab when complete. PRIVILEGED I understand I am providing statementis) for a safety investigation and I acknowledge that a promise of con?dentiality has been extended to me by Investigating Of?cer or Board Freudian! This privileged 72 hour and 7 day history form will be placed in Tab when complete. This 72 hour and 7 day history form is one of many tools the mishap InvestigatOr may use to help determine the cause of this mishap. Your participation ls both critical and appreciated and may help prevent future mishaps. Please answer these questions to the best of your ability when you are not rushed or distracted Be as speci?c and detailed as possible. All answers address events prior to the mishap and recovery events Today?s Date: I, '4 [Mishap Airborne Systems . Engineer 2] Statement Completed By: (print (Signature) [Medical Member] ISB or SIB Investigator Administering This Form: (print) R-151 64-14848, Class A, 30 Apri115, AFSAS #739726 Aerospace Medicine Flight 72-HOUR HISTORY REPORT Please list the daily activities you did during the last 72 hours. Provide the times of the events as well as the activity In the chronological order. It? you cannot remember the exact time of the event, provide the closest proximate time you can remember. A 7 . . 46m (AH WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up. how rested did you feel?) TIME ARRIVED AT WORK: 7W, BREAKFAST: (What time did you hav: breakfast? List all food and drinks consumed) MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) ?ow 64 LUNCH: (What time did you have lunch? List all food and drinks consumed) JM 54/qu mew AE ACTIVITIES: (List all the things you did, all food and drinks consumed) TIME DEPARTED WORK: DINNER: (What time did you have dinner? List all food and drinks consumed) 52,511, [go/e Bear 2 inc-Hi5 EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) Lowland ammo TIME YOU WENT TO SLEEP: ALCOHOL CONSUMPTION: (List all types, amount. and times consumed) Ago/a Cider Beer 5 Battle 5 MEDICATIONS: (List all medications take, prescription and over the counter. dose and time consumed) I WW Wham.? DAY 2 (48 HOURS PAST) [Mishap Airborne Systems Engineer 2] NAME (LAST. SSAN: R-152 V, 64-14848, Class A, 30 April 15, AFSAS #739726 ?u WAKE UP TIME: (What time did )?Ct?l wake up? [low many hours did you sleep? How many times did you get up? When you woke up, how rested did you feel?) 1 Jim ARRIVED AT WORK: BREAKFAST: (What time (lid you have breakfast? List all food and drinks consumed) in? Mooh/ MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) (What time did you have lunch? List all food and drinks consumed) I (on 19M, AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) 0Lth (no I ?4 Mt Hibufvvx WORK: (What time did you have dinner? List all food and drinks consumed) (093? ?4"(30415 EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) (dock) on {Maw TIME you WENT TO swag; (Opt/t ALCOHOL CONSUMPTION: (List all types. amount, and times consumed) Noun, (List all medications take. prescription and over the counter, dose and time consumed) [Mishap Aitbane Systems Engineer 2] A ME R-153 V, 64-14848, Class A, 30 April 15, AFSAS #739726 3 [24 HQURS hr?i WAKE UP TIME: (What time did mwake up? How many hours did you sleep? How many times did you get up? When you wokeoip, how rested did you feel?) 1 (dead TIME ARRIVED AT WORK: BREAKFAST: (\Nhat time did you have breakfast? List all food and drinks consumed) Nope MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) 0mm INONL LUNCH: (What time did you have lunch? List all food and drinks consumed) N6 in, AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) (bf/(ta Nat k. h? ?42?399 DEPARTED WORK: DINN ER: (What time did you have dinner? List all food and drinks consumed) Number MS 1 ML: Sea? EVENING ACTIVITIES: (List all be things you did. all food and drinks consumed) TIME YOU WENT TO SLEEP: ALCOHOL CONSUMPTION: (List all types, amount, and times consumed) IQ-ppl; (MCCK 836'"; MEDICATIONS: (List all medications take, prescription and over the counter, dose and time consumed) I M111 Mama [Mishap Airborne Systems Engineer 2] NAM (LAST. R-154 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 4 (TODAY) ?hm WAKE UP (What time did you wake up? How many hours did you sleep? How many times (3d you get up? When you woke up. how rested did you feel?) Vt?) (910ch TIME ARRIVED AT WORK: BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) 75:, MORNING ACTIVITIES: (List all the things you did. all food and drinks consumed) 04 five lg, LUNCH: (What time did you have lunch? List all food and drinks consumed) AFTERNOON ACTIVITIES: (List all the things you did. all food and drinks consumed) out?t 11/, Took, (19,7. Lug/k TIME DEPARTED WORK: 44. 7530? DINNER: (What time did you have dinner? List all food and drinks consumed) [Jaw EVENING ACTIVITI ES: (List all the things you did, all food and drinks consumed) ?li?cr 0/ ark TIME YOU WENT TO SLEEP: ALCOHOL CONSUMPTION: (List all types, amount. and times consumed) A) (col/v MEDICATIONS: (List all medications take, prescription and over the counter. dose and lime consumed) mo/A ARRIVAL TIME AT SQUADRON (If aw BRIEF TIME: /{30 STEP TIME: M, ao TAKE QEFTIME: 1 TIME: 7" [Mishap Airbome Systems Engineer 2] NAME (LAST, FIRST): R-155 64-14848, Class A, 30 April 15, AFSAS #739726 23 JULY 2001 257 7 Kiwi HISTORY FOR AERIAL VEHICLE INCIDENT 7 The 14 day lust.on is less detailed than the 72-hour histoxy. Please note any signi?cant life events that have occuzmd over the past Mo weelcs (example selected for promotion, death in family, work, FLYING, mmlage dim- :23: ?annel dif?culty, woman/leave. illness, cm). Include Caffeine, Mods, Alcohol and Tobacco, exercise and 8 . [Mishap Aibome Systems FULL Engineer 2] RANK :24, mew.an Ac' ldaypriorto mishap: Dates? my" 4 ?epic (Mar 3944' 2dayspn?ono mishap: Date &r kr 3dayspriorlomishap: Date Agc 7k/ 2 ?wk 4dayspxiortomishap3Dntc 4V - 911/ Sdaysp?artomishaptDatc 2" Ax! /o 6days pn?ortomishapzDatc d?r l??m .- F?ij 877? R-156 64-14848, Class A, 30 April 15, AFSAS #739726 R9.3. SIB INTERVIEW 11 MAY 15 Page 1 of 2 (In-Privileged Witness Statement QM: (Date) [Mishap Airborne Systems Engineer [Pilot bet] I 2] 99255 have been advised by (Name, Grade, Organization, of Mme?) (Name oflnves?galar) a safety investigator of the mishap that occurred on 7p 41, [Strivolving g; 125 4/ 57' (Date) (Equipment SN) 8. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of m'mhap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. [Mishap Airborne Systems Engineer 2? 9174/!9 Name (Last. First. MI) and Rank/Grade 65/ 2 not!? otgnamre R-157 V, 64-14848, Class A, 30 April 15, AFSAS #739726 [M'Shap gm /5 Engineer 2] Aircraft Diagrams R0135 -- comm! - FWD NAVIGATOR 31mm - STATION wormm. anew man 9? MM - nasz'msn 1-19 R-158 64-14848, Class A, 30 April 15, AFSAS #739726 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of SrA Role: [Mishap Airborne Systems Engineer 2] Airborne Systems Engineer 2 343rd Reconnaissance Squadron Interviewers: (President) (Pilot Member) Date: 11 May 15 [Pilot Member] : This is a non-privileged interview with [MASE2] being conducted on 11 May [Pilot Member] 2015 at 10:15 AM by for the safety investigation board convened for the recent mishap. We’re investigating the mishap involving a RC-135V that occurred on 30 April 2015. This investigation is being conducted on the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap and in order to prevent recurrence. A promise of confidentiality is not being extended to you. Your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant of a Freedom of Information Act request. Do you understand the promise of confidentiality has not been extended to you? [MASE2] : Yes. [Pilot Member] : For the record, would everyone present introduce his self by stating your name, rank, and affiliation with the board, starting with the witness. [MASE2] [President] [Pilot Member] [MASE2] [Pilot Member] : Uh, Senior Airman : Colonel : Captain [MASE2] 343rd. the safety investigation board president. , pilot member. Alright, uh, how you doing today, man? : Good. : Good. Alright, would you mind just stepping us through the events as, uh, you saw them? [MASE2] Okay, so we were on the, uh, runway and, um, we were going about 50 knots when one of the ops, um, over interphone, or over call, um, said there was a fire in the back, um, that’s when I looked up, saw the flames coming out of the galley, and, um, started putting on my fire fighter equipment which is the, uh, facemask and hook up my oxygen, and, um, radio… or my mic and everything to it. Um, and by the time we came to a stop, um, I got everything ready, um, someone threw a fire extinguisher down the, um, hall.. or the aircraft there so we could reach it, [MASE 3] um, went to go grab the fire extinguisher and by that time the aircraft like filled up with, like, way too much smoke. Flame was, um, huge. It was probably about three feet long [MSSD] coming out of that, coming out of the galley, and, um, at that point, uh, was saying that like plastic was literally like dripping from that top of the aircraft where all the wires are and everything, and, uh, that’s when I heard over my gas mask setup I had on, um, maintenance called over saying that we were egressing the aircraft and that’s when, uh, we decid… that’s when we started egressing then, um, Sergeant [MAMS] ’s eyes they got filled with smoke so they R-160 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 were burning and so he just held on to my shoulder while we egr-egressed the aircraft. And that’s it, we didn’t actually start the… or we didn’t, like, start the, uh, fire extinguisher or anything or hook it up or disconnect anything on it because it was just, uh, it was too much at that point, that we weren’t going to be able to do anything and were better off egressing. [Pilot Member] : Okay. To, uh, give me a frame of reference, can you mark out where you were sitting? [MASE2] : Okay [Pilot Member] [MASE2] : Here. : Oh. I was sitting right here. [Pilot Member] [MASE2] : Alright. And, uh, where was Airman [MASE3 sitting? ] : Uh, Sergeant [MASE3 ? ] [Pilot Member] : or Sergeant [MASE3 , I’m sorry. ] [MASE2] : That’s fine. And then there was another, we had a raven, he was sitting right here, and, um, I can’t think of his name off the top of my head right now, but I’ll say Raven. [Pilot Member] : Okay, that Raven is sitting right there? [MASE2] : Yeah, and then we had another airman there. [Pilot Member] [MSSD] right there. Right there, and then there was : Okay, thank you. [MASE2] : Then we had this airman. This is the airman who, he’s this, this gentleman, he tossed the, the fire extinguisher that sits right here. So, and he just threw it upright between me and [MASE3] so that we could grab it and start fighting the fire, um, but, uh, the aircraft like filled up with smoke way too much, quick. [Pilot Member] : Can you just mark down which one of those airmen handed you the fire.. or rolled the fire extinguisher? [MASE2] : Okay. This guy, he handed us the fire halon. [Pilot Member] [MASE2] : Okay. : It makes it easier [Pilot Member] [MASE2] : Okay. : So, that would have been, um, the gentleman who is sitting in position twelve. So… [Pilot Member] : Perfect. Now, uh, when you heard, cause you heard, heard fire before you saw the fire, right? R-161 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE2] [Pilot Member] Yeah. : Alright, when you looked up can you, uh, describe what you saw? [MASE2] : Um, yeah. So the flame was like coming out, like, literally like between the two of these things like a blow torch shooting out over this. [President] [MASE2] [President] : You can draw on that… : Oh, I can draw on those, okay. : Yeah, Yeah, and as best you can… [MASE2] : Oh, I’ll use a pencil because this is wax, so it won’t take… so it was probably coming like, like so. Like right here in this corner. You see this little like corner right here? It’s kind of hard on this picture here but it was shooting out like literally like over all these wires right here, and there’s also the oxygen line so I think, it was a pure orange flame, like a really clean looking orange flame and, um, it was big, so I don’t know if at that point it, you know, was being fed by that oxygen line. [Pilot Member] : Okay [MASE2] : We did have the, uh, we deviated from our checklist and we had the refrigerators on with the blowers, uh, so that our food would stay cool and everything like that, so, um, but it didn’t, I mean I, obviously it didn’t look like it was, the flame was coming from down, way down here, it was coming from something like, in this area. [Pilot Member] [MASE2] : What’s, what’s your ACE position? : ACE 2 [Pilot Member] : ACE 2, and you guys don’t have an assigned seat, it’s just in the crew rest area or do you have an assigned seat? [MASE2] : Uh, no, we don’t have an assigned seat. But we, it’s kind of like an unspoken thing where ACE 2s and ACE 4s sit, so… um… [Pilot Member] : Okay. [MASE2] : ACE 4s will typically sit here, um, at this spot because this is where their ETD is. My ETD is all the way, it’s aisle maintenance. [President] : Right, half way through the rack. [MASE2] : Yeah, so, there’s no real way for me to like go over call or anything like that because the button is all the way over here. So what I do is I, I’m on maintenance hot mic and I communicate to either the ACE 3 or the ACE 1, of what’s occurring or what’s happening, and that’s what I was doing when I had my fire mask on is I was communicating to the, uh, the maintenance up here, that’s when they, um, alerted me to that we were egressing the aircraft. So, [MASE3] um, but will typically sit here. There only reason he was not sitting here was R-162 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 because there was a raven sitting here and he kind of just wanted more space so he just went, an empty, to the row that was empty behind him to sit there, and so he also couldn’t hit the call button because he was out of reach of it. [Pilot Member] : Alright. Uh, when you say the galley was a deviation from checklist is it in your checklist, or… [MASE2] [Pilot Member] [MASE2] [Pilot Member] : We have an ACE 5 checklist. : An ACE 5. Whose job is it to run the ACE 5 checklist if… : The ACE 2 and the 4 : the 2 and the 4? [MASE2] [MASE3] [MASE3] : Yeah, so, their, we as, me, and I, are, um, ’s an ACE 4, Sergeant, and I’m an ACE 2. Right now we’re in the transition of 2s becoming 5s and 4s becoming 5s, but we are not there yet. Um, and, so we were running these five checklists. So, typically what will happen is that ACE 4 will run this side of the aircraft. [President] [MASE2] [President] : That’s the left side of the aircraft as you’re looking forward? : Yeah. : Okay. [MASE2] : And then I will run the right side of the aircraft. That’s until… I mean that’s the way it is now. I mean that’s just the easiest simple way because most of my equipment is going to be on the right side and most of his equipment is going to be on the left side and that’s the way, it’s just easier to run the checklist that way. [Pilot Member] [MASE2] [Pilot Member] [MASE2] [Pilot Member] : So do you carry the ACE 5 checklist… Yep : along with your ACE 2? : Oh, no, I carry an ACE 5 checklist. : Just an ACE 5 checklist? [MASE2] : Yeah, we don’t carry, uh, they don’t have 2s. They don’t have a checklist for 2s for 5, or for the new baseline 11 [Pilot Member] : The new baseline 11 [MASE2] : Same with 10. They did away with it all, or, you have a checklist 2 for 10 but until you’re 10… until you’re 5 certed you don’t use the 5 checklist you use your 2 checklist, but on baseline 11 they didn’t make a 2 or a 4 checklist they just made a 5 so that we and then so the 2s and the 4s just split, they have the same checklist we just split, split it based on the side of the aircraft. R-163 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : So you’re going through the transition from 2s and 4s to 5s, but you’re not all the way there yet but they don’t have a 2 and 4 checklist for the baseline 11? [MASE2] : Yeah, the 2 and 4 checklist is the ACE 5 checklist [Pilot Member] [MASE2] : Okay. : If that makes any sense to you. [Pilot Member] : It does make sense. I… look you’re not certed, of, you haven’t fully made the transition, do you guys have to fly with instructors then? [MASE2] : No, because we, we’re cert, like we get qualled on 11 as a 2 to fly the 11 and so, but [MASE 3] I don’t run any of ’s equipment, he runs his own equipment, because I’m not qualified to run his equipment so I only run which is the 2 equipment here. That’s why we do the right side and left side. [Pilot Member] : Alright, and curious, on a baseline 10 and previous baselines, because we still have one 9 floating around there… [MASE2] : Yeah, no, I’m going to fly the 9 haha. [Pilot Member] [MASE2] : Yeah, haha, uh, whose job is it to run the galley in one of those baselines? : It is ACE 4. [Pilot Member] [MASE2] : It is ACE 4? Part of the ACE 4 checklist? : Yeah. [Pilot Member] : Okay [MASE2] : He’s the one that turns on, that’s why we left it that way where its left and right hand side, so, um, because that’s just the way it was on pretty much on like 9 and 10 also. [President] : On the, um, going back to the galley, when you said you turned, you powered it on, um… [MASE2] [President] [MASE2] [President] [MASE2] [President] : Powered, I, I don’t power it on. : Okay so it kind of … : [MASE3] powers it on. : Okay, you said you were just, non-standard that you guys were… : It’s a standard deviation : Okay [MASE2] : Uh, for us to turn on the refrigerator before takeoff because typically we’re turning on after takeoff but it’s pretty standard to turn it on before because that’s where we have our R-164 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 water cooler and like other people’s food will go in this refrigerator and so to keep it cool we turn it on. [President] [MASE2] [President] : And that’s just a switch on the left hand side next to the oven? : Um, well you got the exhaust blower here : Okay. [MASE2] : And then there’s another breaker, um, like right here with more equipment on it for like the toilet and the refrigerator and things. [President] [MASE2] [President] [MASE2] : Okay, so you have to, you have to… : There’s a button, or a circuit breaker you actually push in : You push circuit breakers in, okay, alright. : Yeah, for the, it’s the exhaust blower for the refrigerator so it blows that hot air. [President] : Which way, do you know which way the bl.. do you feel the hot air from the bottom or does it go up this way, do you know? [MASE2] [President] [MASE2] : I… : Don’t know? : I don’t know for sure. [President] : Okay, fair enough. And were these hot water bottles that they, the containers that are supposed to be there, do you remember seeing, are there any [MASE2] [President] [MASE2] [President] [MASE2] [Pilot Member] [President] : They’re not there now. : They’re not, you guys don’t normally fly with those? : No. : Okay. : I’ve never flown with them. : Uh, those are most of the main questions I had. Uh, : Egress? [Pilot Member] : Uh, that was the last thing I was going to talk about because you said had to hold on to your shoulder on the way out [MASE2] [Pilot Member] : Yes : But, uh, backing up to that, how were you notified of egress? R-165 [MASE3] RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE2] : Uh, over maintenance. I was on hot mic, over my headset. Uh, because I’m wearing the firefighter mask so it has the, it’s got the, for me the firefighter mask is a full cover so my eyes are protected and everything and I also had, there’s a headset that’s hooked up to it, and so, [MASE3] and maintenance said oh we’re egressing the aircraft and that’s when me and said [MSSD] hey we’re, it’s time to egress. You know? And then was like oh there’s plastic dripping so we were like alright we got to start going and so we just started going. It got a little backed up over here, I’d say I felt it was slowing down, and then, then it kind of sped up as we got off. But at this point I’d probably say like right here… [President] : Half way through the frame of the aircraft… [MASE2] : That’s when like the smoke was kind of like just staying towards the, the aft area of the aircraft and it like didn’t reach us fully, because it, I mean back here it was like, I mean you couldn’t see a foot in front of you. It was so, it was, it was literally like grey, dark smoke. Like if you were to burn a tire or something like that like type of stuff. [Pilot Member] : Yeah [MASE2] : So, um, you know like plastic burning and things like that, so, yeah, so we got up here and then that’s, we egressed the aircraft and then, um, we went to this side of the nose, um, into the grassy area as paramedics and firefighters showed up, so. [Pilot Member] [MASE2] : So were you on the ground before they showed up? : We were, we never took off. [Pilot Member] : Well I mean, um, did you egress and you were off the runway, you physically were off the runway before the firefighters get there [MASE2] [Pilot Member] : Um, : Or around the same time you think? [MASE2] : It, it was like, yeah, it was like yeah we were, I like may I touched grass and then the firefighters and stuff were like starting to show up and things like that, so and they were pretty [MASE3] quick and then the paramedics came and, uh, and I we had smoke inhalation and so, um, we were getting checked out for smoke inhalation and then we ended up going to the emergency room and getting treated for that. They hooked us up to, uh, breathing equipment and um, pretty much like an inhaler or something like that it was putting smoke into our like a medication that was smoking into our lungs to open up the passageways so we could breathe a little bit easier, because pretty much me and him both felt like our, we were constricted on breathing, um, and then Friday I went and got an inhaler and then Saturday I was feeling better then. [Pilot Member] [MASE2] : How do you feel now? : I feel fine now. R-166 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : Good. Um, going back to the egress, from the point when you noticed or were told there was a fire, till the point where they said egress, how, how… can you estimate how much time that was, how like… [MASE2] [Pilot Member] [MASE2] [Pilot Member] [MASE2] [Pilot Member] : 30 seconds probably. : Okay. : I mean… : So how long do you think you spent on the plane then? : Oh… : From when the fire started to when you were off the plane. [MASE2] [MASE3] : Okay, um, we, and I, we didn’t start getting up out of our seats until the aircraft came to a full stop. And that was just for safety reasons for us, so we didn’t get up and start fighting a fire and then like, this fire was huge, and like you know when the aircraft comes to a stop you know you move or something you get jerked and fall into something, so we waited until we hit, got to the full stop. Then that’s when we got up and tried to fight the fire. I’d probably say within like… I, I’d probably say we spent about… time… it took us a while to get off the aircraft I’d say, like, not a, when I’m saying a while I mean like 45 seconds, a minute to get off the aircraft. But, from the point we got up to fight the fire, and … hey we’re egressing, 30 seconds and that’s when we were like, so I’d probably say like maybe max time 2 minutes to be off the aircraft fully and in the grass. [President] [Pilot Member] : Okay. : You think that’s pretty good? [MASE2] : Yeah, I mean, I, uh, that’s what I’m thinking to myself, I’m like, you know like, If I, uh, we get like, I, um, talking from full stop to off the aircraft, I’m thinking maybe like a minute 30 – 2 minutes, somewhere around there. That’s in my head… [President] : Right. [MASE2] : I mean but, in emergency situations things seem to move a little bit slower than what it is kind of thing, like everything’s in slow motion, so. [President] [Pilot Member] [MASE2] : What about the hatch? : The hatch. So, uh, the left overwing hatch at some point was opened. : Okay, I wasn’t aware of that then. Oh you know what, it, I do, the firefighters opened it. [Pilot Member] [MASE2] : The firefighters did open it? : Yeah, they opened it. R-167 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : Okay. [MASE2] : So, but, for people egressing the aircraft, no, no, nobody, nobody opened that, nobody went out that. [Pilot Member] : Okay. [MASE2] : So the firefighters did open it. I remember watching them open it and, uh, actually when they did open it, that’s when, uh, the reason they opened it, I remember was, I could hear on the radio because I was with the paramedics and everything, the reason they opened it was because it was filling up with way too much smoke, and then they opened it, and then also the hole started burning. But that’s when the hole started… [President] [MASE2] : Through the fuselage? : Yeah, like, you’d see huge puffs of smoke and then you just saw a huge flame shoot out. [President] : Was that flame that you saw shoot out, was it similar to the same color or same consistency as the flame you saw when you turned? [MASE2] [President] [MASE2] : It was orange. : Same thing? : Yeah. [President] : Not like your firefight, not like your camping type flame, but did it look like that or did it look more pronounced? [MASE2] : It was, it was, uh, it was, uh, orange flame but there you could see black, and I think that was because it was burning, but I’d probably say it was only sticking out the aircraft maybe a foot and a half maybe. [President] : Okay. [MASE2] : Something like that. But when we were in there it was, I mean it was, it was a really clean orange looking flame, like, um, like what I would compare it to is like when you like you’re starting a charcoal grill and you’re like oh I’m going to spray all this stuff on it or you’re might be having some fun on your charcoal grill and it’s lit and you’re like I just want a big fire. It was like that. Like it was like you just squirted a bunch of lighter fluid on this thing and just… (makes fwoosh sound) kind of thing. [Pilot Member] : Hmm. [MASE2] : It was a clean oran, really nice looking orange flame versus like, if it was like an electrical fire or something you’d see a lot more like dirt in the flame, and it, I didn’t see any of that, so. R-168 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [President] : Now I know you didn’t smell anything when you had the mask on, or... you shouldn’t have. [MASE2] : Yeah, yeah. I was switching between the two oxygen masks when I… took in some of the smoke and everything like that then. [President] [MASE2] [President] : But before, you didn’t notice any smell before someone said fire or anything? : No, no. I didn’t notice any type of smell or anything like that. Um. : And you were facing aft as well, correct? [MASE2] : Yeah. Yeah. And then when they did say fire I was going through, um, my checklist because we also, because the aircraft was, we kind of stayed on the taxiway for a little bit before we got on the runway, uh, because we were waiting for clearance and things like that. Um, and the aircraft was getting a little war, bit warm. So we didn’t run our pre, our taxi, our taxi checklist yet because the aircraft was getting hot. And I have a JTT and things like that back here, um, which would be in this, um, which sits about like right here, is the JTT. Um, which is sib, I don’t, uh… [President] [MASE2] [President] : I don’t know what a JTT is. : Yeah, um, it’s, it’s a data link. : Okay. [MASE2] : Um, for sib. But the JTT terminal is right here and typically it has a blower and everything on it, which, um, heats up the aircraft a lot quicker. Um, and the aircraft was getting pretty hot. And actually, another interesting thing too, I just remembered, our ACE 3 while we were doing our, our, um, during our taxiing and everything, he was getting some interesting readings but I don’t think, I think it was more in the processor rack than back here, but he was getting like, like 2000 degree temperatures or something like that, and so he thought it was an issue with the ECP which is the, um, the system that kind of monitors temperatures. [President] : And you say that was the ACEs 3? [MASE2] : ACE 3. He, he monitors all of the cooling on the aircraft. Um, and on ECP which is the processor that displays all those temperature readings, he saw like some weird reading. I, I’m not sure if it was like 5000 degrees but I know it was like really, we were all like ah, that’s weird, maybe if aircraft’s hot and he’s like I’m going to restart the processor and see if that fixes the issue because sometimes that happens. And so, and he was like, yeah, I would hold off on turning on your guys’ equipment just because of the temperature is so hot. So, that’s when we held off and we were like okay, I’ll start the JTT up when we take off because we had enough time for the JTT, it takes 15 minutes for it to go through its bit tests and everything, that before we got to the box, so I was like I’m cool with waiting on that. [President] : So then you did not turn the JTT on at all during… [MASE2] : I did not. If I did turn the JTT on I might, I might have gone back there and maybe seen something, but I, I didn’t turn it on because of the temperatures. R-169 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [President] [Pilot Member] [President] [MASE2] [President] [MASE2] [President] : Okay. Anything else? : No sir. : Do you have anything else that you can think of or interested to tell us? : No. : Okay. : That’s it. : Okay. [Pilot Member] : If no one has any further questions we will now conclude this interview. I’d like to remind you again, that you are not offered a promise of confidentiality and that your statement is not protected and will be released to any follow on investigation of this mishap, and may be releasable to the public subject to the Freedom of Information Act. We request to you, correction, we request that you refrain from this discussion, your testimony, and any information shared with you today, regarding this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [President] : Very good. Thank you. R-170 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 R9.4. SIB NON-PRIVILEGED INTERVIEW – 18 MAY 15 SIB Interview of SrA Role: [MASE2] Airborne Systems Engineer 2 343rd Reconnaissance Squadron Interviewers: (President) (Pilot Member) Date: 18 May 15 [Pilot Member] : This is a non-privilege interview with [MASE2] being conducted on 18 May [Pilot Member] 2015 at 1010 local by for the safety investigation board convened for the recent mishap. We’re investigating this mishap involving a RC-135V that occurred on 30 April 2015. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent reoccurrence. A promise of confidentiality is not being extended to you. Your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [MASE2] : Yes. [Pilot Member] : For the record, would everyone present introduce-introduce yourself by stating your name, rank, and affiliation with the board starting with the witness. [MASE2] : Uhm my name is [President] [MASE2] : Okay, Colonel , Senior Airman uh and I’m ASE2 on the RC-135. , Board President. [Pilot Member] : Captain , Pilot Member. Welcome back. So uh just a couple quick questions just to clear you up, then we can get you out of here. [MASE2] : Okay. [Pilot Member] and [MASE3] : Uh after your previous interview, I did have one question. You guys; as in you said something about refilling an oxygen bottle. [MASE2] : Okay. Yes, yeah uh so we had to refill some oxygen bottles, but that was before when we were pre-flighting the jet. So, uhm what happened was the jet just landed and then we were taking the jet, and AFE never came out and cleaned the oxygen masks or made sure the oxygen bottles were at the proper pressure and everything like that. And during our preflight uhm we had-where we had to check our oxygen bottles to make sure that they’re at 300 or the aircrafts pressurization; and so mine- I think, I’m not 100% sure but one of them was had no oxygen and the other one had like half-oxygen in it. So we checked those and then we did the standard procedure for zero oxygen in one bottle is ya know refill it three times then uh- and uh then it should be good; and we just refilled mine then I think it was. It was one of the two we had in there but yeah we had to refill some oxygen bottles so- in the crew rest area. [Pilot Member] [MASE2] [Pilot Member] : Okay. Did you use the uh oxygen fill line in the crew rest area? : We did. : For both bottles? R-171 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE2] [Pilot Member] : Yes. : Okay. The one bottle that was half-full, you just filled it up to uh how much PSI? [MASE2] : It’s 300 or the pressurization of the aircraft- whatever it’s pressurized to on the aircraft then. [Pilot Member] [MASE2] : Okay. And the other bottle you did the uh: We filled it up, discharged it, filled it up, and discharged it three times. [Pilot Member] : Okay. Did you guys open up a T.O. for purging a bottle, or was this uh recalling from your training? [MASE2] [Pilot Member] [MASE2] [Pilot Member] : Just recalling from out training. : Okay. Uh do you know what T.O. system covers oxygen systems? : Which T.O. does? Uhh.. : Or more specifically, the ones that call for purging a bottle and then filling it up again. [MASE2] [Pilot Member] [MASE2] : I don’t remember off-hand, no. I’d have to look it up. : Okay. : I’d have to go into EPubs gold and figure it out, but yeah I don’t remember off hand though. [Pilot Member] [MASE2] : Okay. That is one of my questions. : Okay. [Pilot Member] : Alright, uh and now I’m going to ask you a question that’s specific to the flight that happened, and in general. You said before, that ASES have fight-fighting responsibilities. [MASE2] [Pilot Member] : Yes. : Alright. So, are ASES always designated as the firefighters? [MASE2] : It- They’re designated as the primary. So- primary firefighter for uh forward of the maintenance stations is going to be the ASE3 and then AFT of the maint station is either going to be- it’s going to be like ASE4 or 2. It’s typically designated during ya know mission planning or any.. pretty much whenever the AC designates it whose going to be the firefighter. Uhm typically it’s the ASE4 but I want to say- I said I’d take it on this flight so- it’s also because I’m closer to the equipment where I sit; it’s like right next to me- right here so it’s easier for me to do it, but uh otherwise if- if someone is closer to the fire, then it’s always ya know.. please don’t sit there and not do anything. Grab a- grab a uh fire-or a uh fire extinguisher and try to put the fire out, you know what I’m saying? Uh don’t sit there and wait. Try to- try to be- try to react to that situation in the appropriate way though- so. [Pilot Member] : Alright. On this sortie did the AC designate the firefighters, or did the TC designate firefighters? Or did no one designate it; it was just a uh implicit instruction? [MASE2] : I want to say- this one; the TC was getting his check ride; so I’m trying to remember right now. It was uh I want to say it was… Major was giving the evaluation to uh R-172 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MTC] I want to say for TC. And I think- I think what Major said was- He asked who wanted to be the firefighter after the maint station, and I said I’d do it just cause I’m closer to it, though. Uhm and then the ASE3 was it, but he also said ya know if there is a fire ya know one of the ravens will get it because they’re closer to the firefighter equipment; because the firefighter equipment for forward of the maintenance station is in the uh flight deck. So[Pilot Member] : Okay. Was the designated during the mass crew brief, or was the a CMC crew brief where that was asked? [MASE2] : It was during the mass crew brief. So, yeah. [Pilot Member] : Okay. Do you know of any regulation that stipulates who has to fight fires, or who has to- if they need to, designate firefighters? [MASE2] : Uh, no. I don’t- I know that in my check- on the ASE5 checklist is has me checking the firefighter mask to make sure it operates. So that’s typically why I always kind of become the firefighter because it’s also- I mean, even on the ASE2 checklist it had me checking the firefighter masks, so… on the ASE5 checklist, yes that’s the 2 and the 4 combined kind of deal but, since it’s next to my- where I sit all the time I always check it. I hook it up to oxygen and I hook it up to the microphone so I make sure I can talk and hear and everything too; during preflight. [Pilot Member] : Okay. Sir, that’s all the questions I had. [President] : Okay, I just have one question going back to the refill of the air bottles. You did that on the recharge stations that’s right next to the galley, right? [MASE2] [President] : Yes. : And that was before- that was when you showed up before the flight deck showed up? [MASE2] [President] [MASE2] [President] : Oh, we show up with the flight deck. : Same time? Okay. So how long is that before like engine-start? : Uh, about an hour. : Okay. And you- when you purge the oxygen bottle, you purge it right there at the station? [MASE2] : Yeah. [President] : and then refill, and then purge, and then refill and then purge, okay. Is that a normal practice you guys do a lot; are you comfortable doing those? [MASE2] [President] : Refilling and purging? : Yeah. [MASE2] : Yeah, I’m comfortable doing it but typically we don’t do that, though. AFE handles it and I know when we got out to the jet like all the oxygen masks were astray and everything and we were kind of like- AFE did not come out here and service this plane. And so the pilot- the AC, he called AFE and had them come out; and he was like ‘yeah we just didn’t have time just, when that jet landed and you guys came out, we didn’t have time to come out there.’ And so he told him to; ‘Hey, you’ve got time now so why don’t you start doing it now then.’ So I don’t R-173 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 know if it was- I- I don’t know if it got finished, or what. So but I mean based off my- my; when we get out to the plane and my preflight and everything I kind of made sure everything was kind of taken care of ya know in the crew rest area. [President] [Pilot Member] : Okay. I’m good. : Do you have anything else that you think? [MASE2] : Yeah, actually there was. So during our engine start we were having issues with engine two, and engine two wasn’t starting properly and so they were messing around with it, talking to ground maintenance, trying to figure out if- finally figured it out and uhm the engine started. But, I was talking to someone and they were telling me possibly there was like a line of something like that- gas or something like that that runs for engine two back there. So I didn’t know- I totally forgot to think about that ‘cause we were having engine two issues. So but, that’s about it… I’m trying to think of anything else. Nope, that’s it. That’s all I can think of. [Pilot Member] : Perfect. Alright. If no one has any further questions, we will now conclude this interview. I would like to remind you again that you were not offered a promise of confidentiality and that your statement is not protected and will be released to any follow-on investigation of this mishap and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony and any information shared with you today regarding to this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [MASE2] : Thank you. R-174 V, 64-14848, Class A, 30 April 15, AFSAS #739726 R10. TSGT mommy? (MASE3) R10.l. ISB NON-PRIVILEGED WITNESS STATEMENT 30 APR 15 Page 1 of 2 Non-Privileged Witness Statement (Date) I. l, 331?3 ,havebeenadvisedby (Name, Grade, Organization, of West) (Name of Investigator) a safety investigator of the mishap that occurred on Y3 involving if: 1'56" 2' 729,9 (Date) (Equipment 4! SN) This investigation is being conducted under the provisions of AH 91-204 solely for the purpose of mishap prevention within the United States Air ore: and to determine all factors relating to the mishap in order to prevent recurrence. i understand I am being interviewed as a witness in a safety investigation and acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. - [61; Name (List, First, MI) and Ran rude Elinor amt?F 343% 5442575! Dun) Title R-175 64-14848, Class A, 30 April 15, AFSAS #739726 Page 1 of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of AH 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. WITNESS STATEMENT OF: 3b Nam: (last, First, MD and Run Grade .- my 0/ch 293 as; Duty Title 19/ Reference attached document for witness account of event. This document is being emeredjbr accounting purposes and for witness ?3 acknowledgement of this being thefarln they should have received for completion of a written statement. Nae member is chair: of command will only review the ?nal mishap report if acquired through appropriate safety channels MW 91-204 para 3. 4. 5. R-176 V, 64-14848, Class A, 30 April 15, AFSAS #739726 NON-PRIVILEGED ESS STATEMENT Date of the mishap SQ 53$ IS . Crew position (as applicable) A 5g 3 Time you began duty ?5 l. l, have been advised by of the following: 0mm 1 This investigation is being conducted under the provisions of 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand being interviewed as a witness in a mishap investigation and I acknowledge that a promise of con?dentialtiy has n01 been extended to me. This witness statement may be released to the public pursuant to a Freedom of Information Act request. c, The chain of command will review the ?nd mishap report. Provide Ill account of Grit-hand observations of whet happened. a description of prevailing conditions. circumstances. and associated ?cuts (use reverse for continuation). SWINE as?. Jud, 0C Posh, \Nl'i?aA ?aw-1&8 jkoo'i?my of?? op rt rand Jar M-mwa, I *1 M1 *7 5'70 50 tau? "64? Mr? 50+. ew? r??m-Pt common) ER. in ?Hie. (L . 12% as abcr?tec}/ L33 "1 ?Maxim natal we Myth/4:: dean?er o? *b (has) *6 1? J31 balkv) 659? pew mm?h ?Hic ?ag, and; ?Bgib 5L 302A dur'b' ABA Ipcioiv w. mm com/F Mower 4w, .3er MS mm? or r? ?c?gmtpogh New ri? w'ni bL Josiain +5 ?to row a, rue mama? hm) ?Wen rte smut m4. pin-3? Net?s hula-Am 0.14? MQM ?Jam in? 415:COWegci'n Ska- ?re-Jam?. by.) M?sik d? 3-1? ?hadn?t? ?res} q;p\ Shr?pi M. 05 (03k Fare.? agar-mead ?The above atatem is unc to the best of my knowledge belief." Signed. R-177 64?14848, Class A, 30 April 15, AFSAS #739726 R102. 72-HOUR, NON-PRIVILEGED HISTORY 30 APR 15 72 HOUR AND 7 DAY HISTORY This investigation is being conducted under the provisions of AFI 91~204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. This form is being administered by an investigator from the interim Safety Board 088) or Safety Investigation Board (SIB). The statement you prowde will either be privileged or non-privileged applicable 91-204 guidelines. [21 NON-PRNILEGED i understand i am being interviewed as a witness in a satety Investigation and I acknowledge that a promise of con?dentiality has not been extended to me My witness statements may be utilized for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of information Act request This non-privileged 72 hour and 7 day history form be placed In Tab when complete PRIVILEGED i understand i am providing statement(s) for a safety investigation and acknowledge that a promise of con?dentiality has been extended to me by Investigating O?barprBoaId Resident This privileged 72 hour and 7 day history form will be placed in Tab when complete. This hour and 7 day history term is one of many tools the mishap investigator may Use to help determine the cause of this mishap. Your participation IS both critical and appreciated and may help prevent future mishaps. Please answer these questions to the best of your ability when you are not rushed or distracted. Be as speci?c and detailed as possible All answers address events prior to the mishap and recovery events. Today's Date: 3? APR Statement Completed By: (print) isignatur [Medical Member] BS or SIB investigator Administering This Form: (print) . R-178 64-14848, Class A, 30 April 15, AFSAS #739726 Aerospace Medicine Flight 72-HOUR HISTORY REPORT Please list the daily activities you did during the last 72 hours. Provide the times of events as well at the activity in the chronological order. It? you cannot remember the exact time ofthe event, provide the closest proximate time you can remember. DAY 1 (72 HOURS PAST) WAKE UP TIME: (What time did you Wake up? How many hours did you sleep? How many times did you get up? When you woke up, how rested did you feel?) {a ?2 mtg) TIME ARRIVED AT WORK: BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) 76?) ?(as omit MORNING ACTIVITIES: (List all the things you did, all food and drinks cansunwd) ACI- COM-Q LUNCH: (What time did you have lunch? List all food and drinks consumed) 13?, J4 .LL pockb AFTERNOON ACTIVITIE (List all the things you did, all food and drinks consumed) let oping, mm :53 TIME DEPARTED WORK: N07- m? ?all QINNER: (What time did you have dinner? List all fund and drinks consumed) 9 HM d?d?w? ?1f, "06?s maltr- EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) ?t?V TIME YOU WENT TO SLEEP: 2,25% ALCOHOL CONSUMPTION: (List all types. amount, and times consumed) Mo?s/E MEDICATIONS: (List all medications take, prescription and over the counter, dose and time consumed) Mo NC DAY 2 (48 HOURS PAST) NAME (LAST. SSAN: R-179 V, 64-14848, Class A, 30 April 15, AFSAS #739726 WAKE Ul? (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up, how rested did you feel?) dz, 3* mgr-{u} I AKBIVED AT WQBK: (37500 BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) Mm? d?d' coll-L/ pm?? 5m MORNING ACTIVITIES: (List all the things you did. all food and drinks consumed) #1 097102. m?L Ll INCH: (What time did you have lunch? List all food and drinks consumed) 333$ Choc-Law Lot-?f: Mr' un?t?, JiltLL AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) wit. my 25 MIL MK ?new, TIME DEPARTED WORK: [5'00 DINNER: (What time did you have dinner? List all food and drinks consumed) nadir" C0 r'rj EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) divided pea-cth Gr wait-v '2 5 Mus TIME YOU WENT TO SLEEP: [(9wa ALCOHOL CONSUMPTION: (List all types. amount. and times consumed) LIME MEDICATIONS: (List all medications take. prescription and over the counter. dose and time consumed) NAME (LAST. FIRST): R-180 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 3124 HOURS PAST) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? llow many times did you get up? When you woke up, how rested did you feel?) $256 5% raw TIME ARRIVED AT WORK: BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) P?D?mr? 9?34: I. New MORNING ACTIVITIES: (List all the things you did. all food and drinks consumed) WOW Hanna ?db ML LUNCH: (What time did you have lunch? List all food and drinks consumed) Ina)? paid?) ?Mgr Jump; AFTERNOON ACTIVITIES: (List all the things you did. all food and drinks consumed) omit Writ! alt-4? TIME WORK: DINEE R: (What time did you have dinner? List all food and drinks consumed) ?fnahcii?u olw-l? 00kg, writ? EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) +v (124an I TIME YOU WENT TO SLEEP: ?w ALCOHOL CONSUMPTION: (List all types. amount. and times consumed) NONE (List all medications take, prescription and over the counter. dose and time consumed) NAME (LAST, R-181 64-14848, Class A, 30 Apri115, AFSAS #739726 DAY 4 from? WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you gel up? When you woke up. how rested did you feel? (Cilia lw? :11qu AT WORK: 62? BREAKEAST: (What time did you have breakfast? List all food and drinks consumed) Clnqamn l?all'b MORNING ACTIVITIES: (List all the things you did. all food and drinlut consumed) def-t, I.th watrb LUNCH: (What time did you have lunch? List all food and drinks consumed) Why AFTERNOON ACTIVITIES: (List all the things you did. all food and drinks consumed) wd?er- Gd WQRK: DINNER: (What time did you have dinner? List all food and drinks consumed) We EVENING ACTIVITI ES: (List all the things you did. all food and drinks consumed) {37; 3.391..) TIME YOU WENT TO SLEEP: I ALCOHOL CONSUMPTION: (List all types. amount, and times consumed) Moog (List all medications take, prescription and over the counter, dose and tune consumed) P?bvwo? Mb d7}? leuwma "?6?th ARRIVAL TIME AT SQUADRON (If different than above): BRIEF TIME: [Lolql TAKE OFF TIME: (325? TIME: NAME (LAST. FIRST): R-182 V, 64-14848, Class A, 30 April 15, AFSAS #739726 23 JULY 200] 257 7 141m! HISTORY FOR AERIAL VEHICLE INCIDENT 7 The 14? day history is less detailed than the 72-hour histoxy. Please note any signi?cant life events that have accused over the past two weeks (example selected for promotion, death in funny, work, FLYING, mam?age dll?- malty, ?nancial di?culty, vacation/luv; Illness, eta). Include Ca?cine, Meds, Alcohol and Tobacco, exercise and hours slept RANK Q5: Mishap dayrDate 3Q AFC Ar, may?, Idayprim?tomishap: Dal: a AFK do? MIL 2dayspriono mishap: Date 23? ?r 6 h? ?at? 2 lul?L 3 daysprior to mishlp: Date AFC 7hr} 4 days priorto mishap: Date '1 k" #W?mhnb Pu?h? AF: 6 Ar; 400' Ag: 1? Jos?d IL 7:13 spriortomjshapzDate Ag 7/ V5. f? 64-14848, Class A, 30 April 15, AFSAS #739726 R10.3. SIB NON-PRIVILEGED INTERVIEW 11 MAY 15 Page 1 of2 Non-Privileged Witness Statement I P'Iot 1.1, )@,havebeenadvisedby '1 (Name, Grade. Organization, of We?) ?ame of Investigator) a safety investigator of the mishap that occurred on 30 :5 involving ng(Date) (Equipment SM n. This investigation is being conducted under the provisions of AF I 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I undde an being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Eva, Name (Last. ?rst. M1) and Ra ra lime (MP 313 (3 575%? Duty Title 0L R-184 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 Aircraft Diagrams RC-135 I PLOT COMPAHTMENT - FWD NAWGATOR STATION STATION n' I Mm" CHEW MEMBER 1-19 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of TSgt Role: [MASE3] Airborne Systems Engineer 4 343rd Reconnaissance Squadron Interviewers: (Pilot Member) Date: 11 May 15 [Pilot Member] [MASE3] : This is a non-privileged interview with being conducted on 11 May 2015 at 15:15 local by for the Safety Investigation Board convened for the recent mishap. We're investigating the mishap involving an RC-135V that occurred on 30 April 2015. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap and in order to prevent recurrence. A promise of confidentiality is not being extended to you; your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidential- confidentiality has not been extended to you? [MASE3] : Yes I do. [Pilot Member] : For the record would everyone present introduce yourself by saying your name, rank, and affiliation with the board, starting with the witness. [MASE3] [Pilot Member] : Uh, , uh, the ASE 4 on the RC-135 mishap crew. : And Captain , Pilot Member. [MASE3] how you doing today? [MASE3] : Good. [Pilot Member] : Good. Well good. Well uh tell you what, why don’t you just give us your recollection of uh the mission and pertinent information as you see it. [MASE3] : Ok, um, showed up to the squadron approximately um 3:15 or so, we had a 3:30 brief I believe it was, uh, no problems there. Went through the brief, uh no abnormal questions, anything out of the perp- or out of the ordinary, um, still some questions regarding the mission that we were joking about as far as timing and what was goin’ on but nothing non-standard that we hadn’t seen before. Um, I got on the bus with the front-end crew after checking out my tool kit, um, rode around on the bus to the, um ISS to pick up the rest of the ASEs and then off to base ops to pick up, uh, the rest of the required COMSEC materials. Uh- bus took us then to the jet. Uh, this is approximately, I don’t know, had to have been 16:30, 16:45ish, uh, got on, cleared the forms, uh – actually take a step back we were on the bus and were making several jokes about it because we were getting ready to go into an 8 and a half hour mission and our lavatory was broken. Uh and nobody seemed to think that uh that would be a fun day. Uh, that being in the evening as well. Uh we got cleared onto the jet, dropped off all of our stuff, loaded the software, got cleared power by the uh ASE 1 and ASE 3, and began the preflight procedure, um, I ran through accomplished the preflight with no, uh, no indications of any problems or anything like that. Um, approximately 30 minutes to 45 minutes later the uh OPS showed up on board. R-187 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 Uh, at that time, after all the operators got on board, uh I made the decision to deviate from my checklist, uh, and I turned on the refrigerators, in the aft compartment, to make sure that everyone would have cold lunches. Um, from there, we uh, ran through uh the rest of the preflight, got everything checked out, noted that AFE had not been to the jet, and found out that the jet had flown earlier in the day. AFE had not come out and uh done any of the inspection or cleaning the masks like we were supposed to so we had advised or talked to the pilot about having them called out. Uh, the pilot got AFE called out there, AFE said all they were gonna do is clean it, and we said ok that’s fine, we’ll let you clean it, and then he told us that uh they did not have the truck with the cleaning supplies in it. So they would come back. That point we all opted to uh take the alcohol swabs and clean our own oxygen hook it up and finish preflights. Um, nothing non-standard from then on out, uh, we pulled the air- the jet was rather comfortable temperature at the time. We pulled the air in the stand, the jet, uh started warming up as it does during uh a sunny day, um, it didn’t seem to get abnormally warm, everything was going well, um, started the engines normal, 3412, but when we got to engine number 2, uh, we ran into an issue, the pilots were trying to get it started, um, and they weren’t getting any indication lights, uh, they probably tried to start it 3 or 4 times or so before they called maintenance uh and then were speaking about a manual procedure of some sort. Um, the only thing I gathered from that is that it required them opening a cowling and locking something open or a pin or something to do with the engine number 2. Uh they tried this, managed to get all their indications and a good start on number 2, so and uh, we did our taxi report, uh , got the jet moving, um, from what I could feel it felt like we had wind all the way down to the east end, uh, we entered the runway down at the east end, back-taxied all the way up to the hammerhead, um, I’m sorry, before we even got a chance we taxied down to the east end of the runway and were stuck, uh, holding because of uh a clearance issue. Um, I guess the pilots were able to talk through getting us prepositioned at the end of the hammerhead and then we’d wait up there, so we took the jet uh all the way down the runway up to the hammerhead and then we held at the hammerhead. Uh, at this point all the ASEs were discussing temperatures, uh, based upon the length of our uh sortie as far as getting from the uh takeoff to the box and to the AR. We elected not to turn anything on further because the temperatures were rising, uh, they weren’t anything, again, nothing out of the ordinary, we weren’t seeing any super-hot conditions. Uh the only thing we seen was a possible faulty uh sensor indicator that was nowhere near the back of the jet it was actually located up in the front end near maintenance station um, but that being said we all felt that we had enough time in the 2 and a half hour drive that we could bring everything up and get good systems checks. We elected not to turn anything on. Um, bout this point the uh, the- aircraft was cleared, uh, to take off, we pulled out onto the runway, heard the pilot sa- s- sending uh calling uh for setting the breaks, power was applied, release the breaks, at that point looked up as soon as they released the breaks um didn’t really notice anything, craned my head around and ‘cause I haven’t said it I was sitting – typically I sit here, for access to my ETD, uh, during this day we had a raven that was sitting right here, and with 27 people on board, crew rest was quite empty, so the ASE 2 was sitting in this position, next to the firefighter’s mask like he normally does. I elected to sit one position back, feeling comfortable with everything that was going on that day, um, which now I wish I hadn’t been, um which did not give me good access to my ETD because I had to crawl over this seat. Uh I looked around, somebody nudged me, I looked around and after we started rolling, we noticed there was fire. And when I say fire I mean a pressurized torch shooting out over this area right here. R-188 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : Mhm [MASE3] : Uh just above where the microwave sits and the uh the containers um it wasn’t you know your typical campfire what you expect to see a fire where it was just kinda wafting – this fire was shooting out with force uh probably a good foot and a half, it was making contact with this this wire bundle up here where- the way it was shooting out. Uh at that point, uh I instantly noticed that I really was in a bad spot to sit cause I couldn’t get to my ETD. I called out over private to that we had a fire in the galley, um, at that, also going on at the same time I believe [MSSD] was making calls, uh, the operator sitting at 15 was making calls, it was a whole lotta clutter on the net, and uh each of the nets was just getting- everyone was getting stepped on. It uh, it was kind of frantic for a few minutes. Uh, the pilots recognized that we were that we had a fire, it was prior to S1, they stopped the aircraft, uh and at this point you know all throughout the time stopping I was told that we were doing 50-60 knots depending upon uh I don’t- I don’t remember exactly. Um, I remember sitting in my chair, doing everything I could to try and get cleared up and unbuckled to get the fire extinguisher uh and actually do what we were trained to do, um, because of the fire being here, we opted to get the extinguisher that sits overhead here[Pilot Member] : Mhm [MASE3] Uh just above the MRKs, uh we got the fire extinguisher down, s- s- soon as we stopped, we got the fire extinguisher down, ASE 2 was already putting on his uh, smoke and [MSSD] firefighter’s mask and we were working our way to try and do that. At that point the tapped us on the shoulder and told us we were getting off the airplane, kinda dropped everything that we were doing and started egressing the aircraft. Uh we all went out through the crew entry chute, up in the front, uh and at some point in time, everybody’d gotten off well and we ran into a bottleneck right in the middle of the aircraft here. Um and I guess the question came up and we talked about it afterward is to whether or not we should have abandoned. Um, I- I told, um Major and my feelings on it and they still remain the same is about the crew entry chute, I think that based upon how we seen things when we got off the aircraft if we’d have chose to abandon the aircraft the way we were trained and opening that aft hatch I think we would’ve vented smoke and caused a lot more problems. Uh I think the smoke back there uh was probably giving us time to be able to get into that bottleneck and not run into any further issues for us, you know, had we gone that route. Uh we got down the chute uh pretty expeditiously, lined up in the grass, off of the nose about 45 degrees on the uh pilot’s side of the aircraft, uh at that point we started doing our headcount and talking to the folks that were in the back of the jet [MASE2] as far as, uh, smoke inhalation. Uh I know myself and then , we were not slower to get our oxygen masks on, but we were trying to get multiple things done at the same time and uh him and I I think we were, uh at the time, ended up with quite a bit of smoke. Um, so when the [MSSD] medics came up they’d identified us, and then as well, um [MASE2 and I both were ] having a problem with uh, you know, taking deep breaths. It wasn’t uh, it was kind of like running on a cold day where it was just burning on the way out, they took us to uh, in the ambulance to the ER at Bellevue Medical Center there in uh on 370. Got an inhaler or a- uh, not an inhaler but uh- what do they call that thing a nebulizer, and that seemed to clean everything out. Um, they- we were then brought back in clear- with a clear bill of health and they prescribed an inhaler, if we needed it, and um we came back and started doing all the uh toxicology stuff. R-189 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] [MASE3] [Pilot Member] : It was a busy day. : Uh it was, it was a little more interesting than normal, that’s for sure. : Yeah. How do you feel? [MASE3] : Um, well I was probably useless to everyone Friday morning. I didn’t sleep at all Friday, um, or Thursday, well, Friday morning when we left at uh 2:30 I didn’t sleep ‘til I think probably Saturday so I was up for a good long time. Uh a lot of armchair quarterback in the situation. Everyone said don’t do that don’t do that just let it go and it’s a lot easier I’ve come to find out, particularly with this instance, it’s a lot easier said than done sometimes. [Pilot Member] : Uh, 27 people egress out of the aircraft. [MASE3] : Uh, and everyone’s told me that, s- 27 27 and I understand that but at the same time because 27 people did get off good I have the luxury of being able to armchair quarterback which is, it’s got its, uh, its merits and its faults all at the same time. [Pilot Member] : Yeah. [MASE3] : It just seems funny that uh you know this is I usually I will yell at operators to get out of my chairs and get away so I’m around the ETD and this is the one time it comes and bites you know? It’s like oh my God. [Pilot Member] : Well. That is, that’s one question I had when uh, when this came down. My first task was to figure out where everyone was sitting. [MASE3] [Pilot Member] : Mhm. : And I quickly found out there’s no seating chart, specifically. [MASE3] : No, not at all. And, as far as the ASE 4 is concerned, same with the ASE 2, there is no assigned you-will-sit-here, there is, you know, we’re back there. Um, you know, I’ve known guys who will sit on the other side of the aircraft just to be able to see out of the aft hatch because they like to see the world go by in reverse. Um, normally, like I said, I sit back there, facing my ETD where it’s in - within arm’s reach. Uh that one time I elected to move one chair back, which uh, I don’t think I’ll be doing that again. [Pilot Member] [MASE3] [Pilot Member] : Yeah. Well if uh, if you usually sit here: Mhm : Is the ASE 2 plugged into this- this same COMM panel? [MASE3] : No the ASE 2 is plugged in above the JAF rack it’s called the aisle maintenance, it’s in and around here and what we do is they’ll string the cord over the top of the aircraft and then back down to where he’s sitting here. So the ASE 2 at no point in time has access to his ETD, when we are[Pilot Member] : Ok R-190 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE3] [Pilot Member] [MASE3] [Pilot Member] : From the point when we decide to take off, beyond. : Well when you uh, when you push to talk, : Mhm : Does that go over on, over private or interphone? [MASE3] : So, based upon the ETD configuration, because it’s a multi-configurable item, uh you have the ability to do interphone, private, uh my current setup for that day, typically what I’ll do at takeoff is I have push-to-talk on private and I have maintenance on hot mic. [Pilot Member] : Ok [MASE3] : Uh and that is how I had it configured for that day. Mainly because if we do not have a SIGSOP or if our SIGSOPs falls asleep or whatever the case may be and uh if they’re caught up in something the ASE 4 is also uh, we share the responsibility of making the pressurization calls for the back end of the jet. [Pilot Member] [MASE3] : Mhm : And that’s a call that’s made over private, so like, that’s, typically why I leave it on private. [Pilot Member] [MASE3] [Pilot Member] : Ok. And when you say maintenance, you mean? : So yeah, the 2 up here, and then the ASE 2 and the ASE 4, as far as… : Ok [MASE3] : Maintenance. I mean, we all, collectively, if they call maintenance one person will answer for the group but it’s collectively all of us. [Pilot Member] [MASE3] : Alright so that’s where you were sitting, that’s where [MASE 2] was sitting… : Sir. [Pilot Member] : He uh, Blum was sitting there, he did have access to the firefighting equipment there, you’re sitting there, there was a fire extinguisher. [MASE3] [Pilot Member] : And there was no: Yeah [MASE3] : No chance we were getting that fire extinguisher. By the time the aircraft got stopped. So, when we noticed it, it was a very, uh, like I said very pressurized but it was a very bright orange it was a vivid flame as far as it was concerned. It didn’t look dirty in any way it was a uh you know if it were in any- any other circumstance it was a very pretty flame. Um but there was no smoke or anything else, um all you seen was flame at the time. It wasn’t until you know we’d all looked back the aircraft had come to a stop uh and I believe about, it had to have gotten into these lines up hereR-191 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : Mhm [MASE3] : Before it really started billowing out nasty, nasty smoke. Cause I remember looking at it, as I’m putting on my oxygen mask, going it’s not, there’s not, there’s no smoke back there[Pilot Member] : Mhm [MASE3] : It’s just uh, but by the time we got in our oxygen masks the aircraft had come to a stop, uh it was, the entire back end of the jet was so clouded with smoke that I couldn’t see [MASE2 ] and he was a foot and a half in front of me. As I’m trying to help him get his mask situated so he can – we can do what we’re trained to do. [Pilot Member] : Alright. How uh, how did you notice the fire first, did you see it? [MASE3] : Uh, so I’m sitting here, over the top of my head what you can’t see in this picture is the bunks that sit there. [Pilot Member] : Right. [MASE3] : So, sitting back in the chair a little bit, all you could see was a little orange over the top of it, so all I got for any indication initially for myself was I could see an orange color and that’s not something I was you know, used to seeing as far as, ok, it’s time to look around the corner and see – [Pilot Member] : Ok [MASE3] : Um, you know, and then, as far as odd circumstances, and I - things that I, as an armchair quarterback and things that I cannot explain or, or understand, I spend a good bit of my time looking at this thing, when we start talking about temperatures in the back of the jet. And granted that is a, it’s not the world’s most accurate t – thermometer, I’m guaranteeing, but uh that being said it does measure temperature back there. And at no point at time when I looked at that thing was it ever over 80 degrees. What’s more amusing is this is, pretty much a metal frame it’s sitting on, so there’s con- I mean it’s a good conduction source, as far as I would understand how things work for metal transfer you know heat transfer. And it never got above 80 so I don’t understand what you know, we looked at it quite a few times. Hey what’s the temperature back here, well, my thermometer says it’s 75, 76, 78 degrees back here. So I don’t- I don’t know, it’s kind of weird. And I looked at that quite a bit cause I’m not comfortable when I start sweating on an airplane. Usually makes it- means it’s gonna be a long day. [Pilot Member] : Yeah. Yeah. Uh, alright, I had a question about uh, yellow bottles, that sit underneath these chairs. [MASE3] [Pilot Member] [MASE3] : Mhm. : During preflight, do you guys check those things? : Yep. And uh, it’s, so the procedure is, that each person is responsible for his own oxygen. R-192 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : Right. [MASE3] : Um, I look at all of them, uh throughout the flight, or rather – I – I – I don’t trust the operators, I’ve had them run into some problems before with turning on and off oxygen regulators and not knowing that they’ve put it in emergency setting and leaking that oxygen. [Pilot Member] : Mhm. [MASE3] : So I make it a point to check all of them. Uh, we did notice that there was, when we first got out there this bottle underneath what would be my seat and the bottle underneath what would be [MASE2 ’s seat, um, his bottle was over pressurized as far as what we’re used to seeing the ] bottle indicated something close to 400. [Pilot Member] : Really. [MASE3] : Typically the – we – we see these things at 300. They’re pressurized I mean I don’t see the – the crew chiefs or anybody taking it off the jet normally we just use the jet to re- to purge them and go. Uh, so we uh, elected to drop that fire bottle down and temperature to what we were used to seeing at that 300, uh just bleed it off a little bit. The bottle located underneath my seat was at 0, so [MASE2 and I made the decision, or uh, we talked about it, knowing that the ] crew chiefs were gonna come out there and do the exact same thing we were, we elected we purged it, we emptied it the 3 times, we filled it up 3 times, and on the 4th time after emptying it the 3rd time it fills up the fourth time to the aircraft pressure, no indications on it that it was leaking or anything else, it looked like basically somebody had kicked the regulator over on the bottom of it and put it into emergency or one of the altitude settings. Uh so we purged it and put it back on the jet. Or put it back into play. [Pilot Member] [MASE3] [Pilot Member] : How do you purge a bottle? : Um so the required procedures for us are, uh, we’ll connect to the filler port, here: Mhm. [MASE3] : Um, obviously if it’s at 0, uh, it’s good to go from there. Uh, plug it in, fill it all the way to the top, empty the bottle completely, plug it in, fill it all the way to capacity, pull it off, empty it completely, and do that a third time, filling it up, and emptying it. And after the third time, the bottle is considered purged, we’ll fill it up, and plug it back underneath the seat. And that is uh, that is our procedures for purging it. [Pilot Member] : Ok, so, all 6 bottles, or, sorry, not 6, it would be 8 in this case- [MASE3] : All of them were at, aside from [MASE2 ’s and mine’s, so these 3 here, uh, so 3, 5, 6, 7, ] and 8, 9 of them were all at the normal settings. [Pilot Member] : Ok. And the one that you purged and refilled up would be under a chair you usually[MASE3] [Pilot Member] : Usually : Sit at. R-193 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE3] [Pilot Member] : Yes sir. Sitting underneath the chair I usually sit at. : Ok. Alright. So that was. So they were all good bottles. [MASE3] : Uh, yes, as far as we could tell there was – we purged it and when we filled it back up it didn’t drop in pressure it was holding just fine. [Pilot Member] : Now, I’ve been- I- I’m a pilot. Alright I speak pilot. I uh. And quite honestly your checklists, make my head hurt a little bit. So when I looked at the crew positions, there were ASE 1, 2, 3, 4, [MASE3] [Pilot Member] : Mhm. : And I came across an ASE 5 checklist. [MASE3] : So, for baseline 11, because the RJ is going to a consolidated base ASE 5 position is a combination – combination, I’m sorry, of the ASE 2 and the ASE 4. Basically the ASE 2 and the ASE 4 will no longer be qualified on different systems, we will be qualified on both sets of systems and be known as an ASE 5. Uh that being said, there are very limited ASE 5s out there. However when they built the baseline 11 checkli- checklist it was built based upon knowing that we were going to become ASE 5s. So rather than building an ASE 2 and an ASE 4 checklist separately, they built an ASE 5 checklist that we both run. And uh the way we currently split that up is – and and the way that [MASE2 and I arranged for that day, it’s basically a uh, just a ] cross-talk of us two. Because he is qualified as the 2. He runs the checklist down the copilot’s side of the aircraft[Pilot Member] : Mhm. [MASE3] : And basically hits all the breakers on that side, and then I hit all the breakers on the uh pilot’s side of the aircraft. Uh but the ASE 2 and the ASE 4 share- or, run the same checklist. He just does the applicable steps that are down that side of the aircraft and then I do the other side. [Pilot Member] : Alright. [MASE3] : Uh, until you know, when we get more qualified ASE 5s out there I guess the goal is you could do either or but since neither him nor I qualified that way, I just stick with my systems he sticks with the ones he knows. [Pilot Member] [MASE3] [Pilot Member] : Ok. If you had to, could you guys swap duties? Cause it is ASE 5 qualification. : Um not currently because neither him or I are qualified as an ASE 5. : Ok. [MASE3] : That ASE 5 checklist is in lieu of an ASE 2 and an ASE 4 checklist. We just, it’s part of our uh, baseline 11 upgrade. We run through, we go through and identify all of the differences and then we also talk about the checklist and go ok, these are all the things on your side of the aircraft. R-194 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : Yeah. [MASE3] : Basically um, you know, and he- he will not take care of any extra systems on there that aren’t his, he may push a breaker to it but, you know, as far as it goes I’m still responsible for the system as a whole, you know, fixing it and such. Uh, but, during the uh, um, what do you call it, the difference training, you get a pretty good working knowledge of ok you’re pressing this button, this is what it’s doing. Uh but there is no ASE 2 or ASE 4 checklist that is exclusive on the baseline 11s. [Pilot Member] [MASE3] : Ok. Sounds pretty confusing. To me. : It’s one of those things that I guess you know you’ve gotten used to now. [Pilot Member] : Yeah. So. On a baseline 9 and baseline 10, it’d be the ASE 4 responsible for the pilot’s side of the aircraft. [MASE3] : Um, well, so on a baseline 9 and 10, it kind of goes back and forth. I own all the systems for the OPS 15 and 16, the QRC stuff, I own a lot of stuff in the compartment and the tail compartment when it’s installed, uh, I’m responsible for panels over here, and then down this side. But typically the ASE 2 is responsible for breakers on the forward and aft overhead, uh they have breakers that they touch on the aft left hand circuit breaker panel, um I’m responsible for the aft left hand circuit breaker panel as well as far as breakers and galley, there’s a lot of overlap when you look at the 2 and 4 checklists just because they have radios that are on the aft left hand [Pilot Member] : Mhm [MASE3] : And I’ve got QRCs that are on the aft left hand, uh, but I typically touch all the stuff on this side here as far as receivers and such. [Pilot Member] : Ok. [MASE3] : And then they handle, it’s kinda how we broke it up for the 11 anyways, the majority aside from a couple of boxes, a couple of breakers, the majority of the ASE 2 stuff is on this side and the majority of my stuff is on that side anyways. Uh so basically all we traded off was instead of him coming back here to turn on his radios he now turns on stuff in the SSD racks so I don’t have to touch that side and I turn on stuff for his radios back there. [Pilot Member] [MASE3] : Ok. Uh, when looking at the galley specifically: Mhm [Pilot Member] : Is it a uh, you know it was a deviation to have it turned on? You – did you turn it on or was it turned on from the previous crew? [MASE3] : Uh, I turned on the galley. I turned on only the – so the MAC galley circuit breaker panel which controls this- basically allows power to come to here – [Pilot Member] : Yep. R-195 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE3] : And then I push the breaker in for the refrigerators. Uh and again so we’ve got a breaker on the aft left hand – or on the - I’m sorry – on the galley circuit breaker panel for the refrigerators, and the MAC galley is got a circuit switch, and then the b- the exhaust blowers for the refrigerator were already pushed in at the time. Uh and then I’m required to flip the master power switch that is located on the – the MAC galley control panel. [Pilot Member] : Alright. So the circuit breakers for the blowers were already on? [MASE3] : Yes sir and that’s standard. If the circuit breakers for the blowers are not in, the refrigerators will not come on. [Pilot Member] : Ok. So in order to turn the fridge on, they have to be in? They were already in because nothing tells you, pull them out again? [MASE3] : Um, no because when we kill the power to the switch that are on the MAC galley that also kills that. [Pilot Member] : Ok. [MASE3] : So, I know I’ve come on there a few times and seen that people have just pulled that and left the circuit breaker. Um off the top of my head, I don’t think that they’re in our checklist to pull the refrigerator blower circuit breaker because that switch covers those as well. [Pilot Member] : Right. [MASE3] : But uh, well, it’s been a while since I – it’s been a while since I looked at my checklist right now. Kind of got left on a seat and um I don’t know what happened to it afterward. You guys got it I guess. [Pilot Member] : Um, we might. Uh, now just curious, is it standard to turn the fridge on so people can keep their food cold? [MASE3] : So, yeah, it is a deviation. And this is something I’ve – I’ve gotten a lot of time to think about and play with as well. In my own head. It is a deviation however it is not a deviation – it is normal. I’ve seen – I have done it, I’ve been uh you know not to point any fingers I’ve been taught that that’s ok that that’s acceptable we watch the temperatures. Again it’s one of those reasons I look at the thermometer back in there, um there were no indications within the jet that it was getting too hot. Um but yes it’s, it’s – it is turned on, um, regularly. [Pilot Member] : Alright. Uh, since you check it, what was stored up here? [MASE3] : Um, I don’t normally check those cabinets up there, there’s nothing, we do not keep the jugs on board that would normally be up there. [Pilot Member] : Right. [MASE3] : Uh, typically I don’t even go through those cabinets, um the majority of the time I wanna say there are trash bags sometimes there’s paper plates there. Different things that get put up there. But I could not tell you what was up there that day. Uh, again, really the only people that ever open that up are usually about the OPS 16 or the AMS or the TC, because they’re R-196 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 usually digging in there for toilet paper and trash bags and I know that toilet paper and trash bags have been stored up there before. [Pilot Member] : Yeah. [MASE3] It’s just not one of those areas that uh I’ve even contemplated open up and looking into normally. [Pilot Member] : Right. Well. Uh. Hmm. I almost wanna have a picture of the circuit breakers for the galley. [MASE3] [Pilot Member] [MASE3] [Pilot Member] [MASE3] [Pilot Member] Um, they’re gonna actually be found in the ETMs. : Right. All fans’ circuit breakers pulled? Say again? : Right. Just once again, all the fans circuit breakers were pulled? Fan circuit breakers? : Sorry. For the galley? Uh. [MASE3] See the only fan system I’m aware of is the refrigerator blowers and those would have been running because we had the refrigerators on. [Pilot Member] [MASE3] [Pilot Member] [MASE3] [Pilot Member] [MASE3] [Pilot Member] : Right. : Uh I don’t know of any other fan circuit breakers that are involved with that as… : Alright, just the blowers then? : Yeah. The ovens we- the oven was still pulled, the microwave was still pulled. : They were pulled? : Yeah. : Ok. [MASE3] : And those do not get power from this panel anyways they get power from the aft or the uh galley circuit breaker panel. And all of them are out. [Pilot Member] : Cool. Where’s the galley get its power from? Is that from the 60 hertz over here? [MASE3] : Uh it’s the uh it’s the same thing. So the 60 hertz will feed into the galley circuit breaker panel right here, just above the aft left hand, so it’s this metal grating, the first one you can see. [Pilot Member] : Got it. R-197 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MASE3] : Uh, the 60 hertz feeds over there and then that is also a distribution source for all the 60 hertz in the aircraft. It goes from there to every panel in the jet, from there on. [Pilot Member] : Got it. Alright. That is all I had. You think of anything else that seemed abnormal, uh position? [MASE3] [Pilot Member] : No. : What were your thoughts on the egress? [MASE3] : Said, um, so, one of the hardest things to overcome about this one of the things that was bothering me most of Friday morning and into Friday afternoon is, A- how come we didn’t catch it sooner how come we didn’t have any indications on it and that – that brought me into some TOs and looking though things and I didn’t get a whole bunch of good answers on that. Cause I’m sure as you guys have found, this is probably the best picture you’re going to get of the galley because the ones that are in the TO’s are terrible. Um so that[Pilot Member] : Yeah. [MASE3] : That caused me some heartache- but the biggest thing I’ve run into is we spent a lot of time training, ok this is how you’re gonna get off the airplane. Which we did. We got off the plane. This is how you’re gonna run a checklist. Which we did. This is how you’re going to combat an emergency situation – which we didn’t. Because we never talked about what you can’t do as far as it’s a particular moment – when we were in flight there’s no worry about me not being released from my seat I can get up and go. When you’re at 60 knots and you’re rolling down the runway, locked to a chair, and there’s nothing I can do, so there was a lot of uh, I had a lot of grief over the fact that I couldn’t do anything. My hands were so tied and all I know – if the, if the back end systems are recorded I’m sure you can hear me yelling over and over again going let me out of my seat, clear me up clear me up clear me up because I can’t do anything from where I’m at. Even if I were sitting where I typically sit I couldn’t do anything from where I’m at, I need to get up and be able to do something about it. It’s very difficult getting my head wrapped around the fact that this situation was well beyond our control just because of the exact timing of it and everything else. And obviously, uh, you know, a fire in an aircraft is never good. But we had no ability to do what we were trained to do and we had to just get up and walk away from that. And as somebody that’s been flying doing maintenance in flight as long as I have, it’s very difficult uh being told here’s a problem. But it’s gonna continue to be a problem, just go away from it. And I troubleshoot, I like fixing things, this is what I do[Pilot Member] [MASE3] : Yeah. : And to be in that is kind of a crappy situation, as far as what you- what you’re used to do. [Pilot Member] : Well it sounds like you guys did some stuff beyond your training, like uh, [MASE2 ] recalls, having to lead someone out of the aircraft. [MASE3] : That was me, for the simple fact that uh, side … obviously we, he was putting on uh, uh smoke goggles, or uh, a firefighter’s mask which is full facial coverage. The rest of us in the back had- all I had on was the uh, the quick don. Uh which coincidentally that day, did not R-198 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 seal great, as, from what I recall. But I didn’t have anything on over my eyes. I was- here I’ve got a fire extinguisher in my hand, I’ve got a quick down- don on that the cable doesn’t long enough to get me where I need to go, and I’ve got nothing on and by that time we’d been filling up with smoke so I was using [MASE2 , I put my hand on his shoulder because as we got up here it ] was perfectly fine getting up and egressing. When we got to this bottleneck up here, we were stopped and I don’t think it- I don’t feel we were in any sort of imminent danger but I put my hand on his shoulder because my eyes were starting to dry out and they were irritating me so I was rubbing my eyes and I was using him as my place marker as far as ok, if he moves, I need to get my fingers out of my eye so I can move forward, so I don’t – be rubbing my eyes and look around all the sudden I’m the only person left on the airplane. [Pilot Member] : Yeah. [MASE3] : So I was using him as my, ok, thi-, alright we’re moving again, let me open my eyes up and look out just because tha- that stuff was drying out my eyes really quickly and I’m sure the- between the adrenaline and everything else, you know, it was getting irritated. So yeah, I was using- I was using [MASE2 as my place marker as far as, ok it’s time to start walking again. ] Uh, it worked out good. [Pilot Member] [MASE3] : See? They didn’t train you to do that. So. : Right. [Pilot Member] : Well. That’s uh, that’s it. That’s everything I had. That was uh, that was a fast action from what everyone has said. [MASE3] : Yeah. It really was. You know. From start to stop it didn’t take nearly as long as I’m sure we all played it out in our heads to. Definitely interesting. I don’t think I wanna – I don’t think I need to be recurrent on that anytime soon. [Pilot Member] [MASE3] : Yeah. Uh- tell you what I’m – I’m done. So. If uh, if you don’t have anything else, any questions, I can read the rest of the script and get you out of here. [MASE3] : Alright sir. [Pilot Member] : Alright. If no one has any further questions we will now conclude this interview. I’d like to remind you again that you were not offered a promise of confidentiality, and that your statement is NOT protected and will be released to any follow-on investigation of this mishap, and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony and any information shared with you today regarding this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [MASE3] : Sir. R-199 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 R10.4. SIB NON-PRIVILEGED INTERVIEW – 18 MAY 15 SIB Interview of TSgt Role: [MASE3] Airborne Systems Engineer 4 343rd Reconnaissance Squadron Interviewers: (Board President) (Pilot Member) Date: 18 May 15 [Pilot Member] : This is a non-privilege interview with [MASE3] being conducted on 18 May [Pilot Member] 2015 at 1110 local by for the safety investigation board convened for the recent mishap. We’re investigating this mishap involving a RC-135V that occurred on 30 April 2015. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent reoccurrence. A promise of confidentiality is not being extended to you. Your statement can be released to any sub-subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [MASE3] : Yes. [Pilot Member] : For the record, would everyone present introduce yourself by stating your name, rank, and affiliation with the board starting with the witness. [MASE3] [President] [MASE3] : : Colonel [Pilot Member] : Captain just a few questions: [MASE3] [Pilot Member] [MASE3] [Pilot Member] , and I was part of the mishap crew. , Board President. , Pilot Member. Welcome back, [MASE3] . So uh : Okay. : Uh in a previous interview, you talked about refilling an oxygen bottle. : Yes sir. : I’m just hoping you can tell me more about that. [MASE3] : Uhm so we got on board and for that the uh the yellow walk around bottle that we use underneath my seat was completely empty. Uh we pulled the oxygen bottle out uh and there is a refill port located on the forward side of the galley that hangs down just in front of here. Uh we utilized that. We- the container was already empty uh we checked all the settings on it to uh make sure there wasn’t any uh blatantly obvious problems with the uh bottle itself; uh donned our gloves as per ya know the procedures for us, hooked it up and started the purge process. Uh again that involves uhm filling the bottle to the aircraft pressure, approximately 300 PSI, and then completely emptying the bottle uh three times. Uh we went through that process uh the bottle held the pressure each time and we made sure it wasn’t leaking down before we emptied it uh filled it, emptied it, filled it, emptied it uh three times and had no issues with it. Uh got it back on the last time; again there were no indications or problems with the bottle, so we uh put the bottle back underneath the stree- seat and strapped it down. R-200 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : Okay. Uh do you know what T.O. governs filling oxygen bottles- is that uh a T.O. that you fly with? [MASE3] : I am- off the top of my head I could not tell you. I actually have not even looked at that one in a long time. Uh but no, I do not know off the top of my head. [Pilot Member] : Alright. Is bottle-filling part of ASE training? [MASE3] : Uh as far as the purge procedures, yes it is- I cannot tell you if it’s actually on the tappers, the training records uhm off the top of my head. I know that it’s definitely discussed during the process of purging it uh and then as well uh we go over it because if the crew chiefs aren’t able to get out there, or if they’re taking their time because the crew chiefs are ultimately responsible for that piece of equipment. [Pilot Member] [President] : Okay. Sir, do you have any more questions about oxygen? : Uhm just real quick. Is it pretty common that you guys do this? [MASE3] : Uhm I have run into it so i have been back at Offutt since January. I think I’ve run into it three times in the course of maybe 25-30 flights. Uh the majority of the ones I’ve run into here recently have actually been bottles that were over-pressurized as far as what we’re concerned with; we look at the jet, we get on there and I view what uh what the each of the oxygen regulator panel says for pressure, and then I look at the bottles and if the bottles don’t line up with that then I assume it’s probably been filled off-site and it wasn’t filled by the jet and it was just filled too far. So I’ve drained them down before to what we feel comfortable looking at uh but it’s still within uh ya know- over-pressurized is just what I’m comfortable seeing the jet versus the bottle. Uh as far as ya know filling them up uh I haven’t run into too many times where I’ve had to purge it uh maybe three times out of twenty. [President] : Okay. So do you know if other people- is it fairly common for other people to fill it on the plane? [MASE3] : Uh I know we’ve run into it a few times- I’ve ran into it quite a few times during training where we’ve had- like okay it’s going to take this long for the crew chief to get up here and do it, let’s just do it. Uhm ya know I- I wouldn’t say it’s a hot item we talk about, but obviously if it comes up it is a discussion point. [President] [Pilot Member] [MASE3] [Pilot Member] [MASE3] [Pilot Member] : Okay. : Alright, I’d like to move onto firefighting. : Okay. : Uh in the crew brief, is that the time that someone designates a firefighter? : Yes Sir. : Alright during the mass crew brief or is there a separate CMC crew brief? [MASE3] : Uh typically the uh- it’s either conducted uh- the primary point is that we’ll conduct it the day before the flight uh as part of the mass crew brief uhm and obviously the intent is to get as much of the crew there as possible- there’s always a 1’s or 2’s that say ‘uh I’ve got an appointment’ or something like that. But for the bulk of that I’d say we’ve got 99% of the crew there. It’s briefed then by uh typically the navigator will hit it or the TC will it is as part of their R-201 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 briefing; saying ‘okay, my primary firefighter up front is going to be the ASE3 with the Raven1 backing up. The primary firefighter in the back is going to be the ASE2 or the 4’ depending upon uh ya know each TC kind of does it differently. Ya know we lean kind of in the direction- of the school house leans in the direction of the ASE4; uh the 338th leans towards the ASE4 being the primary firefighter. Uh the 343rd in all the briefings I’ve been to they typically reference the ASE2 and I believe that’s having to do with the fact that the ASE2 as part of his preflight- to preflight the uh firefighters mask. So it kind of makes sense. And then as we typically would sit in the aircraft the ASE2 is closest*Door opens*(Random interruption): Oh, I’m sorry. [MASE3] : So the ASE2 is typically closest to the firefighting mask as it is, so that’s what they do. [Pilot Member] : Okay. Is it written down anywhere who has firefighting responsibilities in any of the T.O.s? [MASE3] : Not that I’m aware of. We just designate one, and then per our checklist- at least for the Baseline 11 models, the ASE5 checklist outlines that one of the two ASE5’s will preflight the firefighting equipment but it does not specify one versus the other because the checklist doesn’t really differentiate between one of the two ASE5s. [Pilot Member] : Okay. Do you ever practice firefighting drills on the aircraft? [MASE3] : Uhm I have- on an RC I’ve never practiced one. I’ve never ran into the issue, uhm I’ve had to dawn the gear before- I’ve done it through training where I’ve put on the firefighters mask and had to run through that process, uhm unfortunately its typically very low-impact as far as it’s not a crew concept when we do these things as far as training is concerned its typically me and an instructor; and the instructor goes ‘okay put on the firefighting’ alright, I’ll put it on- I’ll dawn it and then I’ll hook it up. Uhm we don’t really do it for time, like SERE would go ‘okay put on your anti-exposure suit on, go!’ and then they’d time it; we really don’t uh put that into practice. As far as firefighting uh this is- this has been my first experience with an open flame; I’ve had plenty of smoke and fumes uh but previous aircraft when I was on the gulf-stream they actually had a fire simulator they had where they would light a steel fuselage on fire, something in it on fire get the fire extinguisher and the smoke mask and go, go put the fire out. But uh ya know never on an RC. [Pilot Member] [MASE3] [Pilot Member] : So the gulf-stream is a C-37, right? : Yes sir, sorry. : So uh, on C-37 did you practice in-flight? [MASE3] : Not in-flight like that. They uh didn’t really want us getting too far into it with uh ya know typically we didn’t fly a whole lot of trainers with the back-end crews. It was a DV onboard and I don’t think we would want to see us running around with smoke masks and such on. [Pilot Member] : Roger that. Uh and on the crew brief for the mishap flight, was it covered during the mission planning brief whose crew duties were in- emergency? [MASE3] : uh I’m pretty sure it was the uh- that was specified that the ASE2 was going to be the primary firefighter in the back of the jet, and then I was going to back him up. R-202 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] [President] [MASE3] : Okay. Sir that’s all the questions I had. : All good. : Okay. That’s all the questions we had. Do you have anything else you want to say, or? [MASE3] : Uh, no sir. [Pilot Member] : Alright, then we’ll conclude. If no one has any further questions, we will now conclude this interview. I would like to remind you again that you were not offered a promise of confidentiality and that your statement is not protected and will be released to any follow-on investigation of this mishap and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony and any information shared with you today in regards to this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [MASE3] : Sir. R-203 V, 64-14848, Class A, 30 April 15, AFSAS #739726 R11. 1LT (MR2) Rll.l. ISB NON-PRIVILEGED WITNESS STATEMENT 30 APR 15 Page of). Non-Privileged Witness Statement :12 39; (Dale) 1. at .have been advised by (Name. Grade. Organization. of Witness) (Name of In vestigatar) a safety investigator of the mishap that occurred 01130 a? 15 involving (d?i ?i833 Bil-139 (Date) (Equipment SM 21. This investigation is being conducted under the provisions of 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and my be released to the public pursuant to a Freedom of Information Act request 1 Li 2. Name (Lint, First, MI) and Rank/Grade Ei QI??hmic, \Mxr?y? ORR var Dutv Titlp Signature R-204 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Pagelof NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. 1 understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request WITNESS STATEMENT OF: (C. - Name (Last, Fir-st, MD and Rank/Grade Eled-ro Duh) Till:- otgnamre [Reference attached document for witness account of event. This document is being entered for acaountingpurposos and for witness 's acknowledgement oftht?s being the form they should have received for completion of a written statement. The member ?3 chain of command will only review the ?nal mishap report if acquired through appropriate safety channels IA 91 404 para 3.4. 5. R-205 64?14848, Class A, 30 April 15, AFSAS #739726 NON-PRIVILEGED WITNESS STATEMENT Date of the mishap 30 AEB \5 Crew position (as applicable} Roam/t . Time you began duty have been advised by - of the following a. 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Ol 15 R-206 V, 64-14848, Class A, 30 April 15, AFSAS #739726 R1 1.2. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY 30 APR 15 72 HOUR AND 7 DAY HISTORY This investigation IS being conducted under the provisions of AH 91-204 soieiy for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. ?his term is being administered by an investigator lrorn the interim Saiety Board (i381 0r Sater investigation Board (SIB). The statement you provide will either be privileged or non-privileged applicable AFI 91-204 gutdeiines. [Bl I understand i am being interviewed as 3 Witness in a safety investigation and i acknowledge that a promise of confidentiality has not been extended to me. My witness statements may be utilized for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. This non-privileged 72 hour and 7 day history form will be placed in Tab when complete [3 PRIVILEGED i understand I am providing statement(s) for a safety investigation and acknowledge that a promise of confidentiality has been extended to me by . In vestigarrng OITcer or Board President This privileged 72 hour and 7 day history form will be placed in Tab when complete This 72 hour and 7 day history form is one of many tools the mishap investigator may use to help determine the cause of this mishap. Your participation is both critical and appreciated and may help prevent future mishaps. Please answer these questions to the best ot your ability when you are not rushed or distracted. Be as speci?c and detailed as possible All answers address events prior to the mishap and recovery events Today?s Date: 36 [37? Statement Compicted By: (print) .(slgnature) [Medical Member] or SIB Investigator Administering This Form: (print) R-207 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Aerospace Medicine Flight 72-HOUR HISTORY REPORT Please list the daily activities you did during the last 72 hours. Provide the times of the cw ents as well as the activity in the chronological order. It' you cannot remember the exact time of the event, provide the closest proximate time you can remember. DAY I (72 HOURS PAST) WAKE UP TIME: (What time did you wake up? How many hours did you sleep'.? Now many times did yt get up? hen you woke up, how rested did you feel?) 0(03 0_ ,3 0 Ace, mi res TIME ARRIVED AT WORK: BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) 0373 Wino.) Qy??l A '5qu MORNING ACTIVITIES: (List all the things you did, food and drinks consumed) NU \Ni 'h?klni ?n Wail? ?l ?5 0? LUNCH: (What time did you have lunch? List all food and drinks consumed) on} loaf AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) 699 C1: wot lc TIME DEPARTED WORK: ?0 2 DINNER: (What time did you have dinner? List all food and drinks consumed) Om) romeset? EVEN ACTIVITIES: (List all the things you did. all food and drinks consumed) (Nah/lived ALCOHOL CONSUMPTION: (List all types, amount, and times consumed) Mm MEDICATIONS: (List all medications take, prescription and over the counter, dose and time consumed) ONE, DAY 2 (-18 HOURS PAST) . . . NAME Flash; R-208 RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get '3 hen you woke up. how rested did you feel?) OGDBU Luv-3 5 well. (GS a TIME ARRIVED AT WORK: 033 BREAKFAST: {What time did yon have breakfast? List all food and drinks consumed} aft 5 .m wide?! {Dru-lam MORNING ACTIVITIES: {List all the things you did, all food and drinks consumed) o-C?Slfq work. Lexalk?w? dewj LUNCH: [What time did you have luneh'! List all food and drinks 350(th jiwum 9-514va AFTERNOON ACTIVITIES: (List all the things you did. all food and drinks consumed] 0% a. WM lc TIME neme'ren WORK: {to 3 a DINNER: {What time did you have dinner? List all Food and drinks consumed) FMmeur EVENING ACTIVITIES: (List all the things you did. all fund and drinks consumed) TIME YOU WENT Tn SLEEP: ALCOIIUL CONSUMPTION: (List all types. amount. and times consumed} am? MEDICATIUNS: (List all medications take, prescription and over the counter, dose and time eonsumedl NM NAME (LAST. FIRST): ssaw: \wlm V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 3 (24 HOURS PAST) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? Ho? many times did you get When you woke up. how rested did you feelwatt ARRIVED AT WORK: 00(?5 BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) 0100 When! {Man WH MORNING ACTIVITIES: (List all the thin syou did: all food and drinks consumed) ?g use! mayo? ii LEWC H: (canal time did you have lunch? List all food and drinks consumed) Taco Edi ewes omit: AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) Miss; ov\ (Mam N3 TIME DEPARTED WORK: f] DINNER: (What time did you have dinner? List all food and drinks consumed) EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) wau?k?i' MNAA) TIME mu WENT TO SLEEP: (m3 0 ALCOHOL CONSUMPTION: (List all types, amount. and times consumed) MEDICATIONS: (List all medications take. prescription and over the counter. dose and time consumed) NW R2 NAMF. (LAST, FIRST): R-210 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY -I (TODAY) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up. ow rested did you feel?) 083%: ?313144;? hous- we ?Ki. (2,5 TIME ARRIVED AT WORK: (?30 BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) O?Loo (Nme shake. 431m? (and, MORNING ACTIVITIES: (List all the ?ngs you did, all food and drian consumed) guild, Moofift?c WW5 LUNCH: (What time did you have lunch? List all food and drinks consumed) (330 What! AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consnmed) [No/i4 TIME DEPARTED WORK: DINNER: (What time did you have dinner? List all food and drinks consumed) EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) TIME YOU WENT TO SLEEP: ALCOHOL CONSUMPTION: (List all types. amount. and times consumed) New (List all medications take, prescription and over the counter, dose and t' 2 ime consume a BRIEFTIME: ($30 TAKEOFFTIME: [97,7 NAM a (LAST. FIRST): R-211 V, 64-14848, Class A, 30 April 15, AFSAS #739726 AFPAM91-211 23 JULY 2001 257 7 KDAY HISTORY FOR AERIAL VEHICLE INCIDENT 7 The 14? day history {8 less detailed than the 72-hour history. Please note any signi?cant life events that have occurred overtime past two weeks (example selected for promotion, death in fhmily, work, FLYING, marriage dif?- Eulty, ?lnaucml dl?ioulty, vacation/leave, illness, etc.). Include Ca?'eine, Mods, Alcohol and Tobacco, end ours epL FULL NAME RANK L1 Mishap dayzDatei??nLLSprior to mishap: Date a g{ 8 Waugh-k ham 2 days prior to mishap: Date 25 259,- kw, Shep 3 days prior to mishap; Date 231 3?135 5? \M?s 5' ijk?r Mm 4 dayspriur tomishap: Dam-22 By ?3 he wd?m WA 5 days print to mishap: Date 3?16: ?3 W3 '3 \iLg 6 days prior to mishap: Date 23 3?s Mr; 12m 7 days?rior to mishap: Date Z?wc? - ?3 \n6 9W9 R-212 64-14848, Class A, 30 April 15, AFSAS #739726 R1 1.3. SIB NON-PRIVILEGED INTERVIEW 11 MAY 15 Page 1 of 2 Non-Privileged Witness Statement ll Ml?! IS (Date) I. l, l_ have been advised by Mew (Name, Grade, Organization, of Witness) Want: of Investigator) a safety investigator of the mishap that occurred on 39% involving l3 5 (Date) (Equipment SN) This investigation is being conducted under the provisions of AF I 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in orderto prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released in the public pursuant to a Freedom of Information Act request Name (Last. First, MI) and Rank/Grade Bed-mum wot: it? 0931? Duh! Tit)? Signature R-213 V, 64-14848, Class A, 30 April 15, AFSAS #739726 '7 Aircraft Diagrams R0135 VI 6? -- 0/ - comer L: . - NAVIGATORSTATION - swmow ?69? - ADDITIONAL cam men seamen I 1-19 R-214 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MR2] SIB Interview of 1Lt Role: Raven 343rd Reconnaissance Squadron Interviewers: (President) (Pilot Member) Date: 11 May 15 [Pilot Member] [MR2] : This is a non-privileged interview with , First Lieutenant, United States Air Force, being conducted on Monday, 11May 2015 at 13:50 local by Captain [Pilot Member] for the Safety Investigation Board convened for the recent mishap. We're investigating this mishap involving an RC-135V that occurred on 30 April 2015. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of confidentiality is not being extended to you; your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [MR2] : Yes, I do. [Pilot Member] : For the record, would everyone present introdu- correction: for the record would everyone present introduce themself by saying your name, rank, and affiliation with the board, starting with the witness. [MR2] : Alright, uh, , uh 1st Lieutenant, United States Air Force, uh, and I was uh, on the uh jet during the incident. [MR2] [President] [Pilot Member] [MR2] [Pilot Member] : Colonel : Captain , Board President. , Pilot Member. How you doing today? : Good, good. : Good. Alright if you could uh, just start us out, just telling us about uh the events of the day? [MR2] : Ok, um, so it - the pertinent stuff happened uh right on takeoff, um, I was sitting, uh in the uh far aft uh crew rest seat, uh, towards the wall in the corner there, um, when we uh, started our takeoff roll I was uh just kind of sitting there staring at the wall, um, and then uh, I heard I believe it was uh the OPS 16, uh the Chief, um and several other people probably all yelling fire, uh I actually didn’t see it first I just heard them first and uh then I kind of leaned over, um just to see, you know, if I could see where the fire was, and then uh – um, I- I saw it I think in – in this area, it was up high, uh, like, uh just above – above like where the uh oven and uh that storage compartment is. Um it looked like it was, I remember like an orange flame, um and it looked like it was – it was – pre- pretty, like a pretty pre- almost like a pressurized fire like it looked like it was uh uh very forceful, it wasn’t you know something that you know, started really small and – and grew it looked like it was just right from the get go it was a pretty strong fire, uh at that point uh everyone, you know, when they were yelling fire fire fire, uh, I – they were - pretty sure they were saying that on call, uh, ‘cause I heard it in my headphones, um, and then uh, I merely started getting my oxygen cause it started uh, the smoke started to fill the cabin R-216 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 pretty quickly uh, so my first instinct was just put on my oxygen, um got the regulator on to emergency, um and at that point it – we - the aircraft came to a stop, um we were just - I kind of waited til we uh - til I felt like the aircraft was at a stop, and then I unbuckled, and uh tried to get as far away from that area as I could, um, I- you know I - I considered the extinguisher there, uh but the fire was kind of in between me and the extinguisher, and it was right above kind of where it was so I just figured that probably wasn’t uh wasn’t a good option, cause I could you know I could get burned or something. So I – I just moved back as far as the oxygen hose would – would let me go, um, and there was a lot of smoke it seemed like it got really smoky very quickly, um, so I kind of felt like the oxygen mask was like my lifeline, I didn’t really wanna, uh, take that off. Um, to get farther away and, started considering the uh, the extinguisher behind me. I believe uh we had 2 ASEs sitting behind me, I’m not exactly sure where they were sitting, uh, on takeoff, I just know they were behind me, uh, I think it’s ASE 2 and 4, I believe. Um, and I saw them I think it was them, I don’t know, I saw a couple people, um, it looked like they were going for the – the firefighter mask um and possibly the extinguisher on the wall, um, so at that point I kind of was just standing as far away from the fire as I could and I’m just waiting to see, I don’t know if they were gonna like pass it up or what, I didn’t really wanna take off my mask and run over there. Uh, just cause it was so smoky, um, so we were kinda just, I don’t know – I – just trying to get low to the ground and trying to avoid as much of the smoke as I could. Just waiting, it looked like they were –I don’t know if they were having some trouble getting it off the wall or getting the mask on, it was kinda chaotic and uh, at that point, you know, all the lights went off, I think cause they killed the power, uh and then it just it seemed like fairly quickly after that we – uh - I heard the OPS 16. I didn’t hear anything in my headphones, I might have unplugged the uh – the actual audio in my headphones, um, or inadvertently, I’m not sure, but uh, I - I overheard I think it was the chief saying uh we can all go, just get off get off, uh so at that point I saw people start to filin- to file out towards the front so uh I took off my mask uh immediately, like, I – I probably should have held my breath or something but I mean as soon as I took my mask off I started you know coughing like the smoke was pretty uh, pretty thick and um but then as we uh kinda egressed out towards the front the smoke dissipated and um we were able to get off and that’s pretty much all that I remember uh happening. [Pilot Member] : Uh, how long before a fire response showed up? Do you remember? [MR2] Uh, from after we got off the jet? From when I remember standing off to the off to the nose of the jet and we were kind of watching it maybe a minute had gone by before it seemed like before the fire department got there. Uh, but yeah, I mean I feel like my sense of time might have been a little bit skewed though, like it just ‘cause of the adrenaline and everything, so. [Pilot Member] : Alright. Well then, just curious from the time fire was said to the time getting off the jet, I know your sense of time was skewed[MR2] [Pilot Member] [MR2] [Pilot Member] : Mhm. : Do you have any idea how long that was? : I: I know it’s, like, thinking back in time- R-217 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MR2] : Yeah I mean I would – it felt to me it felt like maybe, maybe 3 minutes from when it was first called, maybe 3-4 minutes from when I was actually you know at the crew entry chute, going down the ladder, um, yeah that would be my best – my best estimate, 3-4 minutes. [President] : Hm. When you uh, when you were sitting and you said you had to lean over, did you – cause you were the closest person to the wall – [MR2] : Mhm. [President] : You couldn’t see anything behind the galley, you didn’t – you had to look around to see the flames? [MR2] : Yeah I don’t – I don’t remember seeing anything right here. I - I kind of, from what I remember, I think it was in this area so I mean yeah I kind of I think I remember I don’t think I had to lean too far over but it was just kind of peaked my head over to the left a little bit and then immediately saw it, it was pretty large. [President] : And you couldn’t- before that, you didn’t hear anything, smell anything, see anything? [MR2] : No, no. Yeah that was the weird thing it didn’t seem like uh it didn’t seem like it started at something small and then grew you know as that’s kind of how I hear of most fires starting is you know you smell the smell something acrid or whatever but this one it just seemed like it caught us all by surprise and it was just immediately a large fire you know it wasn’t something that started, you know, really really small and then grew out of control. [President] : Hm. Did you feel any heat at all, when - once you- you were still strapped in when they came to a stop? [MR2] : Uh, I don’t remember feeling any any heat, no, um, yeah I don’t I don’t remember, I don’t recall that. [Pilot Member] [MR2] [Pilot Member] : Alright. Curious. Uh have you ever set - sat back in the rest area before? : Uh, yes, not in that seat, but I usually sit uh like one of the other rows. : Alright. When you sit back there, how do you guys determine seats? [MR2] : Uh, I think it’s just who - wherever you wanna sit. Uh, actually, we had 6 ravens on that flight, um and the instructor TC recommended I sit in the front because there’s an ET101 um up here and he wanted me to listen to the raven private[Pilot Member] : Ok [MR2] : Um which actually I couldn’t end up doing because only one, only the ASE 2 I believe his uh ETD 101 had raven private programmed in, so I ended up just plugged in to another one anyways I couldn’t even listen to uh raven private but that was why I was up in the very front. [President] : Ok. When you uh did your preflight did you notice anything with your oxygen, do you remember like was the oxygen pressures, were they normal were they abnormal, nothing out of the usual? R-218 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MR2] : Nothing was out of the ordinary I preflighted my oxygen like I usually do and uh nothing struck me as abnormal. [President] : What about the oxygen bottles underneath the uh, seat? [MR2] : Uh, I actually didn’t – didn’t uh check that, that’s- it wasn’t part of the part of our normal[President] : Mhm. Ok. [MR2] : Uh, checklist, to check that. [Pilot Member] : When you sit in the raven position up here, was there a bottle underneath your seat up there? [MR2] Yes there’s 2, there’s 2 bottles there, and that’s part of our – that - those bottles we do check as part of our checklist. [Pilot Member] : Right. So, you’re sitting here and the LAV is there – I’m curious. You smell anything from the LAV, did it smell abnormal? [MR2] [Pilot Member] : Oh, like, like sewage? : Yeah. [MR2] : Uh, I thi- I think it did, actually, I think they were saying that there was – a problem with the LAB, um. [Pilot Member] : But not enough to cause it smelling, um, out of the ordinary, or? [MR2] : I mean it was a little – I’ve smelled it that bad before, it was a little worse than than if I guess had they had completely emptied it out but I remember I thi- I’m pretty sure I remember the uh one of the maintainers saying that the the LAV was inop, uh, for it- it just wouldn’t flush, so. [Pilot Member] [President] : Ok. : Did you store your equipment anywhere in the back? [MR2] : No, actually I left uh I left all my equipment up in the raven compartment, um so all I had back there was just my paper uh baseline 11 checklist, um, and uh and my actual uh hardbound checklist. [President] [Pilot Member] [President] [MR2] [President] : Ok. : That’s it I don’t have anything else. : I don’t either. Do you have anything you wanna add or anything you can think of? : Um, nah I mean I can’t think of anything. : Not gonna sit back there anymore? [MR2] : Uh, [laughter] I mean, no, I, uh I’m fine with it, uh I guess uh I mean I would I would have some, I’d like to ask some questions maybe to the firefighters about you know uh as far as like if if we had opened like the aft hatch if that extra oxygen could’ve made the fire worse, and I don’t know I mean there was all these things kind of going through my head that uh they thought about you know I got to sit down and think about later and kind of wondering like R-219 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 Oh I wonder what would have happened if that – if we had just popped open the aft hatch and jumped out that way, but, uh, yeah. [Pilot Member] [MR2] [Pilot Member] [MR2] [Pilot Member] [MR2] [President] [Pilot Member] [President] : I’m curious have you ever gone down the crew entry chute before? : Uh it- just in egress training I think but that was it. Yeah. : Ok. : Not – not in real life. : Well, now you- now you’ve got two times. : Yeah. : Alright. : Cool. : Anything else? [Pilot Member] : No sir. If no one has any further questions we will now conclude this interview. I’d like to remind you again that you are not offered a promise of confidentiality, and that your statement is NOT protected and will be released to any follow-on investigation of this mishap, and may be released to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony and other information shared with you today regarding this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [MR2] : Alright. Thank you. R-220 V, 64-14848, Class A, 30 April 15, AFSAS #739726 R12. (MSSD) R12.1. ISB NON-PRIVILEGED WITNESS STATEMENT 30 APR 15 Page 1 of2 Non-Privileged Witness Statement (Dan!) I. 1, 54 W15 have been advised by (Name, Grade, Organization. of Witness) (Name of Investigator) a safety investigator of the mishap that occurred on 39 ?5 inVOIVing 13 5 69? (Date) (Equipment if: SM n. This investigation IS being conducted under the provisions of AH 91 ~204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiath has NOT been extended to me. b. My witness statements written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to The public pursuant to a Freedom of Information Act request Ch?l 5 Name (Last, First, MI) and Rank/Grade tovx ?Super . naexclevv?c Duh: Tilly. otgmmue/ R-221 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Page 1 of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of 91-204 solely for the purpose ofmishnp prevention within the United States Air Force and to detetmine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety inVestigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. WITNESS STATEMENT or: U?V?gi/f a Name (Last First, MI) and Rank/Grade Sidqd TOW lv?x?s?wule vki' UIGIOWOOI [Reference attached documem for witness account of event. This document is being enteredfbr accounting pin-poses and for wimess acknowledgement of this being lheform they should have received for completion of a written statement. The member '3 chain of command will only review lhe?nal mishap report if acquired through appropriate safety channels 1/1 91-204 para 3. 4. 5. R-222 V, 64?14848, Class A, 30 April 15, AFSAS #739726 NON-PRIVILEGED WITNESS STATEMENT . .- 1 Date ofthe Mishap &t . Crew posnion (as applicable) Time vou bmut dutv have been advrsed by . )f the followmg. a. Plus is being continued under the provisions of AFI 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. am being interviewed as a witness in a mishap investigation and I acknowledge that a promise of con?dentiality has not been extended to me. This witness statement may be released to the public pursuant to a Freedom of Information Act request. b. The chem of command will review the ?rm! mishap report. (2 Provide an account of tint-hand observations of whet happened, a description or conditions, and associated events (not reverse for continuation). Af?utd i?co 74004 ?Rd .s?sves Law! pr??rcd ?io ?32, V?a?Ol?N'o? ?Jhrpojk? fi?O?isQert-omxd. Tout. w?tik No ?rad +0 bent/$4? 0? :510/5'5 For v. Loot - . qt Q, .m t? tall-4, c. ?64 ??xed a; rekaik MOS a QHS gho?i our H1499 of 0? [Jo S'Ot/h or 4L: a? *he ordeinan Egg! 3? ?3 9r?c 9A I buffet-g +La. Cw: ?Hr-ecot?g 0t 7 over Tu, FIRM Ah?r Yew m; qu 0 kb ?OQb?j?h m; can?; 3: was? s: 3 RM very 06.4 ho?r was calm}, Drawleg-hi (one, m5 censor?! WAR 3?ka Van-i {Jopgdj'e?i qdca?ld Khmdevqo. I rammed and MI . ou-i a; ?Hue, 8(7th (cad 4 have, Mb a MIN jot}! KM, 53am? *6 Crew q? "The above statement is true to the bent of my knowledge and belief." R-223 V, 64-14848, Class A, 30 April 15, AFSAS #739726 R122. 72-HOUR, 7-DAY NON-PRIVILEGED HISTORY 30 APR 15 72 HOUR AND 7 DAY HISTORY This Investigation is being conducted under the prowslons of AF I 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap In order to prevent reCurrence. This form is being administered by an investigator from the Interim Safety Board (ISB) or Safety Investigation Board (SIB) The statement you provide will either be privileged or non-privileged IAW applicable AFI 91-204 guidelines. NON-PRIVILEGED i understand i am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has not been extended to me. My witness statements may be utilized for any valid purpose and be released to any subsequent investigation or this mishap and may be released to the public pursuant to a Freedom of Information Act request. This non-privileged 72 hour and 7 day llstory form Will be placed in Tab when complete. PRIVILEGED I understand I am providing statement(s) for a safety Investigation and I acknowledge that a promrse of confidentiality has been extended to me by Investigating Of?cer or Board President This privileged 72 hour and 7 day history form will be placed in Tab when complete. This 72 hour and 7 day history form is one of many tools the mishap investigator may use to help determine the cause of this mishap. Your participation is both critical and appreciated and may help prevent future mishaps. Please answer these questions to the best ot your ability when you are not mshed or distracted. Be as speci?c and detailed as All answers address events prior to the mishap and recovery events. Today's Date: 3 1? Statement Completed By: (print) (signati. [Medical Member] ISB or SIB Investigator Administering This Form: (print) R-224 64-14848, Class A, 30 April 15, AFSAS #739726 Aerospace Medicine Flight 72-HOIJR HISTORY REPORT Pleme list the daily activities you did during the last 72 hours. Provide the times of the events as well as the activity in the chronological order. liyou cannot remember the cum time of the event, provide the closest proximate time you can remember. DAY I 72 ST WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get When you woke up. how rested did you feel?) ., L- L) 87/ TIME ARRIVED AT WORK: (3201') BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) MORNING ACTIVITIES: (List all the things you did. all food and drinks- consumed) DU 0 r' LUNCH: (What time did you have lunch? List all food and drinks consumed) 7 ACTIVITIES: (List all the things you did. all food and drinks consumed) we [1 TIME DEPARTED WORK: A DINNER: (What time did you have dinner? List all food and drinks consumed) {5'60 .?sk {?gure EVENING (List all the things you did. all food and drinks consumed) l/ TIME YOU WENT TO SLEEP: a 3 0 ALCOHOL CONSUMPTION: (List all types, amount, and times consumed) Q'Yl?lzv" ?A/D-mwi MEDICATIONS: (List all medications lake. prescription and over the counter, dose and time consumed) DAY 2 {48 HOURS NAME (LAST. R-225 V, 64-14848, Class A, 30 April 15, AFSAS #739726 WAKE Ul? TIME: (What time did you woke up? How many hours did you sleep? Hjow many times did you get up? When you woke up. how rested did you feel?) ogm// (weed TIME Alum/ED AT WORK: 0 230 BREAKFAST: (What time did you have breakfast? List all lood and drinks consumed) (c \Bcw MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) Pun WQPK MUECH: (What time did you have lunch? List all food and drinks consumed) (goo 14k own, I fle Kol?euw AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) (N or? k? Wald WORK: (730 .g k. DINNER: (What time did you have dinner? List all food and drinks consumed) EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) PMde ml TV TIMF. YOUWENTTOSLEEP: 1150 5L, ALCOHOL CONSUMPTION: (List all types, amount, and times consumed) MEDICATIONS: (List all medications take, prescription and over the counter. dose and lime consumed) . [we we, NAME (LAST. FIRST): R-226 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 3 (24 HOURS PAST) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up. how rested did you feel?) 0500 5/9, WY Res-ted TIME ARRIVED AT #99 9330 BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) 06m ?L/Cereql MORNING (List all the things you did, all food and drinks consumed) TV/(luckg/ law, ma: LUNCH: (What time did you have lunch? List all food and drinks consumed) I300 /w44-?Y? (List all the things you did. all food and drinks consumed) WW TIME DEPARTED WORK: (7:70 DINNER: (What time did you have dinner? List all food and drinks consumed) . I . SUV-HWI 57?. Mt( g'll'we/ . . . . . OGAKWILILS c155 EVENING YITIES. (List all the things you did, all food and drinks consumed) I- )4 TIME YOU WENT TO SLEEP: ?f?O?S?e also ALCOHOL CONSUMPTION: (List all types, amount. and times consumed) H?hi beget THUG ?veij {amt Wood? MEDICATIONS: (List all medications take, prescription and over the counter, (lose and time consumed) Natu, NAME. (LAST, R-227 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 4 (TODAY) WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up, how rested did you feel?) 05 t? 5/9, (?fty Res?d TIME ARRIVED AT WORK: OQ BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) C7600 Doghmui/?epFee/Em an MORNING ACTIVITIES: (List all the things you did. all food and drinks consumed) Cluck/e)? TV LUNCH: (What time did you have lunch? List all food and rinks consumed) /300 sa 13?an 1L wcH-Lr AFTERNOON ACTIVITIES: (List all the things you did. all food and drinks consumed) wen-t 'f 0 54th? I) Oct 1400 TIME DEPARTED WORK: I) DINNER: (What time did you have dinner? List all food and drinks consumed) queem?ef 1+9 on ?Huz?cmo/ EVENING (List all the things you did, all food and drnil' Its consumed) F?anj au-f' ?to HOSP: qr TIME YOU WENT TO SLEEP: ALCOHOL CONSUMPTION: (List all types. amount, and times consumed) MEDICATIONS: (List all medications take. prescription and over the counter, dose and time consumed) ARRIVAL TIME AT (If minnow BRIEF TIME: 1539 STEP TIME: M30 IAKE on TIME: a5 TIME: 535 NAME sown; R-228 V, 64-14848, Class A, 30 April 15, AFSAS #739726 23 JULY 2001 257 7 WAY HISTORY FOR AERIAL VEHICLE INCIDENT 7 3h: M?dny history is less detailed than the 72-hour history. Please not: gay signi?cant life events that have ovatth pat:l two weeks (ample selected for promotion, death in family, work, FLqu [mu-iagc dim- . . . 81?nan ch?ic ty, vacuum/leave, Illness, eta). Include Caffeine, Mods. Alcohol and Tobacco, exercise and FULL NAME. - (ma-+88? Minbapdayznatc 309$?? mm. 5 Ms of She-9f ldaypriorto magma-E av? 1,542, ?04" ?ee-P Zdaysp?ormmismp;pamw: ?05? +0 6M5 5:999 +0 agJ me?P 4my8pdortomjshap;pw: ((032 +9 h?rs 0(5?669 5dly8p?ormmishapmate3?3AEx-IS: doggy? gh?s 0? Size, (x054 Mm mm? Q?Skfn?m Le, OF bee-3'5 CV4 no+ 7 days prio: to mishap: Date 7'1? (,0?st NH day 3 0" Wk?; R-229 64-14848, Class A, 30 April 15, AFSAS #739726 R12.3. SIB NON-PRIVILEGED INTERVIEW 11 MAY 15 Page 1 of2 Non-Privileged Witness Statement . (Blue) . 1 . I #5 1417;; have been advised by [m ?We? Wattle. Grade, Organization, of Witness) (Name of Investigatorsafety investigator of the mishap that occurred on mvolvmg 1, g~ (Date) (Equipment SM n. This investigation is being conducted under the provisions of AF I 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge theta promise of con?dentiality has NOT been extended to me. b. My witness statements (written 0r may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. wit/m Name (Last. First. MI) andRank/Gfade qu?tio? Super .rx?Le R-230 V, 64-14848, Class A, 30 April 15, AFSAS #739726 7, 5 Aircraft Diagrams RC-135 VI mm coupmwm f/ 29;. - - - ~rwn snmon - mmvnamonsramon Anomom cm men f? -r . Jun?? - - ix 1-19 R-231 64-14848, Class A, 30 April 15, AFSAS #739726 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of CMSgt Role: [MSSD] Signals Search and Development 343rd Reconnaissance Squadron Interviewers: (President) (Pilot Member) Date: 11 May 15 [Pilot Member] [MSSD] : This is a non-privileged interview with being conducted on 11 May 2015 at 1305 local by Captain [Pilot Member] for the safety investigation board convened for the recent mishap. We’re investigating the mishap involving an RC-135V that occurred on 30 April 2015. This inve- this investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of confidentiality is not being extended to you. Your statement can be released to, to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand the promise of confidentiality has not been extended to you? [MSSD] : Absolutely. [Pilot Member] : For the record, would everyone present introduce his self by saying your name, rank, and affiliation with the board starting with the witness. [MSSD] [President] [Pilot Member] [MSSD] [Pilot Member] : Chief Master Sergeant : Colonel [MSSD] . , Board President. : Captain , Pilot Member. How are you doing today, Chief? : I’m doing well, sir. : Good. So if, uh, we could just start off with, uh, the events of the day, uh, as you saw them. [MSSD] : Okay. Do you want me to start at pre-mission plan or step brief or prior to that or anything, uh… [President] : It’s really up to you, where you… [MSSD] : Okay, I’ll just start, uh, when I showed for, uh, at, uh, my place of work. So I showed up around 1400, a little bit before step time, uh, probably about an hour before step time just because it was a late show and you know, uh, circadian rhythms you know had kicked in and I was up. So, uh, I cleaned up some administrative work I had going and then I headed over to the 343rd for our step brief. Uh, all step, uh, indications were the jet was FMC ready to go, uh, and we, you know, there was nothing out of the ordinary, uh, expressed during, uh, the step portion. Uh, we, at that point the front end and the, uh, airborne system engineers, uh, they take a different bus and the back end crew goes back to the 97th to sort of wait for the bus to come back around and, uh, circle back around and pick us up, ferry us out at, to the jet. So there’s no, you know there’s not a lot of traffic for the ASEs to install discs and you know, uh, put… buil- boot the software and so forth. So, uh, we went back there, uh the, we waited about, uh, hmm another hour before the bus circled around at about 1630 to 1700ish. Um, when the bus came you know we, uh, headed out to the flight line, uh, nothing out of the ordinary. We got on, did our preR-233 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 flight checks, uh, uh, s- still nothing out of the ordinary. Um, we began to, uh, you now we started engines and there was a slight problem with, uh, the number 2 engine as I remember and, uh, they couldn’t get it to start, uh, so the pilot, uh, after a couple of attempts to you know get the, uh, motors to turn, or that motor to turn, uh, the pilot called down to the ground maintenance to see, uh, about doing a manual start. Um, the pilot, uh, ran through his checklist and then, uh, the ground crew opened the cowling to pin it, uh, I’m not 100 percent familiar, I’m not a pilot, but, uh, it all sounded, you know, uh, like they were running the checklist according, uh, to how they were supposed to, uh, accomplish this task. Uh, the motor successfully turned and, uh, the, uh, the ground crew buttoned everything back up and gave, the, the pilot the words that, uh, you know the aircraft was, uh, in taxi configuration. Uh, at this point still, nothing out of the ordinary going on. No strange noises, no strange smells, no strange nothing. Uh, so we taxied out, uh, to the, uh, flight line where we ran into another problem, uh, with our clearance. And that held us up for, uh, I want to say 10ish to 15 minutes. Uh, possibly maybe, maybe a little bit longer. But they got that all cleared up and we, uh, we lined up for, uh, for takeoff. Um, the, uh, you know, the, um, pilot pushed up the motors, uh, immediately when the brakes were released, or, you know, it was very tight timing there because he pushed up the motors and released the brakes and we went. But, uh, immediately at that point, uh, the, the flames, uh, started shooting over the top of the, and I’m referencing the picture here… [Pilot Member] : Okay. [MSSD] : for those listening to the recording. Started shooting over the top of the galley area here. Right, uh, I mean they were pouring out of here, uh, this whole area, um, I would say from, uh, we got these two compartments here, they were consuming the entire area over the top. Um, at that point, uh, a few people must have seen it, uh, because there was a lot of chatter on, uh, interphone. Uh, but they weren’t specifying where the problem was so the pilot really didn’t have any ideas, so I reached back, uh, and it’s kind of a cumbersome reach for me, because I have to go back, uh, to hit my call button. Uh, but I did, and that’s when I, uh, just spoke up and said fire in the galley, fire in the galley. And then I, uh, I went back, um, my initial indication, or, uh, reaction if you will, was to reach for the, uh, this fire extinguisher right here. However, at that point, uh, the fire had advanced so much into this, uh, this bundling of wires here, that, uh, uh, uh, the casings were melting, uh, and dripping down so I said that’s not a place I want to be. So at that point I, oh, sorry I should have referenced, I was sitting right here. [Pilot Member] : Okay. [MSSD] : So this is the area of the flames. And, uh, so at that point, uh, I didn’t feel that the, the jet was, uh, stopped, um, this stuff had started smoking, uh, I mean, uh, this is, we’re talking 15 to 20 seconds here tops. Uh, it was smoking very bad and filling up the, the, the aft area of the jet, uh, very quickly. Um, there was a Lieutenant sitting here. Uh, I can’t remember his name. [President] : [MR2] … [MSSD] : Yep, yeah it was a complicated one. Um, and then we had the ASE 4, Tech sitting here, and then the ASE 2, uh, [MASE2 I believe was sitting here, and then we ] had, uh, Sergeant , uh, operator sitting here. So, I turned around at that point to, uh, tell, uh, [MASE3 and [MASE2 , well I saw [MASE2 because the aft fire, uh, fighter’s mask is right by him. ] ] ] [MASE3] [President] : Mhm…. R-234 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MSSD] : So I was looking back and he was fumbling with that, uh, to get it into a oxygen source, uh, but it wasn’t hooked up yet, so that was kind of cumbersome. So, while he was doing that I yelled at [MASE3] here to get a fire extinguisher. Um, and, he was sort of in route but I couldn’t see him because I was looking this way and he was directly behind me. But he was in route to the fire extinguisher. Um, smoke is filling up very, very very quickly, um, and the fire, and the flames, uh, appear to be getting wor, I mean they were, uh, white hot flames coming out of there. It was, it was, uh, quite, uh, quite a sight to see. But, uh, at that point, I heard the, uh, the magic words over interphone come from the pilot, uh, to run the ground, uh, uh, emergency evacuation checklist. Everything, uh, we could not stay ahead of this EP. Uh, it was, uh, evolving too quickly. So at that point, uh, I grabbed the Lieutenant, I grabbed the people back there, and I told them in, uh, chief terms to get the, you know, heck out of the plane, and, uh, I started pushing at that point and, uh, I was, because, uh, by design I’m supposed to be the last one out of the back, uh, and tap the AMS and on the way. When I ran by the AMS I said, uh uh, you know, there’s going to be a chokepoint up here. Uh, I was already, I could already see it because you know going down the, uh, the ladder, uh, you know, it always ends up being a chokepoint when you’re trying to get 27, uh, you know, or plus folks off the jet. [President] : Mhm…. [MSSD] : Um, so I told the AMS hey grab the, uh, over wing hatch and pull it in so we have, uh, some relief of ventilation if you will. Uh, so, uh, he did that, uh, and I kept proceeding out of the jet. We egressed in, uh, a rather orderly fashion, uh, all, all things given. Uh, the only, you know, once I got up to where I could actually see again, uh, because, uh, by the time I was leaving this area I couldn’t see about 2 feet possibly, uh, in front of me. I mean, uh, it consumed the back end of the jet. Um, so much so that I didn’t even bother with the aft hatch, I just, I wanted to get the heck away from, the, the, the situation. Uh, so, we egressed orderly, got into the infield of the, uh, the runway, in the grassy area and waited for emergency responders, and, uh, that kind of sums up, uh, you know, and then the, uh, the emergency guys took over from there and that, that, really, uh, encapsulated, I mean, we, we could not stay ahead of this EP. Uh, it, uh, it consumed, uh, uh, the back end too quickly. So, uh, I think everything worked out as well as it could have, uh, which, you know, resulted in 27 safe, uh, you know, uh, safe egresses, so… [Pilot Member] [MSSD] [Pilot Member] : Yeah. : um, but, uh… : Everybody got off. [MSSD] Exactly, uh, but, uh, that was, uh, as I remember it and as I see it that’s uh, that’s, uh, that’s what I remember. Now, um, there was no sound, no smells, no nothing, no smoke to begin with, uh, you know, which is normally, you know, what happens first, you hear a pop or you know, uh, maybe a, that’s standard, you know, that I have had in the past for smoke and fumes and stuff like that, but, uh, this was just flames, uh, shooting out of there as soon as the, uh, no fumes, no, you know, no, of the normal noises you, uh, hear or smell, uh, when, uh, something like that happens, it was just the flames, straight over the top. And you know, uh, it’s like one of those, uh, uh, you know the ovens you see where they, you know, shoot, uh, flames out like a pizza oven, you know, where you can hear the, I mean it was just like that, just R-235 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 shooting right over the top of the galley. So, it was, uh, it was, uh, that’s the first fire I’ve ever been in and, uh, that’s enough. So… [Pilot Member] : Hahaha, yeah. [President] : Did you, um, see exactly where the source was or was it, could it, was it behind the compartment? [MSSD] Well, uh, my vantage point is from, oops, sorry, uh, is from about right here so I couldn’t s…, I couldn’t see anything back here coming this way. It was just pouring right over the top. [President] : The top. Okay, okay. [MSSD] : So, I don’t know, you know, this is speculation on my point, I don’t know if this line had to do with it, this ox line right here or what, but it was just coming, uh, it was, it was like this, it was shooting over the top. [President] : Could you tell what the, if, if the wire bundles here that are right above it, were those secondary to it? [MSSD] [President] : Those were secondary. Uh, they were… : So these were definitely not on fire? [MSSD] : They were, no they were definitely not. It was coming out from behind the, the galley area, over the top of the galley. And, uh, secondary is when the, uh, a lot of the insulation here, and I know by design it’s not supposed to burn but, uh, you get anything hot enough it’s going to burn. And the wire bundles, uh, were, uh, a major source of the smoke, uh, because you could tell once they started melting that’s when the smoke started consuming the back end very very quickly. So… [Pilot Member] : What, uh, what color were the flames, if you can recall? [MSSD] : Uh, they were like a, uh, a, uh, you know they were a whiteish, yellowish, uh, flames. You know… [Pilot Member] : Okay. [MSSD] They, uh, they weren’t blue, uh, that I can recall, so… or I didn’t see any blue, so you know, I, I’m not saying that the blue wasn’t back in the… [President] : Right. [MSSD] : you know behind the galley where I couldn’t see, but, as they were coming over the wires here it was a white or a yellow. [Pilot Member] [President] : Okay. : And when, did you notice any change? [MSSD] : And it wasn’t creeping flames either. It wasn’t like they were creeping because it was, they were being forced out of there. [President] : Something, okay, that’s what I was getting to, so, okay. R-236 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : Uh, going back to prior to taxi, there was, uh, we heard from a couple reports that the call, all, all stations on call, there was little hang up there. Do you recall what that was? [MSSD] : Prior… oh, okay. Yes, okay. So, uh, uh, it was minor. The three, the IO, uh, trainee, um, she couldn’t get her call position to work, uh, the ASE 2 who’s normally the communications on the jet guy, he went in, uh, up there and, uh, did some magic and, uh, then she checked in just fine with the call. Uh, after, uh, second attempt. [Pilot Member] : Okay. [MSSD] : But, uh, yeah. That, uh, I mean, I do remember that now. Uh, but it was, uh, it seemed to fix itself before we took off. But we didn’t leave the chalks until it was fixed. [Pilot Member] : Right. No, no, so every station was able to transmit on call? [MSSD] : Yes. [Pilot Member] : And, uh, the call light worked? [MSSD] : Yes. [Pilot Member] : Okay. [MSSD] : Yes, well I, and I specifically remember, uh, because normally it starts with me or the 16 op for the call, you know, a check, and, uh, I remember the co-pilot came over and said, uh, you know, all ops on call, you know, check in on call, and he didn’t flip the, you know, for the lights. And I said 16 without lights, and he, oh, and flipped the lights, you know, so… [Pilot Member] : Got it. [MSSD] uh, everything, all the lights worked. Uh, and, uh, you know, and before we left the chalks, everybody could check in on call, so… [Pilot Member] [President] : Okay. : So you think the on call light was just a switchology for someone up front? [MSSD] : They, they do it, uh, every now and again, the, the co-pilot will, uh, you know, it will take him a second, and, but as soon as I say no lights, he goes, oh, and then they magically come on, right, so… [Pilot Member] [MSSD] [Pilot Member] [MSSD] [Pilot Member] [MSSD] [Pilot Member] [MSSD] [Pilot Member] : Rog, magically worked after : After pimping. Right. Yes. : Then, uh, Chief… : Sir? : You are in a horrible position to smell that lavatory. : Yes. : uh… : It was broken for the day as well, so. : Yeah. Did that make the jet smell different from normal, or…. R-237 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MSSD] : Yeah, well, uh, to be quite honest I’ve been doing this a long time and, uh, it, it didn’t smell out of sorts that day, uh, you know, it was leaking on the floor and you could see the, uh, liquid, uh, you know, sort of gravitating towards the back of the jet. Um, but, uh, I’ve smelt it much worse, uh, you know in the heat of the desert and stuff like that where, you know, they either, uh, the ground crew doesn’t, uh, service it, or the, uh, we run out of blue tabs in the desert and all they have is water to, you know, sort of filter though there. So, it, it wasn’t anything, you know, out of the norm. You know it wasn’t overly overbearing. [Pilot Member] [MSSD] [Pilot Member] [MSSD] [Pilot Member] : Okay. : I, you know, I didn’t really notice anything. : Sweet. : So… I think that’s about it. : Yeah. [MSSD] : A couple lessons learned and, you know, you know, a lot of questions of that what ifs, you know. But, uh, uh, you know, I, I’ve talked to the folks in maybe some 847s need to be submitted for, uh, you know, uh, having the firefighter mask and, uh, pre-positioned with an ox bottle, you know, so, because it, that was one thing I turned around and I was like man he’s, he’s got his hands full. And even if, you know, uh, he did, by chance, have it hooked up, what is he going to do at that point, because now he’s got to hold an ox bottle and a fire extinguisher. Right? So how effective is he actually going to be? Um, and, you know, quite frankly I’m, I’m, I’m rather glad that, uh, I didn’t make it to this, uh, fire extinguisher and start going because I had, uh, you know, in, in the heat of the moment, you know I wasn’t thinking of this but, you know, as you run through, uh, the events as they unfold, if I would have started shooting here, well, I don’t know what had been melted or anything behind here and I had a poor Lieutenant sitting here. The blast from the fire extinguisher could have pushed something out the side and it would have landed all over him, you know, so. You know, everything happens for a reason, I guess, but, uh, you know, uh, there’s a lot of, uh, lot of what ifs in my mind as, uh, you know, what could have happened. But, uh, thankfully, uh, none of that, you know, transpired and, uh, we all just, you know, you shouldn’t fight fires in the, on the ground anyway right… [President] [MSSD] [President] : No. right. : you should just run from the, run from the fire. Let the professionals handle it. : These doors they have above the microwave that are for the heated water bottles… [MSSD] : Normally, uh, you know, you, you have the holes in here, uh, and that’s where they nor, uh, you know, uh, they’re, they’re never there unless you go down to Greenville where the dif jet delivers, uh, otherwise there’s, uh, you know, cleaning supplies and stuff like that. You know, uh, to clean up the galley and, uh, sometimes they’ll have aluminum foil and such like that up there, um, so you don’t have drippings on the bottom of the oven. Stuff like that, but, uh, um, the water bottles, um, were not in there, uh, I think, I, I looked up there and, uh, you know, uh, this one here might have had some toilet paper in it. Um, that’s where we stash the extras, uh, some trash b, you know actually I had to call for trash bags so there were no trash bags up there but it was just like general cleaning supplies, you know, paper towels, stuff like that. [President] : Any spray can, aerosol? R-238 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MSSD] [President] [MSSD] [President] [MSSD] : There’s potential there but, uh, uh, I can’t be for, for certain. : Okay. But it wasn’t empty? : No, it was not completely empty there was, uh, miscellaneous items up there. : Okay. : Uh, I don’t recall what the, exactly they were, so. [President] : In, uh, so from the time that you saw the flames to the time that you exited the aircraft, how much time do you think that total was about? [MSSD] : Exited the aircraft? Um, I would say about, uh, 2 to 3 minutes. It was not very long, uh, he got the jet, and the pilot got the jet, uh, stopped relatively quickly. We were only doing, I think they came out and said 50 knots by the time, uh, they started slowing down, um, and, uh, the, the, this, the part that slowed us down the, the most was just like I said the chokepoint of getting out the, uh, the crew entry chute. But, uh, um, you know, I, I guess in hind sight I could have, uh, when I popped the, uh, over wing hatch, I could have, but I, I just, you know, I just wanted to get as far away from the, the smoke as possible and, uh, I wasn’t going to go back to look if the flaps were down, and you know, if the engines were shut down and all that stuff. I was just, you know, uh, it kind of happened quick so I didn’t listen for those, uh, those key indicators. I don’t know if I’m diming myself out there or not but, you know, I, I’ll just say I was trying to get the heck out of there, so. [Pilot Member] [MSSD] [Pilot Member] [MSSD] [Pilot Member] : So, uh, I’m just gonna pass… You popped the hatch personally? : No, no, no, when I walked past the AMS… : Yeah : I said hey pop that because it will, we’re going to have a choke point here… : Yeah [MSSD] : uh, and, if the, there’s no way for the smoke to escape, you know, uh, and he said sounds like a good idea, and so he popped it on his way behind me, uh, because he’s the last one out of the back… [Pilot Member] : Right. [MSSD] : before he taps the TC, but he’s waiting for me to pass him so he knows that everybody’s out of the lav and all that stuff, so. [Pilot Member] : Do you know what he did with the hatch? Did he toss it on the seats, or? [MSSD] : Um, you know I didn’t, I didn’t, uh, stick around to take a look. Uh, you know, I don’t think he tossed it on the seats. There’s no seats readily available there. If anything he probably tossed it on top of the, uh, life rafts. [Pilot Member] : Okay. [MSSD] : Because they’re right forward of the wing there. So, or just laid it down right there, so. But I didn’t notice the fire guys when they were going in through that, uh, actually it worked out for the best because, uh, to get the fire guy through the crew entry chute with the R-239 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 hose and everything probably would have been a bigger pain in the rear than getting them through the over wing and back. So, you know… [Pilot Member] : Yeah. [MSSD] : Hurray for me, I guess, you know. But, uh, that’s, that wasn’t by design, you know. So… [Pilot Member] [President] : I’m good sir? : Okay. I’ve got nothing else. Do you have anything else you need to add? [MSSD] [President] : No, do you guys want, uh, anything drawn on here or detailed anymore? : No, I think you gave us a pretty good account of that, so, I think we’re fine. [MSSD] : You guys, just out of curiosity, uh, do you all, uh, when you do these like ever go to the jet and do like a video reenactment? Because that would be kind of… [President] : Yeah, well we’re still working that piece, so right now… [MSSD] [President] : Okay. : we have folks who are out there looking at the plane… [MSSD] [President] : Okay. : ting, tearing it apart, but that’s what part of the timeline piece is what we need. [MSSD] : Okay. Okay, then, uh, I’m all good. [Pilot Member] : Awesome. Okay, sir? If no one has any further questions we will now conclude this interview. [President] : Nope. [Pilot Member] : I’d like to remind you again that you are not offered a promise of confidentiality and that your statement is not protected and will be released to any follow-on investigation of this mishap, and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony and other information shared with you today regarding this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [MSSD] [Pilot Member] : You’re welcome. : Thank you. R-240 64-14848, Class A, 30 Apri115, AFSAS #739726 R13. MSGT [Production Superintendent] R13.1. ISB NON-PRIVILEGED WITNESS STATEMENT 30 APR 15 Page 1 of2 Non-Privileged Witness Statement 0 (Date) 1. n5. .havebeenadviscd by_ Wane, Grade. Organization. of Witness) (Norrie of Investigator) a safety investigator oflhe mishap that occurred on 30 gm involving Q5 '15? (Dm) (Equipment ?9 SM a. This investigation is being conducted under the provisions 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. [understand lam being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. 13. My witness statements (written or verbal) may be used for any valid purpose and be released to any wbsequcnt investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. 4 Name (Last, First, MI) and Rank/Grade Pdlo Sufn/L R-241 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Page 1 of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of AFT 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. WITNESS STATEMENT OF: Name (Last, ?rst, MI) and Rank/Grade SW,va W41- Signature [Reference attached document for witness account of event. This document ls being entered for accounting pwposes and witness is acknowledgement qfthi: being the ?rm they should have received for completion of a written statement. The member '3 chain of command will only review the ?nal mishap report if acquired through appropriate safety channels IA 91 -204 para 3.4. 5. R-242 V, 64?14848, Class A, 30 April 15, AFSAS #739726 NON-PRIVILEGED WITNESS STATEMENT Date. oi'thc mishap Crew position (as applicable) 3,143. Time you began duty 1 7930 l. 5m ?an/Jig? have been advised by - of the following: Nu: ind: -u undue-v 2L this investigation is being conducted under the provisions 91-204 solely for the purpose of mishap prevention withm the United State: Air Fame and to determine. all Grams relating to the mishap in order to prevent rectmence. i understand I am being interviewed as a witness in a mishap investigation and acknowledge that a promise of con?dentiality has not been extended to me. b. This witness statement may be released to the public pursuant to it Freedom of information Act request. l'hc chain of command will review the final mishap report. Provide an account of find-hand observations of whet happened, a description of prevailing conditions. circumstances, and associated events (use reverse for continuation). jwim u-i? mall. at- man 3:4. My mm, ?Am a? 54.1{3525 Gut "lL/K?fg lauded 0+ Ho? .t-s Sta/kc at]: 14-: dog. 4% ?Pd? 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Cb :0 T: .166 $.1Wft. \vm :2 $xon+ 2/ hell rt. 9f S'v? 76 515 {kl ?mv?avkh .NGEJ ?2.01 6% 93 9.2L a? rb?. 1 ts Est. .323 \xqu Wk: V, 64-14848, Class A, 30 April 15, AFSAS #739726 R13.2. 7-DAY NON-PRIVILEGED HISTORY 30 APR 15 72 HOUR AND 7 DAY HISTORY This Investigation is being conduded underthe provisions of AF I 91-204 solelyforthe purpose of mishap prev ention with?n the Un tied States Air Force and to determine all factors relating to th mishap In ordmo prevent recurrence. This form is being administered by an investigator from the Interim Safety Board (ISB) or Safety Investigation Board(SIB). The statemert you provide will either be privileged or non-privileged IAW applicable AFI 91-204 guidelines. EL NON-PRIVILEGED I understand I am being interviewed as a witness in a safety investigation and acknowledgethat a promise of confiderrti ality has not been extendedto me. My witness statem erts may be utilized for any valid purpose and be releasedto anysubsequent Investigation ofthis mishap and may be released to the public pursuant to a Freedom of Information Act request. This non-privileged 72 hour and 7 day history form will be placed in Tab when complete. El PRIVILEGED I understandl am providing statement(s) for a safety investigation and I acknowledge that a promise ofcor?dentiality hasbeen extendedto me by rnveaugamg vmoerorsoam mm This privileged 72 hour and 7 day history form will be placed in Tab when complete. This 72 hour and 7 day history form Is one of manytools the mishap Investigator may use to help determinett-e cause ofthis mishap. Your participation is both critical and appreciated and may help preventfuture mishaps. Please answerthese questions to the best ofyour ability when you are not rushed ordistracted Be as specific and detailed as possible. All answers address events prior to the mishap and recovery events. Today?s Date: 33 3 Statement Completed By: (punt) [Sign ature ISB or SIB Investigator Administering This Form: (print) R-245 R0135 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Aerospace Medicine Flight HISTORY REPORT Please list the daily activities you did during the last 72 hours. Provide the times of the events as well as the activity in the chronological order. it you cannot rememher the exact time of the event, provide the closest proximate time you can remember. DAY 1 (72 25$] 0533 WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How (why many times did you get up? When you woke up, how rested did you feel?) 34' ?are .- A a In TIME ARRIVED AT N??v a? hat or?? BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) .l Imam-l. 0590 ACTIVITIES: (List all the things you did. all food and drinks consunit.d) ko'l? om- 6'150. Red-:4. GAVE Low-v Helm. LUNCH: (What time did you have lunch? List all food and drinks consumed) Afst I ha. P?er mm Sula AFTEREQQE ACTIVITIES: (List all the things you did, all food and drinks consumed) mud. 4?4. WA ply-all L- bx 4.0, (ugh TIME DEPARTED WORK: um OPP DINNER: (What time did you have dinner? List all food and drinks consumed) [HOSoh?Jia__ 94? EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) wick-A Malta: TIME WENT TO SLEEP: 8300 ALCOHOL CONSUMPTION: (List all types. amount. and times consumed) N) MEDICATIONS: (List all medications take, prescription and over the counter, dose and time consumed) ?In DAY 2 (48 HOURS PAST) NAME (LAST, FIRST): SSAN: R-246 V, 64-14848, Class A, 30 April 15, AFSAS #739726 WAKE UP TIME: (What time did you wake up? How many hours did you sleep? [low many times did you get up? When you woke up. how rested did you feel?) 0900 to has 41% Kw. TIME ARRIVED AT WORK: moo BREAKFAST: (What time did you have breakfast? List all land and drinks consumed) loo.) wire; MORNING ACTIVITIES: (List all the things you did. all food and drinks consumed) {inlay-L ii?? LUNCH: (What time did you have lunch? List all food and drinks consumed) Snail-alas. ?(In AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) NM (Jr qu TIME DEPARTED 9.330 DINNER: (What lime did you how: dinner? List all food and drinks consumed) lcpl' MIL path? WM [9'0 EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) muck pm a} are; Hoke TIME YOU WENT TO SLEEP: 0345 an} 11w?? ?aw-m ALCOHOL CONSUMPTION: (List all types. amount, and times consumed) In MEDICATIONS: (List all medications take. prescription and over the counter, dose and time consumed) ?in NAME (LAST. FIRST): ssm:_ R-247 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY 4 ST WAKE UP TIME: (What time did you wake up? How many hours did you sleep? Ho? many times did you get up? When you woke up, how rested did you feel?) o?wo - 9? Swol- ARRIVED AT WORK: m; BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) bag} Mi'lk at? MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) mul- tut-5 (at how? Svf/lt'u' Add? LUNCH: (What time did you have lunch? List all food and drinks consumed) AFTERNOON ACTIVITIES: (List all the things you did, all food and drinks consumed) wk. ch our. on: ?was DINNER: (What time did you have dinner? List all food and drinks consumed) shut. In; uni-x EVENING ACTIVITIES: (List all the things you did, all food and drinks consumed) Wit-A TIME YOU WENT TO SLEEP: 0 7km ALCOHOL CONSUMPTION: (List all types. amount, and times consumed) P/h MEDICATIONS: (List all medications take. prescriptIOn and over the counter, dose and time consumed) IMMXI R-248 W3 V, 64-14848, Class A, 30 April 15, AFSAS #739726 DAY -I WAKE UP TIME: (What time did you wake up? How many hours did you sleep? How many times did you get up? When you woke up. how rested did you feel?) 093:: 9' h? TIME ARRIVED AT WORK: ?430 BREAKFAST: (What time did you have breakfast? List all food and drinks consumed) my: on 3 ?9 Out?t MORNING ACTIVITIES: (List all the things you did, all food and drinks consumed) A4444 huh Fwd-a LUNCH: (What time did you have lunch? List all food and drinks consumed) NO and HAUL. AFTERNOON ACTIVITIES: (List all the you did. all food and drinks consumed) wk mid? TIME DEPARTED WORK: (0, ?Wk DINNER: (What time did you have dinner? List all food and drinks consumed) ciaoo 1 to BMthu-ch wkn. EVENING ACTIVITIES: (List all the things you did. all food and drinks consumed) out. gamut m? screw Cum. Noun TIME YOU WENT TO SLEEP: ALCOHOL CONSUMPTION: (List all types. amount, and times consumed) 9! um MEDICATIONS: (List all medications take. prescription and over the counter. dose and lime consumed) ARRIVAL TIME AT SQUADRON {If different than above): BRIEF TIME: STEP TAKE OFF MISHAP TIME: 5% NAME (LAST. FIRST): 1325' R-249 64-14848, Class A, 30 Apri115, AFSAS #739726 23 JULY 2001 257 7 HISTORY FOR AERIAL VEHICLE INCIDENT 7 The 14? day lustory is less detailed than the 72-hour history. Please note any signi?cant life events that have occurred ovur past two weeks (ample selected for promotion, death in family, work, FLYING, marriage dim? t(inky. dimculty, vacation/leave, illness, eta). Include Caffeine, Mcds, Alcohol and obaoco, exercise and cum 3 ep . FULL RANK Mishapday20m 30 521W: (Agata-l (9.3 Ms ldaypn'ortomishaptDate 5H All??J 51.46, cm sump 2dayspriortomishapzDate g1 egg/r: (.hts slur mu (Hawk ka 073ml?.sz pr my} 013:?- case ha m?r wa 4daysprioxtomsshapmm are Mean: Rabid an" 8 ?ts $5.319 KM Sic-f 5 days prior to mishap? Date Folk?; PT M-l- Gas/M. 37H ?i atlwd Ark 8 Ms $l?p 5N3 .SquS 7days priortomlshapzDatc . on: up rid-ORB 0w. .l (OMS. $1479 Mow/?4A R-250 64-14848, Class A, 30 April 15, AFSAS #739726 R13.3. SIB NON-PRIVILEGED INTERVIEW 13 MAY 15 Page 1 of2 Non-Privileged Witness Statement /5 g; a? 0/ are) I have been advised by - [Maintenance Member] (Name, Grade, Organization, of Witness) (Name of Investigator) a safety investigator of the mishap that occurred on ?g 532 15? involving :2 5? (Date) (Equipment SM n. This investigation is being conducted under the provisions of AF I 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Name (Last, First, MI) and Rank/Grade (to? GA bun. Tithe Signature R-251 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of MSgt Role: [Production Superintendent] Production Superintendent 55th Maintenance Squadron Interviewers: (Investigating Officer) (Maintenance Member) Date: 11 May 15 [Maintenance Member] [MMX] : This is a non-privileged interview with , Master Sergeant, United States Air Force, being conducted on Wednesday, 13 May 14:23 hours by Lieutenant Colonel [Maintenance Member] for the Safety Investigation Board convened for the recent mishap. We're investigating the mishap involving an RJ-135 that occurred on 30 April 2015. This investigation is being conducted under provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of confidentiality is not being extended to you; your statement can be released to any subsequent investigation of this mishap and may be released to public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [MMX] : Yes sir. [Maintenance Member] : For the record would everyone present introduce yourself by stating your name, rank, and affiliation with the board, starting with the witness. : [Investigating Officer] : Captain , Master Sergeant, production superintendent. , Investigating Officer. [Maintenance Member] : And I am Lieutenant Colonel , and I am the Maintenance Member. And all I have for you is a series of questions. And, and like I said before, the reason that I wanted to pull you in is because you had an extremely descriptive, uh, recount of the event. So with your profess- with your experience as a – as a production superintendent, you had - I think you had the right distance from everything to see how everything went. So I just wanted to get your general opinions about the issue. So my first question for you is, what was your general impression of the launch, of 4848. And I know it was the second launch of the day. [MMX] : Um, beginning of the launch, the crew seemed very needy, they wanted, they were complaining about the O2 masks being outside of their bags[Maintenance Member] : Right. [MMX] : They wanted life support to come out and put them inside their bags. Um they also were missing two D rings that were part of the life support equipment. That’s when I directed um Tech Sergeant uh Phoenix 5 driver to give me 2 D rings to put ‘em on board the aircraft so they had a full inventory. Um, during the engine start, typical engine start. Uh my statement – my statement about the engine 2 would not rotate, uh we called over our Phoenix 8 truck which is our mechanical section, uh they determined with the pilot’s discretion to do a manual start on the number 2 engine, and from there they shut down the engine and did the manual start valve on the right hand side of the inboard column. Uh engine operated as normal after start sequence and then they continued uh the launch sequence. Uh the jet taxied out with no issues. Went towards Charlie 3, everything seemed normal. They were waiting down at the R-252 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 runway 30 hammerhead to get clearance to do the taxi back to runway 12. Like I said in the statement 4127 was in the pattern. Um, I watched it taxi from Alpha 3. I was - from my vantage point I pulled into Alpha 3 which was the actual - its parking spot to watch the – the launch sequence. I taxied back to runway 12 at that time all you can see was the vertical fin. You couldn’t see the full aircraft at that time. Um, so I positioned my vehicle facing runway 12 to get a better angle of the tail, cause there’s times we’ll see a – we call – I call it a landshark. You just see the vertical tail fooling around. Um in my rearview mirror I did see an E4 taxi, you know um, and that’s when we started, I started seeing the tail move again. I was like oh maybe it’s just moving for alert bird, you know getting out of position so alert bird can go on station um. During that time Phoenix 5, Tech Sergeant , called me, he was making his vantage point going up the hill to see what was going on too. Which is not uncommon for us to go watch it from upper ramp you know if we don’t see takeoff any time soon. And um, he called me on the radio, saying uh pro-super they were egressing the aircraft. Um, typical protocols. Get ahold of MOC, you know, see what they know. Lot of times they won’t relay information – the crew won’t relay information to the command post[Maintenance Member] : Mhm. [MMX] : Um, and to MOC. And it’s also that delayed time effect too. Um so I got ahold of the MOC on the radio and they said they’d call command post and find out what’s going on. Uh soon as Sergeant told me that they were egressing I made my view point – I made a decision to drive up to the upper ramp to see what was going on. Because people are egressing the aircraft and we don’t know, something’s going wrong with the airplane. Um, during my route up I went through Charlie 1, the cyber truck, the maintenance team was driving very slowly. I told them get out of my way, pull off to the left hand side please. And – and probably went more faster than I probably should have went up the hill. [Laughter] At that time it was considered an emergency. Um. And then uh by the time I made it up and around to the upper ramp I was facing the fire department, uh they were calling the ground emergency, or the all call radio via MOC, fire onboard aircraft. Um, I stopped my truck, at that time I made a call, uh wrote down the times and I started thinking, who do I need to call. Um, by the time I got over to meet up with Sgt uh at Lima taxiway, uh I can see at that time – uh this could possibly be bad. Cause the fire department was already on scene. Um. And then I made the phone call. At the time our pro-super phone was actually dead, had no battery life so I used my personal cell phone. [Laughter] Another illegal thing, sorry. [Maintenance Member] : It’s alright. [MMX] : To make a phone call to uh, Senior Master Sgt , he was in my personal contact list and I told Senior Master Sergeant 848’s on fire. It’s getting hosed down by the fire department right now. I need you to call Captain . And he’s like, ‘What?’ 848’s on fire. Getting hosed down. Please call Captain . I gotta go. I just said, I gotta go. Um, and at that time me and Sgt [MMX] watched the fire department. One was at the nose of the aircraft and one was at the aircraft left hand side foaming, and uh putting water on the plane. You can- we couldn’t see actual flames from our vantage point, you can see the black smoke. Um from the aft section of the tail. At that time I didn’t know it had burned through the um, fuselage. And one, I don’t know what time it was, but the fire chief uh called for maintenance assist, so it was Sgt ’s vehicle and my vehicle that went into the area. I told Phoenix 8 uh they were monitoring the line. And Phoenix 9 was up there I told Phoenix 9 just to stand by. Be in a R-253 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 posture mode. There’s no reason for avionics to be in there at the moment. Um during that tiduring that sequence Sgt already made the call to get the emergency uke, tow team available and they also met us up at the Lima taxiway. Um so we went and saw the on-scene commander or the fire department and the on-scene commander kinda took that standby posture. I first asked where the aircraft commander is to see his recounts of what happened. And he told me that uh the galley started uh, that the fire started at the galley area. Uh he kind of went into detail that he said that he was starting takeoff roll, he got to 45 knots, he heard fire in the background, then he uh did the emergency protocol of getting on the binders and made the call of egress the aircraft. I told him I was like, I’m thankful that your 27 souls are safe, uh it would – this - it could have been a lot worse. And I did talk to some of the back-enders, there was a Chief that was in the back I don’t – I don’t recall his name. And he told me literally the same thing, that it started at the galley. Um. During that time frame, uh on-scene commander and the fire chief, and Sgt and myself um, he was asking about the oxygen regulator stuff and Sgt was trying to instruct them how to turn off the O2 to the fire department. I guess the O2 was feeding the line, feeding the fire. And then it um it eventually went out I think cause we depleted all of our oxygen. And without - without having my boards on me I think oxygen was right around 60- 61 liters total. [Maintenance Member] [MMX] : Couple questions for you. : Yes sir. [Maintenance Member] : Did you ever note 4848 as a chronic – a chronic LOX venter, or losing LOX on a regular basis, or having to be serviced chronically? [MMX] [Maintenance Member] [MMX] [Maintenance Member] [MMX] [Maintenance Member] : No sir. I don’t- I don’t reca- we service a lot of airplanes. : But not this one in a particular – : No I: A chronic loser. : No I don’t. : Cause I saw on the forms that it went from – it had multiple sorties throughout the week. [MMX] [Maintenance Member] : Yes they were flying, two times a week. : And – and it was – this 64 started and then it was 61, and it was 61 for three successive[MMX] : Mhm. [Maintenance Member] : Servicing notations. So 61 would be your dead on, dead on accurate where it was? Um, but you weren’t – you weren’t you’re not of the opinion that it was a bad actor for oxygen systems? [MMX] [Maintenance Member] [MMX] : No sir. : Losing oxygen. : When I did my ER at the time, there was nothing on those forms that made my hair stand up. R-254 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Maintenance Member] [MMX] : Ok. : I felt very confident with that ER. [Maintenance Member] [MMX] : Did uh, other than the masks being out. : Mhm. [Maintenance Member] [MMX] : Why would they be out? : Post flight inspection. From the first go. [Maintenance Member] : And who accomplishes that? [MMX] : It’s your um, life support AFE they call them, um, I don’t know what the acronym stands for. [Investigating Officer] : Aircrew flight equipment. [Maintenance Member] : Were they able to get on the aircraft to put them back? Cause I know it was a turn – it was a 4 hour turn – [MMX] [Maintenance Member] : Yes they did go out to the aircraft. : So they were on the aircraft. [MMX] : Yes. They came out once and then after they fixed the masks and talked to the crew, whatever they did upstairs, uh, the crew notified the ground guy in regards to the D ring, 2 D rings that were missing, that were supposed to be part of the bag. Then I called them back out for that. Uh well I called them and they said well that’s not our part, so that’s when I contacted Sgt . [Maintenance Member] : Are you aware of any tasks that require electro-environmental to tamper with oxygen lines or connections? [MMX] : Tamper? [Maintenance Member] : Any type of maintenance where they would actually have to deal with the lines, not servicing but actually deal with lines. [MMX] [Maintenance Member] : Yes sir. : What would those be? [MMX] : Uh if they’re doing – if they were doing a LOX converter change, they’d have to disconnect lines from each converter, um, build up vent valves – that’s the – build up vent valves is where you hook up your oxygen cart to it, from the outside in. [Maintenance Member] : Ok. [MMX] : If they have to, like the control unit for the actual mask assembly, pull that out and there’s lines that go to that too. [Maintenance Member] [MMX] : And that is a crew chief task or an ENE task? : ENE task. [Maintenance Member] : Would you happen to work any code for any of these? Just – just things that pop out in my face. Um. In your statement as well, you asked – the – fire department, asked you R-255 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 for help in shutting off the oxygen. Did they have knowledge of where the shutoff valves were, and in your expert opinion, if they didn’t, should they have known that? [MMX] : They personally didn’t ask me, they talked to Sgt much handling that situation. [Maintenance Member] , Sgt was pretty : Ok. [MMX] : He took the lead on that one. Um, when he told me where it was at, I didn’t even know where it was, ‘cause these jets have been modded so many times. So um, should in my personal opinion, should the fire department know where it’s at? Yes. [Maintenance Member] : Ok. From the time that he was out there, the guy that was with you that advised him, do you, do you know how long it was before they actually got in there to shut it off or did it vent out before they even got in there to shut it off? [MMX] : It vented out. They tried multiple times, I think maybe 3 times going in there trying to find it. And Sgt was very detailed on where it was, when I was listening to him. And there was at times when me and - that Sgt weren’t together at times, you know, I was bouncing from place to place and he was giving them additional directions. From about when I heard Sgt talk to the fire chief and the fire member that was actually going in, he was very detailed with them. [Maintenance Member] [MMX] : Ok. So in in the through flight that you did --? Through flight? Quick turn? : I can’t recall. [Maintenance Member] : Ok. In the inspection that you did before you- before the aircraft was generated for launch. Was there anything that you noted that was out of place, out of sequence? Anything crazy, above and beyond masks being out of place? [MMX] : During my walk around inspection for my exceptional release, um, normal business. Everything looked air worthy. I did not go in – interior though. I did not do an interior inspection. Be the time – being – we didn’t have much time from day shift turning it – believe day shift did the quick turn – to me being on the line, cause I was solo that night, I was one deep person, uh, I didn’t have time to get upstairs. Could I have time – make it a point to go upstairs? Probably. [Maintenance Member] : Additional questions? [Investigating Officer] : Nope. Just, uh, well, one. Uh you said you knew of some scenarios where ENE would work on the LOX system. Or, the oxygen lines. [MMX] [Investigating Officer] [MMX] [Investigating Officer] [MMX] [Investigating Officer] : Mhm. : Inside the airplane? : Yes sir. : Near the masks, those type of connections? : Um, which masks are you talking about? Location? : Galley area. R-256 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MMX] : The um in the front of the galley I wanna say, going off vague memory and visual, I wanna say there’s three regulators[Investigating Officer] : Yep. [MMX] : That are right there. Um, if they had to do maintenance on that area, they’d, being, not being a SME, systems maintenance expert here, you gotta take that out. Off that galley. [Investigating Officer] : Ok. [MMX] : Um, the LOX converters, there’s that panel just forward of your galley, you open it up and there’s the he – we call it the hell hole panel, you know, um, usually there’s bags and equipment stored down there, there’s three LOX converters that are down there that they climb into. [Investigating Officer] : Ok. So if you were gonna do maintenance on the regulators themselves, you would disconnect them from the oxygen lines. [MMX] [Investigating Officer] : Um I can’t really answer that 100%, I’m not the system expert on that. : Fair enough. [MMX] : Um I don’t, I don’t have the tech data in front of me, so. [Maintenance Member] : Yeah that’s… the regulators are worked on by any – at the at the output of the source. Right? [MMX] : Yes sir. [Maintenance Member] : So at the end of the line. But in- beyond that, connections beyond that, because I know there’s tons of connections – [MMX] : Mhm [Maintenance Member] : T-fittings, there’s things, elbow off, or have you ever seen them mess with any of those? [Investigating Officer] : Like the little blue B nuts that connect – [MMX] : No I’ve never seen them, like, physically. The only extent of electrician ENE work around LOX converter, or around that area, is LOX converters. Build up vent valves and LOX converters. [Maintenance Member] [MMX] [Investigating Officer] : Alright. : Uh usually are our culprit of leaks. LOX leaks. : Alright that’s all I’ve got sir. [Maintenance Member] : Alright. That’s all I have. Anything else you’d like to offer? If no one else has any further questions, we will now conclude this interview. I’d like to remind you again, sir, that you were not offered a promise of confidentiality, and that your statement is NOT protected and will be released to any follow-on investigation of this mishap, and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony or any information shared with you today regarding this mishap to avoid possible spread of incomplete and counter-productive information until the board has adjourned. Notify R-257 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 the board immediately if you become aware of a possible release of information. Thank you for your time. [MMX] [Maintenance Member] : Yes sir. : Any concerns? Alright. Sign here. R-258 64-14848, Class A, 30 Apri115, AFSAS #739726 R14. 68-07 mm" ?mm? ?1 R14.1. ISB NON-PRIVILEGED WITNESS STATEMENT 30 APR 15 Page 1 of2 Non-Privileged Witness Statement I - l. (Date) I. l, ,havebeenadvisedbyl 0 (Name, Grade. Organization. of Witness) (Name of Investigator) a safety investigator of the mishap that occurred on 54'; 49;? involving I 35?1,? "u - My; 8 (Date) (Equipment SM a. This investigation is being conducted under the provisions of 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a pmnuse of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Gs-o? Mame (Last, ran, MD and Rank/Grade pi?! Signeture R-259 V, 64-14848, Class A, 30 April 15, AFSAS #739726 Page 1 of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of AH 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. WITNESS STATEMENT OF: 65.07 Name (Last. First. MI) and Rank/Grade ?wpy?rcr? Duh: Ti?o (/Signature Reference attached document for witness account of event This document is being accounting purposes and for witness ?5 acknowledgement of this being the form they should have received for completion ofa written statement. The member '3 chain of command will only review the ?nal mishap report if acquired through appropriate safety channels 91-204 para 3. R-260 64?14848, Class A, 30 April 15, AFSAS #739726 FOR OFFICIAL USE ONLY NON-PRIVILEGED WITNESS STATEMENT Dale of the mishap Crew position (as applicable) Time you begun duty Q730 0/0 .b 14 :11 - 1.2351 55ml; have been advised by _ofthc following: a This is being conducted under the provisions of AH 91.204 solely fur the purpose of mishap mthin the United States Air Force and to determine all factor: relating to the mishap in nrder to prevent recurrence. I understand i am being interviewed as a witness in a mishap lnvesxtgation and I acknowlwge that a promise of con?dentiality has not been extended to me. b. This witness statement maybe released to the public pursuant to Fmdom of Act request. u. The chain of command will review the ?nal m'LQhap report. Provide an account of ?rst?hand observations otwlut happened, a description of prevailing conditions, circumstances. and associltod events (use for continuation). 610M WG-5 Gn- 'the. ON Vere, omml ?ne or.) .4051 391906 on 5?51 7Q, 9&5? ?ue/marl up?! Drivel 76 ?mm 5mm M5 Show 053% (Pan?s Lay-r). prow EMH Wt 'owuw (Subunit-MT?) 7ft Varof?o Dlamr, I Saw Plums 76m 951? Tat? Jug ?ll/am Lay 5055? Plum. 1% 5per my haiku, NU ?l?lxrfa it.th 90/5?? 75 kw?m Me, ?aw! "lie; Fl;me Ol?wga aka? J- S?m??tL I Saw WleA ?9wa 6207 Umblj?y wot 360.17 "rat, W54: rte, wuj dig 7th Tim. GT 165 Ami-5r we, Teal-l Ad a, Lax heal Elly-?4 amt ?Macaw-'79 ?lm?V if Opp Tit Snead Call om Glow Fl' ?Nos 5?0ch To (#656 To 5Wllenv; manual we, ?12 dc?my Sam Dun wof'K We TWO at: (cafe, Ma?rrz? Fromm plarle. ?The above statement is true to the best of my knowledge and ballet" Sig )ate. Bulky a I R-261 64-14848, Class A, 30 April 15, AFSAS #739726 R142. SIB NON-PRIVILEGED INTERVIEW 13 MAY 15 Page 1 of2 Non-Privileged Witness Statement lg . (Dare) 1. l, Q54 2 Ce? have been advised by Member] (Name, Grade, Organization, qf Witness) minute of Investigator) a safety investigator of the mishap that occurred on 413:5 involving int?! Bill, g- mew, 5 (Date) (Equipment SM 3. This investigation is being conducted under the provisions of 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. 1). My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of information Act request. Name (Last, First, MI) and Rank/Grade ?re ?gure: Signature R-262 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Firefighter 1] SIB Interview of Mr. Role: Firefighter 55th Civil Engineering Squadron Interviewers: (Pilot Member) Date: 13 May 15 [Pilot Member] [MFF1] : This is a non-privileged interview with being conducted on 13 May 2015 at 10:20 local by Captain for the Safety Investigation Board convened for the recent mishap. We're investigating this mishap involving an RC-135V that occurred on 30 April 2015. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of confidentiality has not being extended to you; your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [MFF1] : Yes. [Pilot Member] : For the record, would everyone present introduce yourself by stating your name, rank, and affiliation with the board, starting with the witness. [MFF1] [Pilot Member] [MFF1] : [MFF1] : Captain , with the Offutt Fire Department, GS-7. , pilot member. How you doing today, sir? : Good, good. You? [Pilot Member] : Good. So uh if you wouldn’t mind just stepping us through the events of the day as you saw them. [MFF1] : Alright. Uh, we got toned out for a ground emergency, uh around 6:30 I’m not exactly sure of the time. Uh I was on engine 9 which is our first run pumper, uh the rescue truck also that day, uh we responded out there to the runway, saw smoke coming from the back of the plane, uh my job was to go in, so we got off the truck, uh laddered the, the plane’s wing, went in the plane with the handline over the wing uh I was first on the handline so went over the - went all the way to the back of the plane uh which was smoky about halfway I guess, the closer you got the more smoke there was obviously, uh saw flames about 3 feet high. Hit it with the handline, uh knocked it down after about 3 bursts, uh of foam and water, uh at that point we heard some hissing, uh come to find out that was the O2 line that had burst. And then, uh after I sprayed I had to leave the aircraft because uh my airpack malfunctioned. So I went back out got a new airpack came back in, uh. Pretty much after that the - the fire had been put out uh we were looking for the O2 shutoff which was difficult ‘cause we couldn’t find it. Uh even with the crew members trying to describe where it was. [Pilot Member] : Mhm. [MFF1] : Uh I guess that con- configuration of plane is the only plane in inventory that has the O2 shutoff where it’s at. And once we did get it shut off, uh we did some clean up, you know making sure the fire was totally out, wrapped up our stuff went back to the station, and R-263 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 then we got rung out again for possibly rekindle of the plane, I’m not even sure what time that was maybe 10 o’clock or so. [Pilot Member] : Alright. [MFF1] : So we go back out there, went in, there, there wasn’t actually rekindle there was just some – some smoldering insulation and residual what-not, at that point we had to cut the air ducting, um, do a little extra damage to get to a 100% sure that it wasn’t gonna rekindle. Wrapped up and called it a day. [Pilot Member] : Alright. Uh who was with you on your engine? [MFF1] : Uh I think it was was driving, I don’t remember, I think it was [MFF2] as the crew chief, was with me, I don’t remember who the fourth person on the truck was, and then myself. I don’t – yeah I don’t remember who the fourth was. [Pilot Member] : Who was uh who was fire attack that day? [MFF1] : Uh myself and the crash truck and [MFF2] were on the handline. And I think a crew chief from were in with us also. [Pilot Member] : Uh, do you guys always go over the overwing hatch? Is that how you usually enter the aircraft? [MFF1] [Pilot Member] [MFF1] [Pilot Member] [MFF1] [Pilot Member] [MFF1] : Yes. Mhm. : Uh, what side – pilot’s side or copilot’s side? : Pilot’s side. : Pilot’s side always? : Yes, that’s the rescue side. : Ok. Pilot’s side’s rescue side. : Yeah. [Pilot Member] : Uh, once you get inside the overwing hatch, what are your priorities once you get onboard the aircraft? [MFF1] : Uh, we actually split at that point, ‘cause usually there’s at least 4 of us, there’s always 2 in 2 out, uh so 2 people go into the cockpit, uh shut down the aircraft, disconnect the batteries, and start ventilation. The other 2 take the fire attack. And that – of course that depends on where the fire was. But in this case it was me and [MFF2] who went to the back of the plane with the fire – and put the fire out while the other 2 did their thing. [Pilot Member] : Ok. Uh, the handline. Were you able to get the handline all the way back to the fire, right away or did? [MFF1] : No, after - it didn’t take long I mean it seemed long, but we were having trouble because of the configuration of the plane pulling the hose through we got caught on something, the way the handline went in the door I think it got caught on the door, and when we got that freed up it got caught on something else, so it took - I – I guess an extra at most a minute to pull the handline all the way back, but. [Pilot Member] : And after that it was what 3 shots to knock down the flame? R-264 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MFF1] [Pilot Member] : Yep. : Did it go out or uh I’m assuming that’s what knock down meant. : Yeah. Yeah. At that point I could see no more flame, um and actually that 3rd burst I did was just for effect, just to make sure I guess after I had left cause my airpack malfunctioned, uh, and [MFF2] put a couple tiny flames out. [MFF1] [Pilot Member] : Ok. Uh were you still on board the aircraft when they started hitting it with foam from the outside? [MFF1] : Yes. Yep. [Pilot Member] : So was that uh in conjunction with you spraying or did you knock it down first and then the foam came in? [MFF1] : Yeah. We knocked it down first and then the foam started coming in. Uh if I remember right Mr the uh Assistant Chief had seen flames on the outside where we didn’t see those flames from the inside. [Pilot Member] : Ok. Alright. Uh, how would you usually shut off the engines in the front of the airplane? Would you guys go for the throttles, start levers, T handles? [MFF1] : Yeah. Uh generally and- and again this is situational but it’s throttles, bottles, battery, APU. [Pilot Member] : Ok. [MFF1] : So we always start with the throttles and then T-handles if the engines were on fire and then the batteries and APU, and then we go disconnect the battery physically after that. [Pilot Member] : Ok. And then is uh shutting off the oxygen anywhere in there or is that just- [MFF1] : Generally not on 135s cause they don’t have a, a shutoff. Like that. Uh, a main one I should say. [Pilot Member] [MFF1] [Pilot Member] [MFF1] [Pilot Member] [MFF1] [Pilot Member] [MFF1] [Pilot Member] [MFF1] : So uh, you guys do 135 egress training, correct? : Yes. : Yeah. Uh. When you do egress training, what kind of 135s do you guys train on? : Whichever one they give us, it’s not specific. : Right. So uh 5 different 135 variants sitting on the ramp. :, Right and we’re at the mercy of whoever can give us the plane I guess. : Oh. I lied. 6 different 135 variants. : Oh. [Laughter] : Alright do you know where the uh the shutoff is on this on 848 now? : Yeah, oh definitely yes. [Pilot Member] : How long would you say it took to uh find someone who knew where the shutoff was and actually go shut it off? R-265 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MFF1] [Pilot Member] [MFF1] [Pilot Member] [MFF1] [Pilot Member] [MFF1] [Pilot Member] : Um, times a blur when it comes to that. : Yeah. : I couldn’t even, I couldn’t even guess. Not- not: Was it – : Feasibly. : Was it still hissing when you shut it off or? : Very little. I mean it basically bled itself out. : Right. Ok. Can you describe the color of the smoke, color of the flames? [MFF1] : Yeah the smoke was a whitish grey, as far as I could see, ‘cause again it was you know, dark and smoky. Uh the flames were a bright orange and yellow, from what I saw, about 3 feet high when I when I hit it. Um, after that, uh I mean the whole plane filled up with smoke after that, so. And it was the same darkish grey smoke type stuff. [Pilot Member] : Ok. Uh, one question. The uh, you guys have a piece of equipment that’s known as the penetrator? [MFF1] [Pilot Member] [MFF1] : Uh, we have – called a spat tool or crash 5. : Is crash 5 uh the one that will penetrate the skin of the aircraft and spray inside? : Yeah. [Pilot Member] : Since you’re on fire attack and you’re side – inside the aircraft, is it you’re called to use that or is it the engine operators called to use that or who is called? [MFF1] [Pilot Member] : It’s actually – it would have been the assistant chief. : Assistant chief. [MFF1] : Uh, that day the truck was in maintenance. For batteries, I think. I’m not sure what it was in there for but it wasn’t available. [Pilot Member] : With the situation you saw, on that day, would that have been used, or? [MFF1] : Um, I don’t think it would have made a difference. Honestly. Where that fire was was coming from and then the O2 after that. I mean our chances of hitting that O2 line with that thing probably would have been even worse. Um. I think we did less damage by not penetrating in this instance, personally. [Pilot Member] : Alright. Sounds good. Alright. Those are all the real questions I have. Do you have any questions for me or anything else to say? [MFF1] [Pilot Member] [MFF1] : Not that I can think of. : Alright. Perfect. Then we will conclude. : Awesome. Thank you. [Pilot Member] : Yep. If uh no one has any further questions we will now conclude this interview. I’d like to remind you again that you were not offered a promise of confidentiality, and that your statement is NOT protected and will be released to any follow-on investigation of this mishap, R-266 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony and any information shared with you today regarding this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [MFF1] : Thank you. R-267 64-14848, Class A, 30 Apri115, AFSAS #739726 R15. 68-07 ?We'd (MFFZ) R15.1. ISB NON-PRIVILEGED WITNESS STATEMENT 30 APR 15 Page I of). Non-Privileged Witness Statement 4m" in - (pm) 1. I, cm ,havebeenadvised by. (Name. Grade, Organization, of mess) (Name of Investigator) a safety investigator of the mishapthat occurred on .70 Jill/involving Re (Dal!) (Filament SM This investigation is being conducted under the provisions of 91 -204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of information Act request. if 1/ 7 4/ Name (Last, First. and Rank/Grade firs/71, R-268 64-14848, Class A, 30 April 15, AFSAS #739726 Page 1 of NON-PRIVILEGED WITNESS WRITTEN STATEMENT FORM This investigation is being conducted under the provisions of 91-204 solely for the puxpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I undersde am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. WITNESS STATEMENT OF: - MM Name (last, ?rst, MI) and Rank/Grade signature [Reference attached document for witness account of event. This document ts being entered for accounting purposes andfar witness is acknowledgement of this being the form they should have received for completion ofa written statement. The member '3 chain ofcommand will only review the ?nal mishap report if acquired through appropriate safety channels IAW 91-204 para 3. 4. R-269 64?14848, Class A, 30 April 15, AFSAS #739726 FOR OFFICIAL USE ONLY NON-PRIVILEGED WITNESS STATEMENT Date arm: 36? 'l 6?0 . me position (as applicable) 1% Time you began duty . . - - . l. t, jg?w a. This investigattnn is being conducted under the pmvisions of-Al-"l 91-204 solely for the put-pas: of mishap prevention thhin the United States Air Force and to dctetminc all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in mishap investigation and I acknowledge that a pmmise of con?dentiality has not been extended to ms. h. This witness statement may be released to the public pursuant to Freedom oflnformntion Act request u. The chain of command will review the ?nal mishap report. the following: u? Provide an account at rim?hind observation: at what happened. a description at prevailing conditions. and associated twents (use reverse [or .9) . 4.. ?mm/ a? {0636 I "my mm/ airy (FEW WV 119;; I {/Kl?i?zrn/ if?f /0 my ((50 01/- J?poorfJ f/Nf/ft/ Ak? 0 lbw/N ?Mum, tum Mimi {vino/?7? 4/1 )0 Mr {far d-J? Daft/of} 7% ball Hy CW, I (544? f? . ?ow 0 ?Go W?i)wr gm tM/o/m?m 2?7? 9 wall SW W, p/mwd ow up? perm, 0? Corr/WA th/f bW/lfd ?hOll f0 /f ?The above statement is true to the best of my knowledzt: and belief." Sitmc haw! FOR OFFICIAL USE ONLY 64-14848, Class A, 30 April 15, AFSAS #739726 R152. SIB NON-PRIVILEGED INTERVIEW 13 MAY 15 Page 1 of 2 tin-Privileged Witness Statement MM 1? 9 o; [P'lol?til??r] I t. Wm] 01-07 ,have been advised by? (Name, Grade. Organization. of Wm) (Name oflnm?gatar) a safety investigator of the mishap that occurred on 3,201 3Q amt involving 90 /,if 1/ (Date) (Equipment SN) a. This investigation is being conducted under the provisions of AH 91 204 solely for the purpose of mishap prevention within the Unith States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. .v i ?07 01/ Name (Last, First, AH) and Rank/Grade Duh: Till! I I Signature R-27l RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of [Mishap Firefighter 2] Role: Firefighter 55th Civil Engineering Squadron Interviewers: (Pilot Member) Date: 13 May 15 [Pilot Member] [MFF2] : This is a non-privilege interview with being conducted on 13 [Pilot Member] May 2015 at 0915 local by for the safety investigation board convened for the recent mishap. We’re investigating the mishap involving a RC-135V that occurred on 30 Apr 2015. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent reoccurrence. A promise of confidentiality is not being extended to you. Your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [MFF2] : Yes. [Pilot Member] : For the record, would everyone present introduce yourself by stating your name, rank, and affiliation with the board starting with the witness. [MFF2] [MFF2] : Base fire department. . Uh GS-7, civilian. Uh 55th C-E-S slash C-E-F-O Offutt Air Force [Pilot Member] : Captain [MFF2] : Good, yourself? : (chuckles) Good. So uh you were on duty on April 30th, correct? [Pilot Member] [MFF2] , Pilot Member. How are you doing today? : Yes. [Pilot Member] : Alright. Uh would you mind just stepping us through what happened that day uh as you saw? [MFF2] : Uh yeah uh we got toned out for a uh smoke uh in an aircraft. I was on uh engine 9, which was uh also duties as a rescue crew. Um. So we uh responded; there was four of us on the truck. Um got on scene, uh crews that were already on scene said that they had smoke coming from the rear of the aircraft. Um no- I did not see any visible flames at the time. Uh so myself and our crew chief get off the truck; at that time there was already uh- we had already laddered the wing um which is normal- normal for us. Crew members we already off the aircraft. Um so our normal entry is we go up over the wing into the cargo- the side cargo door. [Pilot Member] : Mhm. [MFF2] : Um and then we take two hand lines in uh with us for an interior attack. Uh laddered [MFF1] the wing, uh myself and uh , , and uh made entry into the aircraft. Um once we got up onto the wing- we normally uh- we don’t- don’t go on air, our :S-EB-A: air until we actually get to the door, or whatever. Uh one of the big key things was once we got on the wing you could- definitely have visible smoke inside the aircraft there was definitely a white-ish, grey-ish smoke. And I make the comment to- the rest of the guys were uh putting their R-272 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 regulators on, so I made a comment to my crew chief; I was like ‘it definitely smells electrical, like electrical burning smell.’ That was, I don’t know, key for me anyways that it- it smelled like something electrical was burning; which we’ve had in the past ya know, a burnt motor or what have you. Um so uh we made entry into the aircraft uh visibility was slim-to-none. Um so we were trying to get ventilation going; one of that- part of that is we open up the main- main hatch on the side, that’s kind of our procedure to get that opened up- to get ventilation going. So one of the guys went to work on that as we were trying to uh pull a hand line back towards the ya know back to the aft of the aircraft; which we were having troubles ‘cause it’s always a struggle getting it up over the wing and if you ain’t got enough guys pulling hose for you, it’s- it’s uh hectic. Um [MFF1] was on the front of the hand line- I was behind him. He kind of- we weren’t getting hand line back, so he kind of ventured off to get to the back of the aircraft; and I remember him coming back and saying ‘We’ve have fire back there’ and he was like ‘We need hand line, we need hand line.’ So my main purpose was I went back as far as I could to try to pull- feed hand line to him uh we got- we got to the back um and he was on the hand line. I hadI had yet to see any fire and I kept making the comment ‘we need to get ventilated, so we can see what’s going on.’ And then he did uh he opened the nozzle- we uh had to be pretty close to the rear of the aircraft; he opened the nozzle a couple of times and then he had his uh- must have been hitting the fire or whatever he saw; I didn’t see any, but I was probably five feet back from him trying to pull hose still. And then he had problems with his uh air pack, so then he begin toto leave and then came up with me, and I was like- I kept thinking to myself ‘We gotta get some of this smoke outta here so we can see what’s going on.’ And then so I- I came across and opened up the- the hatch that was is on the opposite side..that would have been thethe copilot’s side. I got that hatch opened up and then I grabbed the hand line and just did hydraulic ventilation; which is basically just- you just spray out the cargo door with like a fog pattern, and it just sucks the smoke with it and it takes it right out. So literally I probably did that for about 5-10 seconds, and it was- I mean we were clearing that aircraft out bigtime. And then that’s when I seen the- the first fire that I seen, which was basically where it had burnt through the top of the aircraft. So then we took the hand line and hit that with uh a little bit; and by that time it was- the crews from the outside were hitting it with foam, so foam was coming- I mean it was coming down in on us, basically. And at the time so far the fire was pretty much out. They continued to dump foam on it for a while from the outside; which I’m not sure what they seen from the outside, but as far as we were concerned the fire was pretty much out. There was still some sort of smoke, and you could hear like a rushing sound which we assumed was like O2 oxygen line, or something running; which we later ran into troubles getting that shutoff.. specific- that specific line, or whatever. But um had a little bit of smoldering uh we did uh I-I do remember right in these- these compartments here we- we got those opened up and there was some books and stuff, what have you, in here; and those were pretty burnt- burnt up quite a bit. Um so you know as we were doing that we were trying to get- eliminate anything where it was smoldering, so we were pulling down ya know the insulation and uh making sure that it wasn’t in between the uh the skin of the aircraft. Uh I mean as far as the interior that was pretty much…what we had- what we had going. Um I mean obviously there was- I mean there was a lot of the lines and stuff that run up through there that was ya know all melted which might have been where we were getting the electrical smell from. But uh I don’t know if there are any other questions that you have? R-273 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : I have uh, a few specific questions. Just to-to clarify. So when you respond to an aircraft, how do you determine which wing you want to go in? … ‘Cause you say you like to uh you laddered the wing[MFF2] [Pilot Member] [MFF2] [Pilot Member] [MFF2] [Pilot Member] : Yeah, it’s always- always the pilot’s- pilot’s side. : Always the pilots side no matter which side the fire is on, if you can see it? : Yepp. : Okay. : - For an interior attack, yep. : -For an interior... alright. [MFF2] : That’s our uh or 135 like egress procedures. And along with that ya know the- you’d have the- if you still had people on the aircraft ya know your priority would be doing a searchrescue situation. So if you needed to get it shut down then ya know then you’d send your guys up and get the pi- get the aircraft shut down. Obviously that was- that was all done. [Pilot Member] : Alright. Uh so you mentioned priorities; priorities is search-rescue first, and then shut down the engines. What are you priorities after that? [MFF2] : Uh it would be, well if you have people on the aircraft it would be obviously ya know- you want to save life, properly ya know. So make sure everybody is off the aircraft and then aircraft shutdown and then you want to get ya know attack the fire. And then after you attack the fire, you get ventilation. I mean get ventilation; go in get the smoke out of there. Uh and then that’s- yeah that would be it. [Pilot Member] [MFF2] [Pilot Member] : Okay. Uh… Who was the crew chief? : Uh, Captain : . was the crew chief. Now you heard the hissing sound after the fire was out[MFF2] [Pilot Member] [MFF2] [Pilot Member] : Yep. : And you assumed oxygen at the point? : Right. : Uh do you know where the oxygen shutoff is on the B-model? [MFF2] : Uh what it ended up being was we had a- a- that was one of our- our big things was trying to figure out where that was. What happened was it… we- our uh instant commander onscene was talking with the flight crew and they were saying that it was on the- the right… right side of the aircraft behind two seats that you slide back. [Pilot Member] : Okay. [MFF2] : There was a couple of shutoff valves. Well what got confused was it was actually the actually the copilot’s side, and not the pilot’s side. So we were looking in the- there was a compartment down here that we actually- a hatch that opens up and literally you can crawl down inside there and look for- I mean guys were inside there literally looking for these valves. And we couldn’t find them, and it ended up being on the other- the opposite side of the copilot’s side. R-274 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 And the only reason we kind of thought it was oxygen is because all these seats along here- the crew members must have been on oxygen; their masks were laying there. And you could still hear them- evidently they set them down, and you could hear them rushing still. So that’s what led me to believe that it was an oxygen line of something still rushing air out. [Pilot Member] : Okay. [MFF2] : that was making some fog and thinking- leading people thinking that something was still burning, or still smoldering more than it- than it was I guess; but… which and then we did have to go back out there a second time because it was still smoking, or whatever. I uh- we came in there and we were looking and we had a heck of a time trying to find where it was and then I actually went in there, and then I believed it was- there is a black tube that runs along the center of that aircraft, like a ventilation duct. And I was like- what I had thought was, which ended being I think might have been what it was, was that tube runs there, but then there is still a bunch of insulation that lays up on top of that. So I said- I told the other guys in there, I was like ‘I think it’s up in there, and I think you can’t get it ‘cause you got these big- these big cables or wires that run along there, too’ and we didn’t want to cut those ya know basically there were some tabs in there that you could cut and get it moved out, but we ended up cutting that tube- a section of that tube out; pulling that out of the way and was able to get the insulation out from on top of it. [Pilot Member] : How long after the original incident did it start smoldering up there? [MFF2] : Uhh. Well I think it was- geez I don’t remember the time, but I think it was about 6:30 I think when the whole thing started; we got back to the station, we were cleaning up… 9ish- 9:30, somewhere around there. I was actually in the shower and then we got called back out down there; which crews were still out there. And then we were out there ‘til midnight, or so. So.. in those time frames, I guess. But we- I mean we… ya know hunted for a little bit of smoke for-for quite a while... pulling just little pieces out ya know thinking that might be it; and you can kind of see just maybe a little bit of smoke- a little bit, and then it’d kind of disappear and it wasn’t….nothin’..terrible, but obviously you don’t want it to rekindle ya know more than- than what it is but.. And not try to do too much damage ya know, [Pilot Member] : When you guys practice egress on an aircraft do you know what kind of aircraft you guys practice on? [MFF2] [Pilot Member] : Yeah, 135’s. : Alright. Do you know which variant? [MFF2] : Uh, no. Just…everything…any aircraft that we can get, or the crew lets us on uh… yeah what’s available for the day or month or[Pilot Member] [MFF2] [Pilot Member] [MFF2] [Pilot Member] : Is there any requirement to practice on every single aircraft at Offutt? : Yes. Uh far as 135’s, yes but the configurations can vary. : Okay. : Yeah I don’t- if that’s what you’re asking…yep...yeah. : Alright. R-275 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MFF2] : Yeah so we don’t specif- specify ‘alright we need an egress on this specific’ but it is 135 specific, I guess. [Pilot Member] : I just have one more real question; Uh the penetrator… that’s what I know it as. The uh machine? [MFF2] : Alright, [Pilot Member] : to penetrate the skin, would uh that piece of equipment had been used for this type of fire? [MFF2] : Uh I mean it’s a possibility, but with the fire already have been coming through the skin… it already- it wasn’t like it a fire that was like smo- or like inside the skin that you couldn’t get to. So really the skin had already been penetrated so to use that I guess- If you had, if it would had spread maybe or if it was in a different area of it was still smoking coming in between the pieces of skin then obviously you could have, but I don’t think there was a need ofI’m not sure what you would have penetrated with to put anything out, I guess. [Pilot Member] : Whose uh whose call on scene is it to uh use that equipment if they had to deem it so? [MFF2] : Uh it would be… First off it would be your uh crash truck uh crew chief’s, and then overall your instant commander; your AC, [Pilot Member] : As the guy on the airplane would you say ‘yes go ahead, use it’ or ‘No, don’t use it’? [MFF2] : That... The-They would probably see that more from the outside than what we would do from the inside of the aircraft. [Pilot Member] : Okay. Alright that’s uh that’s all the questions I have. [MFF2] : Far as…yeah far as the fire it was knocked down, I mean real soon, so…far as us, I don’t see much…I mean, just ya know having more people maybe pull some line, but ya know everything went pretty smooth as far as inside where we were at, I guess. [Pilot Member] [MFF2] : 27 souls got off and the fire was extinguished, so. : Yeah, right. Yeah that’s about all I got, unless you got more questions. [Pilot Member] : No sir, I do not. Alright, with that we will conclude. If no one has any further questions, we will now conclude this interview. I would like to remind you again you were not offered a promise of confidentiality and that your statement is not protected and will be released to any follow-on investigation of this mishap and may be releasable to the public subject to the Freedom of Information act. We request that you refrain from discussing your testimony and other...correction any information shared with you today in regards to this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [MFF2] : Thank you. R-276 V, 64-14848, Class A, 30 April 15, AFSAS #739726 R16. SRA (IASE) R16.1. SIB NON-PRIVILEGED INTERVIEW 19 MAY 15 Pngelof2 Non-Privileged Witness Statement MA .. (Dale) . ?953% have been advised by "mm" . (Name, Grade, Organization, of Witness) (Name of Investigator) a safety investigator of the mishap that occurred on 33 (5 involving 12L - I 35-14 (Date) (I'l?lluili'?w?t ?9 SM a. This investigation is being conducted under the provisions of AF 1 91404 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and [acknowledge that a promise of con?dentiality has NOT been extended to me. la. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. St A Name (Last, First, NH) and Rank/Grade Duty Title Signature R-277 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of SrA Role: [Instructor Airborne Systems Engineer] Airborne Systems Engineer 5 Specialty Chief 338th Combat Training Squadron Interviewers: (Investigating Officer) (Pilot Member) Date: 19 May 15 [Investigating Officer] [IASE] : This is a non-privileged interview with Senior Airman , uh, being conducted on Tuesday 19 May 10, uh, 1025 actually 1030, um, 2015. Captain is the investigating officer for the safety investigation board convened for the recent mishap. We’re investigating the mishap involving an RC-135 tail number 6414848 that occurred on, uh, 30 April 2015. This investigation is being conducted under the provisions of AFI 91-204 for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of confidentiality is not being extended to you. Your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confident, confidentiality has not been extended, uh, and for the record would, I’m sorry, do you understand that? [IASE] : Yes, I do. [Investigating Officer] : And, uh, would everyone present introduce yourself by stating your name, rank, and affiliation with the board, starting with the witness. [IASE] : Okay. So I am, uh, Senior Airman , um, I am at the 338th Combat Training Squadron which is the formal training unit for the Rivet Joint. I am the ASE 5 specialty Chief, and, uh, yeah. [IASE] [Investigating Officer] [Pilot Member] : I’m Captain : Captain [IASE] [Pilot Member] , the Investigating Officer. , Pilot Member. [Investigating Officer] : Uh, okay, so that’s the formal briefing. Um, so like I explained to you, we’re trying to determine how ASEs train with the use of oxygen bottles, specifically as regards for purging. [IASE] : Okay. [Investigating Officer] : And, uh, so if you could explain to me how you learned it, um, or, uh, or if to your knowledge there’s any tech order guidance that… [IASE] : So, how I learned it, um, and, uh, since it’s been a little bit, but, uh, so how I learned it, um, is that if the, obviously the TO states that the bottle cannot, or is not supposed to fall under 50, and, um, when you go about your checklist you are to verify that it’s at 300 PSI which is typical aircraft pressure. So, um, if it’s below 50 it requires purging, um, and the kind of common, um, understanding amongst the community that I’ve experienced is that, um, purging involves, um, uh, so dumping the bottles, uh, contents by flipping to its EMER and letting it completely exhaust, refilling it to 300, dumping it, refill, dump, so you’re looking at 3 dumps, and on the 4th refill you keep the bottle at 300 and you put it back. Um, now, um, this is on the R-278 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 grounds of how I teach it as well; however, I always teach a level of crew coordination, so, um, on the Rivet Joint, uh, typically the Form 46 AFE gear type of thing is maintained by the Ravens and most importantly, um, by the TC and, and the aircraft commander so if a bottle is below 50 I am going to go about purging, but before I do that I’m going to notify the TC that there is a bottle that’s, um, at or below 50 PSI and let him know that I am going to continue with purging unless he wants me to do otherwise. [Investigating Officer] : Okay. [IASE] : Um, so, if, if, the ground, or the call is to be made that hey these bottles are maintained by the crew chiefs do we want to let it, them make the decision on whether or not to just replace the bottle or if they want to purge it or whatever then I would leave it to the, uh, the TC to make that call. [Investigating Officer] [IASE] [Investigating Officer] : TC, got it. So, you, you typically would bring it to the TC’s attention? : Mhm. : Unless you have, uh, like a training requirement to, to do the purging and, uh, all that… [IASE] : Right, so, for instance, um, our first 2 events are, uh, on ops group trainers so, uh, the jet’s just parked on the ground with power. [Investigating Officer] : Okay. [IASE] : Um, on those events we are teaching emergency equipment, and one of the things we do is talk about the NA-1 and we purge it and refill it to show the students how to go about refilling an oxygen bottle. [Investigating Officer] : Okay. [IASE] : That is on the, the MTL, the task list that we train off of that’s produced by Ops Group Training. [Investigating Officer] [IASE] [Investigating Officer] [IASE] [Investigating Officer] [IASE] : Um, the, the TRSS commander sent me a copy of you guys’ syllabuses. : Okay. : A couple of copies and I don’t know if you wouldn’t mind looking at this e-mail… : Of course. : and helping me out here, basically. Uh, here’s what he sent me. : Okay. [Investigating Officer] : Uh, ASE 4, retail, TTL, uh, May 2013, I don’t know, I’ve got 4 files here and I don’t know if… [IASE] [Investigating Officer] [IASE] [Investigating Officer] : So, um… : Looking at these syllabi… : Realistically those are all out of date and rescinded, um… : Okay, alright. R-279 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [IASE] : But, um, I, I mean I’d like to say that they have the same procedures on them or in them that the ASE 5 would contain as they’re both Baseline 10 syllabi. Um, but, uh, I would, I would actually have to go back and verify that those are… [Investigating Officer] [IASE] [Investigating Officer] [IASE] [Investigating Officer] [IASE] [Investigating Officer] [IASE] [Investigating Officer] [IASE] : Can you get me a syllabus that… : I can. : that we can… Yes. : at least say hey these dudes in, in their syllabus are required to train to this… : Right. : for X reason. : Right. : It makes sense to me. I fly the AWACS, and we have bottles in the back. : Right. [Investigating Officer] : We use, we have bottle refill teams for firefighting and stuff like that. We actually train with it in the jet. Like we’ll do like simulated fire drills. [IASE] [Investigating Officer] [IASE] : Right. : Do you guys so anything with that or with the… : No we don’t, um, and that’s unfortunate. That’s something that we’ve been trying to, um… [Investigating Officer] [IASE] [Investigating Officer] : Incorporate… : bring about, um… : Yeah. [IASE] : The, yeah, we, we work a lot with the Brits, and, um, the common consensus is that the Brits do a lot of things right. That, um, for one reason or another there are a little bit unrealistic for our force. One of things they do is they do a lot more intensive work on, um, IFEs and handling emergency situations, and, and, firefighting procedures and going about that. Um, for instance, uh… I’m sorry go ahead. [Investigating Officer] : Sorry. And this in unrelated to the topic of the bottles, but why do you think it’s unrealistic? [IASE] : Um, as far as what they do that makes more sense? Well, for one, they have a much smaller force. Um, for two, they have, um, only one airplane which means that, um, you know, uh, probably going to increase the uptime of that airplane being that the maintenance only has one airplane to work on... [Investigating Officer] : Yeah, it makes sense, makes sense. [IASE] : and keep running. Um, so they have a much smaller force, they have a much more experienced force. Not only that, um, you know, they had the, the NIMROD incident and that R-280 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 fuels a lot more people to think with that mindset. Um, it’s unfortunate and I, um, actually had this, uh, quite a while ago with the old PIO incidents. I had a TC tell me well, it hasn’t caused an incident yet, it’s probably not going to. Which is a really silly and, um, unsafe way of thinking, but it’s unfortunately out there. [Investigating Officer] : Well, just, we’ll talk about it more after the interview, but so you know, AWACS, which essent, the crew is fairly similar. [IASE] : Right. [Investigating Officer] : Uh, the, we train every time we have a mission sortie with mission, full mission crew in the back, uh, we do a, uh, a drill of some sort, whether it’s rapid loss of pressure or fire in the cabin, whatever. And we actually happen to have dudes like simulating jumping into lobes or hell hole, whatever… [IASE] [Investigating Officer] [IASE] [Investigating Officer] [IASE] [Investigating Officer] [Pilot Member] [IASE] [Pilot Member] : Right. : with bottle, like, it’s kind of a pain but it’s good training. : Yeah. : So, anyway we’ll talk about that after. : Okay. : But, did you have any questions for him, [MFF2] ? : Uh, as far as refilling an oxygen bottle, do you know what TO covers that? : Oh goodness, um, I would, oof, first thing, place I would look would be the Dash 1… : Okay. [IASE] : Um, so, uh, but I, I might actually have to do some digging to get the, the full… but I’m, um, my educated guess is yeah, Dash 1. [Investigating Officer] : Okay. After, after we get done and you go back, if you have some time, if you could try to find us some guidance, um… [IASE] [Investigating Officer] [IASE] : On the refilling? : On refilling, uh, slash purging, whatever. : Okay. [Investigating Officer] : If it’s not there it’s not there and it’s not a big deal. Um, we’re just, it’s just a piece of our investigation we need an answer to. [IASE] [Investigating Officer] [Pilot Member] [IASE] [Pilot Member] [IASE] : Of course, yeah. : And, uh, anyway… : Uh, and also along the firefighting, you’re an ASE 5 instructor… : Yes sir. : Were you ever an ASE 4 or ASE 2? : I was an ASE 2 previously. R-281 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Pilot Member] : Previously? When you do emergency procedures brief, is someone designated as a firefighter? [IASE] : Yes, so the TC, um, when they’re, when we’re doing our mission planning brief, our step brief, the TC will designate, um, the way they used to do it was they designate the ASE 3 to coordinate for, or to be a primary firefighter on the front. Some of the TCs would like to say that it would be a Raven 1 that would help him out with gear. Um, but then they would designate either the 2 or the 4 in the back. Nowadays, because we have two 5s in the back they just kind of leave it to one of us. Um, with that said, we as the ASEs always briefed okay so he named you the primary firefighter, um, so what does that mean? Uh, well if I’m not the primary firefighter am I just going to sit in my seat the whole time and like… no that’s not… I mean, sure you’ll be the first one there, but, um, the way that we teach it typically is that if there is a fire, you’re going to have one person respond immediately, to, um, try and, uh, at least in a smoke or fume situation you’re going to have one person respond immediately to try and sniff out where the actually fumes are coming from and kill power to associated equipment. And you’re going to have a second guy donning the gear because it does take some time. [Investigating Officer] : Who runs that? Like who’s like, let’s say a fire breaks out… who is in charge of directing the firefighting operation? [IASE] : So, uh, I think a, I’m unfamiliar with, uh, I , I have to find it, where it is in the reg but the, there is a reg that states that the TC is responsible for coordinating all, um, firefighting in the back of the aircraft. Um… [Investigating Officer] [IASE] [Investigating Officer] : However… : However, the way we teach it is that, um… : The ASEs are going to run it? [IASE] : The ASEs are going to run it. So, um, we, we tell the ASE 1 students, um, that their first call is should be over interphone to the pilot that hey, there’s a fire in the back… [Investigating Officer] : Okay. [IASE] : and we’re going to proceed with troubleshooting, and then to request that the AMS and TC push their coordination to mission net so that we can punch off mission net on the firefighters boxes so that they don’t have to listen to them talk because with the smoke mask on, with everything going on, it is already hard enough to hear just with what’s going on with hot mic. [Investigating Officer] [IASE] [Investigating Officer] [Pilot Member] : Okay. : So… : Makes sense to me. [MFF2] ? : What seat do you sit in for takeoff? [IASE] : Um, so in crew rest, uh there’s four rows on the right side, um, my favorite seat, if you will, is the one, uh, just in front of the back, so, um, typically, I can show you here, um, I usually sit in this chair, um, so pretty much in line with the window. The other ASE 5 typically sits at the back. We separate by aisle and aft maintenance. R-282 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Investigating Officer] : Okay. [IASE] : So aft maintenance is typically going to sit in this row because their box is there. Aisle maintenance’s box is right up here so they’re running a cord to themselves. And I usually, most of them sit in this general area. So, but, uh, with uh, uh, 338 sorties having full mission crew compliments of 36, um, we’ll, uh, sit in various places depending on, uh, seat availability. [Pilot Member] : So it goes on seat availability and where your comm cord’s coming from. Has nothing to do with firefighting equipment or… [IASE] : No. So the other reason why I sit here is because the firefighter’s equipment bag in the back is actually located right on the ceiling above me, and it is part of the ASE 5 checklist to pre-flight that smoke mask to check for, um, mic, and interphone, um, capability and speakers as well. So, I like to sit there or have someone sitting there so that if it does break out I can tear it off the wall with my seatbelt on and get it ready. [Pilot Member] [IASE] [Investigating Officer] [IASE] [Investigating Officer] : But there, but there’s no regulation to sit there? : No, no, no, no, no, no that’s all, that’s all wherever you want. : Uh, using your brain and logic and… : Right. : Got it. [Pilot Member] : My last questions are going to be about the ASE 5 base 11 and checklist. Uh, now this is a local checklist made by 55th OSS OST and approved by OGV. Is there an expanded part of this checklist, do you know? [IASE] : No. No. I will, I will precursor that. I am not actually baseline 11 certified. But what I can tell you from my knowledge of the 11 checklist and, uh, and all that stuff, that is, that’s effectively where the buck stops for ASE checklists. [Pilot Member] [IASE] [Pilot Member] : Alright. So you’re an ASE 5 baseline 10? : Correct. : Alright. So looking at that checklist now, is there an expanded part of this checklist? [IASE] : No. [Pilot Member] : No? [IASE] : No. That’s it. [Pilot Member] : Alright, now tell me this. Why do you have to have the galley off prior to takeoff? [IASE] : Um, so, why is an excellent question. Um, for that I can tell you I’m, I don’t actually know the, the answer as to why the decision was made to keep the galley off. I can tell you from my personal experience and from the common knowledge around the ASE corps is that, um, if you lose something behind that galley you don’t go after it. Um, many an ASE have been, uh, shocked by the galley. Um, it’s, it’s happened. Everybody knows about it. Everybody talks about it. R-283 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Investigating Officer] [IASE] [Investigating Officer] : So… : So, um… : More specifically, um, is it a common practice to power the galley up on the ground? [IASE] : It does happen. Yes. Um, so deviations are authorized for us. Um, now there’s actually a TO that states under what circumstances you can deviate. Unfortunately those aren’t really, um, talked about. When we talk about deviations in our checklists for check ride purposes it’s okay if you want to deviate. Make sure you’re letting your evaluator know and knowing exactly why you’re doing it and have a good reason, um, also understanding that when you are deviating, um, you are at some times, um… [Investigating Officer] : Assuming risk… [IASE] : accepting risk. Correct. So, um, a lot of times the galley is powered on before takeoff. Reason being, um… [Investigating Officer] : Refrigerators… [IASE] : Refrigerators, microwaves, um, if we’re delayed on the ground for a long time sometimes people want to cook food on the ground. [Investigating Officer] [IASE] [Pilot Member] : Okay. : That happens. : How does it shock you? [IASE] : Um, so, uh, we’ve, there’s like this story that all goes around about someone, uh, putting, uh, like a plate or a piece of foil or something like that on top of the microwave and then, um, it falling underneath, or behind it, and they reach back to get it and there’s, um, there’s some, uh, tiebreakers back there… [Investigating Officer] : Yes there are. [IASE] : that will arc, um, and that’s typically the, um, the understanding. Now, I’ve never seen the back of a galley, uh, pulled out of an aircraft and I’ve never actually been, um, intrigued enough to reach back there and test it, but, um, this is what I’ve heard and that’s kind of what’s passed around the ASE community. So… [Investigating Officer] [IASE] [Investigating Officer] [IASE] [Investigating Officer] [IASE] [Investigating Officer] [IASE] : So people have seen it arc before? : Um, again I’m going off of what I’ve been told, but yeah. : Okay… : Um… : Okay… : Yeah. : Wow. : But there’s always subject to exaggeration. R-284 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Investigating Officer] [Pilot Member] : Sure. Anything else? : No, that’s all I have. [Investigating Officer] : Okay let’s see. So we’ve talked about, oh, bottle purging, we talked about that on the tape, right? [IASE] : Yeah. [Investigating Officer] : Got it. Um, so to your knowledge right now, that procedure may or may not be contained in the tech order, but it has been taught by ASEs since you’ve been around? [IASE] [Investigating Officer] : Yes. : Okay. [IASE] : Um, to my knowledge I, I don’t know. I’d have to look it up. Um, but that’s been taught by ASEs and other crew members as well, um, Ravens and CMC that I’ve seen. [Investigating Officer] [IASE] : Okay. So I think we’re done asking you questions. I’ll finish up… : Okay. [Investigating Officer] : but the, the admin here. Nobody has any further questions we’ll now conclude this interview. Um, so [IASE] , I’d like to remind you again that you are not offered a promise of confidentiality and that your statement is not protected and will, and will be released to any follow on investigation of this mishap, uh, and may be releasable to the public subject to the Freedom of Information Act. That’d be like if someone, uh, a civilian was to ask for it… [IASE] : Right. [Investigating Officer] : they could go though FOIA. We request that you refrain from discussing your testimony and any information we shared with you today regarding this mishap to avoid the possible, possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of the information. Thanks for your time. [IASE] : Okay. Thank you. R-285 V. 64-14848, Class A. 30 April 15, AFSAS #739726 R17. MR. Wm" ?em? (MM) R17.1. SIB NON-PRIVILEGED INTERVIEW - 26 MAY 15 Memorandum For Contractor Representatives Serving As Technical Experts To Safety Investigations. MEMORANDUM FOR [Mishap Mechanic] - vim m5 (Nan-Air Force technical expert is full name and compan /orgarrization) FROM: com Penman do new ems: A rim: 3 736 726 (S13 President) SUBJECT: Protection of USAF Privileged Safety Information l. In response to my request for technical assistance, the Air Force and your employer have agreed that you will serve as a technical expert for the Safety Investigation Board (SIB) over which I preside. Unless you speci?cally identify in?ammation in any technical report you provide to the SIB as proprietary data or con?dential analysis or opinion. it will be included in the releasable portion (Part I) of the 818?: ?nal report. If you want us to treat any part of' your report as privileged information so we can protect it from disclosure outside the Department of Defense, you must speci?cally request such protection. In such case it will be included in the privileged portion (Part 2) of the fennel safety report and will be used solely for misth~ prevention purposes. 2. The military safety privilege protects information provided under a promise of con?dentiality and the deliberative process of the 818. It enhances the 818?s ability to identify potential causes of mishaps quickly and accurately so we can prevent their recurrence. This process must have the highest degree of reliability to maintain combat readiness. national security. and public safety. 3. In accepting your appointment to serve as technical expert, you must also agree to safeguard our safety privilege. You may be given access to privileged information and you must not disclose to anyone, including your employer, any privileged information derived from our investigation. You will prepare only one copy of your technical report for the SIB. You will destroy or surrender to me any notes documents, computer ?les, or other materials, produced or obtained during this investigation, if they contain privileged information You must not make copies of any privileged documents (including analytical computer products, con?dential tape recordings, and staged phorographs) for use outside the proceedings of this board. You may not have a copy of Part ll of the Board?s final report or any part of a draft thereof. You must report to me (or, alter the SIB is dissolvad, to HQ Air Force Safety Center) any attempt by anyone, other than a SIB member or other duly authorized person, to obtain any con?dential or deliberative information from you about this investigation. 4. Before beginning your service to this SIB, please sign and date the endorsement below. 1 will give you acopy of this memorandum. R-286 V, 64-14848, Class A, 30 April 15, AFSAS #739726 (SIB President?s signature block) Endorsement To: Ema Pewwvi {Zonal CMA #739724 ?lm 2w; (SIB President) (Date) I acknowledge understanding of the contents of this memorandum and receipt of a copy thereof and I agree to comply with the duties and responsibilities stated therein. Filmical expert's slgnamre black) R-287 R0135 V. 64-14848, Class A, 30 April 15, AFSAS #739726 Page I of 2 Non-Privileged Witness Statement 2t. MY [Mishap Mechanic] [Mai mam] - In enance I [w b? ,havebeen adwsedby (Name, Grade, Organization, of Witness) (Name of a safety investigator of the mishap that occurred on Soogg If involving ?5513; $848 (Date) (Equipment SN) a. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. i understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. [Mishap Mechanic] Name (Last, First, MI) and Rank/Grade TIN. Signature R-288 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Mechanic] SIB Interview of Mr. Role: Aircraft Mechanic L3 Interviewers: (President) (Investigating Officer) (Maintenance Member) (AFSEC Representative) Date: 26 May 15 [Maintenance Member] : This is a non-privileged interview with Mr. [Mishap Mechanic] being conducted on Tuesday, 26 May 2015 by Lieutenant Colonel for the Safety Investigation Board convened for the recent mishap. We're investigating the mishap involving an RC-135V aircraft 4848 that occurred on 30 April 2015. This investigation is being conducted under provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of confidentiality is not being extended to you; your statement can be released to any subsequent investigation of this mishap and may be released to public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [Mishap Mechanic] : Yes. [Maintenance Member] : For the record would everyone present introduce yourself by stating your name, rank, and affiliation with the board, starting with the witness. [Mishap Mechanic] [President] [Investigating Officer] : Uh [Mishap Mechanic] : Colonel , Board President. : Captain [Maintenance Member] , Investigating Officer. : Lieutenant Colonel , and I am the Maintenance Member on the board. [AFSEC Rep] : Chief Master Sergeant Mr. : And I’m local union member. , Air Force Safety Center Representative. local 967 uh representative- uh I’m representing [MM] as a [Maintenance Member] : The first thing I’m going to do is I’m going to give you this ticket to; it’s a production ticket. [Mishap Mechanic] : Okay. [Maintenance Member] : And I just want you to review it- take the time to review it, before I ask you any questions. Uh can you describe your duties related to this particular ticket on the aircraft 4848? [Mishap Mechanic] : To that ticket, exactly? [Maintenance Member] : Yes. R-289 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Mechanic] : Okay, this ticket is the crew rest installation. The crew rest installation uh- that’s actually all the lines and stuff that go up to the crew seat- the crew rest seats. They also they’re lines that go to the galley uhm also that goes over to the aft baggage area. [Maintenance Member] : Are you aware of any clamping requirements in the oxygen system itself; and there’s a drawing right here if you want to point to anything, please feel free. [Mishap Mechanic] : Oh, okay. Uhm clamping requirements, are you talking about bonding clamps, or you’re talking about securing it at[Maintenance Member] : Securing the lines to the aircraft. [Mishap Mechanic] : Okay. Securing all the lines to the aircraft is uh is not actually just called out like specifically you have to Adel it here or there. It’s uh described in the print as uh where per like TPS- I think it’s every twenty inches to secure it and just make sure it’s not moving around; also uh not to be routed where it’s not used as a handle- into the pilot chute they use it as a handle, and uhm that’s basically the uh best way you can get it routed to keep from… [Maintenance Member] : Right. If you look at this drawing and it shows you where the galley is, here, and the lines coming in pushing from the other side, uh and the ‘T’ fitting that is here; the drawing calls for a clamp to be here, here, and in here- and here. [Mishap Mechanic] : Yes. Okay. [Maintenance Member] : Do you know if that’s the standard configuration on most Rivet Joint aircraft that are produced? [Mishap Mechanic] : Yes, uhm they should be, I’m not sure if it’s on this print or not, but there’s a print that shows it going up the galley, and then down the galley. And this is the flex line that shows it coming across. Most of all of them I’ve seen like this are Adel. If it’s- usually I see the two Adels there- secure there. And that line, which is a uh braided hose, goes up to the next hardline that comes across. This line right here is secured to the stringer, or to what structure, I think there’s some overhead structure there too that it can be secured to. But yeah, most of them are like this straight across. [Maintenance Member] : And as a curious question, that fitting that’s here on the end of this assembly, that attachment- is it usually a straight attachment, or an ‘L’ attachment? [Mishap Mechanic] : I think… I think it’s a... I think it’s a ‘L’ attachment. [Maintenance Member] : Okay. [Mishap Mechanic] : I think is. I think it’s a uh, what do you call it… an elbow. Because the way it comes across it would have it- the line would have to go up to meet to it. [Maintenance Member] : Okay. Can you tell me the procedure you use to connect this assembly, the tube assembly, to the hose assembly here? [Mishap Mechanic] : The procedure? [Maintenance Member] : Yes sir. [Mishap Mechanic] : Okay uhm, let’s see. Depending on which lines you get back first, okay we firstwell you want to know the whole procedure completely, or? [Maintenance Member] : Just the procedure to fit them together. R-290 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Mechanic] : Okay. Alright, let’s just say we have all of the proper parts we need. Okay this right here would be routed, or supposed to be, okay. And then the next one would be routed where, I guess, as much as you need it to come up so it doesn’t hit anything, and then that line would be put, the uh flex line, would be put across there. This would be secured, and when this one comes down, you’d have to secure them. And then you go back and uh where- see what the torque is, torque the nuts down, and torque them down and then start securing these to the stringers and to the uh galley stuff where it goes. [Maintenance Member] : Okay. So if I’m hearing you correctly, you put them finger-tight first, and then you come back and you torque them to value? [Mishap Mechanic] : Yes sir. And because- well the reason is because you don’t want to try and torque them with nothing sitting there, because it’s going to be too hard to- you don’t want to twist anything. So you finger tight them first, and then start securing them, and then torque them; because we still have to have a leak-check, and all that done. [Maintenance Member] : Uhm when you- when you go back to torque them, how can you tell whether you’ve torqued one or not; like you have one, then you go do something and you’re like okay I’ve finger-tighted them and now I have to torque them down, how do you know which ones you hit and which ones you didn’t hit? [Mishap Mechanic] : Uhm, well If you were to- if you were to miss one like not to torque it, when we do our leak-check you would obviously find it real quick. [Maintenance Member] : Okay. So the catchall is the leak-check [Mishap Mechanic] : Basically, yeah. Because I mean if you have a lot of lines and of course if you miss one, you’d know when- when you do the leak-check. That’s- That’s actually the basic reason we do a leak check, to make sure we have everything tight like we’re supposed to. [Maintenance Member] : Okay. The uh solvent used to leak-check the uh adjoining lines, where does that solvent come from; is that something made, or is that something that’s manufactured somewhere else and then it’s used? [Mishap Mechanic] : Uh that is the leak-check we all use uhm for all our leak-checks, basically. I- I think it’s from this company, but it’s all the same leak-check. [Maintenance Member] : So it’s nothing something people are like concocting on their own or making on their own? [Mishap Mechanic] : Mm-mm. No, no. [Maintenance Member] [Mishap Mechanic] : So it’s off the self, like I got this. : No, no one is just making it on their own. [Maintenance Member] : Okay. Do you recall how- what the torque values are on those nuts when you have to attach the assemblies, or is it just off the top of your head? [Mishap Mechanic] : No, I would have to go to the TPS I think it’s the 3-100 for the oxygen system, or something like that. [Maintenance Member] [Mishap Mechanic] : Sure. Of this copy, can you show me which one it is, sir? : Right here, 4-1. R-291 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Maintenance Member] : That’s where it tells you what to do, and do you know the value, or do you have to look at the 4-1? [Mishap Mechanic] : Yeah, you just have to look it up. You see where it says uh ‘hand tighten’ and then to torque [Maintenance Member] : Would any of these torque values match? [Mishap Mechanic] : Yes. Let’s see…what size line is it… it would be one of these, but I’m trying to remember what size exactly was the line. [Maintenance Member] : Oh, the line. : Yeah, it has a different size of 8th, quarter, and 3/8ths tubing, so the diameter or the size of the line... [Mishap Mechanic] [Maintenance Member] [Mishap Mechanic] : Well because the smallest one would be the [Maintenance Member] [Mishap Mechanic] : It’s the smaller diameter tube, I believe? : So it would be 5/16ths ? : I think you’re right, 5/16ths. So it’s limited to 100 to 125 [Maintenance Member] : Okay. And is that a great amount of pressure, in your opinion? Or is it just like, check it with the torque wrench, and call it a day? [Mishap Mechanic] : Uhm, I don’t think- that’s not really a lot. I don’t think it’s a whole lot. I mean it’s- to me calling it a lot would be really ya know getting to it and being aluminum it’s just.. [Maintenance Member] : Yeah, okay. The uh torque striping is used on some and not on all connections. When is it used, and when is it not used? [Mishap Mechanic] : Uhm the torque striping goes back to when I first learned oxygen system, which was probably 17 years ago, the guy who trained me was using the green torque striping, told me that’s what it was for; the green for oxygen. Uhm here recently, we stopped using the torque striping, because uh custumer body said he doesn’t want to use that. Uhm I think they looked it up, and it wasn’t, what do you call it, uh oil based. But we- we got away from that because he didn’t want to use it; so we stopped using it. I don’t think that anybody there actually said to use it, but I still go back to when I first learned it, when I first started working here. So that’s eliminated. [Maintenance Member] : Uh, in the ticket. [Maintenance Member] : Okay, uh, in the ticket, um, are, you’re, it says you’re qualified to stamp off your own work there because you’ve been doing this for 17 years. Obviously it’s a lot, long time. [Mishap Mechanic] : Yep. [Maintenance Member] : Um, do you know if there was another person that came behind you and quality check this area after it was completed? [Mishap Mechanic] : Like actually checked it themselves? Like when… [Maintenance Member] : You know like quality assurance will come by and they’ll do other, they’ll do jobs to check over people. Do you know, do you recall if there was… if you… R-292 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Mechanic] : Well there’s always, uh, even if I stamp it off… [Maintenance Member] [Mishap Mechanic] : there is a, uh, what do you call it, company finals? [Maintenance Member] [Mishap Mechanic] : Mhm… : they have to go back and look at certain areas. [Maintenance Member] [Mishap Mechanic] : Yes. : And when they go back, and even if, if it’s not me… [Maintenance Member] [Mishap Mechanic] : Mhm… : Okay. : And they’re still certain areas of the aircraft they think is broke down in 5 or 6 areas. [Maintenance Member] [Mishap Mechanic] : Okay. I have one final question for you. : Okay. [Maintenance Member] : Here is a picture of some fittings that are used, that were in the oxygen system on the mishap aircraft. [Mishap Mechanic] : Okay. [Maintenance Member] : I’ve seen this one, but I’m having trouble identifying this one. Can you tell me where that one possibly could have come from or if it’s a suitable suppl, substitute? [Mishap Mechanic] : Would it could, what the, oh this sym, this, the number on it, like a symbol? You talking about this? [AFSEC Rep] [Mishap Mechanic] : Yeah. : Um, all I can say is, on the flex hoses, like where that team you’re talking about… [Maintenance Member] : Mhm… [Mishap Mechanic] : Okay. If the line isn’t brand new and it’s an existing line and it’s called out to put in this line and you go to the cap’s crib and get it, that probably was still on that. That’s all I can, that’s all I can, you know, if it’s a new fitting… [Maintenance Member] : Right. [Mishap Mechanic] : and it come, if, if the flex line is new and they go to the cap’s crib and I get it and then, then the next line is new and it says to get a T fitting we go to the oxygen kit and there will be a new fitting in there. [Maintenance Member] [Mishap Mechanic] : Okay. : It’ll be in a plastic bag with a green, uh, piece of paper and it means oxygen cleaned. [Maintenance Member] : Alright. [Mishap Mechanic] : The only way it would have a different one if it’s, if the line your using wasn’t a new one and they went and said this is, you know, this is the line you need, you go, you go to R-293 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 ticket, you go to cap’s crib, here’s the line, inside a plastic bag and it already has the T fitting on it. [Maintenance Member] : Okay. The, uh, are you aware if the oxygen systems that you install are kitted and completely brand new for Baseline 11s or are they piece-mealed, meaning that one, once you get those lines whatever you get out the plastic bag is what you’re putting in? [Mishap Mechanic] : Um… [Maintenance Member] : And it could be used. [Mishap Mechanic] : On Baseline 11 that’s, that’s pretty new. Um, I’m not sure yet, um, but the guys who are doing the oxygen now, I’ve noticed that, uh, most everything’s coming new. I mean I haven’t really seen anything, I guess, used, that have the used, because all the lines, um, we have to mock up our own lines… [Maintenance Member] : Right. [Mishap Mechanic] : and once we mock them up we’ve got to stamp the, um not stamp, yeah stamp it and staple the ticket to it… [Maintenance Member] : Mhm… [Mishap Mechanic] : send it off, and then they have to make a copy of that line we made. Of course clean it and then send it back in the plastic with the ring sleeve in it. [Maintenance Member] : Right. Um, by looking at that picture would you say that that is a newer fitting or an aged fitting? [Mishap Mechanic] : This one here? [Maintenance Member] : Yes sir. [Mishap Mechanic] : That would look like a, like an older one to me, just because of the color of it. Because most of the new ones are dark blue. [Maintenance Member] [Mishap Mechanic] : Mhm… : And that just looks like an aged fitting. [Maintenance Member] : Right. And are you aware of that fitting being a suitable substitute… well, let me ask you a better question. Do you think that fitting is listed in this oxygen ticket? I’ll just give it back to you. [Mishap Mechanic] : That’d be an AN fitting. No, because, are the parts, on this one would be on that oxygen clean kit. [Maintenance Member] [Mishap Mechanic] : Well, I mean that looks like a, like an older fitting. [Maintenance Member] [Mishap Mechanic] : Right. And that one is not? : Mhm… : But I mean, that, that’s, it looks like an older fitting. [Maintenance Member] : Okay. R-294 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Mechanic] : But it’s not, it’s not called out on there. Now, in a oxygen clean kit that’s where all the fittings would be. [Maintenance Member] [Mishap Mechanic] : All your parts would come from there. [Maintenance Member] [AFSEC Rep] [Mishap Mechanic] [AFSEC Rep] [Mishap Mechanic] [AFSEC Rep] [Mishap Mechanic] : Yes sir. : Roger. Alright, that’s really all I have. Anyone else have any questions? : I’ve got one for you sir. When you, you do disassembly as well, right? : No. : Okay, so it’s a different group? : Mhm…. Arriv… um, see, I think it’s arrival assessment. : Okay. : Does all that. [AFSEC Rep] : Uh, so you, if you were going out to do your assembly and you, you had all your parts to do it, um, is the expectation based on that drawing, is that you guys, you’re working with only new parts or do you sometimes, do you sometimes get refurbished parts or parts that came off the airplane before? [Mishap Mechanic] : I’ve been doing it so long that it used to be more of we’re using these parts because the kits weren’t required to have so many new parts, you know, and still, till like right now like that, to that galley you’ll have now there’s a brand new line going down but them two lines that come across are still the original parts. Those aren’t new. So you still have a couple original parts. You still have a couple original fittings that go in there because there still attached to those lines and they don’t come in the kit so that’s what you’re supposed to use. I mean, granted they’re still capped, bagged, and stuff when they’re removed but I personally don’t, they wa, I don’t remove that si, my part of my job, mine is reinstalling it. [AFSEC Rep] : Okay. And then during your, your reinstallation, what do you, what do you guys use as a reference to inspect parts if you can tell that they’re not brand new? I mean does your, does your work document, does that cover, if reusing parts, inspect for X, Y, and Z, or do you have to use maybe like a different reference to inspect those parts? The used ones of course. [Mishap Mechanic] : Well, um, me personally I always inspect them, make sure that, you know, they’re not cross-threaded, um, corrosions on it, um, you know of course basically if I, if I get the line, I can see the, the bag’s open, I’m not going to use that. I mean that’s, I might throw out a DR to get a brand new part because there’s no way I’m going to use that part. That’s the, I mean, I, I, I’m not sure if my ticket actually says to inspect or not but that’s the process, one of the processes we do when it first comes in. [AFSEC Rep] [Mishap Mechanic] [AFSEC Rep] [Mishap Mechanic] [AFSEC Rep] : Okay. Like the one that, the one that he showed you there… : Yeah. : Do you, would, do you see any issues with that one or is that one… : Me? : Would that be one that you would install? R-295 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Mechanic] : I, I, I basically, I wouldn’t think I would install this because it’s all scuffed up and everything, and… [AFSEC Rep] [Mishap Mechanic] : You would not? : No. [AFSEC Rep] : Okay. Um, and then my, my other question was the torqueing procedure, uh, when you guys, you guys, so you guys go around and put an initial torque on all the, on all the lines, right? [Mishap Mechanic] : Mhm… [AFSEC Rep] : And then I, I think I remember from our visit out there that you guys pressurize the system with nitrogen… [Mishap Mechanic] : Yes. [AFSEC Rep] : as a leak check, so you’re not using oxygen? That sounds like a great procedure. And if you guys, so if it, if it pressurizes and it holds it, then that initial torque that you guys out on, the 50 in/lbs or whatever is where you guys leave it. It’s only when it fails that you guys go around and do, uh, like 100 in/lbs torque or something on it? [Mishap Mechanic] : Well, we go by and, uh, once we get it on, like I was telling him, you know, we, we torque them. [AFSEC Rep] [Mishap Mechanic] [AFSEC Rep] [Mishap Mechanic] [AFSEC Rep] [Mishap Mechanic] [AFSEC Rep] [Mishap Mechanic] [AFSEC Rep] [Mishap Mechanic] : Torque them to… : To, to, to what it says on here? : The first torque? : Yes. : Okay. : Torque it and then if it leaks more then we put, we torque it like a little bit more. : Then go up to… : Ye, yes. : the second torque? : Mhm… [AFSEC Rep] : Okay. And then I, I understand the torque stripe thing. That’s, those are the only two question I had though. Appreciate it. [Investigating Officer] : So, uh, one question if you don’t mind. [Mishap Mechanic] : Yeah. [Investigating Officer] : Uh, you were explaining how there’s situations where some of the components, or you said in the past some of the components would be still on the airplane when you get out there to do the installation. [Mishap Mechanic] : No, not still on the airplane. They’re existing… R-296 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Investigating Officer] : Okay. [Mishap Mechanic] : like, um, we got cap’s crib down. We had, when we have them, um, like when I remove the parts, we didn’t have as many new parts. Like on a ticket that when we’re requ, required to put so many new, uh, basically new lines… [Investigating Officer] : Right. [Mishap Mechanic] : You know now since they, since they changed so many different designs that we’ve, basically eliminate this line and build a new line. But back then, before we had that new line it would be existing line, so, for example, on the left hand side on the racks they used to be all the same O lines. [Investigating Officer] : Okay. [Mishap Mechanic] : So we each put them in. Now I think there’s only like one existing line there and the rest are new. [Investigating Officer] : Okay. I think that, uh, I’m good. [Mishap Mechanic] [Investigating Officer] : And the torque stripe thing… : Mhm… [Mishap Mechanic] : I personally myself, I actually like the torque stripe because it shows if anybody, you know, broke it open or anything. And that was what I told, uh, uh, Body. I said because without it there I don’t know if somebody broke it loose and all of a sudden that was loose and now it’s me. I can’t see it. [Investigating Officer] : Mhm… [AFSEC Rep] : And that was, you said that was a new found change? Like they had just implemented that? [Mishap Mechanic] [Investigating Officer] : Mhm…Like a couple of planes ago. Yeah. : I’ve got one more. [Mishap Mechanic] : Yep. [Investigating Officer] : So you said, um, in the past the kits or the about amount of parts that you would reuse are greater than currently. [Mishap Mechanic] [Investigating Officer] : Um, because of process changes and all that? [Mishap Mechanic] [Investigating Officer] : Changes. : Has it been, how long has it been? Just kind of evolved slowly over time? [Mishap Mechanic] [Investigating Officer] : Yes. : Mhm. It’s different changes. : Okay. Thanks. [Maintenance Member] : These, excuse me, these, uh, write ups here, I mean these, uh, I forget the name… [Mishap Mechanic] : Adels? R-297 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Maintenance Member] [Mishap Mechanic] : Mhm. [Maintenance Member] [Mishap Mechanic] : You install the Adel… : Mhm. [Maintenance Member] [Mishap Mechanic] : Adels. : yourself? Or do you have to get sheet metal to do it? : No, we do it. [Maintenance Member] : Okay. And again, I mean I asked you earlier are you, do you know if every single aircraft, if our Rivet Joint comes through, should have those two according to the drawing right, right here, right here? [Mishap Mechanic] : I don’t know if everyone does because I don’t do every single… [Maintenance Member] [Mishap Mechanic] : one. [Maintenance Member] [Mishap Mechanic] : had one here… : They should be secured because that would be too, too loose just hanging there. [Maintenance Member] [Mishap Mechanic] : Have the ones you’ve done… : Yes. [Maintenance Member] [Mishap Mechanic] : Alright. : Right. : Yeah, it should be secured, should have a green, like sleeve on it. [Maintenance Member] : Mhm. The, uh, in your opinion, if it wasn’t cinched down, what do you think the effect would be on that line? [Mishap Mechanic] : Um, this won’t be secure, and this one, it, this one right here on the side will be secured. [Maintenance Member] [Mishap Mechanic] : This basically we just have a li, like play, just to move around. [Maintenance Member] [Mishap Mechanic] : Right. : Right. : Not much though because it’s not that long and it goes straight up. [Maintenance Member] : Right. [Mishap Mechanic] : So I mean it was, but it’s, it’s on, it’s on top of the galley too. I mean it would, it would, when it’s secured there, I mean it’s, it’s not moving around at all. [Maintenance Member] : Right. Uh, if it’s allowed to move, do you think it has the ability to allow the B nuts to release off the other assembly and cause the assembly to go apart if it’s not secured and just, you know? Thinking, because it, I’m curious. [Mishap Mechanic] : I don’t think it could. No, because one’s like this and the other one’s down here. [Maintenance Member] : Mhm. R-298 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Mishap Mechanic] : I don’t, I mean I don’t see how it could. [Maintenance Member] : Okay. [AFSEC Rep] : Sir, on the top of the galley, if you guys don’t already have holes in the top of the galley, would you drill them to install those clamps? [Mishap Mechanic] : Yes. [AFSEC Rep] : You guys would… okay. That’s all I was wondering. Because if they weren’t there, and somebody was going in there, and there was a conflict between the guidance that shows I should have 3 or 4 clamps here, but there’s no holes in the galley, where am I going to hook these things to? So you, you guys would make the print match that airplane, drill some holes? [Mishap Mechanic] : Yes. [AFSEC Rep] : Okay. [Maintenance Member] [Mishap Mechanic] : No. We get the prints on time with us. [Maintenance Member] [Mishap Mechanic] : When you guys do the work do you see these prints? Or are you just kind of… : Okay. So you see the prints. : And we already make sure they’re up there, you know, because they got changes and stuff. [Maintenance Member] [President] : Alright. : I have no questions so I’m good. [Maintenance Member] : Yes sir. Anything else you’d like to add sir? Alright. If anyone, if no one has any further questions we will now conclude this interview. Sir, I’d like to remind you again that you are not offered a promise of confidentiality and that your statement is not protected and will be released to any follow on investigation of this mishap and may be releasable to the public subject to the Freedom of Information Act. We request you refrain from discussing your testimony and any information shared with you today regarding the mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information and thank you for your time. [Mishap Mechanic] : Okay. R-299 V. 64-14848, Class A, 30 April 15, AFSAS #739726 R18.l. SIB NON-PRIVILEGED INTERVIEW - 26 MAY 15 Memorandum For Contractor Representatives Serving As Technical Experts To Safety Investigations. MEMORANDUM FOR [Quality Control Manager] MID (Sir/sun? came. (Nan-Air Force technical expert?s full name and company/organization) ?26m! new [Kw/354,4 (MW ifs/y; e372)! as" SUBJECT: Privileged Safety Information 1. In response to my request for technical assistance, the Air Force and your employer have agreed that you will serve as a technical expert for the Safety Investigation Board over which 1 preside. Unless you speci?cally identify information in any technical report you provide to the SIB as proprietary data or con?dential analysis or opinion. it will be included in the releasable portion (Part 1) of the 813?s ?nal report. If you want us to treat any part of your report as privileged information so we can protect it from disclosure outside the Department of Defense, you must speci?cally request such protection. in such case it will be included in the privileged portion (Pan 2) of the formal safety report and will be used solely for mishap- prevention purposes. 2. The military safety privilege protects information provided under a promise of con?dentiality and the. deliberative process of the SIB. It enhances the 813?s ability to identify potential causes of mishaps quickly and accurately so we can prevent their recurrence. This process must have the highest degree of reliab?ity to maintain combat readiness. national security. and public safety. 3. In accepting your appointment to serve as technical expert. you must also agree to safeguard our safety privilege. You may be given access to privileged information and you must not disclose to anyone, including your employer. any privileged information derived from our investigation. You will prepare only one copy of your technical rcpon for the SIB. You will destroy or to me any notes, documents, computer ?les, or other materials, produced or obtained during this investigation. if they contain privileged information. You must net make copies of any privileged documents (including analytical computer products. con?dential tape recordings. and staged photographs) for use outside the proceedings of this board. You may not have a cepy of Part II of the Board?s ?nal report or any part of a dra? thereof. You must report to me (or, after the 813 is dissolved, to HQ Air orcc Safety Center) any attempt by anyone, other than a SIB member or other duly authorized person, to obtain any con?dential or deliberative information from you about this investigation. 4. Before beginning your service to this SIB, please sign and date the endorsement below. I will give you a copy of this memorandum. R-300 V, 64-14848, Class A, 30 April 15, AFSAS #739726 6113 President ?3 signature block) Endorsement To: 509/6? ?zsm/eML ?4 y. 21: gay (SIB President) (Date) I acknowledge understanding of the contents of this memorandum and receipt of a capy thereof. and I agree to comply with the duties and responsibilities stated therein. hechnical exped 's signature block) R-301 V, 64-14848, Class A, 30 April 15, AFSAS #739726 NON-PRIVILEGED WITNESS STATEMENT 21;, $1 I [Quality Control Manager] (Date) I. . have been advised by [Mammn?je Memm?l (Name, Grade, Organization. of Witness) Wattle of Investigator) a safety investigator of the mishap that occurred on 30:53: involving new 48% (Dale) (Equipment SN) This investigation is being conducted under the provisions ofAFl 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand lam being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. [Quality Control Manager] New (Law, Firm, MD and Rank/61E Comma? Mom eat- Durv Title o'rgnature R-302 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of Mr. [Quality Control Manager] Role: Quality Control L3 Interviewers: (President) (Investigating Officer) (Maintenance Member) (AFSEC Representative) Date: 26 May 15 [Maintenance Member] : This is a non-privileged interview with [Quality Control Manager] being conducted on Tuesday 26 May 2015 by Lieutenant Colonel [Maintenance Member] for the safety investigation board convened for the recent mishap. We’re investigating the mishap involving an RC-135V, aircraft 4848 that occurred on 30 April 2015. This investigation is being conducted under the provisions of Air Force Instruction 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of confidentiality is not being extended to you. Your statement can be released to any subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [Quality Control Manager] : Yes sir. [Maintenance Member] : For the record, would everyone present introduce yourself by stating your name, rank, and affiliation with the board starting with the witness. [Quality Control Manager] : I’m [Quality Control Manager] . I’m a quality control manager here at L3 Mid. [President] [Investigating Officer] : Colonel : Captain [AFSEC Rep] , Board President. , Investigating Officer. : Chief Master Sargent Air Force Safety Center representative. [Maintenance Member] : Lieutenant Colonel , the Maintenance Member. The documents that you have in front of you, uh, illustrate a few things. Let me refer to the drawings first because I have a particular question about the fittings that attach this hose assembly to the galley. [Quality Control Manager] : Mhm… [Maintenance Member] [Quality Control Manager] : On some aircraft that we’ve seen, these two Adels… : Yes sir, Adel clamps. [Maintenance Member] : are there. According to this drawing, the Adels are supposed to be there. But on some other aircraft we found them absent. Is it a requirement to have those there, in your, in your opinion? [Quality Control Manager] : Uh, looking at this drawing, these two here are required. [Maintenance Member] [Quality Control Manager] : Yes sir. : Yes sir. R-303 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Maintenance Member] : Okay, that pretty much puts the drawing to bed. We obviously are trying to get clarification on how, or what is the procedure to properly torque these, the hose assembly and the tube assembly together. So, judging from the, from the document that you have on the left, which is the TPS 3-100, what is the procedure that technicians would use to torque and what are the specifications of torque? I.e. what’s the minimum? What’s the maximum? And how do they arrive in that range when they’re torqueing plumbing systems and oxygen lines? [Quality Control Manager] : Okay, referring to the TPS 3-100… [Maintenance Member] : Yes sir. [Quality Control Manager] : Uh, when we’re talking about, uh, connections to initial torqueing, which is 3-4-1, it does say to hand-tighten them, uh, originally, until the seal was firmly together. Then of course the nuts shall not… shall have an initial torque of 50 plus or minus 10 in/lbs prior to doing any pressure testing to it, according to this. And of course you do have a final torqueing. And the final torqueing’s just talking about repeating, tightening, and re-torqueing to eliminate leaks while not to exceed the 100 in/lbs. And then of course it says to repair or replace as necessary if leaks do occur. [Maintenance Member] : Yes sir. [Quality Control Manager] : And of course it refers you to, um, 4-5-1, which is a table, which is table 2. And it talks about the, uh, different size tubings and it looks like where they’re going with a, a 5/16th aluminum tubing. And it does talk about, uh, AMS 4071 aluminum. A minimum torque would be 100 in/lbs with a maximum of 125. [Maintenance Member] : Yes sir. [Quality Control Manager] : So initial torqueing would be 50, going through its pressure testing, and continuing repeating the tightening up to a minimum of 100 in/lbs. That’s the way I read the TPS. [Maintenance Member] : Roger that sir. Are there any scenarios where technicians would stop at 50 and not go to the range of 100-125 in/lbs? [Quality Control Manager] : I don’t see any, anything here that draws me to where they would stop. Uh, with my experience out on the floor, uh, I wouldn’t assume someone would. Uh, I would think he’d go to the minimum. Even after you’re doing your, your, your pressure testing, and no leaks, I would say you’d have to go to 100 in/lbs before you can call that tasking complete… [Maintenance Member] [Quality Control Manager] : Roger. : with no leaks. [Maintenance Member] : If it leaked at 100 what does that publication tell you to do? How do you proceed if you’re going to, if you, if you have it torqued at 100 and it’s still leaking, what’s your procedure then if it says, uh, not to exceed 100? [Quality Control Manager] : If it says not to exceed 100 in/lbs? [Maintenance Member] [Quality Control Manager] : Uh, if a leak occurs, it says repair or replace as necessary. [Maintenance Member] [Quality Control Manager] : Yes sir. : Okay. : That, it’s what the procedure physically says here. R-304 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Maintenance Member] : Okay. [Quality Control Manager] : Even though that the table does say maximum 125, I read nec… I wouldn’t go any further. I’d, I’d have to stop what I’m doing. [Maintenance Member] [Quality Control Manager] : Or I, go get repaired or replace it. [Maintenance Member] [Quality Control Manager] : Alright. : Right. : But my torqueing I’ll, shouldn’t go any higher because it says not to exceed. [Maintenance Member] : Yes sir. So if the torque is at 90, and the document says that it needs to be between 100 and 125, would you think that the document itself would be flawed with that reasoning? [Quality Control Manager] : Looking at this I would say, because this is telling me not to exceed 100… [Maintenance Member] : Yes sir. [Quality Control Manager] : So, if I was reviewing this as finalized in a document I would say this here is, uh, contradicts what this paragraph here says. [Maintenance Member] [Quality Control Manager] : 3-4-2. [Maintenance Member] [Quality Control Manager] : Roger that sir. And anoth, another question going back to the fittings… : Okay. [Maintenance Member] [Quality Control Manager] : Roger that. : uh, the Adels… : Mhm… [Maintenance Member] : If these Adels are absent, do you think that it, the, the fittings themselves, the nuts are not attached with the proper torque that it could back off… do move it a little bit? [Quality Control Manager] : I, I, I would think you, you would have to say it, it could… [Maintenance Member] [Quality Control Manager] : Very big possibility because we all understand vibration. [Maintenance Member] [Quality Control Manager] : Yes sir. : It could, if I didn’t have my minimum torque. [Maintenance Member] [Quality Control Manager] : Yes sir. : Roger that sir. For, uh, the illustration on your left… : Okay. [Maintenance Member] : we’ve been, we’re curious about this fitting. I can’t find that fitting in the oxygen ticket… [Quality Control Manager] : Okay. [Maintenance Member] : as a listed part. Do you recognize that fitting and would you think that it would be a part of this ox, oxygen systems that are installed here? R-305 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Quality Control Manager] : Well, without seeing a part number I would think that’s the AN T fitting. But, could, I just know that the T fittings that’s on these, if I remember correctly, like 8N, 824s. But I don’t see them on here. [Maintenance Member] [Quality Control Manager] : Yeah. [Maintenance Member] [Quality Control Manager] : Weatherhead. : Huh. Would that be the name brand or is that just what they’re calling it? [Maintenance Member] [Quality Control Manager] : These are known as Weatherhead. Have you ever heard of that? : No. [Maintenance Member] [Quality Control Manager] : But if, if I’m not mistaken… let me borrow this for a second… : Uh, a name brand, uh… : Okay. [Maintenance Member] : and apparently, eh, an aged company, that, and the fitting hasn’t been produced for some time… [Quality Control Manager] : Okay. Hmmmmm. [Maintenance Member] : So one of the questions that we’ve been asking, uh, uh, a few different individuals is when we’re installing oxygen systems they’re kitted. [Quality Control Manager] : True statement. [Maintenance Member] : So are all of the pieces of the system new or are some of them old pieces that were good? What’s the requirement? [Quality Control Manager] : It really, its, it bases down to our BOM, the building material. [Maintenance Member] : Yes sir. [Quality Control Manager] : Uh, it will tell me new kitted, or, or how, or, or whatever it says. A new will come packaged up in original package. Um, these normally do come new. Just by experience of being here, I, they normally do… [Maintenance Member] : Yes sir. [Quality Control Manager] : uh, for the oxygen system. Um, and it also boils down to a removal list because a removal list, as a mechanic, tells them what to do with that component… [Maintenance Member] : Roger. [Quality Control Manager] : Scrap it, retain it, return it to the customer, whatever. And then that flows down to the install ticket because if it’s retained then it will stay on here that this, it’s existing. [Maintenance Member] : Yes sir. [Quality Control Manager] : But sometimes, I don’t want to say it’s confusing, but sometimes when we use the word ex, existing it’s obtained through a mod so it could be a new part. And we go through, um, I don’t see one here but the building material from the drawing itself. And, and it calls out a specific part number. And that’s usually what’s issued to a mechanic. [Maintenance Member] : Yes sir. Have you seen this type before? R-306 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Quality Control Manager] : I, I really, I really couldn’t say. [Maintenance Member] : Or let me, let me, let me ask you a better question. If you were to go out and see that fitting on one of your aircraft how would you respond? [Quality Control Manager] : If I was inspecting it… [Maintenance Member] : Yes sir. [Quality Control Manager] : and there’s no known part number on it or known, um, marking features that I, that I recognize, then I would have to have somebody investigate that fitting… [Maintenance Member] : Yes sir. [Quality Control Manager] : or whatever that component may be. But in this case, with me not seeing a part number or, or recognizing the symbol… [Maintenance Member] [Quality Control Manager] : Uh, I would have to raise that question. [Maintenance Member] [Quality Control Manager] : Right. : Roger that. : Knowing that I’m looking at it… [Maintenance Member] : Yeah. [Quality Control Manager] : I mean it’s… but I, I’m really trying to, that symbol’s really what I’m looking at, uh, it’s hard for me to give you a positive answer on that one. That’s hard to say. [Maintenance Member] [Quality Control Manager] : Yes sir. : That’s hard to say. [Maintenance Member] : Yes sir. [AFSEC Rep] : As far as the way that it looks, if it, if it had AN markings on it, sir, would this, I mean would this pass the, your guys’ guidance for inspecting the part before you put it back in? [Quality Control Manager] : The mechanic on the floor, if, if they can positively identify it… [AFSEC Rep] [Quality Control Manager] : then they can use it. [AFSEC Rep] [Quality Control Manager] : If it, let say… : Okay. : If, if they, they’re taught that if they have no clue what it is, it’s no longer a good part. [AFSEC Rep] : Okay. Appearance wise though I mean it looks like… [Quality Control Manager] : Appearance wise, I mean, all four of them are close, and if it doesn’t have a part number or a, a known symbol, you know some manufacturers have symbols, than I would hope that a mechanic would raise that concern or even an inspector, uh, raise that concern. [Maintenance Member] [AFSEC Rep] [Quality Control Manager] : Yes sir. : But the condition of the part looks okay? : That? Uh, I wouldn’t use that for myself, the way it looks in this picture. R-307 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [AFSEC Rep] : Not, not specifically the part number but just the condition of it? [Quality Control Manager] : The condition of it, I wouldn’t. Not to put on a, an aircraft, uh, for leaving. I mean, I’ve seen them come in and then remove them, inspect them, and say it’s not, uh, uh, it’s not serviceable. [Investigating Officer] [Quality Control Manager] [Investigating Officer] : Based on what? : The condition of it. : Well, I mean, okay. [Quality Control Manager] : Yeah. I don’t, I personally don’t recognize the symbol so I, it’s hard for me to comment on that. [AFSEC Rep] : From a, from a quality standpoint, do you guys, do you guys have a requirement after the technicians install the stuff to go back out to the airplane. Do you guys specifically look at this, like, oxygen system plumbing, like the life-sustaining, uh, piece of the airplane? [Quality Control Manager] : Not in detail to… [AFSEC Rep] [Quality Control Manager] : Okay : part numbers… [AFSEC Rep] : Okay [Quality Control Manager] : and things of that nature. Uh, our concerns is touchy, feely, grab, twist, uh, blueprint stuff, securing that type of stuff when we’re looking at it. [AFSEC Rep] : So you guys would, you guys would take a print and if there were, you guys, it would be within your scope to identify missing hardware or… [Quality Control Manager] : Yes sir. [AFSEC Rep] [Quality Control Manager] : Okay : In, in a quality, when I’m, when I’m looking at a, at a closeout. [AFSEC Rep] : Okay [Quality Control Manager] : Now if I’m auditing a process I’m just making sure the, the mechanics are following our processes and procedures. [AFSEC Rep] : Something that’s in work versus we’re getting ready to deliver the airplane… [Quality Control Manager] : Correct. If I’m flying over shoulder, just like the military quality program, I’m over the shoulder watching that individual follow, uh, tech data versus what he or she is doing. [AFSEC Rep] : Okay. So let’s just assume this airplane’s getting ready to go home. You take their, their tickets out and you, you go line by line through their ticket or do you guys have a separate, a separate QC? [Quality Control Manager] : Uh, uh, it, we only got one QC. So our role, uh, as quality control… [AFSEC Rep] : Mhm… R-308 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Quality Control Manager] : is we have an audit plan, uh, and, uh, our plan is obviously to determine the health of the program. So we do what we call final audits and in-process audits. [AFSEC Rep] : Okay. [Quality Control Manager] : In-process audits is the mechanics physically working it. Final audits is the paper work’s coming through our office. We do 100 percent paperwork trail. Uh, but we do, uh, sampling. So if this has been stamped off I would carry it to the work area and follow it, so, I’d be looking at drawings making sure that the routing, securing, and all that’s done. Uh, part numbers sometimes are very hard to determine it would have the correct part. We lean 100 percent on our, uh, certified mechanics. Easiest way to put it, uh, our certified program here, uh, person that’s not certified is a 3-level… [AFSEC Rep] : Right. [Quality Control Manager] : in the Air Force. Level 1 is a 5-level, level 2 is a 7-level. So that 7-level, when they sign it off it’s, it’s there and it’s certified as good. [AFSEC Rep] : Okay. [Quality Control Manager] : Uh, quality’s just there to determine the health of the program. Then on the flip-flop side we also have the, the closeout process. So everything that’s identified as safety of flight, uh, we, we 100 percent look at it. Then we turn around and present it to the 645th. Then they do the same thing with it. [AFSEC Rep] : So and then, in the case of this oxygen system installation at the galley, you guys would have looked at all that installation? [Quality Control Manager] : We would only look that, all this detailed stuff, if we would have done a final or an in-process. [AFSEC Rep] : Oh, okay. [Quality Control Manager] : On the, on our company closeout for this work area, which is 1160-1360, 200 inches floor to floor. So we look at the whole floor and that’s one closeout and we call it a final. [AFSEC Rep] [Quality Control Manager] : Okay. : So they present it to us and we go up and look at everything you can see. [AFSEC Rep] : Right. [Quality Control Manager] : We don’t dig into it. And when we’re satisfied that it meets our process and procedures and tech data we turn it over to the 645th and they do the same. So we’re not looking at part numbers… [AFSEC Rep] [Quality Control Manager] : and detailed stuff. Securing is one of the things that we are looking at. [AFSEC Rep] [Quality Control Manager] : Right. : Do you guys know if you, if you happen to look at this particular area on… : RJ1? [AFSEC Rep] : 4848 yeah. R-309 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Quality Control Manager] : We did look at, uh, the company file, 1160-1360, uh, under the mandatory call that we call in our book, uh, in our mandatory call book, um, 1160-1360 electrical company finals. [AFSEC Rep] : Does that include this particular area or is it? [Quality Control Manager] : We would look in this area for, uh, securing, uh, routing, uh, and then of course category separates, uh, electrical. We’re making sure electrical and oxygen lines aren’t touching. Secured together, things of that nature. [AFSEC Rep] : Okay. What, what criteria do you guys use for the, for the separation of oxygen lines and like electrical wiring? [Quality Control Manager] : Well we got TPSs that we go through, uh, drawings, and then, uh, tech data if it covers it in, in one of the TOs. [AFSEC Rep] : In one of, like the, in this case maybe, uh, 1-1A-14 for electrical wiring or... do you guys go to those… [Quality Control Manager] : Uh, we use it as a general… [AFSEC Rep] : Right. [Quality Control Manager] : Uh, if we don’t have a drawing or a TPS on our mod stuff, then, then we would go to the general 1-14. [AFSEC Rep] : Okay, but… [Quality Control Manager] : But, but if it’s aircraft where we don’t do the modification to, then it’s all TO. If it’s a mod that we do, it’s drawings and TPSs. [AFSEC Rep] : Okay. So in this case where, uh, you, you probably didn’t modify the oxygen system, but it’s being routed through your modifications, you guys normally wouldn’t allow the oxygen lines to rest against those harnesses? [Quality Control Manager] : No sir we wouldn’t. And, and, and we say it wasn’t modded, but that’s out mod. [AFSEC Rep] [Quality Control Manager] : L3 put that system on. [AFSEC Rep] [Quality Control Manager] : Right. : The harnesses or the… : Both, the harnesses and oxygen. [AFSEC Rep] : Okay. [Quality Control Manager] : The oxygen system, uh, isn’t a Boeing routing where it’s at now so L3 at one point put it on. So it, it follows our TPS. [AFSEC Rep] : Do you know what the separations are just off hand like the minimums or anything or… [Quality Control Manager] : I’m a big guy that says 1 inch minimum on a generic when I’m looking. When it gets to category separations and oxygens I usually look it up then go out there, try not to memorize it. Because we got too many out there. [AFSEC Rep] : We may, we may ask you to just, if you can provide that to us or pinpoint, you know, where those, where that criteria is… R-310 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Quality Control Manager] : The criteria for separation? [AFSEC Rep] : and get it back to us, yeah. I would, I would definitely appreciate that document. That’s, that’s all I have. [President] : So the only question that I have had, is to kind of clarify that you guys basically do a spot inspection, instead of all them, as far as the QC process before it goes to the 645th? [Quality Control Manager] : Uh, we, we call them closeouts. [President] [Quality Control Manager] : Okay, but that’s a spot insp… : We look at the whole are, yes sir. [President] : Okay. [Quality Control Manager] : We’re not detailing any specific, uh, tasking, or, or closeout. Um, the ones that are identified as needing those specifics are on the tickets themselves then they’re called out as a customer mandatory call. And, uh, the 645th identifies what they want to see in those purposes. And then our safety of flight program identifies what is considered safety of flight and they have to look at it too. [Investigating Officer] [Quality Control Manager] [Investigating Officer] [Quality Control Manager] [Investigating Officer] [Quality Control Manager] [Investigating Officer] [Quality Control Manager] [Investigating Officer] [Quality Control Manager] : Have you, have you seen a leak check performed on these systems? : Uh, I personally have, yes sir. : How? : We got two sets of them. : The, the fluid that you use to perform those… : Okay. : do you know what kind that is? : It’s, it’s, it’s called right out of the, the TO. It’s that soap and water mixture… : Okay. : and we got it in, in little squirt bottles and we squirt all the fittings, elbows, T fittings, B nuts. [Investigating Officer] : Is that purchased or is it made here? Like… [Quality Control Manager] : I’ll, I, that should be purchased here because if we got it in big gallon jugs that we pour into our little squirt bottles. [Investigating Officer] [Quality Control Manager] [Investigating Officer] [Quality Control Manager] [Investigating Officer] : Okay. : So it’s a vendor, you know, we purchase it… : Got it. : and vendors bring it in. : Thanks. [Maintenance Member] : If no one has any further questions we will now conclude this interview. I’d like to remind you again that you are not offered a promise of confidentiality and that your R-311 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 statement is not protected and will be released to any follow on investigation of this mishap and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony and any information shared with you today regarding this mishap to avoid the possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [Quality Control Manager] : Thank you sir. R-312 64-14848, Class A, 30 April 15, AFSAS #739726 [Materials 8. Processes Engineer] R19.l. SIB NON-PRIVILEGED INTERVIEW - 26 MAY 15 Memorandum For Contractor Representatives Serving As Technicnl Experts To Safety Investigations. MEMORANDUM FOR Ewngig'gammsses I L's (Now-Air Farce technical expert'squ name and company/organization) DA) FROM. (0755/) (SIB President) SUBJECT: Protection of USAF Privileged Safety information I. in reSponse to my request for technical assistance, the Air Force and your employer have agreed that you will serve as a technical expert for the Safety tnvesrtgation Board (SIB) over which I preside. Unless you speci?me identify information in any technical report you provide to the SIB as proprietary data or con?dential analysis or opinion, it will be included in the releasable portion (Part I) of the 818's ?nal report. If you want us to treat any part of your report as privileged information so we can protect it from disclosure outside the Department of Defense, you must speci?le request such protection. in such case it will be included in the privileged portion (Part 2) of the formal safety report and will be used solely for mishap- prevention purposes. 2. The military safety privilege protects information provided under a promise ol'con?dentiality and the deliberative process of the SIB. ll enhances the 513's ability to identify potential causes of mishaps quickly and accurately so we can prevent their recurrence This process must have the highest degree of reliability to maintain combat readiness. national security. and public safety. 3 In accepting your appointment to serve as technical expert, you must also agree to safeguard our safety privilege. You may be given access to privileged information and you must not anyone, including your employer, any privileged information derived nom our investigation. You will prepare only one copy of your technical report for the SIB. You will destroy or surrender to me any notes, documents. computer ?les, or other materials, produced or obtained during this investigation, if they contain privileged inf'onnation- You mist not make copies of any privileged documents (including analytical computer products. con?dential tape recordings, and staged photographs) for use outside the proceedings of this board. You may not have a copy of Part II of the Board?s ?nal report or any part of a dra? thereof. You must report to me (or. after the SIB is dissolved, to Air Force Safety Center) any attempt by anyone, other than a SIB member or other duly authoan person, to obtain any con?dential or deliberative information from you about this investigation. 4 Before beginning your service to this SIB, please sign and date the endorsement below I will give you a copy of this memorandum. R-313 V, 64-14848, Class A, 30 April 15, AFSAS #739726 (SIB President?s signature black) ls! Endorsement acknowledge understanding of the contents of this memorandum and receipt of a copy thereof, and I agree to comply with the duties and reaponsibililies slated themein. (Technical expert '5 signature block) R-314 V, 64-14848, Class A, 30 April 15, AFSAS #739726 NON-PRIVILECED WITNESS STATEMENT [Materials Processes (Date) 1. 1. Engineer] have been advised by [Ma'mmanw Meme? (Name, Grade, Organization, of Witness) (Name of Investigator) a safety investigator of the mishap that occurred on 3' ?(i1 5 involving Edgy Mr- 908% (Dale) (Equipment 4! SM 3. This investigation is being conducted under the provisions of AF I 91-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. b. My witness statements (written or verbal) may be used for any valid purpose and be released to any Subsequent investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. [Materials 8. Processes Engineer] Name (Last, First. MI) and Rank/Grade 2? Vila-c.6556 EA Qtae??k Dun Title Signature R-315 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 & Processes SIB Interview of [Materials Engineer] Role: Materials and Processes Engineer L3 Interviewers: (President) (Investigating Officer) (Maintenance Member) (AFSEC Representative) Date: 26 May 15 [Maintenance Member] & Processes : This is a non-privileged interview with [Materials being conducted on Engineer] Tuesday, 26 May 2015 by Lieutenant Colonel for the Safety Investigation Board convened for the recent mishap. We're investigating the mishap involving an RC-135 aircraft 4848 that occurred on 30 April 2015. This investigation is being conducted under provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of confidentiality is not being extended to you; your statement can be released to any subsequent investigation of this mishap and may be released to public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [Materials & Processes Engineer] Yes sir. [Maintenance Member] : For the record would everyone present introduce yourself by stating your name, rank, and affiliation with the board, starting with the witness. [Materials & Processes Engineer] Uh my name is engineering group for L3 mid. [President] : Colonel [Investigating Officer] Captain [AFSEC Rep] , I work as a chemical engineer for materials and processes , Board President. , Investigating Officer. : Chief Master Sergeant Air Force Safety Center Representative. [Maintenance Member] : And I am Lieutenant Colonel , and I am the maintenance member. Addressing torque values that are listed in TPS3-100; from the way that the document is written, how can a technician take what is written and apply it to uh the physical act on the aircraft with reference to how torque values are applied to- to connectors in the oxygen system? [Materials & Processes Engineer] They should have some sort of torque value checker when you’re- the initial torque is 50 +/- 10 inch pound. So they should use some sort of torque value checker that will definitely tell them what the value is. [Maintenance Member] : Okay uh on the next page, if I could get you to turn it over...here there is a table of torque values, and in particular we’re looking at the 5/16ths line. The minimum range is 100 and the highest range is 125 inch pounds for a 5/16ths inch line. However, on the front side that we were looking at before it says the maximum that the value will be torqued to is 100 inch pounds. How would a technician uh find- what would be the physical process if a technician actually getting from 50, the initial torque value called out in that step, getting the uh- getting the connectors tightened to the torque ranges required by the table as written in the TPS3-100? R-316 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Materials & Processes Engineer] So they will keep tightening it until they get 100 inch pound. Uhm same with the torque uh with the tool in checking the torque value at the same time as you have done initially. [Maintenance Member] : If they go over 100, because we all see that 100 is the minimum required by the table then they bust the limit that’s required in the sentence in the 342. So according to what’s written, they should never exceed 100, but the minimum required by the table is 100. [Materials & Processes Engineer] Yes, so they’re shooting for the minimum torque value. [Maintenance Member] : And what we see right now is the- I don’t see a process written that takes them from 50 to 100. [Materials & Processes Engineer] Right. [Maintenance Member] : So what I’m trying to understand is, how- how would a technician be reasonably expected to take it from the initial torque to the final torque that matches the table, in your opinion; just your opinion? [Materials & Processes Engineer] : I would assume that the technician would use like a wrench, or a tool they have in the duct line or the manufacturing side and obviously checking the torque value at the same time not to go beyond the limit. So they’re using some sort of tool. [Maintenance Member] [AFSEC Rep] : Yeah, a torque wrench; clicky torque wrench. : Uhm so you’re primary function is- you draft this, right? This document, the TPS. [Materials & Processes Engineer] Uh so this is the version V, uh ya know it starts on version A, 20-30 years ago. [AFSEC Rep] [Materials & Processes Engineer] : Right. So I’m maintaining the TPS: [AFSEC Rep] : Okay, so when you guys do reviews are they like annual reviews? [Materials & Processes Engineer] Uh we do every three years unless uh someone brings up uh an issue; uh for instance: this revision V was written in 2014 uh the changes were related to quality, actually. Uh cleanliness of uh the end of the hoses where we put plastic bags. [AFSEC Rep] [Materials & Processes Engineer] : Okay. So that was the purpose of this revision written in 2014, I mean uh revised in 2014. [AFSEC Rep] : So when you guys get these and they’re- it’s for the three-year revision, do you guys, you guys pull out the tech data and you you match the- what’s your guys’ QC process to make sure all of those steps are still valid? [Materials & Processes Engineer] Uhm so uh I uhm draft a copy and we send it out to different departments including: uh quality, uh I would stress uhm uhh planning, so they all review the TPS. [AFSEC Rep] [Materials & Processes Engineer] Uhm I don’t know if you know uhm [AFSEC Rep] [Materials & Processes Engineer] : When you say quality, who are you- who is your quality? : Is he an L3 employee? Uh yes sir. Hanger dock line. R-317 ? RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [AFSEC Rep] [Materials & Processes Engineer] : Okay. We also send a copy to the 645th. [AFSEC Rep] : Okay. Who uh in the 645th gets it? [Materials & Processes Engineer] : I know uh their name uh[AFSEC Rep] and uhm there’s two other gentlemen; I can send you : Okay. [Materials & Processes Engineer] But uh all TPSs’- so uh we require at least six signatures from L3 and then it goes to uhm 645 uh and planning, system engineering, uh manufacturing, and they all review it. Uh so if we get any feedbacks we obviously uh put it back into the TPS before it gets released. h [AFSEC Rep] [Materials & Processes Engineer] : Okay so you guys- so initially you solicit the feedback Yes. [AFSEC Rep] : But there is no one that is like physically responsible for matching that document to the TO requirements? [Materials & Processes Engineer] Uhm… Not uhm on the revision state. At some point uh for example: this is state V uh maybe at C or in between somewhere uh it was added, and it was checked at that point. [AFSEC Rep] : Okay so at one point, probably early in the drafting of this document, it was a direct reflection of the tech data; and then over time it was just kind of[Materials & Processes Engineer] Yes, so uh tech data you mean the T.O.? [AFSEC Rep] : The T.O., yes. I’m sorry. [Materials & Processes Engineer] : Uh T.O., so yes. It should reflect the TO but it’s not- I don’t think it fully uh subset off of a T.O. [AFSEC Rep] : Right, it’s not- you can tell by looking at it that it’s not the exact language, but the intent is for your product- since you don’t, you- your, the employees here are not expected to pull out the RC-135 applicable tech data. All of the processes are embedded within these TPS documents. [Materials & Processes Engineer] : Uhm- [AFSEC Rep] : Other than the like ground handling and the other- [Materials & Processes Engineer] : Uhm I’m not 100% sure if all data is embedded here from the T.O. uh because we also work with part of the T.O. directly. [AFSEC Rep] : Okay. [Materials & Processes Engineer] : Uh so for example: the technician or the engineer who is working, they have access to a T.O. that they’re following directly. [AFSEC Rep] : For the most part, I mean you can see that these- it looks like a step-by-step process to get you through the work ticket; if they had to go somewhere else there’s going to be a trigger or something in there that says ‘use this other guidance.’ R-318 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Materials & Processes Engineer] : Right. And that can be- so uh that can be in the planning ticket, which mentions a T.O. specifically, or a paragraph from the TO specifically, or a work instruction part T.O. And then it also may include workpart TPS- this TPS. [AFSEC Rep] : Since the technicians, they’re not required to be familiar with the RC135 specific tech data and they rely exclusively on this, they may not realize when there is a difference, right? The only time that there’s going to- that someone might recognize a difference is if they recognize a problem with the steps that they’re complying with in here, or through the quality process somebody is identifying updates to the tech data. [Materials & Processes Engineer] Uh I would say from quality; it should come up from quality if there is a discrepancy. [AFSEC Rep] : And quality, just for the record, is- that’s the 6 L3 employees plus the- [Materials & Processes Engineer] Uh I say the hanging dock and line quality, because I’m not the uh I don’t think this TPS uhm uh contains all tech data. Uhm[AFSEC Rep] [Materials & Processes Engineer] : And the hanger dock in line process is an L3 function. Yes sir. [AFSEC Rep] : Okay. [Materials & Processes Engineer] And also the uhm I think uh a technician or engine- the technician or who is doing the work uh go by a work order uh and a planning ticket, yes something like this. So they would mention like more specifically like ‘do this set of instruction par this TO’ or this TPS or some other OEM instructions. [AFSEC Rep] [Maintenance Member] : Okay, and that is the work order of that installation of that: It is. [AFSEC Rep] : -Galley area. Okay, so if you can take a look at that and see if there is any additional or or contradicting torqueing guidance. [Materials & Processes Engineer] : (pages flipping)… Is this another reference to ZN2G12 or- [Maintenance Member] [Materials & Processes Engineer] So they’re basically referring to the drawing. [Maintenance Member] [Materials & Processes Engineer] : Those are uh to install the supports, or what they call Adels…these. : Mhm And does the drawing mention uh what work instructions? If it’s an L3 drawing most did this. [Maintenance Member] : There are TPSs that are referenced, but there’s not- not the one in particular that I see. I was just wondering if it was marked somewhere else. [Materials & Processes Engineer] : Is this- Just wondering how, what the technician; uh which work instruction, because I mentioned sometimes work- we uh list the T.O. specifically. [Maintenance Member] : Mhm. [AFSEC Rep] : And in this case there’s no, so we we’re not seeing any- any reference to any other guidance forR-319 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Materials & Processes Engineer] Yeah, uh usually somewhere; I’m sure there’s somewhere the technician would find a reference for a work instruction. [AFSEC Rep] [Materials & Processes Engineer] : This isn’t considered a work instruction? Yeah, so it would say ‘TPS3-100’, for example. Uh a T.O. number or some of the TPS [Maintenance Member] [Materials & Processes Engineer] : The technicians we’ve talk to so far, they’re familiar with that in particular. : Okay. [AFSEC Rep] : In this, since there are instructions that make it into this document, are they based on the guidance in the TPS3? [Materials & Processes Engineer] : Uh 3-100? [AFSEC Rep] : Like the special- special guidance or special wording in here that for the completion of the task is it- does it stem from these documents? [Materials & Processes Engineer] Uh. If it’s like for each one, like installing oxygen systems, yeah. Yeah. [AFSEC Rep] : Right. If there is a like some caveats in here or something- [Materials & Processes Engineer] Uhm yeah, most likely. Uh I mean I’ve seen uh for example paint uh I’ve seen we follow T.O. 118 or 11691 very closely and we specifically mention them in the plane ticket. [AFSEC Rep] [Materials & Processes Engineer] : Okay. So they would open up a T.O. and look at the T.O. instead of our uh TPSs. [AFSEC Rep] : Okay. And we’re looking at work order… [Materials & Processes Engineer] So I was trying to find uh what exactly the work instruction was, and uh so it mentions ZN2G12 uhm… [AFSEC Rep] [Materials & Processes Engineer] : But, for the record, we’re looking at work order number- 76596949. [AFSEC Rep] : Okay. And I guess my overarching question is: when you’re reviewing the TPSs and there is an affected work order out there, do those as companions; are they reviewed at the same time? [Materials & Processes Engineer] It should, yeah. [AFSEC Rep] [Materials & Processes Engineer] : So if I make changes here that they reflect- : Or if it doesn’t, then I would hear back from whoever is working it or quality- [AFSEC Rep] : So they’re trying to accomplish the steps, they would see conflicting guidance in a work order and that’s when it would come to your attention? [Materials & Processes Engineer] Right. [AFSEC Rep] : Okay. And then just shifting gears just a little bit; you said that you’re a chemical engineering background? [Materials & Processes Engineer] Yes sir. R-320 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [AFSEC Rep] : Are you familiar with any chemicals that you guys use with the oxygen system that may have chlorine in it? [Materials & Processes Engineer] Uh, what substance? [AFSEC Rep] [Materials & Processes Engineer] : Chlorine. : Chlorine, uhm. [AFSEC Rep] : Like in your leak detect, or any of that. Any process that you can think of that might have chlorine- other than just regular tapwater.. [Materials & Processes Engineer] : Anything related to oxygen system? Uhm no, not that I know of. All the materials are e, and I don’t think any of them has chlorine in it. No the grease, uh part mil spec 27617 uh for oxygen system uh I think it’s in the T.O. also uh the grease that we use; uh the thread seal tape, uhm I don’t see any other chemicals. [AFSEC Rep] [Materials & Processes Engineer] I think it’s yes water-based. Uh yeah I’m pretty sure that doesn’t have chlorine in it. [AFSEC Rep] [Investigating Officer] [Materials & Processes Engineer] [Investigating Officer] [Materials & Processes Engineer] [Investigating Officer] [Materials & Processes Engineer] [Investigating Officer] : Your leak detect it’s- usually it’s a water mixture : Okay. : I have a question for you, sir. Yes sir. : So you said uhm this particular work document- the one, TPS what is it 3-100? Yes sir. : Is sourced in some parts from the tech orders. Yes. : Is there some process that would alert you or your office if there is a change to the tech order so that- [Materials & Processes Engineer] [Investigating Officer] [Materials & Processes Engineer] [Investigating Officer] [Materials & Processes Engineer] So that we can – : incorporate the change? Yes, so uh there is not a current process that would alert us. : Okay. Uhm and since also we don’t specifically mention any T.O. in this TPS; sometimes we do, but not for this TPS. [Investigating Officer] : Okay. But the implication is that the TPS should uhm build upon the T.O., while capturing the guidance that’s in there, right? [Materials & Processes Engineer] [Investigating Officer] Right. : Okay. Just- that’s all. [AFSEC Rep] [Maintenance Member] [Materials & Processes Engineer] : I’m good. : Anything else you’d like to offer sir? Uh, no sir. R-321 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Maintenance Member] : Alright. If any- if no one has any further questions, we will now conclude this interview. I’d like to remind you again, that you were not offered a promise of confidentiality, and that your statement is NOT protected and will be released to any follow-on investigation of this mishap, and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony or any information shared with you today regarding this mishap to avoid possible spread of incomplete and counter-productive information until the board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [Materials & Processes Engineer] Can I- would you mind if I add one more thing? [Maintenance Member] [Materials & Processes Engineer] : Please. : I was just thinking about what you just said. [Maintenance Member] : Sure. [Materials & Processes Engineer] So; compliance with the T.O. uhm since we don’t mention anything specifically on the TPS uhm I’m 100%- I’m not sure how to answer your question on like compliance with the T.O. Uh sometimes we could comply with some specific T.O. that we mention in the TPS and I didn’t see any reference to a T.O. for this specific TPS 3-100. So I wasn’t sure uh I mean uh- if it’s a requirement obviously we do uh[AFSEC Rep] : I think his- I think his specific question was the tasks that are covered in that TPS are also covered in the RC135 2-3-5 or whatever the T.O. is. So if next week a warning comes out that says ‘stop using this chemical’, is there a mechanism for you guys to be notified at the same time- so you guys don’t; especially if you just did your review five days ago, now you gotta wait two years and 360 days to see that again. That’s what I’m wondering is there- do you guys get notified about T.O. changes; I guess is the ..? [Materials & Processes Engineer] No, we don’t. [AFSEC Rep] : Okay so that could- that could happen where you would go a long period of time with the updates of[Materials & Processes Engineer] Unless quality is notified, and it comes from quality. Uh quality is obviously more involved with the customer. [Maintenance Member] : I was just thinking in my mind that would probably come from quality assurance and then be fed to you. [Materials & Processes Engineer] Yes sir. [Investigating Officer] [Materials & Processes Engineer] : Right, thanks. : That’s all (chuckles) [Maintenance Member] [Materials & Processes Engineer] : That concludes the interview. : Thank you. R-322 64-14848, Class A, 30 April 15, AFSAS #739726 R20 MAJ [Mental Health Flight Commander] R20.1. SIB NON-PRIVILEGED INTERVIEW 27 MAY 15 Page i of 2 Non-Privileged Witness Statement 3 (20/5/ l. havebeenadvisedby__ (Name, Grade, OrgMiz?hJ?ou, of Witness) (Name oflnvem'gator) a safety investigator ofthe mishap that occurred on Mvolving Q01st 21 - (1348 (Date) (Equipment dc SM n. This investigation is being conducted under the provisions of AFI 9l-204 solely for the purpose of mishap prevention within the United States Air Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a safety investigation and I acknowledge that a promise of con?dentiality has NOT been extended to me. la. My witness statements (written or verbal) may be used for any valid purpose and be released to any subseqth investigation of this mishap and may be released to the public pursuant to a Freedom of Information Act request. Name (last, and Rani/Grid: 1% MC a 3-, R-323 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 SIB Interview of Maj Role: [Mental Health Flight Commander] OIC, Mental Health Clinic 55 MDG Interviewer: (Medical Member) Date: 27 May 15 [Medical Member] [MFHC] : This is a non-privileged interview with being [Medical Member] conducted on Wednesday, the 28 May 2015 at 1405 by for the Safety Investigation Board convened for the recent mishap. We're investigating the mishap involving an RC-135V that occurred on 30 April 2015. This investigation is being conducted under the provisions of AFI 91-204 solely for the purpose of mishap prevention and to determine all factors relating to the mishap in order to prevent recurrence. A promise of cond- confidentiality is not being extended to you; your statement can be released to any subsequent investigation of this mishap and may be released to the publ- public pursuant to a Freedom of Information Act request. Do you understand that a promise of confidentiality has not been extended to you? [MHFC] : Yes. [Medical Member] : Thank you. For the record would everyone present introduce yourself by stating your name, rank, and affiliation with the board, starting with the witness. [MHFC] : [Medical Member] : Thank you. today, ma’am? [MHFC] , Mental Health Flight Commander, Offutt. , Medical Member, SIB. So how are you doing : Great. [Medical Member] : Good. Um so, we had gone over this when we had gone over your processes, but if we could just recap briefly… Um, how does, uh, the mental health clinic address special duty status? [MHFC] : So, for PRP the member checks in with the PRP clinic, and they get their PRP badge, um, and they come up have their appointment and then they wait for us to complete their note and then they’re escorted down to PRP with whatever recommendation we have for the disposition, and then the disposition is made by the PRP clinic. Um, for flyers if we have a recommendation of DNIC or DNIF, then we call down to the flight medicine clinic and make the recommendation. Um, so both of those things we’re doing same duty day. [Medical Member] : Understood. Uh if you have no changes to the recommendation of any sort then uh, flight medicine just does their usual note scrub as I understand. [MHFC] : Right, if there’s not anything to say, yes. [Medical Member] : And the only follow up you get is a uh, alert box that says, “Hey, your note has been updated.” Is that right? [MHFC] [Medical Member] [MHFC] : It’s um, oh, not an alert box. : Ah, more like the notification tab for AHLTA. : And you can see that they looked at it. R-324 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Medical Member] Definitely. OK. So the uh, aeromedical disposition is the main purpose of flight medicine review and uh, also to uh, get everything plugged in and make sure that they are still within stand- medical standards of flying. [MHFC] : Right. [Medical Member] Um, you deal with this a lot of um, with flyers who are going through um, a myriad of issues. To include, uh, you know just normal bereavement stuff all the way to uh major depressive disorders and other um, more severe psychiatric conditions. [MHFC] : Sure. [Medical Member] We uh, we looked at the local policy, um that was written regarding uh, aeromedical dispositions, and this is[MHFC] : Sure. [Medical Member] In the uh, SGOW OI 44-03, I believe section 7 3, ah entries in the medic- uh in the mental health flight record and the medical record will be accomplished before the end of the duty day of the appointment for all sensitive duty. And HI patients and within 72 hours of routine- and within 72 hours for routine cases. Every encounter will delineate the patient’s PRP slash fly status recommendation in the disposition portion of the SOAPP note. PRP notes will be hand-carried to the PRP clinic for disposition, and recommendations for DNIF or DNIC require an immediate phone call to the flight medicine clinic. Okay, so following this OI, it seems that uh, the recommendation should be phoned in all the time. Is that what I’m getting from this, or is that uh[MHFC] [Medical Member] [MHFC] [Medical Member] [MHFC] [Medical Member] [MHFC] : If there’s a recommendation for DNIC or DNIF. Okay, got you. So if uh there is no recommendation for anything, really then : Then we wouldn’t call. Then there’s no expedite request or anything like that. : Hmmm.. Ah, rather there’s no uh immediate action taken to contact flight med: Right, right. [Medical Member] …and alert them of the issue. No, definitely. Thank you. So, um, this is uh being brought up, um, because when I was looking through the medical record of a- a certain mishap aircrew member I noticed a uh telephone triage appointment. Uh telephone triage appointments, uh it looks to me to be as a triage and disposition. Um getting a basic understanding of their symptoms, and then finding- and then deciding whether or n- deciding on the acuity of their appointment and what action needs to be taken. Is that a good basic summary of what the[MHFC] : Yes. [Medical Member] And if I’m stealing words out of your mouth or putting words into your mouth, please let me know. [MHFC] : Sure. R-325 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [Medical Member] So, what would you uh, say about this particular telephone encounter? (pause) And for the record, um is there- could you please uh just read out the things that are of any significance to you while reading through it? [MHFC] [Medical Member] : Oh, sure. Um, like positive review of systems type things. [MHFC] : Okay, so uh the member is calling to get some advice and counseling for anger management. It’s an active duty patient who is uh voluntary. Um, they’re not PRP, and they are flying status and TS SCI. They’re not calling about anything deployment related. And they do have history of mental health treatment, um when in training for air sickness at Vance. Rated his.. personal perception of his severity as severe. [Medical Member] Okay. [MHFC] : Decreased interest, focusing on his feelings, hard to focus on his family life. Increased feelings of worthlessness, um he clarified saying he feels guilty about his feelings and how he acts. [Medical Member] Okay. [MHFC] : His energy and concentration are down. Not hopeless, not suicidal, not homicidal, never attempted suicide in the past. He is briefed on emergency procedures, and got scheduled for a routine appointment. [Medical Member] Okay, and then we have the- a note the following day, um the previous one is 14 October 2014 and this one is 15 October 2014. [MHFC] : Yes. [Medical Member] The patient did not show for the ten o’clock encounter. And let’s see here – sorry, thank you. He said that he did not want services at the moment, but would be sure to contact the clinic if he feels he need to- needs to in the future. Now I believe that he said that uh he had been uh seeking mental health services off base. Did you get that from this or[MHFC] : He did in the past mhmm. [Medical Member] Okay, on and off for about two years. Now um, the the reason I’m talking to you about this is um, I notice that theres no uh, aeromedical disposition or uh I guess proof of[MHFC] [Medical Member] uh, [MHFC] [Medical Member] [MHFC] : There isn’t. -review by a flight surgeon on the notes. Now if this was uh d- this provider here , um: Technician. Technician, oh, okay, got you. : The provider is . [Medical Member] Okay, so the technician was uh signed off on it was is that correct. R-326 , and the physician um who RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MHFC] : Mhmmm, well there are two technicians. So one is an administrator, this is a technician. is an administrator, is a doctor. [Medical Member] : Okay I’ve got you. So um as far as mental health goes. [MHFC] [Medical Member] [MHFC] : In the mental health clinic. : Correct. : Ah, does does- does Dr. [Medical Member] [MHFC] [Medical Member] is, I guess is the final authority on the note, : Yes. [Medical Member] [MHFC] , and well this is is a technician. uh typically put an aeromedical disposition down, is uh uh, deal with a lot of flyers? : (sighs) I don’t know whether she always puts a disposition down. : Okay. : Um, she should. And, I don’t know how many flyers she has on her caseload. : Okay. [MHFC] : But they’re just normally distributed across providers and I doubt she has any more or less than others. [Medical Member] [MHFC] [Medical Member] [MHFC] [Medical Member] : Understood, um given the-. : Well she hadn’t worked here very long at this time though. : Oh, so she was fairly new. : Very new. Yes. : Okay I got you. Alright, uh so she got there that year, like July timeframe, the usual time? [MHFC] [Medical Member] [MHFC] : Yes, yes. August, August maybe something like that. : Okay I gotcha so this was definitely, probably among the first. : Definitely. [Medical Member] : Yes. And I am uh, I’m, I am guessing that uh, you have a triage provider or is that incorrect? Do these go to um, a provider that is able to handle the workload? [MHFC] : So, the phone calls that come in on a daily basis go to the on-call provider. So that’s probably why this went to her. [Medical Member] : Okay. [MHFC] : And then, probably since she was such a new provider at the time she had availability and got scheduled for the next day. [Medical Member] : Oh. R-327 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 [MHFC] : Cause she had open appointments probably. So, so a lot of times this will just be for the TCONs, it will be whoever triaged it doesn’t mean that the person is going to get an appointment with them. In this case that happens to be her in both cases. [Medical Member] : Okay, I’ve got you. So she, it seems like she uh just hadn’t yet been fully uh… integrated. [MHFC] [Medical Member] : I suppose that is possible. : Okay, so was sh- you know her, personally? [MHFC] [Medical Member] : Yes. : And uh, you’re familiar with her practice. [MHFC] [Medical Member] : Yes. : Um, would she have any reason to not put an aeromedical disposition down. [MHFC] [Medical Member] : I have no idea. : Okay. I see. [MHFC] : (laughs) You’ll have to ask her. [Medical Member] That’s a good answer. So, the normal- the norm would be to put an aeromedical disposition down. [MHFC] : Yes. [Medical Member] : And , this did not have it in this uh, during this uh particular encounter. Okay, so I think that we are about done with this, um, I guess the background of this encounter. If there are no further questions we can conclude the interview. [MHFC] : I don’t have any questions. [Medical Member] : Okay, I, I don’t have any further questions either. If no one has any further questions we will now conclude this interview. I would like to remind you again that you were not offered a promise of confidentiality, and that your statement is not protected, and will be released to any follow-on investigation of this mishap, and may be releasable to the public subject to the Freedom of Information Act. We request that you refrain from discussing your testimony and any information shared with you today regarding this mishap to avoid the possible spread of incomplete and counter information until the br- board has adjourned. Notify the board immediately if you become aware of a possible release of information. Thank you for your time. [MHFC] [Medical Member] : Okay, thank you. : Alright. R-328 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 TAB S RELEASABLE PHOTOGRAPHS, VIDEOS, DIAGRAMS, AND ANIMATIONS S1. RELEASABLE PHOTOS ..................................................................................................... 2 S1.1. MISHAP AIRCRAFT POST FIRE .............................................................................. 2 S1.2. EXTERNAL FUSELAGE DAMAGE .......................................................................... 3 S1.3. FIRE DAMAGE LOOKING TOWARDS AFT PORTION OF AIRCRAFT .......... 4 S1.4. FIRE DAMAGE TO UPPER PORTION OF GALLEY ............................................ 5 S1.5. FIRE DAMAGE TO LOWER PORTION OF GALLEY .......................................... 6 S1.6. GALLEY MID-SECTION WITH MICROWAVE AND OVEN REMOVED......... 7 S1.7. LOWER GALLEY WITH REFRIGERATORS REMOVED ................................... 8 S1.8. FORWARD INBOARD CORNER OF GALLEY LOOKING AFT ......................... 9 S1.9. GALLEY LOOKING AFT WITH FUSELAGE HOLE VISIBLE ......................... 10 S1.10. TOP OF FUSELAGE WITH RIGHT WING VISIBLE ........................................ 11 S1.11. FIRE DAMAGE THROUGH TOP OF FUSELAGE ............................................. 12 S2. RELEASABLE VIDEOS .................................................................................................... 13 S2.1. HANGER 2 WEST SECURITY CAMERA .............................................................. 13 S3. RELEASABLE DIAGRAMS ............................................................................................. 14 S3.1. CREW SEATING CHART ......................................................................................... 14 S3.2. MISHAP LOCATION .................................................................................................. 20 S4. RELEASABLE ANIMATION ........................................................................................... 21 S-1 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 INTENTIONALLY LEFT BLANK RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1. RELEASABLE PHOTOS S1.1. MISHAP AIRCRAFT POST FIRE S-2 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 51.2. EXTERNAL FUSELAGE DAMAGE RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1.3. FIRE DAMAGE LOOKING TOWARDS AFT PORTION OF AIRCRAFT S-4 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1.4. FIRE DAMAGE TO UPPER PORTION OF GALLEY S-5 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1.5. FIRE DAMAGE TO LOWER PORTION OF GALLEY S-6 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1.6. GALLEY MID-SECTION WITH MICROWAVE AND OVEN REMOVED S-7 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1.7. LOWER GALLEY WITH REFRIGERATORS REMOVED S-8 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1.8. FORWARD INBOARD CORNER OF GALLEY LOOKING AFT S-9 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1.9. GALLEY LOOKING AFT WITH FUSELAGE HOLE VISIBLE S-10 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1.10. TOP OF FUSELAGE WITH RIGHT WING VISIBLE S-11 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S1.11. FIRE DAMAGE THROUGH TOP OF FUSELAGE S-12 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S2. RELEASABLE VIDEOS S2.1. HANGER 2 WEST SECURITY CAMERA The following videos were secured from a security camera on Hanger 2 West facing North. The video files can be found in the following files S2.1.1. c_RWfveGJ.Hanger_2_West_6.mp4 S2.1.2. c_RWfveGJ.Hanger_2_West_6.2.mp4 S-13 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S3. RELEASABLE DIAGRAMS S3.1. CREW SEATING CHART S-14 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 Seat: Pilat Seat: CDPilat Seat: Jump Seat Seat: Navigator 1 PILDTS HAVE Seat: Navigator 2 RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 Seat: Raven Seat: Raven RX Seat: Tactical Conrdinatnr TC ASE Seat: Airborne Evstem Engineer 3 Seat: Airborne System Engineer 1 RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 Seat: Operator 5 ASE DLO AA AMS :53 Seat: Operator 2 Seat: Operator 1 Seat: Operator 3 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 Seat: Operator 1" Seat: Operator Seat: Operator(OP} 4 Seat: Operator (OP) 8 Seat: Operator 9 Seat: Operator (OF) 113 . . . . 1,100 Seat: Operator 11 Seat: Operator 12 -- 1,203 1301."! Se at: East Area RC-I35V, 64-14848, Class A, 30 April 15, AFSAS #739726 Seat: Operator 15 Seat: Dperator 16 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 83.2. MISHAP LOCATION *5 8?20 RC-135V, 64-14848, Class A, 30 April 15, AFSAS #739726 S4. RELEASABLE ANIMATION No data available. S-21 TAB T PERSONNEL RECORDS, NOT INCLUDED IN TAB G T1. INDIVIDUAL TRAINING PLAN OF [Aerospace Propulsion Apprentice] ...................... TT-3 T2. INDIVIDUAL TRAINING PLAN OF [Production Superintendent] ................... TT-22 T3. INDIVIDUAL TRAINING PLAN OF T4. INDIVIDUAL TRAINING PLAN OF T5. INDIVIDUAL TRAINING PLAN OF T6. INDIVIDUAL TRAINING PLAN OF [Crew Chief 2] ............. TT-71 T7. INDIVIDUAL TRAINING PLAN OF [Crew Chief 3] ............. TT-88 T8. INDIVIDUAL TRAINING PLAN OF [Production Superintendent 2] [Aerospace Propulsion Journeyman] [Crew Chief 1] [Crew Chief 4] RC-135V, T/N 64-14848, 30 April 2015 1 ............. TT-26 .............................. TT-30 ...................... TT-53 ...................... TT-107 INTENTIONALLY LEFT BLANK 64-14848, 30 April 2015 2 1. IDENTIFICATION DATA LAST NAME - FIRST NAME - MIDDLE INITIAL [Aerospace Propulsion Apprentice] GRADE/RANK Airman First Class DAFSC/JOB SERIES 2A631C INDIVIDUAL TRAINING RECORD INDIVIDUAL'S SIGNATURE DATE 2015-05-04 Individual Training Record RC-135V, T/N 64-14848, 30 April 2015 T.3 1. Tasks Knowledge And Technical References 2A6X1-000 001 CFETP 2A6X1 - AEROSPACE PROPULSION Attachment 2, GENERAL TASKS 1 December 2012 2A6X1-000 001.001 CAREER FIELD PROGRESSION TR: AFI 36-2101 TR: AFI 36-2101 2A6X1-000 002 AF OCCUPATIONAL SAFETY AND HEALTH (AFOSH) PROGRAM TR: AFI 127-01 Vol 1 and 3; AFIs 21-101, 91-202, 91-203, 91-204, 91-213, 91-301, 91-302, AFPAM 90-902; and applicable aircraft/engine TOs 2A6X1-000 002.001 AFOSH standards 2A6X1-000 002.002 Hazards of AFSC 2A6X1-000 002.003 Maintain safe work area 2A6X1-000 002.004 Aircraft Safe For Maintenance 2A6X1-000 002.005 Restraint harness (e.g., Fall protection/prevention equipment) 2A6X1-000 002.006 Risk Management (RM) 2A6X1-000 003 Operations Security (OPSEC) Vulnerablilities for AFSC 2A6X1(C/D/E/F/G) TR: AFI 10-1101 2A6X1-000 004 FOREIGN OBJECT DAMAGE (FOD) PROGRAM TR: AFI 21-101 and applicable MAJCOM instructions 2A6X1-000 004.001 Apply FOD prevention practices 2A6X1-000 004.003 Dropped Object Prevention Program (DOPP) 2A6X1-000 005 HAZARDOUS MATERIALS AND WASTE HANDLING ACCORDING TO ENVIRONMENTAL STANDARDS TR: AFJMAN 24-204 2A6X1-000 005.002 Types of hazardous materials/fluids 2A6X1-000 005.003 Handling procedures 2A6X1-000 005.004 Storage and labeling 2A6X1-000 005.005 Proper disposal 2A6X1-000 006 ENLISTED SPECIALTY TRAINING TR: AFIs 36-2201 and 36-2232 and applicable MAJCOM directives 2A6X1-000 006.001 Trainee responsibilities 2A6X1-000 006.002 OJT Trainer Responsibilities 2A6X1-000 006.002.002 Provide trainee theory and train on actual equipment 2A6X1-000 006.002.003 Provide feedback on training 2A6X1-000 007 TECHNICAL PUBLICATIONS TR: AFPD 21-3, TOs 00-5-1, 00-5-2, and 00-5-15 2A6X1-000 007.001 TO System 2A6X1-000 007.002 Use Technical Orders/Pubs 2A6X1-000 007.003 TCTOs 2A6X1-000 007.004 AFTO Form 22 2A6X1-000 008 SUPPLY MANAGEMENT TR: AFMAN 23-110 and TOs 00-20-3 and 00-20-1 2A6X1-000 008.003 Use Status Tags 2A6X1-000 008.004 AF Form 2005 2A6X1-000 008.007 Priority system 2A6X1-000 008.010 Precious Metal Recovery 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 5 5 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2014-10-09 2014-10-20 - - A - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - 2b c - - - - 2014-10-09 2014-10-20 - 1a b - - - - 2014-10-09 2014-10-20 - - B - - - - 2014-10-09 2014-10-20 - A - - - - - 2014-10-09 2014-10-20 - A - - - - - 2014-10-09 2014-10-20 - 2b c - - - - 2014-10-09 2014-10-20 - A - - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - - - - - - - 2014-11-17 2014-11-20 - - - - - - - 2014-11-17 2014-11-20 - - - - - - - 2014-10-09 2014-10-20 - B B - - - - 2014-10-09 2014-10-20 - 2b - - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - a b - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - A B - - - - 2014-10-09 2014-10-20 - A B - - - - RC-135V, T/N 64-14848, 30 April 2015 T.4 1. Tasks Knowledge And Technical References 2A6X1-000 009 MAINTENANCE MANAGEMENT TR: AFI 21-101, TOs 00-35D-54, 00-20 series, AFMCI 21-103,AFMAN 21-104, TO 2-1-18 and applicable MAJCOM directives 2A6X1-000 009.006 Maintenance accountability 2A6X1-000 009.009 Use Land Mobile Radios (LMR) 2A6X1-000 010 MAINTENANCE INSPECTION SYSTEMS AND FORMS TR: AFCSM 21 series, AFI 21-101; TOs 00-20 series, 00-35D-54; applicable aircraft work unit code manuals and applicable MAJCOM directives 2A6X1-000 010.001 Flight inspections 2A6X1-000 010.001.002 Hourly inspections 2A6X1-000 010.001.003 Special Inspections 2A6X1-000 010.002 IMDS 2A6X1-000 010.002.001 Use IMDS 2A6X1-000 010.002.002 Complete CBT Course (IMDS for Flightline and Backshop) 2A6X1-000 010.004 DOCUMENT MAINTENANCE ACTIONS 2A6X1-000 010.004.001 Use AFTO Form 350 2A6X1-000 010.004.002 Use AFTO Form 781 series(A,H,J,K) 2A6X1-000 010.004.003 AFTO Form 244/245 2A6X1-000 010.004.008 In-Process-Inspections (IPI) 2A6X1-000 010.004.008.001 Theory 2A6X1-000 011 HAND TOOLS TR: TO 32-1-101 2A6X1-000 011.001 Select 2A6X1-000 011.002 Use 2A6X1-000 011.003 Inspect 2A6X1-000 011.004 Care 2A6X1-000 012 GENERAL MAINTENANCE TR: TOs 1-1A-8, 1-1A-14, 2-1-111, 44B-1-15, and applicable aircraft/engine TOs 2A6X1-000 012.001 Select engine hardware 2A6X1-000 012.002 Use engine hardware 2A6X1-000 012.003 Use hardware safety devices 2A6X1-000 012.004 Bearing handling 2A6X1-000 012.005 Proper handling of Electrostatic Sensitive Discharge (ESD) Devices 2A6X1-000 013 ELECTRICAL SYSTEMS 2A6X1-000 013.001 Electrical fundamentals 2A6X1-000 013.002 Trace wiring diagrams, circuits and schematics 2A6X1-000 013.003 Use Multimeters 2A6X1-000 014 ENGINE MAINTENANCE TR: TOs 00-20-1, 00-35D-54, 1-1A-8,2J-1-13, 2-1-111, and applicable aircraft/engine TOs 2A6X1-000 014.001 Perform preliminary maintenance procedures 2A6X1-000 014.001.001 Work area 2A6X1-000 014.001.002 Support equipment 2A6X1-000 014.001.003 Engine 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2014-11-17 2014-11-20 - A B - - - - 2014-11-17 2014-11-20 - - - - - - - 2014-10-29 2014-11-20 - A B - - - - 2014-10-29 2014-11-20 - A B - - - - 2014-11-17 2015-01-09 - a - - - - - 2014-11-17 2015-01-09 - - - - - - - 5 2014-10-29 2014-11-20 - 2b b - - - - 5 2014-10-22 2014-10-29 - 1a - - - - - 5 2014-10-29 2014-11-20 - 2b b - - - - 2014-10-29 2014-11-20 - A B - - - - 5 2014-10-09 2014-10-20 - 2b - - - - - 5 2014-10-09 2014-10-20 - 2b - - - - - 2014-10-09 2014-10-20 - 2b b - - - - 2014-10-09 2014-10-20 - - b - - - - 5 2014-10-29 2014-11-20 - 2b c - - - - 5 2014-10-29 2014-11-20 - 2b c - - - - 5 2014-10-29 2014-11-20 - 2b c - - - - 2014-10-29 2014-11-20 - A B - - - - 2014-10-29 2014-11-20 - - A - - - - 2014-10-29 2014-11-20 - A B - - - - 2014-10-29 2014-11-20 - - b - - - - 5 2014-10-29 2014-11-20 - 1a b - - - - 5 2014-10-29 2014-11-20 - 2b b - - - - 5 2014-10-29 2014-11-20 - 2b b - - - - 5 2014-10-29 2014-11-20 - 2b b - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T.5 1. Tasks Knowledge And Technical References 2A6X1-000 014.002 Engine plumbing 2A6X1-000 014.002.001 Remove 2A6X1-000 014.002.003 Install 2A6X1-000 015 SPECIAL/MEASURING TOOLS TR: TOs 32-1-101, 32-1-201, and applicable engine TOs 2A6X1-000 015.001 Depth Gauge 2A6X1-000 015.001.001 Select 2A6X1-000 015.001.002 Use 2A6X1-000 015.002 Micrometers 2A6X1-000 015.002.001 Select 2A6X1-000 015.002.002 Use 2A6X1-000 015.003 Torque Wrenches 2A6X1-000 015.003.001 Select 2A6X1-000 015.003.002 Use 2A6X1-000 015.004 Engine Fixtures/Tooling 2A6X1-000 015.004.001 Select 2A6X1-000 015.004.002 Use 2A6X1-000 016 TEST EQUIPMENT TR: Applicable engine TOs 2A6X1-000 016.001 Vibration analyzer 2A6X1-000 017 SUPPORT EQUIPMENT TR: TOs 35A4 series, 35D3 series, 35D4 series, and applicable aircraft/engine TOs 2A6X1-000 017.001 Hoisting equipment 2A6X1-000 017.001.002 Operate power overhead 2A6X1-000 017.004 Personnel Stands 2A6X1-000 017.004.001 Inspect prior to use 2A6X1-000 017.004.002 Operate 2A6X1-000 017.005 Transportation Equipment 2A6X1-000 017.005.001 Inspect prior to use 2A6X1-000 017.005.002 Operate 2A6X1-000 017.007 Powered Support Equipment 2A6X1-000 017.007.001 Perform inspection 2A6X1-000 017.007.002 Operate Electrical Power Units (Gas Turbine/ Diesel) 2A6X1-000 017.007.003 Operate Air Conditioner 2A6X1-000 017.007.004 Operate Foodlight Set 2A6X1-000 017.007.005 Operate Pneumatic Air Cart 2A6X1-000 017.007.006 Operate Self Generating Nitrogen Cart 2A6X1-000 017.007.007 Operate Portable Ground Heater 2A6X1-000 018 ENGINE INSPECTION AND PREVENTIVE MAINTENANCE TR: TOs 00-20 series, 33B4-2-22-1,33-1-37 series, and applicable aircraft/engine TOs 2A6X1-000 018.002 Vibration analysis 2A6X1-000 018.003 Oil Analysis Program (OAP) / Joint Oil Analysis Program (JOAP) 2A6X1-000 018.004 Obtain Engine Oil Sample 2A6X1-000 018.005 Borescope 2A6X1-000 018.005.001 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 5 2014-11-17 2014-11-20 - 2b b - - - - 5 2014-11-17 2014-11-20 - 2b b - - - - 2015-01-22 2015-01-26 - 2b b - - - - 2015-01-22 2015-01-26 - 2b b - - - - 2015-01-22 2015-01-26 - 2b b - - - - 2015-01-22 2015-01-26 - 2b b - - - - 5 2014-10-29 2014-11-20 - 2b b - - - - 5 2014-10-29 2014-11-20 - 2b b - - - - 2015-01-29 2015-01-30 - 2b - - - - - 2015-01-29 2015-01-30 - 2b - - - - - 2015-03-05 2015-03-05 - - - - - - - 2015-01-09 2015-01-09 - 2b - - - - - 2014-11-17 2014-11-20 - 1a b - - - - 2014-11-17 2014-11-20 - 1a b - - - - 2015-01-30 2015-03-05 - 1a a - - - - 2015-03-05 2015-03-05 - 1a - - - - - 2014-11-17 2015-01-09 - - - - - - - 2014-11-17 2015-01-09 - - - - - - - 2014-11-17 2015-01-09 - - - - - - - 2014-11-17 2015-01-09 - - - - - - - 2014-11-17 2015-01-09 - - - - - - - 2014-11-17 2015-01-09 - - - - - - - 2014-11-17 2015-01-09 - - - - - - - 5 - - A - - - - 2014-11-17 2014-11-20 - A B - - - - 2014-11-17 2015-01-09 - a - - - - - 2014-11-17 2014-11-20 - A B - - - - RC-135V, T/N 64-14848, 30 April 2015 T.6 1. Tasks Knowledge And Technical References Fundamentals 2A6X1-000 019 ENGINE PRESERVATION SHIPMENT AND STORAGE TR: TOs 00-20-4, 00-20-5, 00-85-20,2J-1-18, 2-1-111, 6J3-1-12, and applicable engine TOs 2A6X1-000 019.001 Prepare Engine for Shipment 2A6X1-000 019.003 Engine/Module/Components In Shipping Container 2A6X1-000 019.003.001 Removal 2A6X1-000 019.003.002 Installation 2A6X1-000 019.004 Engine/Module/Components 2A6X1-000 019.004.001 Preserve 2A6X1-000 019.004.002 De-preserve 2A6X1-000 019.005 Corrosion Control 2A6X1-000 020 AIRCRAFT INSTALLED ENGINE TESTING TR: Applicable aircraft/engine TOs 2A6X1-000 020.002 Perform Ground Observer/Fireguard Duties 2A6X1-000 020.003 Engine Adjustments 2A6X1-000 020.004 Evaluate Engine Performance 2A6X1-000 020.005 System and Component Troubleshooting 2A6X1-000 020.006 Noise Suppressor/ Hush House 2A6X1-000 020.006.004 Operate Flaps/Slats System With Slats Disabled 2A6X1-000 020.006.005 Operate Auxiliary Hydraulic System 2A6X1-000 022 SMALL GAS TURBINE ENGINE and AUXILIARY POWER UNIT (APU) TR: Applicable engine TOs 2A6X1-000 022.001 Constructional Features 2A6X1-000 022.002 Operating Principles 2A6X1-000 022.003 Systems 2A6X1-000 023 GENERAL MAINTENANCE/PRODUCTION TEAM MAINTENANCE TASKS TR: Applicable aircraft and engine TOs 2A6X1-000 023.001 Organizational Level Technical Order Familiarization 2A6X1-000 023.002 Perform Flight Line Safety/Precautions/Security Familiarization 2A6X1-000 023.003 Introduction To Aircraft/Airframe Familiarization/Egress 2A6X1-000 023.006 Statically Ground Aircraft 2A6X1-000 023.007 Apply/Disconnect External Electrical Power Unit 2A6X1-000 023.008 Perform Jacking Team Member 2A6X1-000 023.009 Perform Refuel/Defuel Team Member Duties 2A6X1-000 023.012 Remove/Install Aircraft Maintenance Access Panels 2A6X1-000 023.013 Use Aircraft Interphone System 2A6X1-000 023.014 Perform Aircraft Marshaling Procedures 2A6X1-000 023.017 Perform Wing/Tail Walker Duties 2A6X1-000 023.019 Perform Launch/Recovery Procedures 2A6X1-002 001 GENERAL MAINTENANCE TF33/TF34 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-03-05 2015-03-05 - - b - - - - 2015-03-05 2015-03-05 - - B - - - - 2015-03-05 2015-03-05 - - B - - - - 2015-04-20 2015-04-27 - a a - - - - 2015-03-31 2015-04-10 - a a - - - - 2015-03-31 2015-04-10 - - B - - - - 2014-11-17 2014-11-20 - - - - - - - 2014-11-17 2014-11-20 - - A - - - - 2014-11-17 2014-11-20 - - - - - - - 2015-01-30 2015-03-17 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2014-11-17 2015-01-09 - A B - - - - 2014-11-17 2015-01-09 - - - - - - - 2014-11-17 2015-01-09 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2014-11-24 2014-11-24 - - - - - - - 2014-11-24 2014-11-24 - - - - - - - 2014-11-10 2014-11-21 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2015-01-09 2015-01-26 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2014-11-24 2014-11-24 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2014-11-17 2014-11-20 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T.7 1. Tasks Knowledge And Technical References (B-52H, KC-135E / A-10) Attachment 4 2A6X1-002 001.001 Constructional Features 2A6X1-002 001.002 Engine Systems 2A6X1-002 001.003 Open engine cowling 2A6X1-002 001.004 Close engine cowling 2A6X1-002 001.005 Engine Garlock Seals 2A6X1-002 001.006 Use Interactive Electronic Technical Manual System (IETMS) 2A6X1-002 002 ENGINE MAINTENANCE TR: TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicable aircraft/engine TOs 2A6X1-002 002.001 Engine accessories 2A6X1-002 002.001.001 Engine Anti-ice Valve 2A6X1-002 002.001.001.001 Remove 2A6X1-002 002.001.001.003 Install 2A6X1-002 002.001.002 Fuel System 2A6X1-002 002.001.002.001 Theory 2A6X1-002 002.001.003 Fuel pump 2A6X1-002 002.001.003.001 Remove 2A6X1-002 002.001.003.003 Install 2A6X1-002 002.001.004 Fuel control 2A6X1-002 002.001.004.001 Remove 2A6X1-002 002.001.004.003 Install 2A6X1-002 002.001.005 Fuel Oil Cooler 2A6X1-002 002.001.005.001 Remove 2A6X1-002 002.001.005.003 Install 2A6X1-002 002.001.006 Fuel Filter 2A6X1-002 002.001.006.001 Remove 2A6X1-002 002.001.006.003 Install 2A6X1-002 002.001.010 Pressurizing and Dump Valve (P and D) 2A6X1-002 002.001.010.001 Remove 2A6X1-002 002.001.010.003 Install 2A6X1-002 002.001.011 Exciter 2A6X1-002 002.001.011.001 Remove 2A6X1-002 002.001.011.003 Install 2A6X1-002 002.001.012 Igniter Plug 2A6X1-002 002.001.012.001 Remove 2A6X1-002 002.001.012.003 Install 2A6X1-002 002.001.013 Igniter Lead 2A6X1-002 002.001.013.001 Remove 2A6X1-002 002.001.013.003 Install 2A6X1-002 002.001.014 Thermocouple Harness 2A6X1-002 002.001.014.001 Remove 2A6X1-002 002.001.014.003 Install 2A6X1-002 002.001.015 Thermocouples 2A6X1-002 002.001.015.001 Remove 2A6X1-002 002.001.015.003 Install 2A6X1-002 002.001.018 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 5 5 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-01-30 2015-03-05 - B B - - - - 2015-03-31 2015-04-27 - B - - - - - 2014-10-22 2014-10-29 - - - - - - - 2014-10-22 2014-10-29 - - - - - - - 2015-03-31 2015-04-13 - - - - - - - 2014-11-24 2014-11-24 - - - - - - - 2015-01-21 2015-01-26 - - - - - - - 2015-01-21 2015-01-26 - - - - - - - 2015-01-21 2015-03-11 - - B - - - - 2015-01-30 2015-03-16 - 2b - - - - - 2015-01-30 2015-03-16 - 2b - - - - - 2015-01-30 2015-03-16 - 2b - - - - - 2015-01-30 2015-03-16 - 2b - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2014-11-21 2014-12-04 - - - - - - - 2014-11-21 2014-12-04 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - 2b - - - - - 2015-01-30 2015-03-16 - 2b - - - - - 2015-01-30 2015-03-16 - 2b - - - - - 2015-01-30 2015-03-16 - 2b - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T.8 1. Tasks Knowledge And Technical References Compressor Bleed Valve 2A6X1-002 002.001.018.001 Remove 2A6X1-002 002.001.018.003 Install 2A6X1-002 002.001.019 Compressor Bleed Valve Actuator 2A6X1-002 002.001.019.001 Remove 2A6X1-002 002.001.019.003 Install 2A6X1-002 002.001.023 Oil Pump 2A6X1-002 002.001.023.001 Remove 2A6X1-002 002.001.023.003 Install 2A6X1-002 002.001.024 Oil Tank 2A6X1-002 002.001.024.001 Remove 2A6X1-002 002.001.024.003 Install 2A6X1-002 002.001.024.004 Service 2A6X1-002 002.001.025 Oil Pressure Relief Valve 2A6X1-002 002.001.025.001 Remove 2A6X1-002 002.001.025.003 Install 2A6X1-002 002.001.025.004 Adjust 2A6X1-002 002.001.027 Oil Filter/Screens 2A6X1-002 002.001.027.001 Remove 2A6X1-002 002.001.027.003 Install 2A6X1-002 002.001.033 Gearbox 2A6X1-002 002.001.033.001 Remove 2A6X1-002 002.001.033.003 Install 2A6X1-002 002.001.037 Fan Blades 2A6X1-002 002.001.037.005 Repair (Blend) 2A6X1-002 002.001.038 Fan trim balance 2A6X1-002 002.001.038.001 Fan Case 2A6X1-002 002.001.038.001.001 Remove 2A6X1-002 002.001.038.001.003 Install 2A6X1-002 002.001.040 Inlet Guide Vane (IGV) Case 2A6X1-002 002.001.040.001 Remove 2A6X1-002 002.001.040.003 Install 2A6X1-002 002.001.041 Bearings 2A6X1-002 002.001.041.001 Remove 2A6X1-002 002.001.041.003 Install 2A6X1-002 002.001.042 Carbon Seals 2A6X1-002 002.001.042.001 Remove 2A6X1-002 002.001.042.003 Install 2A6X1-002 002.004 Turbine Section 2A6X1-002 002.004.004 Quick Engine Change (QEC) accessories TR: Applicable Aircraft/Engine TOs 2A6X1-002 002.004.004.002 Tachometer Generator 2A6X1-002 002.004.004.002.001 Remove 2A6X1-002 002.004.004.002.003 Install 2A6X1-002 002.004.004.003 Fuel Flow Transmitter 2A6X1-002 002.004.004.003.001 Remove 2A6X1-002 002.004.004.003.003 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-01-26 2015-01-30 - 2b - - - - - 2015-01-26 2015-01-30 - 2b - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2014-10-22 2014-10-29 - a - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-05 2015-03-05 - a - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-26 2015-03-31 - - - - - - - 2015-03-31 2015-04-10 - - - - - - - 2015-03-31 2015-04-10 - - - - - - - 2015-03-31 2015-04-13 - - - - - - - 2015-03-31 2015-04-13 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-03-31 2015-04-10 - - - - - - - 2015-03-31 2015-04-10 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T.9 1. Tasks Knowledge And Technical References Install 2A6X1-002 002.004.004.004 Low Oil Pressure Switch 2A6X1-002 002.004.004.004.001 Remove 2A6X1-002 002.004.004.004.003 Install 2A6X1-002 002.004.004.005 Oil Pressure Transmitter 2A6X1-002 002.004.004.005.001 Remove 2A6X1-002 002.004.004.005.003 Install 2A6X1-002 002.004.004.006 Oil Differential Pressure Switch 2A6X1-002 002.004.004.006.001 Remove 2A6X1-002 002.004.004.006.003 Install 2A6X1-002 002.004.004.007 Oil Temperature Sensor 2A6X1-002 002.004.004.007.001 Remove 2A6X1-002 002.004.004.007.003 Install 2A6X1-002 002.004.004.010 Constant Speed Drive (CSD) (TF33 only) 2A6X1-002 002.004.004.010.002 Remove 2A6X1-002 002.004.004.010.004 Install 2A6X1-002 002.004.004.011 Generator (TF33 only) 2A6X1-002 002.004.004.011.002 Remove 2A6X1-002 002.004.004.011.004 Install 2A6X1-002 002.004.004.013 CSD/IDG Filters 2A6X1-002 002.004.004.013.001 Remove 2A6X1-002 002.004.004.013.003 Install 2A6X1-002 002.004.004.014 CSD Oil Tank (TF33 only) 2A6X1-002 002.004.004.014.001 Remove 2A6X1-002 002.004.004.014.003 Install 2A6X1-002 002.004.004.014.004 Service 2A6X1-002 002.004.004.015 CSD/IDG Oil Cooler 2A6X1-002 002.004.004.015.001 Remove 2A6X1-002 002.004.004.015.003 Install 2A6X1-002 002.004.004.016 Engine Starter 2A6X1-002 002.004.004.016.001 Remove 2A6X1-002 002.004.004.016.003 Install 2A6X1-002 002.004.004.016.004 Service 2A6X1-002 002.004.004.017 Starter Control Valve 2A6X1-002 002.004.004.017.001 Remove 2A6X1-002 002.004.004.017.003 Install 2A6X1-002 002.004.004.019 Hydraulic Pump 2A6X1-002 002.004.004.019.001 Remove 2A6X1-002 002.004.004.019.003 Install 2A6X1-002 002.004.004.023 Tail pipe/Tail cone 2A6X1-002 002.004.004.023.001 Remove 2A6X1-002 002.004.004.023.003 Install 2A6X1-002 002.004.004.024 Engine ThrottleLinkage 2A6X1-002 002.004.004.024.001 Remove 2A6X1-002 002.004.004.024.003 Install 2A6X1-002 002.004.004.024.004 Rig 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-04-13 2015-04-14 - - - - - - - 2015-04-13 2015-04-14 - - - - - - - 2015-04-13 2015-04-14 - - - - - - - 2015-04-13 2015-04-14 - - - - - - - 2015-04-13 2015-04-14 - - - - - - - 2015-04-13 2015-04-14 - - - - - - - 2015-04-13 2015-04-14 - - - - - - - 2015-04-13 2015-04-14 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-04-27 2015-04-28 - - - - - - - 2015-04-27 2015-04-28 - - - - - - - 2015-03-31 2015-04-20 - - - - - - - 2015-03-31 2015-04-20 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - - - - - - - 2015-01-30 2015-03-16 - 2b - - - - - 5 2015-01-30 2015-03-16 - 2b - - - - - 5 2015-01-30 2015-03-16 - a - - - - - 2015-03-05 2015-03-10 - 2b - - - - - 2015-03-05 2015-03-10 - 2b - - - - - 2015-04-27 2015-04-28 - - - - - - - 2015-04-27 2015-04-28 - - - - - - - 2015-04-27 2015-04-28 - - - - - - - 2015-04-27 2015-04-28 - - - - - - - 2015-04-20 2015-04-27 - - - - - - - 2015-04-20 2015-04-27 - - - - - - - 2015-04-20 2015-04-27 - - - - - - - 5 5 5 5 5 RC-135V, T/N 64-14848, 30 April 2015 T.10 1. Tasks Knowledge And Technical References 2A6X1-002 002.004.004.027 Ring Cowl 2A6X1-002 002.004.004.027.001 Remove 2A6X1-002 002.004.004.027.003 Install 2A6X1-002 002.004.004.028 Nacelle Anti-ice Valve 2A6X1-002 002.004.004.028.001 Remove 2A6X1-002 002.004.004.028.003 Install 2A6X1-002 002.004.004.029 Engine Mounts 2A6X1-002 002.004.004.029.001 Remove 2A6X1-002 002.004.004.029.002 Disassemble 2A6X1-002 002.004.004.029.004 Assemble 2A6X1-002 002.004.004.029.005 Install 2A6X1-002 002.004.004.030 Nose Dome 2A6X1-002 002.004.004.030.001 Remove 2A6X1-002 002.004.004.030.003 Install 2A6X1-002 002.004.004.031 Thrust Reverser 2A6X1-002 002.004.004.031.002 Remove 2A6X1-002 002.004.004.031.004 Install 2A6X1-002 002.004.004.031.005 Rig 2A6X1-002 002.004.004.032 Thrust Reverser Actuator 2A6X1-002 002.004.004.032.001 Remove 2A6X1-002 002.004.004.032.003 Install 2A6X1-002 002.004.004.033 Blocker Door 2A6X1-002 002.004.004.033.001 Remove 2A6X1-002 002.004.004.033.003 Install 2A6X1-002 002.004.004.034 Translating Cowl 2A6X1-002 002.004.004.034.001 Remove 2A6X1-002 002.004.004.034.003 Install 2A6X1-002 002.004.004.036 Thrust Reverser Control Valve 2A6X1-002 002.004.004.036.001 Remove 2A6X1-002 002.004.004.036.003 Install 2A6X1-002 003 ENGINE INSPECTION and PREVENTIVE MAINTENANCE TR: TOs 00-5-14, 00-20 series, and applicable aircraft/engine TOs 2A6X1-002 003.002 Clean Gas Turbine Aircraft Engines and Associated Parts 2A6X1-002 004 ENGINE REMOVAL and INSTALLATION IN AIRFRAME 2A6X1-002 004.001 Remove Engine 2A6X1-002 004.002 Install Engine 2A6X1-002 005 ENGINE RIGGING TR: Applicable Aircraft/Engine TOs 2A6X1-002 005.001 Rig 2A6X1-004 001 ENGINE INSPECTION AND PREVENTIVE MAINTENANCE F108/CFM56 (KC-135R) Attachment 6 2A6X1-004 001.001 Constructional Features 2A6X1-004 001.003 Clean Gas Turbine Aircraft Engines and Associated Parts TR: TO 2J-1-13 2A6X1-004 001.006 Operate, /Retrieve/ Data From Turbine/ Engine Monitoring System or Data 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-03-31 2015-04-10 - - - - - - - 2015-03-31 2015-04-10 - - - - - - - 2015-01-30 2015-03-11 - - - - - - - 2015-01-30 2015-03-11 - - - - - - - 2015-04-28 - - - - - - - 2015-04-28 - - - - - - - 2015-04-28 - - - - - - - - - - - - - - 2015-01-30 2015-03-05 - - - - - - - 2015-01-30 2015-03-05 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2015-03-31 2015-04-20 - - B - - - - 2015-03-31 2015-04-20 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T.11 1. Tasks Knowledge And Technical References Download Transfer Unit (DDTU) 2A6X1-004 002 ENGINE MAINTENANCE TR: TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicableaircraft/ engine TOs 2A6X1-004 002.001 Perform Preliminary Maintenance Procedures 2A6X1-004 002.002 Apply External Electrical Power 2A6X1-004 002.003 Apply External Pneumatic Power 2A6X1-004 002.004 Perform Engine Maintenance 2A6X1-004 002.004.001 Fan Blade TO 2J-F108-2-1 2A6X1-004 002.004.001.001 Remove 2A6X1-004 002.004.001.003 Install 2A6X1-004 002.004.001.004 Repair (Blend) 2A6X1-004 002.004.002 Fan Outlet Guide Vanes 2A6X1-004 002.004.002.001 Remove 2A6X1-004 002.004.002.003 Install 2A6X1-004 002.004.003 Acoustical Panels 2A6X1-004 002.004.003.001 Remove 2A6X1-004 002.004.003.003 Install 2A6X1-004 002.004.004 Idle Reset Solenoid 2A6X1-004 002.004.004.001 Remove 2A6X1-004 002.004.004.003 Install 2A6X1-004 002.004.006 Bleed Valve and Master Ball Screw Actuator Assembly 2A6X1-004 002.004.006.001 Remove 2A6X1-004 002.004.006.003 Install 2A6X1-004 002.004.007 Bleed Valve and Ball Screw Actuator Assembly 2A6X1-004 002.004.007.001 Remove 2A6X1-004 002.004.007.003 Install 2A6X1-004 002.004.008 VBV Stop Mechanism 2A6X1-004 002.004.008.001 Remove 2A6X1-004 002.004.008.003 Install 2A6X1-004 002.004.009 VBV Fuel Gear Motor 2A6X1-004 002.004.009.001 Remove 2A6X1-004 002.004.009.003 Install 2A6X1-004 002.004.010 VBV Feedback Cable 2A6X1-004 002.004.010.001 Remove 2A6X1-004 002.004.010.003 Install 2A6X1-004 002.004.011 VSV Feedback Cable 2A6X1-004 002.004.011.001 Remove 2A6X1-004 002.004.011.003 Install 2A6X1-004 002.004.012 Throttle Gear Box 2A6X1-004 002.004.012.001 Remove 2A6X1-004 002.004.012.003 Install 2A6X1-004 002.004.013 High Pressure Turbine Clearance Control Valve(TCCV) 2A6X1-004 002.004.013.001 Remove 2A6X1-004 002.004.013.003 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-03-31 2015-04-13 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 2015-01-09 2015-01-09 - - - - - - - 5 2015-01-26 2015-03-05 - - - - - - - 5 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 5 2015-01-21 2015-01-26 - - - - - - - 5 2015-01-21 2015-01-26 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-26 2015-03-05 - - - - - - - 2015-01-21 2015-03-11 - - - - - - - 2015-01-21 2015-03-11 - - - - - - - 2015-01-26 2015-03-10 - - - - - - - 2015-01-26 2015-03-10 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T.12 1. Tasks Knowledge And Technical References Install 2A6X1-004 002.004.014 Fuel pump 2A6X1-004 002.004.014.001 Remove 2A6X1-004 002.004.014.003 Install 2A6X1-004 002.004.015 Main Engine Control/Hydro-mechanical Unit 2A6X1-004 002.004.015.001 Remove 2A6X1-004 002.004.015.003 Install 2A6X1-004 002.004.016 Heat Exchanger 2A6X1-004 002.004.016.001 Remove 2A6X1-004 002.004.016.003 Install 2A6X1-004 002.004.017 Fuel Filter 2A6X1-004 002.004.017.001 Remove 2A6X1-004 002.004.017.003 Install 2A6X1-004 002.004.018 Fuel Nozzles (External) 2A6X1-004 002.004.018.001 Remove 2A6X1-004 002.004.018.003 Install 2A6X1-004 002.004.019 Fuel Flow Transmitter 2A6X1-004 002.004.019.001 Remove 2A6X1-004 002.004.019.003 Install 2A6X1-004 002.004.020 Integrated Drive Generator (IDG) 2A6X1-004 002.004.020.001 Remove 2A6X1-004 002.004.020.003 Install 2A6X1-004 002.004.020.004 Service 2A6X1-004 002.004.021 IDG Oil Cooler 2A6X1-004 002.004.021.001 Remove 2A6X1-004 002.004.021.003 Install 2A6X1-004 002.004.022 Engine Starter 2A6X1-004 002.004.022.001 Remove 2A6X1-004 002.004.022.003 Install 2A6X1-004 002.004.023 Starter Control Valve 2A6X1-004 002.004.023.001 Remove 2A6X1-004 002.004.023.003 Install 2A6X1-004 002.004.024 Hydraulic Pump 2A6X1-004 002.004.024.001 Remove 2A6X1-004 002.004.024.003 Install 2A6X1-004 002.004.027 Tail pipe/Tail cone 2A6X1-004 002.004.027.001 Remove 2A6X1-004 002.004.027.003 Install 2A6X1-004 002.004.028 Fan Cowling 2A6X1-004 002.004.028.001 Remove 2A6X1-004 002.004.028.003 Install 2A6X1-004 002.004.028.004 Open/Close 2A6X1-004 002.004.029 Fan Duct 2A6X1-004 002.004.029.001 Remove 2A6X1-004 002.004.029.003 Install 2A6X1-004 002.004.029.004 Open/Close 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-01-26 2015-03-11 - - - - - - - 2015-01-26 2015-03-11 - - - - - - - 5 2015-01-26 2015-03-11 - - - - - - - 5 2015-01-26 2015-03-11 - - - - - - - 2015-01-29 2015-03-11 - - - - - - - 2015-01-29 2015-03-11 - - - - - - - 5 2014-11-04 2014-11-20 - - - - - - - 5 2014-11-04 2014-11-20 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-01-21 2015-03-11 - - - - - - - 2015-01-21 2015-03-11 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 5 2015-01-30 2015-03-10 - - - - - - - 5 2015-01-30 2015-03-11 - - - - - - - 5 2015-01-21 2015-01-26 - - - - - - - 5 2015-01-21 2015-01-26 - - - - - - - 2015-01-30 2015-03-10 - - - - - - - 2015-01-30 2015-03-10 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2014-11-24 2014-11-24 - - - - - - - 2014-11-24 2014-11-24 - - - - - - - 2014-10-22 2014-10-29 - - - - - - - 2014-11-24 2015-01-09 - - - - - - - 2014-11-24 2015-01-09 - - - - - - - 2014-11-24 2014-12-04 - - - - - - - 5 5 RC-135V, T/N 64-14848, 30 April 2015 T.13 1. Tasks Knowledge And Technical References 2A6X1-004 002.004.030 ANTI-ICE SYSTEM 2A6X1-004 002.004.030.001 Theory 2A6X1-004 002.004.031 Ring Cowl 2A6X1-004 002.004.031.001 Remove 2A6X1-004 002.004.031.003 Install 2A6X1-004 002.004.032 Nacelle Anti-ice Valve 2A6X1-004 002.004.032.001 Remove 2A6X1-004 002.004.032.003 Install 2A6X1-004 002.004.033 Engine Mounts 2A6X1-004 002.004.033.001 Remove 2A6X1-004 002.004.033.003 Install 2A6X1-004 002.004.034 Front Spinner Cone 2A6X1-004 002.004.034.001 Remove 2A6X1-004 002.004.034.003 Install 2A6X1-004 002.004.035 Rear Spinner Cone 2A6X1-004 002.004.035.001 Remove 2A6X1-004 002.004.035.003 Install 2A6X1-004 002.004.036 Oil Pump 2A6X1-004 002.004.036.001 Remove 2A6X1-004 002.004.036.003 Install 2A6X1-004 002.004.037 Oil Tank 2A6X1-004 002.004.037.001 Remove 2A6X1-004 002.004.037.003 Install 2A6X1-004 002.004.037.004 Service 2A6X1-004 002.004.038 Oil Filter 2A6X1-004 002.004.038.001 Remove 2A6X1-004 002.004.038.003 Install 2A6X1-004 002.004.039 Chip Detectors 2A6X1-004 002.004.039.001 Remove 2A6X1-004 002.004.039.003 Install 2A6X1-004 002.004.040 Oil Pressure Transmitter 2A6X1-004 002.004.040.001 Remove 2A6X1-004 002.004.040.002 Inspect 2A6X1-004 002.004.040.003 Install 2A6X1-004 002.004.041 Oil Differential Pressure Switch 2A6X1-004 002.004.041.001 Remove 2A6X1-004 002.004.041.003 Install 2A6X1-004 002.004.042 Oil Temperature Sensor 2A6X1-004 002.004.042.001 Remove 2A6X1-004 002.004.042.003 Install 2A6X1-004 002.004.043 Low Oil Pressure Switch 2A6X1-004 002.004.043.001 Remove 2A6X1-004 002.004.043.003 Install 2A6X1-004 002.004.044 N1 Speed Sensor 2A6X1-004 002.004.044.001 Remove 2A6X1-004 002.004.044.003 Install 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 5 5 5 5 5 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-01-21 2015-01-26 - - B - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-01-29 2015-01-30 - - - - - - - 2015-01-29 2015-01-30 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-01-29 2015-01-30 - - - - - - - 2015-01-29 2015-01-30 - - - - - - - 2015-01-29 2015-01-30 - - - - - - - 2015-01-29 2015-01-30 - - - - - - - 2015-03-16 2015-03-31 - - - - - - - 2015-03-16 2015-03-31 - - - - - - - 2015-01-29 2015-01-30 - - - - - - - 2015-01-29 2015-01-30 - - - - - - - 2014-10-22 2014-10-29 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2014-11-04 2014-12-04 - - - - - - - 2014-11-04 2014-12-04 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-03-11 - - - - - - - 2015-01-21 2015-03-11 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T.14 1. Tasks Knowledge And Technical References 2A6X1-004 002.004.045 N2 Control Alternator 2A6X1-004 002.004.045.001 Remove 2A6X1-004 002.004.045.003 Install 2A6X1-004 002.004.046 Power Management Control 2A6X1-004 002.004.046.001 Remove 2A6X1-004 002.004.046.003 Install 2A6X1-004 002.004.047 T-12 Sensor 2A6X1-004 002.004.047.001 Remove 2A6X1-004 002.004.047.003 Install 2A6X1-004 002.004.048 Compressor Inlet Temperature (CIT) Sensor 2A6X1-004 002.004.048.001 Remove 2A6X1-004 002.004.048.003 Install 2A6X1-004 002.004.049 Exciter 2A6X1-004 002.004.049.001 Remove 2A6X1-004 002.004.049.003 Install 2A6X1-004 002.004.050 Igniter Plug 2A6X1-004 002.004.050.001 Remove 2A6X1-004 002.004.050.003 Install 2A6X1-004 002.004.051 Igniter Lead 2A6X1-004 002.004.051.001 Remove 2A6X1-004 002.004.051.003 Install 2A6X1-004 002.004.052 Thermocouple Harness 2A6X1-004 002.004.052.001 Remove 2A6X1-004 002.004.052.003 Install 2A6X1-004 002.004.053 Thermocouples 2A6X1-004 002.004.053.001 Remove 2A6X1-004 002.004.053.003 Install 2A6X1-004 002.004.054 LPT Cooling Manifold 2A6X1-004 002.004.054.001 Remove 2A6X1-004 002.004.054.003 Install 2A6X1-004 002.004.055 Transfer Gearbox 2A6X1-004 002.004.055.001 Remove 2A6X1-004 002.004.055.003 Install 2A6X1-004 002.004.056 Transfer Gearbox Magnetic/Sealol Seal 2A6X1-004 002.004.056.001 Remove 2A6X1-004 002.004.056.003 Install 2A6X1-004 002.004.057 Accessory Gearbox 2A6X1-004 002.004.057.001 Remove 2A6X1-004 002.004.057.003 Install 2A6X1-004 002.004.058 Accessory Transfer Gearbox Magnetic/Sealol Seal 2A6X1-004 002.004.058.001 Remove 2A6X1-004 002.004.058.003 Install 2A6X1-004 002.004.059 5th Stage Bleed Air Check Valve 2A6X1-004 002.004.059.001 Remove 2A6X1-004 002.004.059.003 Install 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-03-16 2015-03-18 - - - - - - - 2015-03-16 2015-03-18 - - - - - - - 2015-01-26 2015-03-11 - - - - - - - 2015-01-26 2015-03-11 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-01-21 2015-01-30 - - - - - - - 2015-03-16 2015-03-18 - - - - - - - 2015-03-16 2015-03-18 - - - - - - - 2015-01-30 2015-03-05 - - - - - - - 2015-01-30 2015-03-05 - - - - - - - 2015-01-30 2015-03-05 - - - - - - - 2015-01-30 2015-03-05 - - - - - - - 2015-01-30 2015-03-05 - - - - - - - 2015-01-30 2015-03-05 - - - - - - - 2015-03-16 2015-03-18 - - - - - - - 2015-03-16 2015-03-18 - - - - - - - 2015-03-16 2015-03-18 - - - - - - - 2015-03-16 2015-03-18 - - - - - - - 2015-03-16 2015-03-18 - - - - - - - 2015-03-16 2015-03-18 - - - - - - - 2015-03-16 2015-03-31 - - - - - - - 2015-03-16 2015-04-10 - - - - - - - 2015-03-16 2015-03-31 - - - - - - - 2015-03-16 2015-03-31 - - - - - - - 2015-03-16 2015-03-31 - - - - - - - 2015-03-16 2015-04-10 - - - - - - - 2015-03-16 2015-03-31 - - - - - - - 2015-03-16 2015-03-31 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - 2015-03-16 2015-03-17 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T.15 1. Tasks Knowledge And Technical References 2A6X1-004 002.004.060 Speed Control Box 2A6X1-004 002.004.060.001 Remove 2A6X1-004 002.004.060.003 Install 2A6X1-004 002.005 ENGINE RIGGING TR: Applicable Aircraft/Engine TOs 2A6X1-004 002.005.001 Rig Engine Variable Stator Vane (VSV) Feedback Cable 2A6X1-004 002.005.002 Rig Engine Variable Bleed Valve (VBV) Feedback Cable 2A6X1-004 002.005.003 Rig MEC/Throttle Cable 2A6X1-004 002.005.004 PMC test 2A6X1-004 002.005.005 PLA Gain Adjustment 2A6X1-004 003 Aircraft Installed Engine Testing TR: Applicable Aircraft/Engine TOs 2A6X1-004 003.005 Perform Ground Observer/Position C Duties During Engine Run 2A6X1-004 003.007 Audible Ignition System Check-Out 2A6X1-004 003.008 Install, Operate And Remove Trim Equipment 2A6X1-004 003.009 Engine Leak Check 2A6X1-004 005 Engine Removal and Installation In Airframe TR: TOs 1-1A-8, 2J-1-24, and applicable aircraft TOs 2A6X1-004 005.001 Remove Engine 2A6X1-004 005.002 Install Engine 2A6X1-004 005.003 Service Engine 2A6X1-008A 001 Jet Fuel Start (JFS) Attachment 10 2A6X1-008A 001.001 JFS 2A6X1-008A 001.001.001 Remove 2A6X1-008A 001.001.003 Install 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2015-01-21 2015-01-26 - - - - - - - 2015-01-21 2015-01-26 - - - - - - - 7 - - - - - - - 7 - - - - - - - 7 - - - - - - - 7 - - - - - - - 7 - - - - - - - 2014-11-10 2014-11-21 - - - - - - - 2014-11-10 2014-11-21 - - - - - - - - - - - - - - - - - - - - - - - - - - - - 5 5 2015-01-27 2015-01-30 7 7 5 - - - - - - - 2014-11-04 2014-11-20 - - - - - - - 2015-03-31 2015-04-14 - - - - - - - 2015-03-31 2015-04-14 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T.16 JOB QUALIFICATION STANDARD CONTINUATION/WJQS CRITICAL TASK NUMBER TASKS 35980 001 35980 001.001 35980 001.002 35980 001.003 35980 001.004 35980 002 35980 002.001 35980 002.002 35980 002.003 35980 004 35980 004.001 35980 005 35980 005.001 35980 006 35980 006.001 35980 007 35980 007.001 35980 007.002 35980 008 35980 008.003 35980 009 35980 009.001 35980 009.002 35980 009.003 35980 011 35980 011.001 35980 011.002 35980 011.003 TASKS, KNOWLEDGE AND TECHNICAL REFERENCES CERTIFICATION START DATE PREFORM GROUND HANDLING: T.O. 1C-135-2-2-2 De-Ice ACFT T.O. 1C-135-2-2-2 Aircraft wash team member T.O. 1-1-691 Remove and install landing gear down locks T.O. 1C-135-2-2-2 Remove and install tail stand T.O 1C-125-2-2-2 AIRFRAME SYSTEM: T.O. 1C-135-2-7 Operate wheel well doors T.O. 1C-135-2-7 Operate cargo door T.O. 1C-135-2-2-2 Operate crew entry door T.O. 1C-135-2-2-2 PNEUDRAULIC SYSTEM: T.O. 1C-135-2-2-2 Service left / right hydraulic reservoirs T.O. 1C-135-2-2-2 FUELS (REFUEL / DEFUEL): T.O. 1C-135-2-2-2 Refuel / defuel panel operator T.O. 1C-135-2-2-2 PINTLE HOOK: T.O. 1-1A-15 Understands and Operates the Pintle Hook TR T.O. 1-1A-15, par 25.1.1, 25.1.2, 25.1.3 25.1.4, 25.1.5, 25.2 T.O. 36-1-121 and T.O . 36-1-191, para 2.78 JET FUEL STARTER (JFS) T.O. 1C-135-2-4-1-1 JFS Oil Service T.O. 1C-135-2-2-2 JFS Oil Change T.O. 1C-135-2-2-2 AUXILARY POWER UNIT (APU) T.O. 1C-135-2-16 Service Oil T.O. 1C-135-2-16 COMPLETE 2A651 5 LEVEL CDC AFI 36-2201 5 LEVEL CDC VOLUME 1 AFI 36-2201 5 LEVEL CDC VOLUME 2 AFI 36-2201 5 LEVEL CDC VOLUME 3 AFI 36-2201 MISCELLANEOUS SYSTEMS T.O.'s 1C-135-2-4-1-1, 1C-135-2-4-2, 1C-135-2-4-3 Rig T/R Torque arm compensator T.O. 1C-135-2-4-3 Install T/R Torque arm compensator T.O. 1C-135-2-4-3 Remove T/R Torque arm compensator T.O. 1C-135-2-4-3 COMPLETION DATE TRAINEE'S TRAINER'S CERTIFIER'S INITIALS INITIALS INITIALS 2015-01-26 2015-03-05 2014-10-02 2014-10-03 2014-10-22 2014-10-29 2014-10-22 2014-10-29 2014-11-10 2014-11-21 2015-01-22 2015-01-26 2015-01-21 2015-01-26 2015-01-09 2015-01-09 2015-01-09 2015-01-26 2014-10-22 2014-10-29 2014-11-03 2014-11-20 2014-11-03 2014-11-20 2015-01-09 2015-01-09 2014-08-26 2014-09-18 2014-09-18 2014-09-30 2014-10-06 2014-11-04 RC-135V, T/N 64-14848, 30 April 2015 T.17 JOURNAL ENTRIES ENTRY SUBJECT DATE 2014-08-19 Conduct Orientation/Initial Evaluation SIGNATURE INFO REMARKS Within 60 days of assignment the Supervisor will conduct a Workcenter Orientation and Initial Evaluation of qualifications IAW AFI 36-2201. 2015-04-28 task progression Today was started on a new task. He is still progressing well and is determined to be an outstanding engine troop. As his supervisor I am pleased with his progress. 2015-04-27 5 level task completion Today was signed off on multiple tasks after displaying his understanding of each component. Please refer to members ITP for specific tasks. He is progressing well and will be an excellent asset to the shop. 2015-04-20 [Aerospace Today was started on multiple tasks. Please refer to members ITP. He is well on his way to becoming a proficient engine troop. Today was signed off on 2 tasks. Please refer to members ITP for specific tasks. He is showing great progression and desire and is well on his way to becoming a knowledgeable engine troop. Propulsion Journeyman ] 2015-04-20 Task completion 2015-04-20 Today engine troop. 2015-04-13 30 Day Review is a current 3 level awaiting 5 level Task Qualification: 84% is currently waiting time to become a 5 level. continues to research and become more efficent in his understanding of the TF33, F108 and APU systems. Keep up the steller work!!! has been signed off on multiple tasks and started on several more. he is progressing well and continues to show his eagerness to learn these engine systems. 2015-03-31 Tasks 2015-03-17 Tasks was started on multiple tasks. Please refer to members ITP. He is well on his way to becoming a proficient has completed multiple tasks and is now at 61% complete in his TBA. 2015-03-17 EOC C/W has completed his 5 lvl EOC with a score 85% on Jan 26th 2015 2015-03-17 Tasks has completed multiple tasks and is now at 61% complete in his TBA. 2015-03-17 EOC C/W has completed his 5 lvl EOC with a score 85% on Jan 26th 2015 2015-03-16 Tasks has completed multiple tasks and is continuing his training. He is progressing well in his F108 and TF33 engine knowledge training. 2015-03-13 30 Day Review is a current 3 level awaiting 5 level Task Qualification: 54% is currently waiting time to become a 5 level. continues to research and become more efficent in his understanding of the TF33, F108 and APU systems. Keep up the steller work!!! was signed off on several tasks and continues to progress his studies. 2015-03-10 Tasks 2015-03-05 Tasks 2015-02-09 30 Day review 2015-01-20 CDC Comp Review 2015-01-20 Practice EOC has completed multiple tasks and is continuing his training. is a current 3 level awaiting 5 level Task Qualification: 40% is currently waiting time to become a 5 level. continues to research and become more efficent in his understanding of the TF33, F108 and APU systems On 20 Jan 2015, A1C completed his supervisory comp review with scored a 92% on his practice EOC test on Nov. 26, 2014. This is his 3rd score of a consecutive 90% or greater. 2015-01-20 CDC Comp Review On 20 Jan 2015, 2015-01-12 CDC Comprehensive Review Volumes 1 & 2 I have completed a Comprehensive Review with completing the full Comprehensive Review with me 2015-01-06 30 Day Entry is currently 5months in training Task Qual: 22% CDC Status: Completed Training Status: Studying for CDC EoC exam Has taken 3 CDC pretests and has scored over 90%, awaiting shop level review before moving on to the next step Total Review of Trainee#s record was conducted on 6 Jan 2015. has taken his 2nd CDC pre-test and scored a 93%. He is doing well and ready for the 3rd test 2014-11-26 2nd pre-test 2014-11-26 Monthly Upgrade Journal Entry: 2014-11-26 2nd pre-test completed his supervisory comp review with on CDC volumes 1 & 2. He will be studying volume 3 tonight before is progressing well! is currently 3 months in training Task Qual: 40% CDC Status: Completed Training Status: Studying for CDC EoC exam Has taken two practice CDC tests and scored a 93% and a 96% Total Review of Trainee#s record was conducted on 24 Nov. has taken his 2nd CDC pre-test and scored a 93%. He is doing well and ready for the 3rd test 2014-11-21 First CDC Pretest scored a 96% on his first CDC pretest. He needs two more 90% or better. 2014-11-04 Vol 3 CDC's C/W has C/W with Vol 3 of his CDC's. He scored a 100% on his URE's. We did a brief review. well. is ready to start taking pretest. On the 19th of Nov a progress check will be c/w on all the three Vol's 2014-10-21 30 Day Entry is currently in his 2nd month of training Task Qual: Task qual#d 28/329 Total tasks = Task completion 9% CDC Status: Vol. 3 of 3 Total Volumes, issued 7 October 2014, due by 5 November 2014 Is progressing along and learning his job. He is doing well in his CDC's and retaining knowledge very well. has been issued his 3rd Vol. He is aware that he has 30 days from today 20141006 to complete his Vol. His 3rd Vol will be due by 20141105. CORRECTION 2014-10-07 CDC Vol 3 Issue RC-135V, T/N 64-14848, 30 April 2015 T.18 is progressing JOURNAL ENTRIES ENTRY DATE SUBJECT 2014-10-06 CDC Vol 3 Issue SIGNATURE INFO REMARKS has been issued his 3rd Vol. He is aware that he has 30 days from today 20141006 to complete his Vol. His 3rd Vol will be due by 20141004. 2014-09-30 Vol 2 CDC's C/W to 100%. 2014-09-18 CDC Vol 1 C/W 2014-09-18 CDC Vol 2 issue 2014-09-18 CDC Vol 1 C/W 2014-09-15 30 Day Entry 2014-09-09 TBA ROLES REQUEST has C/W with Vol 2 of his CDC's. He scored a 98% on his URE's. We reviewed the ones that he missed and corrected is progressing well. has completed CDC volume 1 with a score of 98%, 7 days early. Volume 2 will be issued today aswell 20140918. is progressing well and has a good attitude toward his training. has been issued his 2nd Vol. He is aware that he has 30 days from today 20140918 to complete his Vol. His 2nd Vol will be due by 20141018. has completed CDC volume 1 with a score of 98%, 7 days early. Volume 2 will be issued today aswell 20140918. is progressing well and has a good attitude toward his training. is currently in his first of training Task Qual: Task qual#d 0/329 Total tasks = Task completion 0% CDC Status: Vol. 1 of 5 Total Volumes, issued 26 Aug 2014, due by 25 Sept 2014 has completed FTAC and will proceed with completion of his Vol 1 of CDC's and OJT task progression. Member will require the below TBA Roles "TRAINEE" 2014-08-28 1st Vol of CDC's On the 26th of Aug, I issued his first Vol of C2A651 CDC's. We went over all of the expections of CDC's (my expections and his expections). his due date will be the 25th of Sept. 2014-08-26 Workcenter Orientation I conducted a workcenter orientation with on 2014-08-22. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. I conducted an initial evaluation with on 2014-08-22. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he was briefed that his training is ultimately his responsibility, and he needs to ensure he reviews his training records at least once a week and actively pursues the training he needs to complete his upgrade. He has also been briefed that tasks should be signed off within 30 days of the start date, unless mission requirements prohibit the completion of the task within that time. The below briefing was given to and . 1. Definition of OJT and types of OJT: 1.1. Training is all training received while performing in a specialty. 1.2. Upgrade Training (UGT). Training to qualify airmen for the award of a skill level. UGT increases skills and knowledge beyond the levels previously acquired. 1.3. Qualification Training (QT). Hands-on performance training designed to qualify a trainee in a specific duty position. This can be training in conjunction with UGT, it can occur after UGT completion, or at any other time training is necessary. 2. Responsibilities of OJT. 2.1. Duties of the Commander. 2.1.1. Responsible for overall unit mission accomplishment through the training program. 2.1.2. Establish controls to ensure training meets mission requirements. 2.1.3. Evaluates a trainee#s potential to progress in UGT. 2.2. Duties of the Unit Training Manager. 2.2.1. Appointed by the unit commander to oversee all unit training issues. 2.2.2. Serves as the focal point for all training within the unit. 2.2.3. Indoctrinates all unit personnel on the concepts, scope, and objectives of training. 2.2.4. Assists in scheduling training. 2.2.5. Initiates TBA and provides to supervisor. 2.2.6. Conducts formal and informal assistance visits to sections and work centers. 2.4. Duties of the Supervisor. 2.4.1. Develops a master training plan. 2.4.2. Initiates and maintains the Individual Training Plan . 2.4.3. Performs an initial evaluation of the trainee#s qualifications/needs within 60 days of assignment to a duty position. 2.4.5. Counsels the trainee when problems occur. 2.4.5. Ensure the trainee meets all mandatory qualification requirements outlined in the Air Force Enlisted Classification Directory to include duty position, HST, and deployment/UTC requirements. 2.4.6. Initiates upgrade action when trainee meets all requirements 2.5. Duties of the Trainer/Certifier. 2.5.1. Plans and conducts training. 2.5.2. Teaches on actual equipment or training aids. 2.5.3. Evaluates training and certifies qualifications. 2.5.4. Maintains knowledge, qualifications, and the appropriate skill level. 2.5.5. Provides training feedback to the trainee and supervisor. 2.5.6. Uses established training evaluation tools and methods. 2.5.7. Determines trainee abilities and training program effectiveness. 2.5.8. Develops evaluation tools. 2.5.9. Identifies the trainee#s strengths and areas needing improvement. 2.6. Duties of the Trainee. 2.6.1. Actively participates in the training process. 2.6.2. Understands the applicable CFETP and career path. 2.6.3. Maintains knowledge, qualifications, and the appropriate skill level. 2.6.4. Becomes a productive member of the unit and work center through task certification. 2.6.5. Budget on- and off-duty time to complete training tasks, particularly for CDC and other self-study requirements. 2.6.6. Request help from your supervisor, trainer, or UTM when having training difficulties. 2.6.7. Task knowledge is needed to perform specific tasks and is gained by studying technical references. 2.6.8. Career knowledge is gained through a planned program of self-study involving CDCs or technical references listed in the CFETP. 3. Criteria for award of a skill level. 3.1. Minimum time requirements. 3.1.1. 5 Skill Level upgrade. Minimum of 12 months. 3.1.2. 7 Skill Level Upgrade. Minimum of 12 months 3.2. Knowledge (CDC or study references from the CFETP Part II). 3.3. Job qualification (satisfies training requirements for the duty position). 3.4. Mandatory requirements (minimum requirements listed in paragraph 3 of the AFS description AFECD) 3.5. Supervisors' recommendation. 4. CDC Administration: 4.1. Supervisor and trainee briefed on use of material. 4.2. Supervisor and trainee inventory the material. 2014-08-26 Initial Evaluation 2014-08-22 UTM Orientation 2014-08-22 UTM Orientation (2) 2014-08-22 UTM CDC Issue Today I issued his C2A651 CDCs. He and his supervisor/flight chief was briefed on the CDC guidelines and both understands the responsibilities of the CDC program. The CDCs will be completed in the specified time frame and documentation will RC-135V, T/N 64-14848, 30 April 2015 T.19 JOURNAL ENTRIES ENTRY DATE SUBJECT 2014-08-22 UTM Orientation (3) 2014-08-22 UTM CDC Issue 2014-08-22 UTM Orientation (2) 2014-08-22 UTM Orientation 2014-08-20 UTM Interview SIGNATURE INFO REMARKS be completed accordingly. Both understands that a comprehensive review must be completed upon completion of the last volume and both understand what constitutes a comprehensive review. Both will follow the requirements as outlined in AFI 36-2201. 4.3. Supervisor and trainee make corrections. 4.4. Supervisor and UTM establishes volume sequence to achieve logical flow based on duty position requirements. 4.5. Supervisor issues first volume and sets a schedule of 30 days per volume (60 days for ARC & IMAs). 4.6. Supervisor documents any deviations from schedule in Journal Entries, and notifies UTM of schedule deviations. 4.7. Trainee studies volume chapter by chapter and answers all exercise questions. 4.8. Supervisor counsels trainee and documents counseling in Journal Entries. 4.9. Supervisor reviews answers using the answer key. 4.10. Supervisor and trainee correct all questions to 100 percent. 4.11. The supervisor retains all URE answer keys. 4.12. Ensure exercises are complete and check for accuracy. 4.13. Provide review training for incorrect answers on the URE. 4.14. File answer sheet in the Upgrade Training (UGT) Folder and maintain until CDC is complete. 4.15. Supervisor issues next volume and follows preceding steps to completion. 4.16. Supervisor completes a comprehensive review of all course materials in preparation for CE 4.17. If the Course Examination (CE) needs to be ordered the supervisor notifies the UTM and the interview process is conducted before the test is ordered. Once it arrives on station, Testing office notifies the supervisor through the UTM.. 4.18. UTM schedules trainee for testing within 30 days after receipt of CE. 4.19. Trainee takes CE. 4.20. Unit TM receives scorecard and forwards to supervisor. 4.21. Supervisor completes review training and annotates the scorecard. 4.22. If the Course Examination is taken by E-exam, the individual is scheduled for their CE upon completion of the interview process. 4.23. UTM schedules trainee for testing within 30 days after the interview process is completed. 4.24. Trainee takes CE. 4.20. Unit TM receives e-Exam scorecard and forwards to supervisor. 4.21. Supervisor completes review training Today I issued _ his C2A651 CDCs. He and his supervisor/flight chief was briefed on the CDC guidelines and both understands the responsibilities of the CDC program. The CDCs will be completed in the specified time frame and documentation will be completed accordingly. Both understands that a comprehensive review must be completed upon completion of the last volume and both understand what constitutes a comprehensive review. Both will follow the requirements as outlined in AFI 36-2201. 2.5. Duties of the Trainer/Certifier. 2.5.1. Plans and conducts training. 2.5.2. Teaches on actual equipment or training aids. 2.5.3. Evaluates training and certifies qualifications. 2.5.4. Maintains knowledge, qualifications, and the appropriate skill level. 2.5.5. Provides training feedback to the trainee and supervisor. 2.5.6. Uses established training evaluation tools and methods. 2.5.7. Determines trainee abilities and training program effectiveness. 2.5.8. Develops evaluation tools. 2.5.9. Identifies the trainee#s strengths and areas needing improvement. 2.6. Duties of the Trainee. 2.6.1. Actively participates in the training process. 2.6.2. Understands the applicable CFETP and career path. 2.6.3. Maintains knowledge, qualifications, and the appropriate skill level. 2.6.4. Becomes a productive member of the unit and work center through task certification. 2.6.5. Budget on- and off-duty time to complete training tasks, particularly for CDC and other self-study requirements. 2.6.6. Request help from your supervisor, trainer, or UTM when having training difficulties. 2.6.7. Task knowledge is needed to perform specific tasks and is gained by studying technical references. 2.6.8. Career knowledge is gained through a planned program of self-study involving CDCs or technical references listed in the CFETP. 3. Criteria for award of a skill level. 3.1. Minimum time requirements. 3.1.1. 5 Skill Level upgrade. Minimum of 12 months. 3.1.2. 7 Skill Level Upgrade. Minimum of 12 months 3.2. Knowledge (CDC or study references from the CFETP Part II). 3.3. Job qualification (satisfies training requirements for the duty position). 3.4. Mandatory requirements (minimum requirements listed in paragraph 3 of the AFS description AFECD) 3.5. Supervisors' recommendation. 4. CDC Administration: 4.1. Supervisor and trainee briefed on use of material. 4.2. Supervisor and trainee inventory the material. The below briefing was given to and . 1. Definition of OJT and types of OJT: 1.1. Training is all training received while performing in a specialty. 1.2. Upgrade Training (UGT). Training to qualify airmen for the award of a skill level. UGT increases skills and knowledge beyond the levels previously acquired. 1.3. Qualification Training (QT). Hands-on performance training designed to qualify a trainee in a specific duty position. This can be training in conjunction with UGT, it can occur after UGT completion, or at any other time training is necessary. 2. Responsibilities of OJT. 2.1. Duties of the Commander. 2.1.1. Responsible for overall unit mission accomplishment through the training program. 2.1.2. Establish controls to ensure training meets mission requirements. 2.1.3. Evaluates a trainee#s potential to progress in UGT. 2.2. Duties of the Unit Training Manager. 2.2.1. Appointed by the unit commander to oversee all unit training issues. 2.2.2. Serves as the focal point for all training within the unit. 2.2.3. Indoctrinates all unit personnel on the concepts, scope, and objectives of training. 2.2.4. Assists in scheduling training. 2.2.5. Initiates TBA and provides to supervisor. 2.2.6. Conducts formal and informal assistance visits to sections and work centers. 2.4. Duties of the Supervisor. 2.4.1. Develops a master training plan. 2.4.2. Initiates and maintains the Individual Training Plan . 2.4.3. Performs an initial evaluation of the trainee#s qualifications/needs within 60 days of assignment to a duty position. 2.4.5. Counsels the trainee when problems occur. 2.4.5. Ensure the trainee meets all mandatory qualification requirements outlined in the Air Force Enlisted Classification Directory to include duty position, HST, and deployment/UTC requirements. 2.4.6. Initiates upgrade action when trainee meets all requirements Today inprocessed with the Maintenance Training Office. At that time he was interviewed to determine his/her training status and CDC enrollment/progression requirements. He is currently in initial 5 level upgrade training. Member will be placed in TSC B in TBA. His C2A651 CDCs were ordered as of today. RC-135V, T/N 64-14848, 30 April 2015 T.20 CERTIFICATION I CERTIFY THAT THIS INDIVIDUAL TRAINING RECORD IS CURRENT AS OF 2015-05-04 _____________________________ TRAINEE SIGNATURE _____________________________ SUPERVISOR SIGNATURE RC-135V, T/N 64-14848, 30 April 2015 T.21 1. IDENTIFICATION DATA LAST NAME - FIRST NAME - MIDDLE INITIAL [Production Superintendent] GRADE/RANK Master Sergeant DAFSC/JOB SERIES 2A574 INDIVIDUAL TRAINING RECORD INDIVIDUAL'S SIGNATURE DATE 2015-05-04 Individual Training Record RC-135V, T/N 64-14848, 30 April 2015 T-22 JOB QUALIFICATION STANDARD CONTINUATION/WJQS CRITICAL TASK NUMBER TASKS 68718 002 68718 002.001 68718 002.002 68718 002.003 68718 002.004 68718 002.005 68718 002.006 68718 002.007 68718 002.008 68718 002.009 68718 002.010 68718 002.011 68718 002.012 68718 002.013 68718 002.014 68718 002.015 68718 002.016 68718 002.017 68718 002.018 68718 002.019 68718 002.020 68718 002.021 68718 002.022 68718 002.023 68718 002.024 68718 002.025 68718 002.026 68718 002.027 68718 002.028 68718 002.029 68718 002.030 68718 002.031 68718 002.032 68718 002.033 TASKS, KNOWLEDGE AND TECHNICAL REFERENCES CERTIFICATION START DATE 83 AMU PRODUCTION SUPERINTENDENT Ensure aircraft Forms & IMDS are Complete, Accurate, & Accomplished AFI 21-101 para 3.11.2 Enforce Tech Data Procedures AFI 21-101 para 4.6.4 Ensure Status Accuracy in Aircraft Forms & IMDS AFI 21-101 para 4.6.5 Perform Ground Radio Procedures / Call Signs AFI 21-101 and Local directives Coordinate Launch Operations AFI 11-218, 91-203, & 21-101 para 4.6.1, 4.8.1.7 Execute Redball Procedures AFI 11-218, 91-203, & 21-101 para 14.30 Coordinate Recovery Operations AFI 11-218, 91-203, & 21-101 para 4.6.1, 4.8.1.7 Project Aircraft Postflight-Lead-in / Parking AFI 11-218, 91-203, & 21-101 para 4.6.1, 4.8.1.7 Formally Debrief Aircrew Local Directives & OJT Initiate Bird Strike Procedures AFI 21-101 para 14.19.7 Ensure JOAP Samples are Completed AFI 21-101 para 4.6.10 Direct Lost Tool Procedures AFI 21-101 para 10.8 and Local directives Explain / Understand Welding Procedures AFI 21-101 Offutt sup 1, Local directives Coordinate Aircraft Tour/Static Display Setups AFI 21-101 Offutt sup 1, Local directives Explain / Understand Aircraft Configurations AFI 21-101 Offutt sup 1, Local directives Review / Explain / Understand All Emergency Checklists And Procedures AFI 21-101 para 3.9.25, 4.6.8 & Local Directives Exhibit Deicing Valve Position AFI 21-101 Offutt sup 1 & Local Directives Perform / Sign Exceptional Release AFI 21-101 4.6.2 Prioritize / Execute Flying and Maintenance Schedules AFI 21-101 para 3.11.5 Attend the MXG daily MX Production / Scheduling Meeting AFI 21-101 para 3.11.6 Understand Actions Required By The Squadron Under OPLAN 8010 or Contingency Plans AFI 21-101 para 3.11.7 Ensure Currency And Direct The Aircraft Generation Sequence under OPLAN 8010 or Contingency Plans AFI 21-101 para 3.11.7 Understand Specific Disaster Control Duties And Squadron Responsibilities Pertaining To Aircraft/SE Movement And Personnel Evacuation AFI 21-101 para 3.11.8. AFI 10-2501, AFMAN 32-4004, AFI 10-229, and unit directives Determine / Track / Report Aircraft Status, Including ETIC AFI 21-101 para 3.11.9 Authorize CANN Actions When Authorized By The MXG/CC And Supervision AFI 21-101 para 3.11.10 Understand The Unit CDDAR Program AFI 21-101 para 3.11.11 Report Status to MOC AFI 21-101 para 3.11.12 Sign / Verify MICAP Conditions Exist and Accurate AFI 21-101 para 3.11.13 Demonstrate Schedule Change Procedures (2407) AFI 21-103 & 21-165 Explain / Understand Cannot Duplicate Procedures (CND) AFI 21-103 & 21-165 Differentiate / Understand Repeat / Recur Procedures AFI 21-103 & 21-165 Execute Aircraft Impoundment Procedures AFI 21-101 Chpt 9, Offutt sup 1, & Local Directives Use Minimum Essential Subsystem List (MESL) AFI 21-103 & 21-165 COMPLETION DATE TRAINEE'S TRAINER'S CERTIFIER'S INITIALS INITIALS INITIALS 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2014-07-09 2014-07-21 2014-07-09 2014-07-21 2015-04-20 2015-04-20 2014-07-09 2014-07-21 2014-07-09 2014-07-21 2014-07-09 2014-07-21 2014-07-09 2014-07-21 2014-07-09 2014-07-21 2014-07-09 2014-07-21 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 RC-135V, T/N 64-14848, 30 April 2015 T-23 JOURNAL ENTRIES ENTRY SUBJECT DATE 2014-07-08 Conduct Orientation/Initial Evaluation SIGNATURE INFO REMARKS Within 60 days of assignment the Supervisor will conduct a Workcenter Orientation and Initial Evaluation of qualifications IAW AFI 36-2201. 2015-04-20 Tasks qualified Due to a TBA task reorg, some tasks have just been loaded to his TBA and signed off because he has been fully qualified. 2015-04-20 task(s) archived on 2015-04-20 12 task(s) archived on 2015-04-20 by employee: 2015-03-03 180 Day Supervisor Review Records have been checked at this time. No defects and/or updates at this time. Individual is fully qualified. 2014-07-09 TBA Roles Pleas give the following roles: Supervisor Ratee I have reviewed training records. He is signed off and qualified to be authorized to Sign All Condition Tags IAW Documentation Guidance IAW TO 00-20-3. I have briefed on authorizing cannibalization actions. We discussed how to verify the need for a cannibalization, including guidance in AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 3.11.10. Conduct and document an initial evaluation of trainee qualifications within 60 days of initial assignment (120 days for ARC), either PCS or PCA work center. Document the evaluation on AF Form 623a or automated version and file in the OJT record. As a minimum the evaluation should include: AFSC, duty position, core and HST, and deployment/UTC requirements. CDC requirements. Note: 30 days per volume. Formal/informal training requirements, such as skills, knowledge, or classroom instruction. Supervisors must evaluate technical school graduates on all tasks taught in the initial skills course as identified in the STS portion of the CFETP. Other local or unique training requirements. Supervisor and trainee responsibilities as outlined in this AFI and other governing directives, such as AFI 36-2101 and the CFETP. Supervisors are encouraged to allow trainees to complete course work during normal duty hours, if mission requirements allow. Supervisors will monitor trainee progress to ensure timely completion of CDCs or ADL course work. I have briefed on authorizing MICAP requests. We discussed how to verify a MICAP condition exists and proper Urgency of Need, including guidance in AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 3.11.13. I discussed Red X certification with . I briefed him on a one-to-one basis covered the importance of always doing the right thing and displaying integrity first. We discussed how signing off a Red X means taking responsibility for the whole area and NOT just the part being inspected. Guidance in signing of Red X is in 00-20-1 para 4.5. I have briefed on signing off IPIs. We discussed what an IPI is and the importance of the IPI. We also discussed the guidance in TO 00-20-1 that governs IPIs, specifically, para 2.23 and para 5.7.3.16.6 and all sub-paragraphs. Additionally, we covered AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 14.20.2.1 and how to properly document IPIs. Conduct and document work center orientations within 60 days of assignment (120 days for ARC). As a minimum, the orientation should include the following information: What the trainee will be doing. Duty hours and shifts, including periods of rest (non-duty time). Safety requirements found on the AF Form 55, Employee Safety and Health Record. All time and training requirements for upgrade and/or qualification training. Responsibilities of trainee, trainer, task certifier, and supervisor. I have reviewed training records. He/she is signed off and qualified to sign exceptional release. 2014-07-09 Certification to Sign All Condition Tags 2014-07-09 Certification to Authorize Cannibalization Actions 2014-07-09 Initial Evaluation 2014-07-09 Certification to Authorize/Verify MICAP Requests 2014-07-09 Certification To Sign Red X In All Systems 2014-07-09 Certification to Sign IPI All Systems 2014-07-09 Work Center Orientations 2014-07-09 Certification to Sign Exceptional Release 2014-07-09 Certification to Sign Repeat/ Recur 2014-07-09 Certification to Sign Off CND 2014-07-09 TBA Roles 2014-07-09 Certification to Sign All Condition Tags 2014-07-09 Certification to Sign Off CND 2014-07-09 Certification to Sign Repeat/ Recur 2014-07-09 Certification to Sign Exceptional Release 2014-07-09 Work Center Orientations 2014-07-09 Certification to Sign IPI All Systems 2014-07-09 Certification To Sign Red X In All Systems 2014-07-09 Certification to Authorize/Verify MICAP Requests 2014-07-09 Certification to Authorize Cannibalization Actions 2014-07-09 Initial Evaluation I have briefed on signing off Repeat/Recurs. We discussed the guidance signing off repeat/recur can be found in 00-20-1 and the AFI21-101_OFFUTTAFBSUP_I 27 September 2010. I have briefed on signing off CNDs. We also discussed the guidance for signing off CND found in AFI21-101_OFFUTTAFBSUP_I 27 September 2010. Pleas give the following roles: Supervisor Ratee I have reviewed training records. He is signed off and qualified to be authorized to Sign All Condition Tags IAW Documentation Guidance IAW TO 00-20-3. I have briefed on signing off CNDs. We also discussed the guidance for signing off CND found in AFI21-101_OFFUTTAFBSUP_I 27 September 2010. I have briefed MSgt Robinson on signing off Repeat/Recurs. We discussed the guidance signing off repeat/recur can be found in 00-20-1 and the AFI21-101_OFFUTTAFBSUP_I 27 September 2010. I have reviewed training records. He/she is signed off and qualified to sign exceptional release. Conduct and document work center orientations within 60 days of assignment (120 days for ARC). As a minimum, the orientation should include the following information: What the trainee will be doing. Duty hours and shifts, including periods of rest (non-duty time). Safety requirements found on the AF Form 55, Employee Safety and Health Record. All time and training requirements for upgrade and/or qualification training. Responsibilities of trainee, trainer, task certifier, and supervisor. I have briefed on signing off IPIs. We discussed what an IPI is and the importance of the IPI. We also discussed the guidance in TO 00-20-1 that governs IPIs, specifically, para 2.23 and para 5.7.3.16.6 and all sub-paragraphs. Additionally, we covered AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 14.20.2.1 and how to properly document IPIs. I discussed Red X certification with . I briefed him on a one-to-one basis covered the importance of always doing the right thing and displaying integrity first. We discussed how signing off a Red X means taking responsibility for the whole area and NOT just the part being inspected. Guidance in signing of Red X is in 00-20-1 para 4.5. I have briefed on authorizing MICAP requests. We discussed how to verify a MICAP condition exists and proper Urgency of Need, including guidance in AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 3.11.13. I have briefed MSgt on authorizing cannibalization actions. We discussed how to verify the need for a cannibalization, including guidance in AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 3.11.10. Conduct and document an initial evaluation of trainee qualifications within 60 days of initial assignment (120 days for ARC), either PCS or PCA work center. Document the evaluation on AF Form 623a or automated version and file in the OJT record. As a minimum the evaluation should include: AFSC, duty position, core and HST, and deployment/UTC requirements. CDC requirements. Note: 30 days per volume. Formal/informal training requirements, such as skills, knowledge, or classroom instruction. Supervisors must evaluate technical school graduates on all tasks taught in the initial skills course as identified in the STS portion of the CFETP. Other local or unique training requirements. Supervisor and trainee responsibilities as outlined in this AFI and other governing directives, such as AFI 36-2101 and the CFETP. Supervisors are encouraged to allow trainees to complete course work during normal duty hours, if mission requirements allow. Supervisors will monitor trainee progress to ensure timely completion of CDCs or ADL course work. RC-135V, T/N 64-14848, 30 April 2015 T-24 CERTIFICATION I CERTIFY THAT THIS INDIVIDUAL TRAINING RECORD IS CURRENT AS OF 2015-05-04 _____________________________ TRAINEE SIGNATURE _____________________________ SUPERVISOR SIGNATURE RC-135V, T/N 64-14848, 30 April 2015 T-25 1. IDENTIFICATION DATA LAST NAME - FIRST NAME - MIDDLE INITIAL [Production Superintendent 2] GRADE/RANK Master Sergeant DAFSC/JOB SERIES 2A676 INDIVIDUAL TRAINING RECORD INDIVIDUAL'S SIGNATURE DATE 2015-05-04 Individual Training Record RC-135V, T/N 64-14848, 30 April 2015 T-26 JOB QUALIFICATION STANDARD CONTINUATION/WJQS CRITICAL TASK NUMBER TASKS 68718 002 68718 002.001 68718 002.002 68718 002.003 68718 002.004 68718 002.005 68718 002.006 68718 002.007 68718 002.008 68718 002.009 68718 002.010 68718 002.011 68718 002.012 68718 002.013 68718 002.014 68718 002.015 68718 002.016 68718 002.017 68718 002.018 68718 002.019 68718 002.020 68718 002.021 68718 002.022 68718 002.023 68718 002.024 68718 002.025 68718 002.026 68718 002.027 68718 002.028 68718 002.029 68718 002.030 68718 002.031 68718 002.032 68718 002.033 TASKS, KNOWLEDGE AND TECHNICAL REFERENCES CERTIFICATION START DATE 83 AMU PRODUCTION SUPERINTENDENT Ensure aircraft Forms & IMDS are Complete, Accurate, & Accomplished AFI 21-101 para 3.11.2 Enforce Tech Data Procedures AFI 21-101 para 4.6.4 Ensure Status Accuracy in Aircraft Forms & IMDS AFI 21-101 para 4.6.5 Perform Ground Radio Procedures / Call Signs AFI 21-101 and Local directives Coordinate Launch Operations AFI 11-218, 91-203, & 21-101 para 4.6.1, 4.8.1.7 Execute Redball Procedures AFI 11-218, 91-203, & 21-101 para 14.30 Coordinate Recovery Operations AFI 11-218, 91-203, & 21-101 para 4.6.1, 4.8.1.7 Project Aircraft Postflight-Lead-in / Parking AFI 11-218, 91-203, & 21-101 para 4.6.1, 4.8.1.7 Formally Debrief Aircrew Local Directives & OJT Initiate Bird Strike Procedures AFI 21-101 para 14.19.7 Ensure JOAP Samples are Completed AFI 21-101 para 4.6.10 Direct Lost Tool Procedures AFI 21-101 para 10.8 and Local directives Explain / Understand Welding Procedures AFI 21-101 Offutt sup 1, Local directives Coordinate Aircraft Tour/Static Display Setups AFI 21-101 Offutt sup 1, Local directives Explain / Understand Aircraft Configurations AFI 21-101 Offutt sup 1, Local directives Review / Explain / Understand All Emergency Checklists And Procedures AFI 21-101 para 3.9.25, 4.6.8 & Local Directives Exhibit Deicing Valve Position AFI 21-101 Offutt sup 1 & Local Directives Perform / Sign Exceptional Release AFI 21-101 4.6.2 Prioritize / Execute Flying and Maintenance Schedules AFI 21-101 para 3.11.5 Attend the MXG daily MX Production / Scheduling Meeting AFI 21-101 para 3.11.6 Understand Actions Required By The Squadron Under OPLAN 8010 or Contingency Plans AFI 21-101 para 3.11.7 Ensure Currency And Direct The Aircraft Generation Sequence under OPLAN 8010 or Contingency Plans AFI 21-101 para 3.11.7 Understand Specific Disaster Control Duties And Squadron Responsibilities Pertaining To Aircraft/SE Movement And Personnel Evacuation AFI 21-101 para 3.11.8. AFI 10-2501, AFMAN 32-4004, AFI 10-229, and unit directives Determine / Track / Report Aircraft Status, Including ETIC AFI 21-101 para 3.11.9 Authorize CANN Actions When Authorized By The MXG/CC And Supervision AFI 21-101 para 3.11.10 Understand The Unit CDDAR Program AFI 21-101 para 3.11.11 Report Status to MOC AFI 21-101 para 3.11.12 Sign / Verify MICAP Conditions Exist and Accurate AFI 21-101 para 3.11.13 Demonstrate Schedule Change Procedures (2407) AFI 21-103 & 21-165 Explain / Understand Cannot Duplicate Procedures (CND) AFI 21-103 & 21-165 Differentiate / Understand Repeat / Recur Procedures AFI 21-103 & 21-165 Execute Aircraft Impoundment Procedures AFI 21-101 Chpt 9, Offutt sup 1, & Local Directives Use Minimum Essential Subsystem List (MESL) AFI 21-103 & 21-165 COMPLETION DATE TRAINEE'S TRAINER'S CERTIFIER'S INITIALS INITIALS INITIALS 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-03-04 2015-03-20 2015-03-04 2015-03-20 2015-04-20 2015-04-20 2015-03-04 2015-03-20 2015-03-04 2015-03-20 2015-03-04 2015-03-20 2015-03-04 2015-03-20 2015-03-04 2015-03-20 2015-03-04 2015-03-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 2015-04-20 RC-135V, T/N 64-14848, 30 April 2015 T-27 JOURNAL ENTRIES ENTRY SUBJECT DATE 2015-01-06 Conduct Orientation/Initial Evaluation SIGNATURE INFO REMARKS Within 60 days of assignment the Supervisor will conduct a Workcenter Orientation and Initial Evaluation of qualifications IAW AFI 36-2201. 2015-04-20 task(s) archived on 2015-04-20 13 task(s) archived on 2015-04-20 by employee: 2015-04-20 Tasks qualified Due to a TBA task reorg, some tasks have just been loaded to his TBA and signed off because he has been fully qualified. 2015-03-26 Certification to sign All Condition Tags 2015-03-26 Certification to Sign Exceptional Release 2015-03-26 Certification to Sign IPI All Systems I have reviewed training records. He is signed off and qualified to be authorized to Sign All Condition Tags IAW Documentation Guidance IAW TO 00-20-3 I have reviewed training records. He is signed off and qualified to sign exceptional release 2015-03-26 Certification to Sign Exceptional Release 2015-03-26 Certification to Sign Red X in All Systems 2015-03-26 Certification to Sign Off CND 2015-03-26 Certification to Sign Repeat/ Recur 2015-03-26 Certification to Sign IPI All Systems 2015-03-26 Certification to Authorize/Verify MICAP Requests 2015-03-26 Certification to Authorize Cannibalization Actions 2015-03-26 Certification to Authorize/Verify MICAP Requests 2015-03-26 Certification to sign All Condition Tags 2015-03-26 Certification to Authorize Cannibalization Actions 2015-03-26 Certification to Sign Repeat/ Recur 2015-03-26 Certification to Sign Off CND 2015-03-26 Certification to Sign Red X in All Systems 2015-02-20 TBA Roles 2015-01-22 Initial Orientation 2015-01-22 Workcenter Orientation 2015-01-22 TBA Roles 2015-01-22 Initial Orientation 2015-01-22 Workcenter Orientation 2015-01-22 TBA Roles I have briefed on signing off IPIs. We discussed what an IPI is and the importance of the IPI. We also discussed the guidance in TO 00-20-1 that governs IPIs, specifically, para 2.23 and para 5.7.3.16.6 and all sub-paragraphs. Additionally, we covered AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 14.20.2.1 and how to properly document IPIs. I have reviewed training records. He is signed off and qualified to sign exceptional release I discussed Red X certification with . I briefed him on a one-to-one basis covered the importance of always doing the right thing and displaying integrity first. We discussed how signing off a Red X means taking responsibility for the whole area and NOT just the part being inspected. Guidance in signing of Red X is in 00-20-1 para 4.5. I have briefed on signing off CNDs. We also discussed the guidance for signing off CND found in AFI21-101_OFFUTTAFBSUP_I 27 September 2010. I have briefed on signing off Repeat/Recurs. We discussed the guidance signing off repeat/recur can be found in 00-20-1 and the AFI21-101_OFFUTTAFBSUP_I 27 September 2010 I have briefed on signing off IPIs. We discussed what an IPI is and the importance of the IPI. We also discussed the guidance in TO 00-20-1 that governs IPIs, specifically, para 2.23 and para 5.7.3.16.6 and all sub-paragraphs. Additionally, we covered AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 14.20.2.1 and how to properly document IPIs. I have briefed on authorizing MICAP requests. We discussed how to verify a MICAP condition exists and proper Urgency of Need, including guidance in AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 3.11.13 I have briefed on authorizing cannibalization actions. We discussed how to verify the need for a cannibalization, including guidance in AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 3.11.10. I have briefed on authorizing MICAP requests. We discussed how to verify a MICAP condition exists and proper Urgency of Need, including guidance in AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 3.11.13 I have reviewed training records. He is signed off and qualified to be authorized to Sign All Condition Tags IAW Documentation Guidance IAW TO 00-20-3 I have briefed on authorizing cannibalization actions. We discussed how to verify the need for a cannibalization, including guidance in AFI21-101_OFFUTTAFBSUP_I 27 September 2010 para 3.11.10. I have briefed on signing off Repeat/Recurs. We discussed the guidance signing off repeat/recur can be found in 00-20-1 and the AFI21-101_OFFUTTAFBSUP_I 27 September 2010 I have briefed on signing off CNDs. We also discussed the guidance for signing off CND found in AFI21-101_OFFUTTAFBSUP_I 27 September 2010. I discussed Red X certification with I briefed him on a one-to-one basis covered the importance of always doing the right thing and displaying integrity first. We discussed how signing off a Red X means taking responsibility for the whole area and NOT just the part being inspected. Guidance in signing of Red X is in 00-20-1 para 4.5. requires Trainee roles in TBA. I conducted an initial evaluation with on 22 Jan 2015. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he/she was briefed that his/her training is ultimately his responsibility, and he/ needs to ensure he reviews his training records at least once a month I conducted a workcenter orientation with on 22 Jan 2015. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. Please grant Supervisor, Trainer and Trainee roles to . I conducted an initial evaluation with on 22 Jan 2015. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he/she was briefed that his/her training is ultimately his responsibility, and he/ needs to ensure he reviews his training records at least once a month I conducted a workcenter orientation with on 22 Jan 2015. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. Please grant Supervisor, Trainer and Trainee roles to . RC-135V, T/N 64-14848, 30 April 2015 T-28 CERTIFICATION I CERTIFY THAT THIS INDIVIDUAL TRAINING RECORD IS CURRENT AS OF 2015-05-04 _____________________________ TRAINEE SIGNATURE _____________________________ SUPERVISOR SIGNATURE RC-135V, T/N 64-14848, 30 April 2015 T-29 1. IDENTIFICATION DATA LAST NAME - FIRST NAME - MIDDLE INITIAL [Aerospace Propulsion Journeyman] GRADE/RANK Senior Airman DAFSC/JOB SERIES 2A651F INDIVIDUAL TRAINING RECORD INDIVIDUAL'S SIGNATURE DATE 2015-05-04 Individual Training Record RC-135V, T/N 64-14848, 30 April 2015 T-30 1. Tasks Knowledge And Technical References 2A6X1-000 001 CFETP 2A6X1 - AEROSPACE PROPULSION Attachment 2, GENERAL TASKS 1 December 2012 2A6X1-000 001.001 CAREER FIELD PROGRESSION TR: AFI 36-2101 TR: AFI 36-2101 2A6X1-000 002 AF OCCUPATIONAL SAFETY AND HEALTH (AFOSH) PROGRAM TR: AFI 127-01 Vol 1 and 3; AFIs 21-101, 91-202, 91-203, 91-204, 91-213, 91-301, 91-302, AFPAM 90-902; and applicable aircraft/engine TOs 2A6X1-000 002.001 AFOSH standards 2A6X1-000 002.002 Hazards of AFSC 2A6X1-000 002.003 Maintain safe work area 2A6X1-000 002.004 Aircraft Safe For Maintenance 2A6X1-000 002.005 Restraint harness (e.g., Fall protection/prevention equipment) 2A6X1-000 002.006 Risk Management (RM) 2A6X1-000 003 Operations Security (OPSEC) Vulnerablilities for AFSC 2A6X1(C/D/E/F/G) TR: AFI 10-1101 2A6X1-000 004 FOREIGN OBJECT DAMAGE (FOD) PROGRAM TR: AFI 21-101 and applicable MAJCOM instructions 2A6X1-000 004.001 Apply FOD prevention practices 2A6X1-000 004.003 Dropped Object Prevention Program (DOPP) 2A6X1-000 005 HAZARDOUS MATERIALS AND WASTE HANDLING ACCORDING TO ENVIRONMENTAL STANDARDS TR: AFJMAN 24-204 2A6X1-000 005.002 Types of hazardous materials/fluids 2A6X1-000 005.003 Handling procedures 2A6X1-000 005.004 Storage and labeling 2A6X1-000 005.005 Proper disposal 2A6X1-000 006 ENLISTED SPECIALTY TRAINING TR: AFIs 36-2201 and 36-2232 and applicable MAJCOM directives 2A6X1-000 006.001 Trainee responsibilities 2A6X1-000 006.002 OJT Trainer Responsibilities 2A6X1-000 006.002.001 Prepare teaching outlines or task breakdowns 2A6X1-000 006.002.002 Provide trainee theory and train on actual equipment 2A6X1-000 006.002.003 Provide feedback on training 2A6X1-000 006.003 OJT Task Certifier Responsibilities 2A6X1-000 006.003.001 Use appropriate method of evaluation and effectively determine trainees ability 2A6X1-000 006.003.002 Give supervisor and trainer feedback on results of training provided, and trainees strengths/weaknesses 2A6X1-000 006.003.003 Training plans and working groups 2A6X1-000 007 TECHNICAL PUBLICATIONS TR: AFPD 21-3, TOs 00-5-1, 00-5-2, and 00-5-15 2A6X1-000 007.001 TO System 2A6X1-000 007.002 Use Technical Orders/Pubs 2A6X1-000 007.003 TCTOs 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 5 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-09-25 2009-09-25 - - A - - - - 2009-09-25 2009-09-25 - A B - - - - 2009-09-25 2009-09-25 - A B - - - - 2009-09-25 2009-09-25 - 2b c - - - - 2011-08-01 2011-08-03 - 1a b - - - - 2009-12-21 2010-01-05 - - B - - - - 2009-09-25 2009-09-25 - A - - - - - 2009-09-25 2009-09-25 - A - - - - - 2010-07-29 2010-08-05 - 2b c - - - - 2009-09-25 2009-09-25 - A - - - - - 2009-09-25 2009-09-25 - A B - - - - 2009-09-25 2009-09-25 - A B - - - - 2009-09-25 2009-09-25 - A B - - - - 2009-09-25 2009-09-25 - A B - - - - 2009-09-25 2009-09-25 - - - - - - - 2011-10-21 2011-10-21 - - - - - - - 2010-10-13 2010-10-13 - - - - - - - 2010-10-13 2010-10-13 - - - - - - - 2011-04-05 2011-04-05 - - - - - - - 2011-04-05 2011-04-05 - - - - - - - 2011-04-05 2011-04-05 - - - - - - - 2009-09-25 2009-09-25 - B B - - - - 2009-09-25 2009-09-25 - 2b - - - - - 2009-09-25 2009-09-25 - A B - - - - RC-135V, T/N 64-14848, 30 April 2015 T-31 1. Tasks Knowledge And Technical References 2A6X1-000 007.004 AFTO Form 22 2A6X1-000 008 SUPPLY MANAGEMENT TR: AFMAN 23-110 and TOs 00-20-3 and 00-20-1 2A6X1-000 008.003 Use Status Tags 2A6X1-000 008.004 AF Form 2005 2A6X1-000 008.007 Priority system 2A6X1-000 008.008 Repair cycle assets 2A6X1-000 008.010 Precious Metal Recovery 2A6X1-000 009 MAINTENANCE MANAGEMENT TR: AFI 21-101, TOs 00-35D-54, 00-20 series, AFMCI 21-103,AFMAN 21-104, TO 2-1-18 and applicable MAJCOM directives 2A6X1-000 009.005 Mobility 2A6X1-000 009.006 Maintenance accountability 2A6X1-000 009.009 Use Land Mobile Radios (LMR) 2A6X1-000 010 MAINTENANCE INSPECTION SYSTEMS AND FORMS TR: AFCSM 21 series, AFI 21-101; TOs 00-20 series, 00-35D-54; applicable aircraft work unit code manuals and applicable MAJCOM directives 2A6X1-000 010.001 Flight inspections 2A6X1-000 010.001.002 Hourly inspections 2A6X1-000 010.001.003 Special Inspections 2A6X1-000 010.001.004 Engine Acceptance Inspection 2A6X1-000 010.002 IMDS 2A6X1-000 010.002.001 Use IMDS 2A6X1-000 010.002.002 Complete CBT Course (IMDS for Flightline and Backshop) 2A6X1-000 010.004 DOCUMENT MAINTENANCE ACTIONS 2A6X1-000 010.004.001 Use AFTO Form 350 2A6X1-000 010.004.002 Use AFTO Form 781 series(A,H,J,K) 2A6X1-000 010.004.003 AFTO Form 244/245 2A6X1-000 010.004.008 In-Process-Inspections (IPI) 2A6X1-000 010.004.008.001 Theory 2A6X1-000 011 HAND TOOLS TR: TO 32-1-101 2A6X1-000 011.001 Select 2A6X1-000 011.002 Use 2A6X1-000 011.003 Inspect 2A6X1-000 011.004 Care 2A6X1-000 012 GENERAL MAINTENANCE TR: TOs 1-1A-8, 1-1A-14, 2-1-111, 44B-1-15, and applicable aircraft/engine TOs 2A6X1-000 012.001 Select engine hardware 2A6X1-000 012.002 Use engine hardware 2A6X1-000 012.003 Use hardware safety devices 2A6X1-000 012.004 Bearing handling 2A6X1-000 012.005 Proper handling of Electrostatic Sensitive Discharge (ESD) Devices 2A6X1-000 013 ELECTRICAL SYSTEMS 2A6X1-000 013.001 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2009-09-25 2009-09-25 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - A B - - - - 2010-01-27 2010-02-10 - a b - - - - 2009-09-25 2009-09-25 - A B - - - - 2009-12-21 2010-01-05 - A B - - - - 2009-12-21 2010-01-05 - - B - - - - 2009-12-21 2010-01-05 - A B - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-12-21 2010-01-05 - A B - - - - 2009-09-01 2009-10-02 - - - - - - - 2011-07-12 2011-07-12 - A B - - - - 2011-07-12 2011-07-12 - A B - - - - 2011-07-12 2011-07-12 - A B - - - - 2009-12-21 2010-01-04 - a - - - - - 2009-09-25 2009-09-25 - - - - - - - 5 2009-09-25 2009-09-25 - 2b b - - - - 5 2009-09-25 2009-09-25 - 1a - - - - - 5 2009-09-25 2009-09-25 - 2b b - - - - 2009-12-21 2010-01-05 - A B - - - - 5 2009-09-25 2009-09-25 - 2b - - - - - 5 2009-09-25 2009-09-25 - 2b - - - - - 2009-09-08 2009-10-02 - 2b b - - - - 2013-10-01 2013-10-08 - - b - - - - 5 2009-09-25 2009-09-25 - 2b c - - - - 5 2009-09-25 2009-09-25 - 2b c - - - - 5 2009-09-25 2009-09-25 - 2b c - - - - 2013-10-01 2013-10-08 - A B - - - - 2010-01-27 2010-02-10 - - A - - - - 2011-07-12 2011-07-12 - A B - - - - 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-32 1. Tasks Knowledge And Technical References Electrical fundamentals 2A6X1-000 013.002 Trace wiring diagrams, circuits and schematics 2A6X1-000 014 ENGINE MAINTENANCE TR: TOs 00-20-1, 00-35D-54, 1-1A-8,2J-1-13, 2-1-111, and applicable aircraft/engine TOs 2A6X1-000 014.001 Perform preliminary maintenance procedures 2A6X1-000 014.001.001 Work area 2A6X1-000 014.001.002 Support equipment 2A6X1-000 014.001.003 Engine 2A6X1-000 014.002 Engine plumbing 2A6X1-000 014.002.001 Remove 2A6X1-000 014.002.003 Install 2A6X1-000 015 SPECIAL/MEASURING TOOLS TR: TOs 32-1-101, 32-1-201, and applicable engine TOs 2A6X1-000 015.001 Depth Gauge 2A6X1-000 015.001.001 Select 2A6X1-000 015.001.002 Use 2A6X1-000 015.002 Micrometers 2A6X1-000 015.002.001 Select 2A6X1-000 015.002.002 Use 2A6X1-000 015.003 Torque Wrenches 2A6X1-000 015.003.001 Select 2A6X1-000 015.003.002 Use 2A6X1-000 015.004 Engine Fixtures/Tooling 2A6X1-000 015.004.001 Select 2A6X1-000 015.004.002 Use 2A6X1-000 016 TEST EQUIPMENT TR: Applicable engine TOs 2A6X1-000 016.001 Vibration analyzer 2A6X1-000 016.002 Jet Cal Analyzer 2A6X1-000 017 SUPPORT EQUIPMENT TR: TOs 35A4 series, 35D3 series, 35D4 series, and applicable aircraft/engine TOs 2A6X1-000 017.001 Hoisting equipment 2A6X1-000 017.001.002 Operate power overhead 2A6X1-000 017.004 Personnel Stands 2A6X1-000 017.004.001 Inspect prior to use 2A6X1-000 017.004.002 Operate 2A6X1-000 017.005 Transportation Equipment 2A6X1-000 017.005.001 Inspect prior to use 2A6X1-000 017.005.002 Operate 2A6X1-000 017.007 Powered Support Equipment 2A6X1-000 017.007.001 Perform inspection 2A6X1-000 017.007.002 Operate Electrical Power Units (Gas Turbine/ Diesel) 2A6X1-000 017.007.003 Operate Air Conditioner 2A6X1-000 017.007.004 Operate Foodlight Set 2A6X1-000 017.007.005 Operate Pneumatic Air Cart 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2011-07-12 2011-07-12 - - b - - - - 5 2009-09-25 2009-09-25 - 2b b - - - - 5 2009-09-25 2009-09-25 - 2b b - - - - 5 2009-09-25 2009-09-25 - 2b b - - - - 5 2009-09-25 2009-09-25 - 2b b - - - - 5 2009-09-25 2009-09-25 - 2b b - - - - 2011-07-12 2011-07-12 - 2b b - - - - 2009-09-25 2009-09-25 - 2b b - - - - 2009-09-25 2009-09-25 - 2b b - - - - 2009-09-25 2009-09-25 - 2b b - - - - 5 2009-09-25 2009-09-25 - 2b b - - - - 5 2009-09-25 2009-09-25 - 2b b - - - - 2009-09-25 2009-09-25 - 2b - - - - - 2009-09-25 2009-09-25 - 2b - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2009-09-25 2009-09-25 - 2b - - - - - 2011-07-12 2011-07-12 - 1a b - - - - 2009-09-25 2009-09-25 - 1a b - - - - 2011-07-12 2011-07-12 - 1a a - - - - 2011-07-12 2011-07-12 - 1a - - - - - 2009-09-08 2009-10-02 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T-33 1. Tasks Knowledge And Technical References 2A6X1-000 017.007.006 Operate Self Generating Nitrogen Cart 2A6X1-000 017.007.007 Operate Portable Ground Heater 2A6X1-000 018 ENGINE INSPECTION AND PREVENTIVE MAINTENANCE TR: TOs 00-20 series, 33B4-2-22-1,33-1-37 series, and applicable aircraft/engine TOs 2A6X1-000 018.002 Vibration analysis 2A6X1-000 018.003 Oil Analysis Program (OAP) / Joint Oil Analysis Program (JOAP) 2A6X1-000 018.004 Obtain Engine Oil Sample 2A6X1-000 018.005 Borescope 2A6X1-000 018.005.001 Fundamentals 2A6X1-000 018.005.002 Use Rigid 2A6X1-000 018.005.003 Use Flexible 2A6X1-000 019 ENGINE PRESERVATION SHIPMENT AND STORAGE TR: TOs 00-20-4, 00-20-5, 00-85-20,2J-1-18, 2-1-111, 6J3-1-12, and applicable engine TOs 2A6X1-000 019.001 Prepare Engine for Shipment 2A6X1-000 019.002 Engine Acceptance Inspection 2A6X1-000 019.003 Engine/Module/Components In Shipping Container 2A6X1-000 019.003.001 Removal 2A6X1-000 019.003.002 Installation 2A6X1-000 019.004 Engine/Module/Components 2A6X1-000 019.004.001 Preserve 2A6X1-000 019.004.002 De-preserve 2A6X1-000 019.005 Corrosion Control 2A6X1-000 020 AIRCRAFT INSTALLED ENGINE TESTING TR: Applicable aircraft/engine TOs 2A6X1-000 020.002 Perform Ground Observer/Fireguard Duties 2A6X1-000 020.003 Engine Adjustments 2A6X1-000 020.004 Evaluate Engine Performance 2A6X1-000 020.005 System and Component Troubleshooting 2A6X1-000 022 SMALL GAS TURBINE ENGINE and AUXILIARY POWER UNIT (APU) TR: Applicable engine TOs 2A6X1-000 022.001 Constructional Features 2A6X1-000 022.002 Operating Principles 2A6X1-000 022.003 Systems 2A6X1-000 023 GENERAL MAINTENANCE/PRODUCTION TEAM MAINTENANCE TASKS TR: Applicable aircraft and engine TOs 2A6X1-000 023.001 Organizational Level Technical Order Familiarization 2A6X1-000 023.002 Perform Flight Line Safety/Precautions/Security Familiarization 2A6X1-000 023.003 Introduction To Aircraft/Airframe Familiarization/Egress 2A6X1-000 023.004 Operate Aircraft Radios 2A6X1-000 023.006 Statically Ground Aircraft 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2009-12-21 2010-01-05 B Trainer Initials Tng Start 5 E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - A - - - - 2011-07-12 2011-07-12 - A B - - - - 2011-07-12 2011-07-12 - a - - - - - 2014-10-20 2014-11-17 - A B - - - - 2014-10-20 2014-11-17 - a a - - - - 2014-10-20 2014-11-17 - a a - - - - 2009-09-25 2009-09-25 - - b - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - B - - - - 2009-09-25 2009-09-25 - - B - - - - 2009-09-25 2009-09-25 - a a - - - - 2009-09-25 2009-09-25 - a a - - - - 2009-09-25 2009-09-25 - - B - - - - 2009-09-08 2009-10-02 - - - - - - - 2011-04-01 2011-04-04 - - A - - - - 2011-04-01 2011-04-04 - - - - - - - 2011-04-01 2011-04-04 - - - - - - - 2011-07-12 2011-07-12 - A B - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-34 1. Tasks Knowledge And Technical References 2A6X1-000 023.007 Apply/Disconnect External Electrical Power Unit 2A6X1-000 023.008 Perform Jacking Team Member 2A6X1-000 023.009 Perform Refuel/Defuel Team Member Duties 2A6X1-000 023.012 Remove/Install Aircraft Maintenance Access Panels 2A6X1-000 023.013 Use Aircraft Interphone System 2A6X1-000 023.014 Perform Aircraft Marshaling Procedures 2A6X1-000 023.017 Perform Wing/Tail Walker Duties 2A6X1-000 023.018 Brake Operator 2A6X1-000 023.019 Perform Launch/Recovery Procedures 2A6X1-002 001 GENERAL MAINTENANCE TF33/TF34 (B-52H, KC-135E / A-10) Attachment 4 2A6X1-002 001.001 Constructional Features 2A6X1-002 001.002 Engine Systems 2A6X1-002 001.003 Open engine cowling 2A6X1-002 001.004 Close engine cowling 2A6X1-002 001.005 Engine Garlock Seals 2A6X1-002 001.006 Use Interactive Electronic Technical Manual System (IETMS) 2A6X1-002 002 ENGINE MAINTENANCE TR: TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicable aircraft/engine TOs 2A6X1-002 002.001 Engine accessories 2A6X1-002 002.001.001 Engine Anti-ice Valve 2A6X1-002 002.001.001.001 Remove 2A6X1-002 002.001.001.003 Install 2A6X1-002 002.001.002 Fuel System 2A6X1-002 002.001.002.001 Theory 2A6X1-002 002.001.003 Fuel pump 2A6X1-002 002.001.003.001 Remove 2A6X1-002 002.001.003.003 Install 2A6X1-002 002.001.004 Fuel control 2A6X1-002 002.001.004.001 Remove 2A6X1-002 002.001.004.003 Install 2A6X1-002 002.001.005 Fuel Oil Cooler 2A6X1-002 002.001.005.001 Remove 2A6X1-002 002.001.005.003 Install 2A6X1-002 002.001.006 Fuel Filter 2A6X1-002 002.001.006.001 Remove 2A6X1-002 002.001.006.002 Inspect 2A6X1-002 002.001.006.003 Install 2A6X1-002 002.001.010 Pressurizing and Dump Valve (P and D) 2A6X1-002 002.001.010.001 Remove 2A6X1-002 002.001.010.003 Install 2A6X1-002 002.001.011 Exciter 2A6X1-002 002.001.011.001 Remove 2A6X1-002 002.001.011.003 Install 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2009-09-25 2009-09-25 B Trainer Initials Tng Start 5 E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - - - - - - - 2009-09-08 2009-10-02 - - - - - - - 2009-09-08 2009-10-02 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-08 2009-10-02 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2011-08-01 2011-08-03 - B B - - - - 2013-10-01 2013-10-08 - B - - - - - 2009-09-08 2009-10-02 - - - - - - - 2011-08-01 2011-08-03 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2013-10-01 2013-10-08 - - B - - - - 2009-12-21 2010-02-02 - 2b - - - - - 2009-12-21 2010-02-02 - 2b - - - - - 2009-12-21 2010-02-02 - 2b - - - - - 2009-12-21 2010-02-02 - 2b - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 7 2012-08-08 2012-08-08 - - - - - - - 5 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-02-02 - - - - - - - 2009-12-21 2010-02-02 - - - - - - - 2009-10-05 2009-10-26 - 2b - - - - - 2009-10-05 2009-10-26 - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-35 1. Tasks Knowledge And Technical References 2A6X1-002 002.001.012 Igniter Plug 2A6X1-002 002.001.012.001 Remove 2A6X1-002 002.001.012.003 Install 2A6X1-002 002.001.013 Igniter Lead 2A6X1-002 002.001.013.001 Remove 2A6X1-002 002.001.013.003 Install 2A6X1-002 002.001.014 Thermocouple Harness 2A6X1-002 002.001.014.001 Remove 2A6X1-002 002.001.014.003 Install 2A6X1-002 002.001.015 Thermocouples 2A6X1-002 002.001.015.001 Remove 2A6X1-002 002.001.015.003 Install 2A6X1-002 002.001.017 Compressor bleed system 2A6X1-002 002.001.017.001 TF33 Theory 2A6X1-002 002.001.018 Compressor Bleed Valve 2A6X1-002 002.001.018.001 Remove 2A6X1-002 002.001.018.003 Install 2A6X1-002 002.001.019 Compressor Bleed Valve Actuator 2A6X1-002 002.001.019.001 Remove 2A6X1-002 002.001.019.003 Install 2A6X1-002 002.001.022 Oil System 2A6X1-002 002.001.022.001 TF33 Oil System Theory 2A6X1-002 002.001.023 Oil Pump 2A6X1-002 002.001.023.001 Remove 2A6X1-002 002.001.023.003 Install 2A6X1-002 002.001.024 Oil Tank 2A6X1-002 002.001.024.001 Remove 2A6X1-002 002.001.024.003 Install 2A6X1-002 002.001.024.004 Service 2A6X1-002 002.001.025 Oil Pressure Relief Valve 2A6X1-002 002.001.025.001 Remove 2A6X1-002 002.001.025.003 Install 2A6X1-002 002.001.025.004 Adjust 2A6X1-002 002.001.027 Oil Filter/Screens 2A6X1-002 002.001.027.001 Remove 2A6X1-002 002.001.027.002 Inspect 2A6X1-002 002.001.027.003 Install 2A6X1-002 002.001.033 Gearbox 2A6X1-002 002.001.033.001 Remove 2A6X1-002 002.001.033.003 Install 2A6X1-002 002.001.037 Fan Blades 2A6X1-002 002.001.037.002 Inspect 2A6X1-002 002.001.037.005 Repair (Blend) 2A6X1-002 002.001.038 Fan trim balance 2A6X1-002 002.001.038.001 Fan Case 2A6X1-002 002.001.038.001.001 Remove 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-10-05 2009-10-26 - 2b - - - - - 2009-10-05 2009-10-26 - 2b - - - - - 2009-10-05 2009-10-26 - - - - - - - 2009-10-05 2009-10-26 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2013-10-01 2013-10-08 - - B - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2013-10-01 2013-10-08 - - B - - - - 2009-12-21 2010-02-02 - 2b - - - - - 2009-12-21 2010-02-02 - 2b - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-10-05 2009-10-14 - a - - - - - 2010-01-27 2010-02-10 - - - - - - - 2010-01-27 2010-02-10 - - - - - - - 2010-01-27 2010-02-10 - - - - - - - 2009-09-08 2009-10-02 - - - - - - - 7 2012-08-08 2012-08-08 - - - - - - - 5 2009-09-08 2009-10-02 - - - - - - - 2009-12-21 2010-02-10 - - - - - - - 2009-12-21 2010-02-10 - - - - - - - 2011-04-01 2011-04-04 - 2b - - - - - 2010-10-13 2010-10-13 - a - - - - - 2013-10-01 2013-10-08 - - - - - - - 5 5 5 7 RC-135V, T/N 64-14848, 30 April 2015 T-36 1. Tasks Knowledge And Technical References 2A6X1-002 002.001.038.001.003 Install 2A6X1-002 002.001.040 Inlet Guide Vane (IGV) Case 2A6X1-002 002.001.040.001 Remove 2A6X1-002 002.001.040.003 Install 2A6X1-002 002.001.041 Bearings 2A6X1-002 002.001.041.001 Remove 2A6X1-002 002.001.041.003 Install 2A6X1-002 002.001.042 Carbon Seals 2A6X1-002 002.001.042.001 Remove 2A6X1-002 002.001.042.003 Install 2A6X1-002 002.004 Turbine Section 2A6X1-002 002.004.004 Quick Engine Change (QEC) accessories TR: Applicable Aircraft/Engine TOs 2A6X1-002 002.004.004.001 TF33 QEC Kit Theory 2A6X1-002 002.004.004.002 Tachometer Generator 2A6X1-002 002.004.004.002.001 Remove 2A6X1-002 002.004.004.002.003 Install 2A6X1-002 002.004.004.003 Fuel Flow Transmitter 2A6X1-002 002.004.004.003.001 Remove 2A6X1-002 002.004.004.003.003 Install 2A6X1-002 002.004.004.004 Low Oil Pressure Switch 2A6X1-002 002.004.004.004.001 Remove 2A6X1-002 002.004.004.004.003 Install 2A6X1-002 002.004.004.005 Oil Pressure Transmitter 2A6X1-002 002.004.004.005.001 Remove 2A6X1-002 002.004.004.005.003 Install 2A6X1-002 002.004.004.006 Oil Differential Pressure Switch 2A6X1-002 002.004.004.006.001 Remove 2A6X1-002 002.004.004.006.003 Install 2A6X1-002 002.004.004.007 Oil Temperature Sensor 2A6X1-002 002.004.004.007.001 Remove 2A6X1-002 002.004.004.007.003 Install 2A6X1-002 002.004.004.010 Constant Speed Drive (CSD) (TF33 only) 2A6X1-002 002.004.004.010.002 Remove 2A6X1-002 002.004.004.010.004 Install 2A6X1-002 002.004.004.011 Generator (TF33 only) 2A6X1-002 002.004.004.011.002 Remove 2A6X1-002 002.004.004.011.004 Install 2A6X1-002 002.004.004.013 CSD/IDG Filters 2A6X1-002 002.004.004.013.001 Remove 2A6X1-002 002.004.004.013.003 Install 2A6X1-002 002.004.004.014 CSD Oil Tank (TF33 only) 2A6X1-002 002.004.004.014.001 Remove 2A6X1-002 002.004.004.014.003 Install 2A6X1-002 002.004.004.014.004 Service 2A6X1-002 002.004.004.015 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2013-10-01 2013-10-08 B Trainer Initials Tng Start 5 5 5 E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - B - - - - 2010-07-30 2010-08-27 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-09-08 2009-10-02 - - - - - - - 2009-09-08 2009-10-02 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-12-21 2010-01-04 - - - - - - - 2009-12-21 2010-01-04 - - - - - - - 2009-12-21 2010-01-04 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-37 1. Tasks Knowledge And Technical References CSD/IDG Oil Cooler 2A6X1-002 002.004.004.015.001 Remove 2A6X1-002 002.004.004.015.003 Install 2A6X1-002 002.004.004.016 Engine Starter 2A6X1-002 002.004.004.016.001 Remove 2A6X1-002 002.004.004.016.003 Install 2A6X1-002 002.004.004.016.004 Service 2A6X1-002 002.004.004.017 Starter Control Valve 2A6X1-002 002.004.004.017.001 Remove 2A6X1-002 002.004.004.017.003 Install 2A6X1-002 002.004.004.019 Hydraulic Pump 2A6X1-002 002.004.004.019.001 Remove 2A6X1-002 002.004.004.019.003 Install 2A6X1-002 002.004.004.023 Tail pipe/Tail cone 2A6X1-002 002.004.004.023.001 Remove 2A6X1-002 002.004.004.023.003 Install 2A6X1-002 002.004.004.024 Engine ThrottleLinkage 2A6X1-002 002.004.004.024.001 Remove 2A6X1-002 002.004.004.024.003 Install 2A6X1-002 002.004.004.024.004 Rig 2A6X1-002 002.004.004.027 Ring Cowl 2A6X1-002 002.004.004.027.001 Remove 2A6X1-002 002.004.004.027.003 Install 2A6X1-002 002.004.004.028 Nacelle Anti-ice Valve 2A6X1-002 002.004.004.028.001 Remove 2A6X1-002 002.004.004.028.003 Install 2A6X1-002 002.004.004.029 Engine Mounts 2A6X1-002 002.004.004.029.001 Remove 2A6X1-002 002.004.004.029.002 Disassemble 2A6X1-002 002.004.004.029.004 Assemble 2A6X1-002 002.004.004.029.005 Install 2A6X1-002 002.004.004.030 Nose Dome 2A6X1-002 002.004.004.030.001 Remove 2A6X1-002 002.004.004.030.003 Install 2A6X1-002 002.004.004.031 Thrust Reverser 2A6X1-002 002.004.004.031.001 Theory 2A6X1-002 002.004.004.031.002 Remove 2A6X1-002 002.004.004.031.004 Install 2A6X1-002 002.004.004.031.005 Rig 2A6X1-002 002.004.004.032 Thrust Reverser Actuator 2A6X1-002 002.004.004.032.001 Remove 2A6X1-002 002.004.004.032.003 Install 2A6X1-002 002.004.004.033 Blocker Door 2A6X1-002 002.004.004.033.001 Remove 2A6X1-002 002.004.004.033.003 Install 2A6X1-002 002.004.004.034 Translating Cowl 2A6X1-002 002.004.004.034.001 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-12-21 2010-01-04 - - - - - - - 2009-12-21 2010-01-04 - - - - - - - 2009-09-08 2009-10-02 - 2b - - - - - 5 2009-09-08 2009-10-02 - 2b - - - - - 5 2009-09-08 2009-10-02 - a - - - - - 2009-09-08 2009-10-02 - 2b - - - - - 2009-09-08 2009-10-02 - 2b - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2009-10-05 2009-10-13 - - - - - - - 2009-10-05 2009-10-13 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-10-05 2009-10-13 - - - - - - - 2009-10-05 2009-10-13 - - - - - - - 2013-10-01 2013-10-08 - - B - - - - 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-15 - - - - - - - 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-38 1. Tasks Knowledge And Technical References Remove 2A6X1-002 002.004.004.034.003 Install 2A6X1-002 002.004.004.036 Thrust Reverser Control Valve 2A6X1-002 002.004.004.036.001 Remove 2A6X1-002 002.004.004.036.003 Install 2A6X1-002 003 ENGINE INSPECTION and PREVENTIVE MAINTENANCE TR: TOs 00-5-14, 00-20 series, and applicable aircraft/engine TOs 2A6X1-002 003.001 Perform inspections 2A6X1-002 003.001.001 Inlet and exhaust 2A6X1-002 003.001.002 Special Inspections (Over Speed, Over Temperature) 2A6X1-002 003.002 Clean Gas Turbine Aircraft Engines and Associated Parts 2A6X1-002 004 ENGINE REMOVAL and INSTALLATION IN AIRFRAME 2A6X1-002 004.001 Remove Engine 2A6X1-002 004.002 Install Engine 2A6X1-002 005 ENGINE RIGGING TR: Applicable Aircraft/Engine TOs 2A6X1-002 005.001 Rig 2A6X1-002 005.002 Inspect 2A6X1-004 001 ENGINE INSPECTION AND PREVENTIVE MAINTENANCE F108/CFM56 (KC-135R) Attachment 6 2A6X1-004 001.001 Constructional Features 2A6X1-004 001.003 Clean Gas Turbine Aircraft Engines and Associated Parts TR: TO 2J-1-13 2A6X1-004 001.006 Operate, /Retrieve/ Data From Turbine/ Engine Monitoring System or Data Download Transfer Unit (DDTU) 2A6X1-004 002 ENGINE MAINTENANCE TR: TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicableaircraft/ engine TOs 2A6X1-004 002.001 Perform Preliminary Maintenance Procedures 2A6X1-004 002.002 Apply External Electrical Power 2A6X1-004 002.004 Perform Engine Maintenance 2A6X1-004 002.004.001 Fan Blade TO 2J-F108-2-1 2A6X1-004 002.004.001.001 Remove 2A6X1-004 002.004.001.002 Inspect 2A6X1-004 002.004.001.003 Install 2A6X1-004 002.004.001.004 Repair (Blend) 2A6X1-004 002.004.002 Fan Outlet Guide Vanes 2A6X1-004 002.004.002.001 Remove 2A6X1-004 002.004.002.003 Install 2A6X1-004 002.004.003 Acoustical Panels 2A6X1-004 002.004.003.001 Remove 2A6X1-004 002.004.003.003 Install 2A6X1-004 002.004.004 Idle Reset Solenoid 2A6X1-004 002.004.004.001 Remove 2A6X1-004 002.004.004.003 Install 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-12-21 2010-01-15 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2009-12-21 2010-01-07 - - - - - - - 2012-03-09 2012-03-09 - - - - - - - 2012-03-09 2012-03-09 - - - - - - - 2010-01-04 2010-01-05 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2013-10-01 2013-10-08 - - B - - - - 2010-01-04 2010-01-05 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2011-08-01 2011-08-03 - - - - - - - 5 2011-07-12 2011-07-12 - - - - - - - 7 2012-08-08 2012-08-08 - - - - - - - 5 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T-39 1. Tasks Knowledge And Technical References 2A6X1-004 002.004.005 COMPRESSOR BLEED SYSTEM 2A6X1-004 002.004.005.001 Theory 2A6X1-004 002.004.006 Bleed Valve and Master Ball Screw Actuator Assembly 2A6X1-004 002.004.006.001 Remove 2A6X1-004 002.004.006.003 Install 2A6X1-004 002.004.007 Bleed Valve and Ball Screw Actuator Assembly 2A6X1-004 002.004.007.001 Remove 2A6X1-004 002.004.007.003 Install 2A6X1-004 002.004.008 VBV Stop Mechanism 2A6X1-004 002.004.008.001 Remove 2A6X1-004 002.004.008.003 Install 2A6X1-004 002.004.009 VBV Fuel Gear Motor 2A6X1-004 002.004.009.001 Remove 2A6X1-004 002.004.009.003 Install 2A6X1-004 002.004.010 VBV Feedback Cable 2A6X1-004 002.004.010.001 Remove 2A6X1-004 002.004.010.003 Install 2A6X1-004 002.004.011 VSV Feedback Cable 2A6X1-004 002.004.011.001 Remove 2A6X1-004 002.004.011.003 Install 2A6X1-004 002.004.012 Throttle Gear Box 2A6X1-004 002.004.012.001 Remove 2A6X1-004 002.004.012.003 Install 2A6X1-004 002.004.013 High Pressure Turbine Clearance Control Valve(TCCV) 2A6X1-004 002.004.013.001 Remove 2A6X1-004 002.004.013.003 Install 2A6X1-004 002.004.014 Fuel pump 2A6X1-004 002.004.014.001 Remove 2A6X1-004 002.004.014.003 Install 2A6X1-004 002.004.015 Main Engine Control/Hydro-mechanical Unit 2A6X1-004 002.004.015.001 Remove 2A6X1-004 002.004.015.003 Install 2A6X1-004 002.004.016 Heat Exchanger 2A6X1-004 002.004.016.001 Remove 2A6X1-004 002.004.016.003 Install 2A6X1-004 002.004.017 Fuel Filter 2A6X1-004 002.004.017.001 Remove 2A6X1-004 002.004.017.002 Inspect 2A6X1-004 002.004.017.003 Install 2A6X1-004 002.004.018 Fuel Nozzles (External) 2A6X1-004 002.004.018.001 Remove 2A6X1-004 002.004.018.003 Install 2A6X1-004 002.004.019 Fuel Flow Transmitter 2A6X1-004 002.004.019.001 Remove 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2013-10-01 2013-10-08 - - B - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 7 2012-08-08 2012-08-08 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-40 1. Tasks Knowledge And Technical References 2A6X1-004 002.004.019.003 Install 2A6X1-004 002.004.020 Integrated Drive Generator (IDG) 2A6X1-004 002.004.020.001 Remove 2A6X1-004 002.004.020.003 Install 2A6X1-004 002.004.020.004 Service 2A6X1-004 002.004.021 IDG Oil Cooler 2A6X1-004 002.004.021.001 Remove 2A6X1-004 002.004.021.003 Install 2A6X1-004 002.004.022 Engine Starter 2A6X1-004 002.004.022.001 Remove 2A6X1-004 002.004.022.004 Sealol/Seal 2A6X1-004 002.004.022.004.001 Service 2A6X1-004 002.004.023 Starter Control Valve 2A6X1-004 002.004.023.001 Remove 2A6X1-004 002.004.023.003 Install 2A6X1-004 002.004.024 Hydraulic Pump 2A6X1-004 002.004.024.001 Remove 2A6X1-004 002.004.024.003 Install 2A6X1-004 002.004.027 Tail pipe/Tail cone 2A6X1-004 002.004.027.001 Remove 2A6X1-004 002.004.027.003 Install 2A6X1-004 002.004.028 Fan Cowling 2A6X1-004 002.004.028.001 Remove 2A6X1-004 002.004.028.003 Install 2A6X1-004 002.004.028.004 Open/Close 2A6X1-004 002.004.029 Fan Duct 2A6X1-004 002.004.029.001 Remove 2A6X1-004 002.004.029.003 Install 2A6X1-004 002.004.029.004 Open/Close 2A6X1-004 002.004.030 ANTI-ICE SYSTEM 2A6X1-004 002.004.030.001 Theory 2A6X1-004 002.004.031 Ring Cowl 2A6X1-004 002.004.031.001 Remove 2A6X1-004 002.004.031.003 Install 2A6X1-004 002.004.032 Nacelle Anti-ice Valve 2A6X1-004 002.004.032.001 Remove 2A6X1-004 002.004.032.003 Install 2A6X1-004 002.004.033 Engine Mounts 2A6X1-004 002.004.033.001 Remove 2A6X1-004 002.004.033.003 Install 2A6X1-004 002.004.034 Front Spinner Cone 2A6X1-004 002.004.034.001 Remove 2A6X1-004 002.004.034.003 Install 2A6X1-004 002.004.035 Rear Spinner Cone 2A6X1-004 002.004.035.001 Remove 2A6X1-004 002.004.035.003 Install 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2009-09-25 2009-09-25 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-12-21 2010-01-04 - - - - - - - 2009-12-21 2010-01-04 - - - - - - - 2011-08-01 2011-08-03 - - - - - - - 2009-12-21 2010-01-04 - - - - - - - 2009-12-21 2010-01-04 - - - - - - - 2011-08-01 2011-08-03 - - - - - - - 2013-10-01 2013-10-08 - - B - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-12-21 2010-01-05 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 5 5 5 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-41 1. Tasks Knowledge And Technical References 2A6X1-004 002.004.036 Oil Pump 2A6X1-004 002.004.036.001 Remove 2A6X1-004 002.004.036.003 Install 2A6X1-004 002.004.037 Oil Tank 2A6X1-004 002.004.037.001 Remove 2A6X1-004 002.004.037.003 Install 2A6X1-004 002.004.037.004 Service 2A6X1-004 002.004.038 Oil Filter 2A6X1-004 002.004.038.001 Remove 2A6X1-004 002.004.038.003 Install 2A6X1-004 002.004.039 Chip Detectors 2A6X1-004 002.004.039.001 Remove 2A6X1-004 002.004.039.002 Inspect 2A6X1-004 002.004.039.003 Install 2A6X1-004 002.004.040 Oil Pressure Transmitter 2A6X1-004 002.004.040.001 Remove 2A6X1-004 002.004.040.002 Inspect 2A6X1-004 002.004.040.003 Install 2A6X1-004 002.004.041 Oil Differential Pressure Switch 2A6X1-004 002.004.041.001 Remove 2A6X1-004 002.004.041.003 Install 2A6X1-004 002.004.042 Oil Temperature Sensor 2A6X1-004 002.004.042.001 Remove 2A6X1-004 002.004.042.003 Install 2A6X1-004 002.004.043 Low Oil Pressure Switch 2A6X1-004 002.004.043.001 Remove 2A6X1-004 002.004.043.003 Install 2A6X1-004 002.004.044 N1 Speed Sensor 2A6X1-004 002.004.044.001 Remove 2A6X1-004 002.004.044.003 Install 2A6X1-004 002.004.045 N2 Control Alternator 2A6X1-004 002.004.045.001 Remove 2A6X1-004 002.004.045.003 Install 2A6X1-004 002.004.046 Power Management Control 2A6X1-004 002.004.046.001 Remove 2A6X1-004 002.004.046.003 Install 2A6X1-004 002.004.047 T-12 Sensor 2A6X1-004 002.004.047.001 Remove 2A6X1-004 002.004.047.003 Install 2A6X1-004 002.004.048 Compressor Inlet Temperature (CIT) Sensor 2A6X1-004 002.004.048.001 Remove 2A6X1-004 002.004.048.003 Install 2A6X1-004 002.004.049 Exciter 2A6X1-004 002.004.049.001 Remove 2A6X1-004 002.004.049.003 Install 2A6X1-004 002.004.050 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2014-10-20 2014-11-17 - - - - - - - 2014-10-20 2014-11-17 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 7 2012-08-08 2012-08-08 - - - - - - - 5 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2014-10-20 2014-11-17 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-42 1. Tasks Knowledge And Technical References Igniter Plug 2A6X1-004 002.004.050.001 Remove 2A6X1-004 002.004.050.003 Install 2A6X1-004 002.004.051 Igniter Lead 2A6X1-004 002.004.051.001 Remove 2A6X1-004 002.004.051.003 Install 2A6X1-004 002.004.052 Thermocouple Harness 2A6X1-004 002.004.052.001 Remove 2A6X1-004 002.004.052.003 Install 2A6X1-004 002.004.053 Thermocouples 2A6X1-004 002.004.053.001 Remove 2A6X1-004 002.004.053.003 Install 2A6X1-004 002.004.054 LPT Cooling Manifold 2A6X1-004 002.004.054.001 Remove 2A6X1-004 002.004.054.003 Install 2A6X1-004 002.004.055 Transfer Gearbox 2A6X1-004 002.004.055.001 Remove 2A6X1-004 002.004.056 Transfer Gearbox Magnetic/Sealol Seal 2A6X1-004 002.004.056.001 Remove 2A6X1-004 002.004.056.003 Install 2A6X1-004 002.004.057 Accessory Gearbox 2A6X1-004 002.004.057.001 Remove 2A6X1-004 002.004.058 Accessory Transfer Gearbox Magnetic/Sealol Seal 2A6X1-004 002.004.058.001 Remove 2A6X1-004 002.004.058.002 Inspect 2A6X1-004 002.004.058.003 Install 2A6X1-004 002.004.059 5th Stage Bleed Air Check Valve 2A6X1-004 002.004.059.001 Remove 2A6X1-004 002.004.059.003 Install 2A6X1-004 002.004.060 Speed Control Box 2A6X1-004 002.004.060.001 Remove 2A6X1-004 002.004.060.003 Install 2A6X1-004 002.005 ENGINE RIGGING TR: Applicable Aircraft/Engine TOs 2A6X1-004 002.005.001 Rig Engine Variable Stator Vane (VSV) Feedback Cable 2A6X1-004 002.005.002 Rig Engine Variable Bleed Valve (VBV) Feedback Cable 2A6X1-004 002.005.003 Rig MEC/Throttle Cable 2A6X1-004 002.005.004 PMC test 2A6X1-004 002.005.005 PLA Gain Adjustment 2A6X1-004 003 Aircraft Installed Engine Testing TR: Applicable Aircraft/Engine TOs 2A6X1-004 003.002 Perform Engine Run (Including Pre-PE Performance) 2A6X1-004 003.003 Engine Trim Position A (Left Seat) 2A6X1-004 003.004 Engine Trim Position B (Right Seat)/Trim Supervisor 2A6X1-004 003.005 Perform Ground Observer/Position C 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2013-10-01 2013-10-08 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2011-07-12 2011-07-12 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 7 2013-10-01 2013-10-08 - - - - - - - 7 2013-10-01 2013-10-08 - - - - - - - 7 2013-10-01 2013-10-08 - - - - - - - 7 2009-09-25 2009-09-25 - - - - - - - 7 2009-09-25 2009-09-25 - - - - - - - 2012-03-09 2012-03-09 - - - - - - - 2012-04-23 2012-05-09 - - - - - - - 2012-04-23 2012-05-09 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T-43 1. Tasks Knowledge And Technical References Duties During Engine Run 2A6X1-004 003.006 Fan Trim Balance 2A6X1-004 003.007 Audible Ignition System Check-Out 2A6X1-004 003.008 Install, Operate And Remove Trim Equipment 2A6X1-004 003.009 Engine Leak Check 2A6X1-004 005 Engine Removal and Installation In Airframe TR: TOs 1-1A-8, 2J-1-24, and applicable aircraft TOs 2A6X1-004 005.001 Remove Engine 2A6X1-004 005.002 Install Engine 2A6X1-004 005.003 Service Engine 2A6X1-008A 001 Jet Fuel Start (JFS) Attachment 10 2A6X1-008A 001.001 JFS 2A6X1-008A 001.001.001 Remove 2A6X1-008A 001.001.002 Inspect 2A6X1-008A 001.001.003 Install 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2012-04-23 2012-05-09 - - - - - - - 2009-09-25 2009-09-25 - - - - - - - 2012-04-23 2012-05-09 - - - - - - - 5 2011-08-17 2011-08-17 - - - - - - - 7 2011-07-12 2011-07-12 - - - - - - - 7 2011-07-12 2011-07-12 - - - - - - - 5 2011-07-12 2011-07-12 - - - - - - - 2009-09-08 2009-10-02 - - - - - - - 2009-09-08 2009-10-02 - - - - - - - 2009-09-08 2009-10-02 - - - - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T-44 JOB QUALIFICATION STANDARD CONTINUATION/WJQS CRITICAL TASK NUMBER TASKS 35980 001 35980 001.001 35980 001.002 35980 001.003 35980 001.004 35980 002 35980 002.001 35980 002.002 35980 002.003 35980 004 35980 004.001 35980 005 35980 005.001 35980 006 35980 006.001 35980 007 35980 007.001 35980 007.002 35980 008 35980 008.001 35980 008.002 35980 008.004 35980 008.005 35980 008.006 35980 008.007 35980 008.007.001 35980 008.007.002 35980 008.007.003 35980 008.007.004 35980 008.007.004.001 35980 008.007.004.002 35980 008.007.004.003 35980 008.007.004.004 35980 008.007.004.004. 001 35980 008.007.004.004. 002 35980 008.007.004.004. 003 35980 008.007.004.004. 004 35980 008.007.004.004. 004.001 35980 008.007.004.004. 004.002 35980 008.007.004.004. 004.003 35980 008.007.004.004. 004.004 35980 008.007.004.004. 004.004.001 TASKS, KNOWLEDGE AND TECHNICAL REFERENCES CERTIFICATION START DATE PREFORM GROUND HANDLING: T.O. 1C-135-2-2-2 De-Ice ACFT T.O. 1C-135-2-2-2 Aircraft wash team member T.O. 1-1-691 Remove and install landing gear down locks T.O. 1C-135-2-2-2 Remove and install tail stand T.O 1C-125-2-2-2 AIRFRAME SYSTEM: T.O. 1C-135-2-7 Operate wheel well doors T.O. 1C-135-2-7 Operate cargo door T.O. 1C-135-2-2-2 Operate crew entry door T.O. 1C-135-2-2-2 PNEUDRAULIC SYSTEM: T.O. 1C-135-2-2-2 Service left / right hydraulic reservoirs T.O. 1C-135-2-2-2 FUELS (REFUEL / DEFUEL): T.O. 1C-135-2-2-2 Refuel / defuel panel operator T.O. 1C-135-2-2-2 PINTLE HOOK: T.O. 1-1A-15 Understands and Operates the Pintle Hook TR T.O. 1-1A-15, par 25.1.1, 25.1.2, 25.1.3 25.1.4, 25.1.5, 25.2 T.O. 36-1-121 and T.O . 36-1-191, para 2.78 JET FUEL STARTER (JFS) T.O. 1C-135-2-4-1-1 JFS Oil Service T.O. 1C-135-2-2-2 JFS Oil Change T.O. 1C-135-2-2-2 AUXILARY POWER UNIT (APU) T.O. 1C-135-2-16 APU Inspection T.O.1C-135-2-16 Intake Door, shaft, and handle installation T.O. 1C-135-2-16 Page 5-29 Para 5-37 Remove T.O. 1C-135-2-16 Install T.O. 1C-135-2-16 Preform APU Operation T.O. 1C-135-2-2-2 APU Fuel system components T.O. 2G-GTCP85-41-2 Remove T.O.2G-GTCP85-41-2 Inspect T.O. 2G-GTCP85-41-2 Install T.O. 2G-GTCP85-41-2 APU Oil system components T.O. 2G-GTCP85-41-2 Remove T.O. 2G-GTCP85-41-2 Inspect T.O. 2G-GTCP85-41-2 Install T.O. 2G-GTCP85-41-2 APU Ignition system components T.O. 2G-GTCP85-41-2 Remove T.O. 2G-GTCP85-41-2 COMPLETION DATE TRAINEE'S TRAINER'S CERTIFIER'S INITIALS INITIALS INITIALS 2010-01-04 2010-02-02 2009-09-08 2009-10-02 2009-09-08 2009-10-02 2009-09-08 2009-10-02 2009-09-08 2009-10-02 2009-09-08 2009-10-02 2009-09-08 2009-10-02 2010-01-04 2010-01-05 2010-05-05 2010-06-02 2009-09-08 2009-10-02 2009-09-08 2009-10-02 2009-09-08 2009-10-02 2011-08-17 2011-08-17 2011-04-22 2011-05-23 2011-08-17 2011-08-17 2011-08-17 2011-08-17 2011-08-17 2011-08-17 2011-08-17 2011-08-17 2011-08-17 2011-08-17 2011-08-17 2011-08-17 2011-04-22 2011-05-23 2011-08-17 2011-08-17 2011-04-22 2011-05-23 2011-07-12 2011-07-12 Inspect T.O. 2G-GTCP85-41-2 2011-07-12 2011-07-12 Install T.O. 2G-GTCP85-41-2 2011-07-12 2011-07-12 Remove T.O. 2G-GTCP85-41-2 2011-07-12 2011-07-12 Inspect T.O. 2G-GTCP85-41-2 2011-07-12 2011-07-12 Install T.O. 2G-GTCP85-41-2 2011-08-17 2011-08-17 2011-04-22 2011-05-23 APU starter system components T.O. 2G-GTCP85-41-2 APU Ducting T.O. 2G-GTCP85-41-2 Remove T.O. 2G-GTCP85-41-2 RC-135V, T/N 64-14848, 30 April 2015 T-45 JOB QUALIFICATION STANDARD CONTINUATION/WJQS CRITICAL TASK NUMBER TASKS 35980 008.007.004.004. 004.004.002 35980 008.007.004.004. 004.004.003 35980 008.007.004.004. 004.004.004 35980 008.007.004.004. 004.004.004.001 35980 008.007.004.004. 004.004.004.002 35980 008.007.004.004. 004.004.004.003 35980 009 35980 009.001 35980 009.002 35980 009.003 35980 011 35980 011.001 35980 011.002 35980 011.003 TASKS, KNOWLEDGE AND TECHNICAL REFERENCES CERTIFICATION START DATE COMPLETION DATE TRAINEE'S TRAINER'S CERTIFIER'S INITIALS INITIALS INITIALS 2011-07-12 Inspect T.O. 2G-GTCP85-41-2 2011-07-12 Install T.O. 2G-GTCP85-41-2 2011-04-22 2011-05-23 Remove T.O. 2G-GTCP85-41-2 2011-07-12 2011-07-12 Inspect T.O. 2G-GTCP85-41-2 2011-07-12 2011-07-12 Install T.O. 2G-GTCP85-41-2 2011-07-12 2011-07-12 2009-02-05 2009-02-26 2009-02-27 2009-03-27 2009-03-27 2009-04-13 2013-10-01 2013-10-08 2013-10-01 2013-10-08 2013-10-01 2013-10-08 APU Plumbing T.O. 2G-GTCP85-41-2 COMPLETE 2A651 5 LEVEL CDC AFI 36-2201 5 LEVEL CDC VOLUME 1 AFI 36-2201 5 LEVEL CDC VOLUME 2 AFI 36-2201 5 LEVEL CDC VOLUME 3 AFI 36-2201 MISCELLANEOUS SYSTEMS T.O.'s 1C-135-2-4-1-1, 1C-135-2-4-2, 1C-135-2-4-3 Rig T/R Torque arm compensator T.O. 1C-135-2-4-3 Install T/R Torque arm compensator T.O. 1C-135-2-4-3 Remove T/R Torque arm compensator T.O. 1C-135-2-4-3 RC-135V, T/N 64-14848, 30 April 2015 T-46 JOURNAL ENTRIES ENTRY SUBJECT DATE 2009-08-24 Conduct Orientation/Initial Evaluation 2015-04-24 180 Day SIGNATURE INFO REMARKS Within 60 days of assignment the Supervisor will conduct a Workcenter Orientation and Initial Evaluation of qualifications IAW AFI 36-2201 V3. is 100% qualified. Total review of his record was conducted on 24 Apr 2015. 0 Discrepancies found. He continues to stay proficient. He is doing a great job. 2014-10-22 180 Day Review is 100% qualified. Total review of his record was conducted on 22 Oct 2014. No Discrepancies found. He is currently deployed. 2014-08-25 Supervisor Deploying/Trainer Appointment On Sep 1 2014 until I, supervision of 2014-06-05 TDY 2014-06-05 leave 2014-06-05 TDY 2014-06-05 leave 2014-05-12 Leave 2014-04-22 180 Day Review , return for my deployment on approx Dec 15 2014 will be under the temperary direct will be going TDY from 20140507 to 20140526. His training will be suspeneded until his return. returned from Leave on 20140605. 100% task qualified staying proficeint in his trianing. will be going TDY from 20140507 to 20140526. His training will be suspeneded until his return. returned from Leave on 20140605. 100% task qualified staying proficeint in his trianing. will be on leave from 27 May - 4 June. is 100% qualified. Total review of his record was conducted on 22 Apr 2014. 0 Discrepancies found. He continues to stay proficient. He is doing a great job. 2013-09-12 TF-33 P-5 Test Failure failed his EPE portion of the TF-33 P-5 test. He will study while TDY and test upon his return. 2013-09-12 TDY will be TDY on the OPEN SKIES from 13 Sept - 24 Sept. 2013-09-12 TF-33 P-5 Test Failure failed his EPE portion of the TF-33 P-5 test. He will study while TDY and test upon his return. 2013-09-12 TDY will be TDY on the OPEN SKIES from 13 Sept - 24 Sept. 2013-09-06 F-108 Eng Run Cert. has been certified on F-108 Eng Run. His 64 has been routed. 2013-08-22 Workcenter Orientation 2013-08-22 Initial Evaluation 2013-08-22 Workcenter Orientation 2013-08-22 Initial Evaluation 2013-06-26 P-5/9 eng run test 2013-05-20 SrA Stevens TBA Review I reaccomplished a workcenter orientation withSrA on 2013-08-22. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. I reaccomplished an initial evaluation with on 2013-08-22. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he was briefed that his training is ultimately his responsibility, and he needs to ensure he reviews his training records at least once a week and actively pursues the training he needs to complete his upgrade. He has also been briefed that tasks should be signed off within 30 days of the start date, unless mission requirements prohibit the completion of the task within that time. I reaccomplished a workcenter orientation withSrA on 2013-08-22. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. I reaccomplished an initial evaluation with on 2013-08-22. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he was briefed that his training is ultimately his responsibility, and he needs to ensure he reviews his training records at least once a week and actively pursues the training he needs to complete his upgrade. He has also been briefed that tasks should be signed off within 30 days of the start date, unless mission requirements prohibit the completion of the task within that time. has scored 100,100,96% on his test On this date TBA has been reviewed. He continues to be fully 5 level qualified and continues to progress further with OJT and Technical Order review. He continues to show enthusiasm and eagerness to continue progression at his current and future skill level. 2013-04-17 Trainer Upgrade needs to become a trainer for everybody in the workcenter for the section 2013-03-06 90 day review I reviewed TBA entries today for accuracy and completion. There were no errors noted on this date. 2012-12-20 90 day Review I reviewed TBA entries today for accuracy and completion. There were no errors noted on this date. 2012-12-20 Informatoin did not go TDY due to a cancelatoin. He is how ever going on the January Blue on Blue. 2012-12-20 90 day Review I reviewed TBA entries today for accuracy and completion. There were no errors noted on this date. 2012-12-06 TDY 10-11 Dec will be leaving for an unknown amount of time. We look foward to having him back soon. 2012-11-29 Blade blend and bvore scope cert has been certified on F108, Tf-33 P9, P5 Blade Blend and F108 Bore scope. I will route his 64 to add him to the SCR. RC-135V, T/N 64-14848, 30 April 2015 T-47 JOURNAL ENTRIES ENTRY SUBJECT SIGNATURE INFO DATE 2012-09-27 TF-33/ F108 Borescope and Blade blend certification REMARKS has been trained and Certified on TF-33 and F108 Bore Scope and Blade Blend by 2012-09-06 90 Day Review I reviewed 2012-08-30 Deployment I 2012-08-09 Tasks Today 2012-06-14 90 Day review I reviewed 2012-06-14 Deployment Return 2012-06-14 90 Day review TBA entries today for accuracy and completion. There were no errors noted on this date. will be deployed from 6 Sep to 15 Dec. will be supervisor/trainer while I am deployed. started and signed off several tasks. #s TBA entries today for accuracy and completion. There were no errors noted on this date. returned from his deployment today. He will be on CTO's for 14 days. I reviewed 2012-06-14 Deployment Return #s TBA entries today for accuracy and completion. There were no errors noted on this date. returned from his deployment today. He will be on CTO's for 14 days. 2012-05-09 TBA Review Went over TBA. He is dong a great job in his deployed location. 2012-04-16 TBA Review Reviewed TBA and he has been progressing well above his peers 2012-03-30 INLETS AND EXHAUST I certified 2012-03-26 F-108 ENG RUN 64 2012-03-09 F108 Eng Run Cert on Inlets and exhaust. He is doing a great job. 64 routed has completed all requirment to run the F-108 eng. I will be add him to the SCR for this. I certified 2012-02-24 Leave on F108 eng run, and also Inlets and exhaust. 64 routed will be on leave from 28 Feb through 02 Mar. 2012-01-27 Feedback Conducted feedback on 25Jan2012, Reviewed responsabilities and expectations. 2012-01-03 Jan Status No updates needs. 2011-11-17 TDY 2011-10-21 TBA Review . His 64 has been routed. is a great worker, he sets the example is working beyond air force standars. Good Job is TDY to Vegas, he will be back the begining part of December. Reviewed 2011-08-22 Leave TBA. Started task and signed off a task. is doing a good job. will be on leave 5-19 September. 2011-08-17 APU TASKS Today started and was signed off on several tasks. He also was certified on APU operation in which his 64 will be routed. 2011-07-20 Initial Orientation Brief Upon review of ' ITP, the Initial Orientation Briefing was conducted, however there was not a journal entry by this supervisor in TBA. Today, a Workcenter Orientation and Initial Evaluation of qualifications was conducted with IAW AFI 36-2201 V3. 2011-07-12 Tasks Today started and signed off several tasks. 2011-07-11 TBA review has just returned back to work after taking his CTO days. He is going very good on his training. 2011-06-16 TDY is still deployed to the desert and will be back the last part of June before he goes on his CTOS 2011-05-23 Task Signed off some task. He is doing a great job. 2011-04-22 TBA Review Reviewed TBA, added task to his TBA. He is doing a great job. 2011-04-05 Task Signed off some task in TBA. RC-135V, T/N 64-14848, 30 April 2015 T-48 JOURNAL ENTRIES ENTRY DATE SUBJECT SIGNATURE INFO REMARKS 2011-04-04 Task Got in touch with 2011-04-01 TBA Reviewed bang up job. at his deployed location, and we are going to sign off a few task, still doing a bang up job TBA, removed some task that he cannot get signed off untill he is Red x Qualified. Started task, he is doing a 2011-03-24 Deployment is still deployed and won't return until June. 2010-12-20 Deployed is deployed for 90 days 2010-10-21 Feedback Today was given his initial feedback. 2010-10-13 F108 Blade Blend Cert has been trained and certified by on F108 B-Blend. His 64 is being routed. 2010-10-13 Tasks restored from archive on 2010-10-13 2010-10-13 F108 Blade Blend Cert 6 Tasks were restored from archive on 2010-10-13 2010-10-13 Tasks restored from archive on 2010-10-13 2010-09-20 Return from Leave 6 Tasks were restored from archive on 2010-10-13 2010-09-16 Records Review Performed a records review on This date. Removed tasks that are not required at his skill level. Member is fully qualified and up to date on his training. has been trained and certified by Has Returned From Leave On 18 Sept. 2010 2010-08-17 Leave 2010-08-05 Task Recertification 2010-08-05 Recertification of Task 000.001.005.001 2010-08-05 Task Recertification 2010-07-30 Start Date For Tach Gen 2010-07-30 Error for Decertification for Task CFETP2A6X1-002-001.008.001.001 2010-07-30 Start Date For Tach Gen 2010-07-29 F108 Blade Blend 2010-07-12 Deployment return on F108 B-Blend. His 64 is being routed. Is Going On Leave From 22 Of Aug Till 17 Sept. has been recertified on task WJQS-35980-00.001.001, 1500 Fan Blade Inspection. Individual has been briefed and understands FOD Prevention practices as outlined in AFI 21-101, Ch 14, para 14.19.2.4. On 3 August, 2010, displayed that he is capable of performing appropriate FOD prevention practices as directed by AFI 21-101, Ch 14, para 14.19.2.4 stating in part "A pocketless, zipperless, buttonless bunny-suit, cloth over-boots or stocking feet, boots removed, for intakes only, will be worn whenever physical entry into an aircraft intake or exhaust is required. has been recertified in This task. has been retrained on FOD prevention practices and displays an in-depth understanding of Air Force and local FOD prevention practices. has been recertified on task WJQS-35980-00.001.001, 1500 Fan Blade Inspection. Individual has been briefed and understands FOD Prevention practices as outlined in AFI 21-101, Ch 14, para 14.19.2.4. Incorrect task was decertified, see tasks 001.005.001 & WJQS 35980-001.002.001. A new start date has been added, awaiting to sign as trainee and I will re-sign off the task as trainer Incorrect task decertified, see tasks 001.005.001 & WJQS 35980-001.002.001 Incorrect task was decertified, see tasks 001.005.001 & WJQS 35980-001.002.001. A new start date has been added, awaiting to sign as trainee and I will re-sign off the task as trainer has been through both F108 and TF 33 blade blend. He is comfortable performing these tasks. has returned from the desert on 20 June and returned back to work. He is still awaiting for his continuation tasks. 2010-05-17 Feedback has a feedback due. He is currently deployed and we will do a feedback once he returns from his deployment 2010-05-13 Deployed is on a deployment. The dates are 15 Mar until the later part of June. 2010-02-25 Award of 5 Skill Level Member has met all mandatory training requirements IAW AFI 36-2201 for award of his/her next higher skill level. MILPDS, IMDS, and TBA has been updated. 2010-02-19 5-Level I recommend 2010-02-16 5-Level Upgrade for 5-level upgrade has been completed on every required 5-level task and is prepared for upgrade. 2010-02-03 Remaining Tasks had 8 old start dates signed off today, and also had his remaining 5 tasks started. He will have his paperwork for upgrade submitted by the middle of the month. 2010-01-16 Task(s) archived on 2010-01-16 2010-01-16 Start Dates Signed Off 10 task(s) archived on 2010-01-16 by employee: 2010-01-16 Task(s) archived on 2010-01-16 10 task(s) archived on 2010-01-16 by employee: had 24 old start dates signed off today he is currentlly on pace to be ready for 5-level upgrade by the end of This month. RC-135V, T/N 64-14848, 30 April 2015 T-49 JOURNAL ENTRIES ENTRY SUBJECT DATE 2010-01-16 Start Dates Signed Off 2010-01-09 Old Start Dates Signed Off 2010-01-04 Training Day 2009-12-21 Started Tasks SIGNATURE INFO REMARKS had 24 old start dates signed off today he is currentlly on pace to be ready for 5-level upgrade by the end of This month. had 22 old start dates signed off today. He is now 87% qualified he will continue to fininsh his training for upgrade. Entire shop has come in for training day, we have reviewed maintenance 101, TBA, and several other training items. Was Started On Numerous Tasks Today 2009-11-13 CDC Test Review Today, and I went over the sections that were missed on his CDC test. I let him know that further studying is needed to prevent him from missing the same questions. He understands and will fully comply with the task presented upon him. 2009-11-11 Comprehensive Review Today, and I completed a comprehensive review over his CDCs. He will continue studying to retain the information. He is ready to take his EOC. 2009-11-09 EOC Pretest Scored Two More 90%'S Last Week. He Is Ready For His EOC 2009-11-03 EOC Pretest Scored A 90% On His EOC Pretest Today. 2009-10-30 New CDC Pretest 2009-10-27 Old start dates completed his first pretest, with the new CDC pretest and scored an 81%. He will continue to study This weekend, and take another pretest on Monday. was signed off on old start dates today. There will be more start dates added to progress with his training. 2009-10-26 Supervised Study On today 2009-10-26 I went over all volumes UREs and self-test questions 2009-10-23 Supervised Study Today on OCT 23 2009 we went over volume 5 section 3-1 to 3-46 he is doing good and is seeming more confident 2009-10-23 SUPERVISED STUDY On OCT 21 2009 we went through volume 4 sectiOn 1-31 thru 1-52 I asked him questions and he seems to be doing well we also went over the self-test questions and UREs On Thursday October 21 2009 we went thru volume 2 sectiOn 5-1 thru 5-46 again went through self-test questions urea and highlighted portion. Today on OCT 23 2009 we went over volume 5 section 3-1 to 3-46 he is doing good and is seeming more confident 2009-10-23 Supervised Study 2009-10-23 Supervised Study 2009-10-23 SUPERVISED STUDY 2009-10-23 Supervised Study 2009-10-21 Update 2009-10-20 Supervised Study 2009-10-20 Supervised Study 2009-10-20 Supervised Study 2009-10-15 Supervised Study 2009-10-15 Supervised Study is ready to test and is On track. On OCT 21 2009 we went through volume 4 sectiOn 1-31 thru 1-52 I asked him questions and he seems to be doing well we also went over the self-test questions and UREs On Thursday October 21 2009 we went thru volume 2 sectiOn 5-1 thru 5-46 again went through self-test questions urea and highlighted portion. ITP was updated to match 5-level upgrade tasks. Today on Oct 20 2009 we went over volume 3 section 1-2 thru 2-48 asked him the self-test questions and the UREs also went over his highlighted sections he is doing well and is making progress. Today on Oct 20 2009 we went over volume 3 section 1-2 thru 2-48 asked him the self-test questions and the UREs also went over his highlighted sections he is doing well and is making progress. Today on Oct 20 2009 we went over volume 3 section 1-2 thru 2-48 asked him the self-test questions and the UREs also went over his highlighted sections he is doing well and is making progress. On 20091013 we went over all volumes, I asked him questions and he seemed to know what he was talking about. He is still improving 2009-10-15 Supervised Study On OCT 15 2009 we went over volume 4 UREs and self-test questions he seems to be struggling and may need more time to study it. I told him to concentrate On This volume On Oct 12 2009 supervised study went alot better he is starting to retain the informatiOn and has a better attudie 2009-10-15 Supervised Study On OCT 14 2009 we went over volume 3 over th UREs and self-test questions he is doing good 2009-10-15 Supervised Study On 20091013 we went over all volumes, I asked him questions and he seemed to know what he was talking about. He is still improving 2009-10-15 Supervised Study 2009-10-15 Supervised Study On OCT 15 2009 we went over volume 4 UREs and self-test questions he seems to be struggling and may need more time to study it. I told him to concentrate On This volume On Oct 12 2009 supervised study went alot better he is starting to retain the informatiOn and has a better attudie 2009-10-15 Supervised Study On OCT 14 2009 we went over volume 3 over th UREs and self-test questions he is doing good 2009-10-14 Oil Servicing was signed off on TF 33 P5/P9 engine oil tank servicing on This date 2009-10-13 SupervSed Study On 2009-10-07 2009-10-13 Supervised Stidy On 20091009 we did some training and E seems TOn a be doing good and keeping up with the pace 2009-10-13 SupervSed Study On 2009-10-07 2009-10-13 Supervised Stidy On 20091009 we did some training and E seems TOn a be doing good and keeping up with the pace 2009-10-13 Tasks Signed Off did alot better with his studying he has been studying and is starting to show improvement did alot better with his studying he has been studying and is starting to show improvement Was Signed Off On Two Tasks On This Date RC-135V, T/N 64-14848, 30 April 2015 T-50 JOURNAL ENTRIES ENTRY DATE SUBJECT SIGNATURE INFO REMARKS 2009-10-06 Supervised Study On 20090930 today we went over more of the UREs and finished up volume 1 he is slowly making progress 2009-10-06 Supervised Study On SEP 28 2009 we went over his his UREs and volume 1 he is doing better 2009-10-06 Supervised Study On OCT 2 2009 did supervised study with he went over UREa and beginning of volume 2 he said that he was not as involved with the study and lacked inicitive. On SEP 28 2009 we went over his his UREs and volume 1 he is doing better 2009-10-06 Supervised Study 2009-10-06 Supervised Study 2009-10-06 Supervised Study 2009-10-05 Training Conducted/Start Dates Added 2009-09-25 Supervised Study 2009-09-25 Supervised Study 2009-09-25 Tasks restored from archive on 2009-09-25 2009-09-25 Supervised Study 2009-09-25 Tasks restored from archive on 2009-09-25 2009-09-25 Supervised Study 2009-09-25 Supervised Study 2009-09-18 UTM CDC Failure Interview 2009-09-18 CDC Supervised Study 2009-09-16 Supervised Study 2009-09-16 CDC Failure Interview (16 Sep 09) On OCT 2 2009 did supervised study with he went over UREa and beginning of volume 2 he said that he was not as involved with the study and lacked inicitive. On 20090930 today we went over more of the UREs and finished up volume 1 he is slowly making progress was trained on the TF33 anti-ice and starter systems on This date. Start dates were also added. On Sept 24 2009 me and went through his home work I asked him to study UREs 2-48 - 4-73 and read 6-6 --4-16 in volume 1 I asked him the questions and he missed 14 out of 40 questions and couldnt tell me about what he read out of volume 1. He s going to redue the same homework tonight and I will expect him to know the material tomorrow. From Sept 22-24 had blade blend class so I told him to keep studying his home work which was to study UREs 2-48 4-73 and read 6-6 - 4-16 in volume 1 185 Tasks were restored from archive on 2009-09-25 Mon Sept 21 2009 we went over UREs 5-53 - 2-48 and reviewed 1-5 - 6-6 in volume 1 185 Tasks were restored from archive on 2009-09-25 On Sept 24 2009 me and went through his home work I asked him to study UREs 2-48 - 4-73 and read 6-6 --4-16 in volume 1 I asked him the questions and he missed 14 out of 40 questions and couldnt tell me about what he read out of volume 1. He s going to redue the same homework tonight and I will expect him to know the material tomorrow. From Sept 22-24 had blade blend class so I told him to keep studying his home work which was to study UREs 2-48 4-73 and read 6-6 - 4-16 in volume 1 17 Sep 09 PAFSC: 2A631 CDC: 2A651 Score: 61% A commander's evaluation was accomplished on 16 Sep 09 in regards to first time CDC failure. Members present: . Course progression: Member was enrolled 28 Jan 09. He completed his volumes (5) in Jun 09. There was sufficient nformation on CDC progression documented in TBA until the final volume was completed. He took one pretest on 23 Jul 09 and scored a 100%. He took a second pretest on 5 Aug 09 and scored a 98%. He took a thrid pretest on 28 Aug 09 and scored a 95%. His supervisor at the time, , did not document the comprehensive review of all volumes in TBA. There was a period of 3 months review and pretesting before member took the course exam and member prepared self-pretest questions as a review. Understanding of the course content: indicated that he had trouble understanding Volume 4 or the CDC#s, but felt confident on the other volumes. Motivation, study habits and preparation: appeared to be motivated to complete this CDC. He felt that he had difficulty in sleeping the weekend prior to the test and that he spent a great deal of time reviewing the CDC#s he previous weekend but focused mainly on URE#s. Supervisor's involvement: appeared to be very involved with the CDC progress. He prepared volume pretest questions in conJunction with other NCO#s in the office to gauge the trainees understanding of the material, however the pretesting questions may have also focused on URE#s. The comprehensive review of all volumes of the CDC seems to be less involved than it should have been and focus on the course exam seemed to be less involved during the preparation period for the member prior to course exam. The reading abilities test was administered to him on 16 Sep 09. No eading comprehension problem was detected. On 17 Sept 09, and I went over pages 1- 25 of volume 1/ unit 1. He was quizzed on random self-test questions as well as going page by page and reading over important information. We also went of volume 1 UREs. He was able to answer most questions but still needs improvement. I gave him the tast to read over units 2-4 of volume 1 for homework and be able to answer the self-test questions. On Sept. 16 2009 I went over volume 1 sectiOn 1-27 he is going to go back over them tonight and be ready for Q and A tommarow. 2009-09-16 Supervised Study conducted an evaluation to determine the ability of , , to progress in the 5 skill level upgrade training following a ailure of the 2A651 Career Development Course (CDC) course exam. After careful review of the member's ITP and journal entries in TBA, Unit Personnel Information File (PIF), and coupled with an in-depth interview with the member and his supervisor, I have concluded that failure was due to both inadequate preparation by the member and supervisory validation of study materials. I recommend that be given an opportunity to retest. He is in supervised study for two hours a day for a minimum of five times a week. I've instructed our training managers, and in the MTF to schedule an AF Reading Abilities Test and the retake exam. On Sept. 16 2009 I went over volume 1 sectiOn 1-27 he is going to go back over them tonight and be ready for Q and A tommarow. 2009-09-03 Pre Test 3 On Aug 28 2009 2009-09-03 Pre Test 2 On Aug 5 2009 2009-09-03 Pre Test On July 23 2009 2010-07-30 Decertification for Task WJQS-35980-001.001.001 2010-07-30 Decertification for Task CFETP2A6X1-002-001.008.001.001 2010-07-30 Decertification for Task CFETP2A6X1-000-001.005.001 has been decertified in This task due to his failure to follow applicable FOD prevention practices while performing 1500hr an blade inspections as outlined in AFI 21-101, Ch 14, para 14.19.2.4. has been decertified in This task due to his failure to follow applicable FOD prevention practices while performing 1500hr an blade inspections as outlined in AFI 21-101, Ch 14, para 14.19.2.4. 2010-07-30 Decertification for Task WJQS-35980-001.001.001 2010-07-30 Decertification for Task CFETP2A6X1-002-001.008.001.001 2010-07-30 Decertification for Task CFETP2A6X1-000-001.005.001 made a 95% On his pretest we did a review over all volumes and seems ready to take his EOC. has made a 98% On his pretest hes ready to get the last one out of the way made a 100% On his pretest he seems confident in his study habits. On 29 July, 2010, was performing a 1500hr fan blade inspection and failed to utilize the appropriate FOD prevention practices as directed by AFI 21-101, Ch 14, para 14.19.2.4 stating in part "A pocketless, zipperless, buttonless bunny-suit, cloth over-boots or stocking feet, boots removed, for intakes only, will be worn whenever physical entry into an aircraft intake or exhaust is equired." In order to become recertified in This task, will be retrained on FOD prevention practices and must display an n-depth understanding of Air Force and local FOD prevention practices. has been decertified in This task due to his failure to follow applicable FOD prevention practices while performing 1500hr an blade inspections as outlined in AFI 21-101, Ch 14, para 14.19.2.4. has been decertified in This task due to his failure to follow applicable FOD prevention practices while performing 1500hr an blade inspections as outlined in AFI 21-101, Ch 14, para 14.19.2.4. On 29 July, 2010, was performing a 1500hr fan blade inspection and failed to utilize the appropriate FOD prevention practices as directed by AFI 21-101, Ch 14, para 14.19.2.4 stating in part "A pocketless, zipperless, buttonless bunny-suit, cloth over-boots or stocking feet, boots removed, for intakes only, will be worn whenever physical entry into an aircraft intake or exhaust is equired." In order to become recertified in This task, will be retrained on FOD prevention practices and must display an n-depth understanding of Air Force and local FOD prevention practices. RC-135V, T/N 64-14848, 30 April 2015 T-51 CERTIFICATION I CERTIFY THAT THIS INDIVIDUAL TRAINING RECORD IS CURRENT AS OF 2015-05-04 _____________________________ TRAINEE SIGNATURE _____________________________ SUPERVISOR SIGNATURE RC-135V, T/N 64-14848, 30 April 2015 T-52 1. IDENTIFICATION DATA LAST NAME - FIRST NAME - MIDDLE INITIAL [Crew Chief 1] GRADE/RANK Senior Airman DAFSC/JOB SERIES 2A554A INDIVIDUAL TRAINING RECORD INDIVIDUAL'S SIGNATURE DATE 2015-05-04 Individual Training Record RC-135V, T/N 64-14848, 30 April 2015 T-53 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 001 Career Ladder Progression-1 Aug 12 TR: Air Force Enlisted Classification Directory (AFECD) 2A5X1 AND 2A5X4-000 001.001 Progression in career ladder 2A5X1 AND 2A5X4-000 001.002 Duties of AFSC 2A5X1 AND 2A5X4-000 003 AF OCCUPATIONAL SAFETY AND HEALTH (AFOSH) PROGRAM TR: AFIs 11-218, 21-101 and 91-301; applicable AFOSH STDs; TOs 00-25-172, 1-1-691, and applicable aircraft TOs 2A5X1 AND 2A5X4-000 003.001 Housekeeping consistent with safety of personnel and equipment 2A5X1 AND 2A5X4-000 003.002 Safety precautions pertaining to aircraft maintenance 2A5X1 AND 2A5X4-000 003.002.001 Engine air intake and exhaust 2A5X1 AND 2A5X4-000 003.002.002 High intensity sound 2A5X1 AND 2A5X4-000 003.002.003 Turbine, propeller, rotor plane of rotation 2A5X1 AND 2A5X4-000 003.002.004 Radio frequency radiation 2A5X1 AND 2A5X4-000 003.002.005 Ground handling of aircraft 2A5X1 AND 2A5X4-000 003.002.006 Hot brakes 2A5X1 AND 2A5X4-000 003.002.007 Use of tools and equipment 2A5X1 AND 2A5X4-000 003.002.008 Servicing aircraft systems 2A5X1 AND 2A5X4-000 003.002.009 Cleaning Agents 2A5X1 AND 2A5X4-000 003.002.010 Solvents 2A5X1 AND 2A5X4-000 003.002.011 Lubricants 2A5X1 AND 2A5X4-000 003.002.012 High pressure gasses 2A5X1 AND 2A5X4-000 003.002.013 Aircraft explosive equipment 2A5X1 AND 2A5X4-000 003.002.014 Composite materials 2A5X1 AND 2A5X4-000 003.002.015 Maintenance resource management TR: AFI 21-101; AFPAM 90-902 2A5X1 AND 2A5X4-000 003.002.016 Electrostatic hazards, static grounding and bonding TR: TOs 00-25-172 and 00-25-234 2A5X1 AND 2A5X4-000 003.003 Portable ground fire extinguishers TR: AFI 32-2001; TO 00-25-172 2A5X1 AND 2A5X4-000 003.003.001 Perform pre-use inspection 2A5X1 AND 2A5X4-000 003.003.002 Position 2A5X1 AND 2A5X4-000 003.003.003 Operate 2A5X1 AND 2A5X4-000 003.004 Foreign Object Damage (FOD) prevention program 2A5X1 AND 2A5X4-000 003.005 Dropped Object prevention program 2A5X1 AND 2A5X4-000 003.006 Hazardous chemicals TR: AFI 90-821 and applicable AFOSH STDs 2A5X1 AND 2A5X4-000 003.006.001 Use 2A5X1 AND 2A5X4-000 003.006.002 Disposal 2A5X1 AND 2A5X4-000 003.006.003 Hazard communication training program 2A5X1 AND 2A5X4-000 003.006.004 Hazardous material handling procedures 2A5X1 AND 2A5X4-000 003.007 AF Form 1492, Warning Tag TR: TO 00-20-1 2A5X1 AND 2A5X4-000 004 MAINTENANCE DIRECTIVES, REFERENCES, and INSTRUCTIONS TR: AFI 33-360 and TO 00-5 series as applicable 2A5X1 AND 2A5X4-000 004.001 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2012-04-25 2012-04-27 - A - - - - - 2012-04-25 2012-04-27 - A - - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2013-04-01 2013-04-29 - A - - - - - 2013-03-25 2013-04-09 - A - - - - - 2012-02-20 2012-02-24 - 2b - - - - - 2012-04-25 2012-04-27 - 1b - - - - - 2012-04-25 2012-04-27 - - - - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - - - - - - - 2013-03-25 2013-04-09 - - - - - - - 2012-04-25 2012-04-27 - A - - - - - 2012-04-25 2012-04-27 - A B - - - - RC-135V, T/N 64-14848, 30 April 2015 T-54 1. Tasks Knowledge And Technical References TO system 2A5X1 AND 2A5X4-000 004.002 Air Force manuals and instructions 2A5X1 AND 2A5X4-000 004.003 Use technical orders 2A5X1 AND 2A5X4-000 004.004 TO improvement reporting 2A5X1 AND 2A5X4-000 006 TRAINING TR: AFIs 36-2201 and 36-2232 2A5X1 AND 2A5X4-000 006.005 Document training records 2A5X1 AND 2A5X4-000 006.006 Purpose and use of Career Field Education and Training Plan (CFETP) 2A5X1 AND 2A5X4-000 007 MAINTENANCE MANAGEMENT TR: AFIs 21-101, 21-103, 21-118, 90-201 and AFMAN 23-110 2A5X1 AND 2A5X4-000 007.001 Basic functions within maintenance 2A5X1 AND 2A5X4-000 007.002 Resource management 2A5X1 AND 2A5X4-000 007.004 Maintenance incident investigation and prevention 2A5X1 AND 2A5X4-000 007.005 Determine and report Aircraft Status 2A5X1 AND 2A5X4-000 008 MAINTENANCE DATA DOCUMENTATION (MDD) TR: AFI 21-101; TO 00-20 Series; applicable aircraft -06 Work Unit Code Manuals 2A5X1 AND 2A5X4-000 008.001 MDD Fundamentals 2A5X1 AND 2A5X4-000 008.002 Aircraft and supporting maintenance records 2A5X1 AND 2A5X4-000 008.002.001 Purpose 2A5X1 AND 2A5X4-000 008.002.002 Automated Forms 2A5X1 AND 2A5X4-000 008.002.007 Document other AFTO 781 series forms 2A5X1 AND 2A5X4-000 008.002.008 Document AFTO Form 244/245 2A5X1 AND 2A5X4-000 008.002.009 Document AFTO Form 350 2A5X1 AND 2A5X4-000 008.003 Maintenance Information Systems (MIS) 2A5X1 AND 2A5X4-000 008.003.001 Purpose 2A5X1 AND 2A5X4-000 008.003.002 Job data documentation (JDD) 2A5X1 AND 2A5X4-000 008.003.002.001 Purpose 2A5X1 AND 2A5X4-000 008.003.002.002 Access JDD 2A5X1 AND 2A5X4-000 008.003.002.003 Create maintenance event 2A5X1 AND 2A5X4-000 008.003.002.004 Defer maintenance event 2A5X1 AND 2A5X4-000 008.003.002.005 Schedule maintenance event 2A5X1 AND 2A5X4-000 008.003.002.006 Close maintenance event 2A5X1 AND 2A5X4-000 008.003.002.007 Use IMDS 2A5X1 AND 2A5X4-000 009 MAINTENANCE MATERIALS/ TOOLS TR:AFI 21-101, TOs 1-1A-8, 1-1A-14, 1-1-691 and 32- series TOs as applicable 2A5X1 AND 2A5X4-000 009.001 Tool control 2A5X1 AND 2A5X4-000 009.002 Select and use special tools 2A5X1 AND 2A5X4-000 009.003 Select/use restraint harness (e.g.; fall protection/prevention equipment) 2A5X1 AND 2A5X4-000 009.005 Hardware 2A5X1 AND 2A5X4-000 009.005.001 Purpose 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - 1b - - - - - 2012-04-25 2012-05-18 - - B - - - - 2012-07-05 2012-07-05 - - A - - - - 2013-04-01 2013-04-29 - - A - - - - 2012-05-10 2012-05-18 - A B - - - - 2012-07-05 2012-07-05 - - B - - - - 2012-07-05 2012-07-05 - - - - - - - 2012-05-10 2012-05-18 - - - - - - - 2012-04-25 2012-05-18 - A B - - - - 2012-04-25 2012-05-18 - A B - - - - 2012-04-25 2012-05-18 - A - - - - - 2012-04-25 2012-04-27 - - - - - - - 2012-04-25 2012-04-27 - 1b - - - - - 2012-05-11 2012-05-30 - 1b - - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - - - - - - - 2012-04-25 2012-04-27 - - - - - - - 2012-04-25 2012-04-27 - - - - - - - 2012-05-10 2012-05-18 - - - - - - - 2012-04-25 2012-05-18 - - - - - - - 2012-04-25 2012-04-27 - - - - - - - 2012-04-25 2012-04-27 - - - - - - - 2012-04-02 2012-04-02 - A B - - - - 2012-05-10 2012-05-14 - - - - - - - 2012-05-11 2012-05-30 - - - - - - - 2012-04-02 2012-04-02 - A B - - - - RC-135V, T/N 64-14848, 30 April 2015 T-55 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 009.005.002 Remove/inspect/install 2A5X1 AND 2A5X4-000 009.006 Electrical connectors 2A5X1 AND 2A5X4-000 009.006.001 Purpose 2A5X1 AND 2A5X4-000 009.006.002 Connect/disconnect 2A5X1 AND 2A5X4-000 009.007 Securing devices 2A5X1 AND 2A5X4-000 009.007.001 Purpose 2A5X1 AND 2A5X4-000 009.007.002 Install/remove safety wire 2A5X1 AND 2A5X4-000 009.007.003 Install/remove cotter pins 2A5X1 AND 2A5X4-000 009.007.004 Safety cable 2A5X1 AND 2A5X4-000 009.008 Lubricants 2A5X1 AND 2A5X4-000 009.009 Sealants 2A5X1 AND 2A5X4-000 009.010 Adhesives 2A5X1 AND 2A5X4-000 009.011 Cleaning agents 2A5X1 AND 2A5X4-000 009.012 Hand tools 2A5X1 AND 2A5X4-000 009.012.001 Purpose 2A5X1 AND 2A5X4-000 009.012.002 Select, inspect and use 2A5X1 AND 2A5X4-000 009.013 Measuring tools 2A5X1 AND 2A5X4-000 009.013.001 Purpose 2A5X1 AND 2A5X4-000 009.013.002 Select and use ruler 2A5X1 AND 2A5X4-000 009.013.003 Select and use thickness gauge 2A5X1 AND 2A5X4-000 009.013.004 Use multi-meter 2A5X1 AND 2A5X4-000 009.013.005 Select, inspect and use torque wrench 2A5X1 AND 2A5X4-000 009.013.006 Select and use micrometer 2A5X1 AND 2A5X4-000 009.013.007 Use depth gauge 2A5X1 AND 2A5X4-000 010 RESPONSIBILITY FOR SUPPLY TR: AFIs 21-101 and 21-118, AFMAN 23-110, TOs 00-20-3 and 00-35D-54 2A5X1 AND 2A5X4-000 010.001 Maintenance supply concept 2A5X1 AND 2A5X4-000 010.004 Ordering parts 2A5X1 AND 2A5X4-000 010.006 Prepare repairable and serviceable parts for turn-in 2A5X1 AND 2A5X4-000 010.008 DIFM Control 2A5X1 AND 2A5X4-000 010.013 DD Forms 1574, 1575, 1576, 1577 and 1577-2 2A5X1 AND 2A5X4-000 011 AIRCRAFT GENERAL TR: AFI 11-218; applicable AFOSH STDs; TOs 00-20-1, 00-25-172, 1-1-691, 1-1B-50 and applicable aircraft TOs 2A5X1 AND 2A5X4-000 011.001 Weight and balance 2A5X1 AND 2A5X4-000 011.002 Determine weight and balance requirements 2A5X1 AND 2A5X4-000 011.003 Inventory aircraft equipment 2A5X1 AND 2A5X4-000 011.004 Safe aircraft for maintenance 2A5X1 AND 2A5X4-000 011.005 Corrosion control program 2A5X1 AND 2A5X4-000 011.005.001 Aircraft cleaning 2A5X1 AND 2A5X4-000 011.005.002 Corrosion identification 2A5X1 AND 2A5X4-000 011.005.004 Aircraft lubrication 2A5X1 AND 2A5X4-000 011.006 Aircraft inspections 2A5X1 AND 2A5X4-000 011.006.001 Cncepts and Types 2A5X1 AND 2A5X4-000 011.008 Aircraft marshalling signals 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2012-04-02 2012-04-02 B Trainer Initials Tng Start 5 E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - 2b - - - - - 2012-04-02 2012-04-02 - A B - - - - 2012-04-02 2012-04-02 - 2b - - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - 2b - - - - - 2012-04-25 2012-04-27 - 2b - - - - - 2013-03-25 2013-04-29 - A - - - - - 2012-04-25 2012-04-27 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2012-04-02 2012-04-02 - A - - - - - 2012-04-02 2012-04-02 - 2b - - - - - 2012-02-20 2012-03-01 - A B - - - - 2012-02-20 2012-03-01 - 2b - - - - - 2012-04-02 2012-04-02 - 2b - - - - - 2013-03-25 2013-04-09 - 2b - - - - - 2012-04-02 2012-04-02 - 2b - - - - - 2013-03-25 2013-04-29 - - - - - - - 2013-03-25 2013-04-29 - 2b - - - - - 2012-04-25 2012-05-18 - A B - - - - 2012-07-05 2012-07-05 - A B - - - - 2012-07-05 2012-07-05 - - B - - - - 2012-07-05 2012-07-05 - - B - - - - 2013-03-25 2013-04-09 - - B - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - - - - - - - 2013-03-25 2013-04-09 - - A - - - - 2012-02-20 2012-03-01 - A - - - - - 2012-08-21 2012-08-27 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-56 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 011.011 Deice aircraft TR: TO 42C-1-2S-2; 14CFR121.629 section 121.629 2A5X1 AND 2A5X4-000 011.013 Aircraft guarded switches 2A5X1 AND 2A5X4-000 011.013.001 Design/function/proper identification 2A5X1 AND 2A5X4-000 011.013.002 Remove and replace covers 2A5X1 AND 2A5X4-000 011.013.003 Operational check 2A5X1 AND 2A5X4-000 012 AIRFRAME TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 012.002 Remove/inspect/install panels 2A5X1 AND 2A5X4-000 012.003 Inspect structural components 2A5X1 AND 2A5X4-000 013 LANDING GEAR TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 013.001 System fundamentals 2A5X1 AND 2A5X4-000 014 UTILITIES TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 014.001 System fundamentals 2A5X1 AND 2A5X4-000 014.001.001 Oxygen 2A5X1 AND 2A5X4-000 014.001.002 Bleed air 2A5X1 AND 2A5X4-000 014.001.003 Pressurization 2A5X1 AND 2A5X4-000 014.001.004 Air conditioning 2A5X1 AND 2A5X4-000 014.001.005 Fire/Overheat warning 2A5X1 AND 2A5X4-000 014.001.006 Fire suppression 2A5X1 AND 2A5X4-000 015 FLIGHT CONTROLS TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 015.001 Fundamentals of flight 2A5X1 AND 2A5X4-000 015.002 Primary flight control fundamentals 2A5X1 AND 2A5X4-000 015.003 Secondary flight control fundamentals 2A5X1 AND 2A5X4-000 015.004 Component identification 2A5X1 AND 2A5X4-000 016 HYDRAULICS TR: TO 1-1A-8 and applicable aircraft TOs 2A5X1 AND 2A5X4-000 016.001 System fundamentals 2A5X1 AND 2A5X4-000 016.002 Remove/install components TR: TO 1-1A-8, Applicable aircraft TOs 2A5X1 AND 2A5X4-000 016.002.001 Tubing/hoses 2A5X1 AND 2A5X4-000 016.002.002 Fittings 2A5X1 AND 2A5X4-000 017 ENGINES TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 017.001 System fundamentals 2A5X1 AND 2A5X4-000 017.004 Joint Oil Analysis Program 2A5X1 AND 2A5X4-000 018 FUELS TR: TOs 00-25-172, 1-1-3, applicable AFOSH STDs and aircraft TOs 2A5X1 AND 2A5X4-000 018.001 System fundamentals 2A5X1 AND 2A5X4-000 018.002 Classify fuel leaks 2A5X1 AND 2A5X4-000 019 ELECTRICAL TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 019.001 AC Electrical system fundamentals 2A5X1 AND 2A5X4-000 019.002 DC electrical system fundamentals 2A5X1 AND 2A5X4-000 019.007 Electrical schematics/diagrams 2A5X1 AND 2A5X4-000 020 AEROSPACE GROUND EQUIPMENT TR: Applicable AFOSH STDs and TO 35A4 series as applicable 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2012-08-27 2012-09-12 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - - - - - - - 2012-04-02 2012-04-02 - A - - - - - 2012-04-25 2012-04-27 - - - - - - - 2012-04-25 2012-04-27 - - - - - - - 2013-03-25 2013-04-09 - 1b - - - - - 2013-03-25 2013-04-09 - - - - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - A - - - - - 2013-03-25 2013-04-09 - A - - - - - 2012-02-20 2012-03-01 - A - - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - - - - - - - 2012-04-25 2012-04-27 - - - - - - - 2013-04-01 2013-04-29 - A B - - - - 2012-09-03 2012-09-24 - - B - - - - 2013-03-25 2013-04-09 - A B - - - - 2012-04-25 2012-04-27 - A - - - - - 2012-05-10 2012-05-18 - A B - - - - 2012-05-10 2012-05-18 - A B - - - - 2012-08-27 2012-09-18 - A - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-57 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 020.001 Maintenance stands 2A5X1 AND 2A5X4-000 020.001.001 Purpose and description 2A5X1 AND 2A5X4-000 020.001.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.002 Self-propelled universal platforms 2A5X1 AND 2A5X4-000 020.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.002.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.003 Aircraft jacks TR: TO 35A2- series as applicable 2A5X1 AND 2A5X4-000 020.003.001 Purpose and description 2A5X1 AND 2A5X4-000 020.003.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.005 Oxygen servicing equipment TR: TO 15X-1-1, 37C2-8- as applicable 2A5X1 AND 2A5X4-000 020.005.001 Liquid oxygen (LOX) 2A5X1 AND 2A5X4-000 020.005.001.001 Purpose and description 2A5X1 AND 2A5X4-000 020.005.001.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.005.002 Gaseous oxygen (GOX) 2A5X1 AND 2A5X4-000 020.005.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.005.002.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.006 Diesel driven air compressors TR: TO 34Y1- series as applicable 2A5X1 AND 2A5X4-000 020.006.001 Purpose and description 2A5X1 AND 2A5X4-000 020.006.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.007 Ground heaters TR: 35E7- series as applicable 2A5X1 AND 2A5X4-000 020.007.001 Purpose and description 2A5X1 AND 2A5X4-000 020.007.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.008 Lighting equipment TR: TO 35F5- series as applicable 2A5X1 AND 2A5X4-000 020.008.001 Purpose and description 2A5X1 AND 2A5X4-000 020.008.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.010 Air conditioning units TR: TO 35E9- Series as applicable 2A5X1 AND 2A5X4-000 020.010.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011 Ground generator sets/gas turbine compressors 2A5X1 AND 2A5X4-000 020.011.002 A/M32A-95 Gas turbine compressors TR: TO 35D12-series as applicable 2A5X1 AND 2A5X4-000 020.011.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011.003 Diesel driven generator sets TR: TO 35C2- series as applicable 2A5X1 AND 2A5X4-000 020.011.003.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011.003.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.012 Tow bar TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 020.012.001 Perform pre-use inspection 2A5X1 AND 2A5X4-000 020.012.002 Connect/disconnect 2A5X1 AND 2A5X4-000 020.013 Tow vehicles TR: TO 36A10 series as applicable 2A5X1 AND 2A5X4-000 020.013.001 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2012-04-02 2012-04-02 - A B - - - - 2012-04-02 2012-04-02 - 2b - - - - - 2013-03-25 2013-04-09 - A B - - - - 2013-03-25 2013-04-09 - - - - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - 2b - - - - - 2012-05-10 2012-05-14 - A B - - - - 2012-05-23 2012-05-23 - - - - - - - 2012-07-20 2012-08-22 - A B - - - - 2012-07-20 2012-08-16 - - - - - - - 2012-07-20 2012-08-22 - A B - - - - 2012-07-20 2012-08-27 - - - - - - - 2012-07-05 2012-07-05 - A B - - - - 2012-07-05 2012-07-05 - - - - - - - 2012-07-05 2012-07-05 - A B - - - - 2012-07-05 2012-07-05 - - - - - - - 2012-07-05 2012-07-05 - A B - - - - 2012-04-02 2012-04-02 - A B - - - - 2012-04-25 2012-04-27 - A B - - - - 2012-04-25 2012-04-27 - 2b - - - - - 2012-02-20 2012-03-01 - - - - - - - 2012-04-02 2012-04-02 - - - - - - - 2013-03-25 2013-04-29 - - B - - - - RC-135V, T/N 64-14848, 30 April 2015 T-58 1. Tasks Knowledge And Technical References Purpose and description 2A5X1 AND 2A5X4-000 020.013.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.014 Self-generating nitrogen equipment TR: TO 35D29-7-6-1 2A5X1 AND 2A5X4-000 020.014.001 Purpose and description 2A5X1 AND 2A5X4-000 020.014.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.015 Gaseous nitrogen servicing equipment TR: TO 35D3- series as applicable 2A5X1 AND 2A5X4-000 020.015.001 Purpose and description 2A5X1 AND 2A5X4-000 020.016 Engine stands and dollies TR: 35D3- series as applicable 2A5X1 AND 2A5X4-000 020.016.001 Purpose and description 2A5X1 AND 2A5X4-000 020.016.002 Perform pre-use inspection and operate 2A5X4-006 001 C-135 QUALITATIVE REQUIREMENTS AIRCRAFT GENERAL 2A5X4-006 001.001 Periodic/Isochronal inspection concept and inspection TR: TOs 00-20 series, Applicable -6 TOs 2A5X4-006 001.001.001 Periodic/Isochronal inspection concept 2A5X4-006 001.001.002 Perform inspections 2A5X4-006 001.001.002.001 Preflight 2A5X4-006 001.001.002.002 Alert 5A 2A5X4-006 001.001.002.003 Alert 5B 2A5X4-006 001.001.002.004 Thruflight 2A5X4-006 001.001.002.005 Quick Turn 2A5X4-006 001.001.002.006 Hourly Post 2A5X4-006 001.001.002.009 Calendar 2A5X4-006 001.001.002.010 Special 2A5X4-006 001.001.002.011 900 Hr Insp 2A5X4-006 001.001.002.012 Time change item 2A5X4-006 001.002 Aircraft communications equipment TR: Applicable -2 TOs 2A5X4-006 001.002.001 Operate radio 2A5X4-006 001.002.002 Use interphone 2A5X4-006 001.003 Perform ground handling TR: AFI 11-218, TO 00-25-172, applicable AFOSH STDs, applicable -1 and -2 TOs 2A5X4-006 001.003.001 Aircraft launch 2A5X4-006 001.003.002 Call flight controls 2A5X4-006 001.003.003 Aircraft recovery 2A5X4-006 001.003.004 Tow aircraft 2A5X4-006 001.003.004.001 Wing/tail walker 2A5X4-006 001.003.004.002 Brake operator 2A5X4-006 001.003.004.004 Tow vehicle operator 2A5X4-006 001.003.005 Jack and level aircraft 2A5X4-006 001.003.005.001 Jacking team member 2A5X4-006 001.003.005.005 Axle jacking 2A5X4-006 001.004 Compute center of gravity TR: Applicable aircraft -5 TOs 2A5X4-006 001.005 Install/remove ground safety devices TR: Applicable -2 TOs 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse 2012-04-25 2012-04-27 C 7-Skill Level QTP (1) Crse (2) CDC - - - - - A B - - - - - 2b - - - - - 2012-05-10 2012-05-14 - A B - - - - 2012-05-10 2012-05-14 - - A - - - - 2012-05-10 2012-05-14 - - - - - - - 2012-05-10 2012-05-14 - A - - - - - 2012-09-03 2012-09-24 - 2b - - - - - 2013-04-01 2013-04-29 - - - - - - - 2013-04-01 2013-04-29 - - - - - - - 2012-09-03 2012-09-24 - 2b - - - - - 2012-09-03 2012-09-24 - - - - - - - 2012-12-11 2012-12-18 - 2b - - - - - 2012-09-24 2012-09-25 - - - - - - - 2012-09-24 2012-09-25 - - - - - - - 2012-12-26 2013-01-02 - - - - - - - 2013-04-01 2013-04-29 - - - - - - - 5 2012-08-27 2012-09-18 - - - - - - - 5 2012-05-10 2012-05-14 - 2b - - - - - 5 2012-05-10 2012-05-14 - b - - - - - 5 2012-05-14 2012-05-18 - 2b - - - - - 5 2012-05-10 2012-05-14 - b - - - - - 5 2012-02-20 2012-03-01 - b - - - - - 5 2012-08-21 2012-08-22 - b - - - - - 2012-09-12 2012-09-12 - - - - - - - 7 2012-04-25 2012-04-27 (2) CDC - 5 - B 5-Skill Level (1) Crse - 5 2013-03-25 2013-04-29 (2) CDC 2012-05-10 2012-05-14 - - - - - - - 5 2012-05-10 2012-05-14 - 2b - - - - - 5 2012-05-10 2012-05-14 - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-59 1. Tasks Knowledge And Technical References 2A5X4-006 001.005.001 Landing gear 2A5X4-006 001.005.002 Landing gear doors 2A5X4-006 001.006 Ground aircraft 2A5X4-006 001.007 Configure/reconfigure aircraft 2A5X4-006 001.007.002 Passenger/personnel 2A5X4-006 001.008 Maintain/store/configure/-21 equipment 2A5X4-006 001.010 Aircraft wash TR: TO - 6WC-3 2A5X4-006 001.010.001 Team member 2A5X4-006 001.010.003 Post wash lube 2A5X4-006 001.011 Maintenance directives, references, & instructions TR: AFI 37-101 Vol 1 and TO 00-5-1 2A5X4-006 001.011.001 Use C-135 technical orders 2A5X4-006 001.012 Maintenance Data Documentation (MDD TR: AFI 21-101, TOs 00-20-1, 00-20-2, and applicable aircraft -06 Work Unit Code Manuals 2A5X4-006 001.012.001 Document AFTO Form 781H 2A5X4-006 001.012.002 Document AFTO Form 781A 2A5X4-006 001.012.003 Document AFTO Form 781J 2A5X4-006 001.012.004 Document AFTO Form 781K 2A5X4-006 002 AIRFRAME SYSTEMS TR: Applicable -2 TOs 2A5X4-006 002.001 Airframe components and structure 2A5X4-006 002.002 Service cargo door reservoir 2A5X4-006 002.003 Operate 2A5X4-006 002.003.001 Crew entry door 2A5X4-006 002.003.002 Cargo door 2A5X4-006 002.003.003 Emergency exit hatch 2A5X4-006 002.003.004 Wheel well doors 2A5X4-006 002.004 Open and close 2A5X4-006 002.004.001 Cowling (F-108) 2A5X4-006 002.004.002 Cowling (TF-33) 2A5X4-006 002.004.003 Panels/doors 2A5X4-006 002.004.004 Windows 2A5X4-006 002.005 Remove and install 2A5X4-006 002.005.002 Cowling (TF-33) 2A5X4-006 002.005.003 Panels/doors 2A5X4-006 002.005.004 Non-explosive seats 2A5X4-006 002.005.008 Door/hatch seals 2A5X4-006 002.005.009 Thermal curtains 2A5X4-006 002.006 Perform aircraft inclement weather procedures 2A5X4-006 002.007 Inspect crew/passenger comfort facilities TR: Applicable -6 TOs 2A5X4-006 002.008 Service crew/passenger comfort facilities 2A5X4-006 003 LANDING GEAR SYSTEMS TR: Applicable -2 TOs 2A5X4-006 003.001 Landing gear components and system 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Trainer Initials 5 Tng Trainee Complete Initialst 2012-04-02 2012-04-02 B - 2b - - - - - 5 2012-04-02 2012-04-02 - 2b - - - - - 5 2012-04-02 2012-04-02 - 2b - - - - - 2013-03-25 2013-04-09 - - - - - - - 2012-04-02 2012-04-02 - - - - - - - 2012-12-05 2012-12-11 - - - - - - - 2012-08-15 2012-08-15 - - - - - - - 5 2013-02-07 2013-04-09 - 3c - - - - - 5 2013-02-07 2013-04-09 - 3c - - - - - 5 2013-02-07 2013-04-09 - 3c - - - - - 5 2013-02-07 2013-04-09 - 3c - - - - - 5 2013-02-07 2013-04-09 - 3c - - - - - 2012-07-05 2012-07-05 - A - - - - - 2013-03-25 2013-04-09 - b - - - - - 5 2012-02-20 2012-03-01 - 2b - - - - - 5 2012-02-20 2012-03-01 - 2b - - - - - 5 2012-02-20 2012-03-01 - 2b - - - - - 5 2012-02-20 2012-03-01 - 2b - - - - - 2012-05-10 2012-05-14 - 2b/b - - - - - 2012-09-18 2012-09-24 - - - - - - - 2012-05-10 2012-05-14 - - - - - - - 2012-04-02 2012-04-02 - - - - - - - 2012-09-18 2012-09-24 - - - - - - - 2012-05-10 2012-05-14 - - - - - - - 2012-08-27 2012-09-18 - - - - - - - 2012-09-03 2012-09-24 - - - - - - - 2012-05-10 2012-05-14 - - - - - - - 2012-07-05 2012-07-05 - - - - - - - 2012-04-02 2012-04-02 - - - - - - - 2012-04-02 2012-04-02 - - - - - - - 2012-08-27 2012-09-18 - A - - - - - Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC RC-135V, T/N 64-14848, 30 April 2015 T-60 B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 1. Tasks Knowledge And Technical References operation 2A5X4-006 003.003 Operate 2A5X4-006 003.003.002 Brakes 2A5X4-006 003.003.004 Anti skid system 2A5X4-006 003.004 Service 2A5X4-006 003.004.001 Snubber 2A5X4-006 003.004.002 Centering cylinder 2A5X4-006 003.004.003 Landing gear struts 2A5X4-006 003.004.003.001 Deflate 2A5X4-006 003.004.003.002 Drain 2A5X4-006 003.004.003.003 Fill 2A5X4-006 003.004.003.004 Inflate 2A5X4-006 003.004.004 Tires 2A5X4-006 003.005 Lubricate landing gear components 2A5X4-006 003.006 Remove and Install 2A5X4-006 003.006.001 Snubbers 2A5X4-006 003.006.002 Centering cylinder 2A5X4-006 003.006.003 Wheel and tire assemblies 2A5X4-006 003.006.003.001 Nose 2A5X4-006 003.006.003.002 Main 2A5X4-006 003.006.004 Anti-skid transducer 2A5X4-006 003.006.005 Carbon brake assemblies 2A5X4-006 003.006.006 Bleed brake assembly (carbon) 2A5X4-006 003.007 Determine serviceability of aircraft tires TR: TO 4T-1-3 2A5X4-006 004 UTILITY SYSTEMS TR: TO 00-25-172, Applicable -2 TOs 2A5X4-006 004.001 Utility components and system operation 2A5X4-006 004.003 Operate 2A5X4-006 004.003.005 Fire/overheat warning system 2A5X4-006 004.003.007 Oxygen system 2A5X4-006 004.004 Oxygen system TR: Applicable -2, -3 TOs 2A5X4-006 004.004.001 Service gaseous oxygen 2A5X4-006 004.004.002 Service liquid oxygen 2A5X4-006 004.005 Inspect TR: Applicable -6 TOs 2A5X4-006 004.005.001 Bleed air system 2A5X4-006 004.005.002 Air conditioning system 2A5X4-006 004.005.003 Pressurization system 2A5X4-006 004.005.004 Anti-ice system 2A5X4-006 004.005.005 Fire/overheat warning system 2A5X4-006 004.005.006 Fire extinguisher system 2A5X4-006 004.005.007 Oxygen system 2A5X4-006 004.006 Air Cycle Machine (ACM) 2A5X4-006 004.006.001 Drain 2A5X4-006 004.006.002 Service 2A5X4-006 005 FLIGHT CONTROL SYSTEM 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2012-02-20 2012-03-01 - 2b - - - - - 2013-03-25 2013-04-09 - - - - - - - 5 2012-05-21 2012-05-21 - 2b - - - - - 5 2012-07-24 2012-07-31 - 2b - - - - - 5 2012-09-17 2012-09-17 - 2b - - - - - 2012-11-01 2012-12-03 - - - - - - - 5 2012-11-01 2012-12-03 - 2b - - - - - 5 2012-07-05 2012-07-05 - 2b - - - - - 5 2012-07-05 2012-07-05 - 2b - - - - - 2013-03-25 2013-04-09 - - - - - - - 2012-09-24 2012-09-25 - - - - - - - 2012-09-24 2012-09-25 - - - - - - - 5 2012-05-11 2012-05-30 - 2b - - - - - 5 2012-05-11 2012-05-30 - 2b - - - - - 5 2012-09-17 2012-09-17 - 2b - - - - - 5 2012-08-21 2012-09-17 - 2b - - - - - 5 2012-12-26 2013-01-02 - 2b - - - - - 5 2012-07-20 2012-08-27 - 2b - - - - - 2012-08-27 2012-09-18 - A - - - - - 2013-04-01 2013-04-29 - - - - - - - 2012-05-10 2012-05-14 - - - - - - - 2012-09-24 2012-09-25 - 2b - - - - - 2012-05-21 2012-05-23 - - - - - - - 2013-04-01 2013-04-29 - - - - - - - 2013-04-01 2013-04-29 - - - - - - - 2013-04-01 2013-04-29 - - - - - - - 2013-04-01 2013-04-29 - - - - - - - 2013-04-01 2013-04-29 - - - - - - - 2013-04-01 2013-04-29 - - - - - - - 2013-04-01 2013-04-29 - - - - - - - 5 2012-09-03 2012-09-24 - b - - - - - 5 2012-09-03 2012-09-24 - b - - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T-61 1. Tasks Knowledge And Technical References TR: Applicable -2 TOs 2A5X4-006 005.001 Flight control components and system operation 2A5X4-006 005.003 Operate flight controls 2A5X4-006 005.003.001 Aileron system 2A5X4-006 005.003.002 Rudder system 2A5X4-006 005.003.003 Elevator system 2A5X4-006 005.003.004 Spoiler/Speed brake system 2A5X4-006 005.003.005 Stabilizer trim system 2A5X4-006 005.003.006 Flap system 2A5X4-006 005.005 Lubricate flight controls 2A5X4-006 005.006 Service gearbox 2A5X4-006 006 HYDRAULIC SYSTEMS TR: Applicable -2 TOs 2A5X4-006 006.001 Hydraulic components and system operation 2A5X4-006 006.003 Service hydraulic system 2A5X4-006 006.003.001 Reservoir 2A5X4-006 006.003.002 Accumulator 2A5X4-006 006.004 Operate 2A5X4-006 006.004.002 Non-engine driven pump 2A5X4-006 007 ENGINES TR: AFI 11-218, applicable AFOSH STDs and -2 TOs 2A5X4-006 007.001 Engine and Auxiliary Power Unit (APU) components and system operation 2A5X4-006 007.003 Perform 2A5X4-006 007.003.006 Audible ignition check 2A5X4-006 007.005 Service 2A5X4-006 007.005.001 Oil system 2A5X4-006 007.005.002 Constant Speed Drive (CSD)/Integrated Drive Generator (IDG) 2A5X4-006 007.005.003 Gear box 2A5X4-006 007.005.004 Auxiliary Power Unit (if equipped) 2A5X4-006 007.007 Take engine oil sample TR: TO 42B2-1-9, 33-1-37 2A5X4-006 007.008 Chip detectors 2A5X4-006 007.009 Inspect installed engine TR: Applicable -6 TOs 2A5X4-006 007.009.001 Turbine 2A5X4-006 007.010 Inspect Auxiliary Power Unit TR: Applicable -6 TOs 2A5X4-006 008 AIRCRAFT FUEL SYSTEMS TR: TO 00-25-172, applicable AFOSH STDs and -2 TOs 2A5X4-006 008.001 Fuel components and system operation 2A5X4-006 008.003 Ground transfer fuel 2A5X4-006 008.003.001 Wing tank transfer 2A5X4-006 008.003.002 Body tank transfer 2A5X4-006 008.004 Refuel aircraft 2A5X4-006 008.004.001 Team member 2A5X4-006 008.004.002 Team panel operator 2A5X4-006 008.004.003 Team supervisor 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2012-05-10 2012-05-14 - A - - - - - 2012-05-10 2012-05-14 - 2b - - - - - 2012-05-10 2012-05-14 - 2b - - - - - 2012-05-10 2012-05-14 - 2b - - - - - 2012-05-10 2012-05-14 - 2b - - - - - 2012-05-10 2012-05-14 - 2b - - - - - 2012-05-10 2012-05-14 - 2b - - - - - 2013-03-25 2013-04-29 - - - - - - - 2013-04-01 2013-04-30 - - - - - - - 2012-05-11 2012-05-30 - A - - - - - 5 2012-07-05 2012-07-05 - 2b - - - - - 5 2012-08-27 2012-09-17 - 2b - - - - - 5 2012-05-10 2012-05-14 - 2b - - - - - 2013-04-01 2013-04-30 - A - - - - - 2013-04-01 2013-04-30 - - - - - - - 2012-05-11 2012-05-30 - b - - - - - 2012-09-12 2012-09-12 - - - - - - - 2013-04-01 2013-04-30 - - - - - - - 2012-09-18 2012-09-18 - - - - - - - 2012-09-03 2012-09-24 - - - - - - - 2013-04-01 2013-04-29 - A - - - - - 2012-09-03 2012-09-24 - 1b - - - - - 2012-09-18 2012-09-18 - 2b - - - - - 2012-08-27 2012-09-17 - A - - - - - 5 2012-08-28 2012-09-18 - b - - - - - 5/R 2012-08-28 2012-09-18 - - - - - - - 5 2012-02-20 2012-03-01 - b - - - - - 5 2012-05-11 2012-05-30 - b - - - - - 7 2013-10-07 2013-11-25 - - - - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T-62 1. Tasks Knowledge And Technical References 2A5X4-006 008.005 Defuel aircraft 2A5X4-006 008.005.001 Team member 2A5X4-006 008.005.002 Team panel operator 2A5X4-006 008.005.003 Team supervisor 2A5X4-006 008.006 Prepare aircraft for fuel cell maintenance 2A5X4-006 008.007 In-Flight Refueling (IFR) system 2A5X4-006 008.007.001 IFR receiver system 2A5X4-006 008.007.001.001 Inspect 2A5X4-006 008.007.001.002 Operate 2A5X4-006 009 ELECTRICAL SYSTEMS TR: Applicable -2 TOs 2A5X4-006 009.001 Electrical components and system operation 2A5X4-006 009.002 Switch guards 2A5X4-006 009.003 Perform operational check 2A5X4-006 009.003.002 Lighting system 2A5X4-006 009.003.003 Indicator warning lights 2A5X4-006 009.004 Remove and install 2A5X4-006 009.004.001 Light lenses 2A5X4-006 009.004.002 Light bulbs 2A5X4-006 009.004.003 Batteries 2A5X4-006 009.004.004 Connect/apply and disconnectexternal electrical power 2A5X4-006 010 EGRESS SYSTEM TR: Applicable -2 TOs 2A5X4-006 010.001 Egress components and system operation 2A5X4-006 010.003 Remove/install emergency escape slides (except RC-135) 2A5X4-006 011 AEROSPACE GROUND EQUIPMENT TR: Applicable AFOSH STDs 2A5X4-006 011.001 Perform pre-use inspection and operate 2A5X4-006 011.001.002 Air conditioning units TR: TO 35E9-series as applicable 2A5X4-006 011.001.003 A/M32A-95 Gas turbine compressor TR: TO 35D12-series as applicable 2A5X4-006 011.001.004 Gaseous nitrogen servicing equipment TR: TO 35D3-series as applicable 2A5X4-006 011.001.005 Oil servicing carts TR: TO 35A17-series as applicable 2A5X4-006 011.001.006 Hydraulic servicing carts TR: TO 35A29-series as applicable 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 5 2012-02-20 2012-03-01 - b - - - - - 5/R 2012-11-20 2012-11-29 - b - - - - - 7/R 2013-10-07 2013-11-25 - - - - - - - 2012-09-17 2012-09-17 - - - - - - - 2012-09-03 2012-09-24 - - - - - - - 2012-09-03 2012-09-24 - - - - - - - 2012-08-27 2012-09-18 - A - - - - - 2013-03-25 2013-04-29 - A - - - - - 2012-05-10 2012-05-14 - 2b - - - - - 2013-03-25 2013-04-29 - - - - - - - 5 2012-05-10 2012-05-14 - - - - - - - 5 2012-05-10 2012-05-14 - - - - - - - 5 2012-08-21 2012-08-22 - 2b - - - - - 5 2013-02-07 2013-04-09 - 2b - - - - - 2012-07-05 2012-07-05 - A - - - - - 2012-07-05 2012-07-05 - - - - - - - 2013-03-25 2013-04-09 - - - - - - - 2013-03-25 2013-04-09 - - - - - - - 2013-03-25 2013-04-09 - - - - - - - 2013-03-25 2013-04-09 - - - - - - - 2013-03-25 2013-04-09 - 2b - - - - - 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-63 JOB QUALIFICATION STANDARD CONTINUATION/WJQS CRITICAL TASK NUMBER TASKS 35961 002 35961 002.001 35961 002.001.001 35961 002.001.002 35961 003 TASKS, KNOWLEDGE AND TECHNICAL REFERENCES CERTIFICATION START DATE COMPLETION DATE TRAINEE'S TRAINER'S CERTIFIER'S INITIALS INITIALS INITIALS HYDRAULICS 1C-135-2-2(-6,-7,-8-13) SERVICE Aircraft hydraulic system before TCTO-509 2012-07-05 2012-07-05 Aircraft hydraulic system after TCTO-509 2012-07-05 2012-07-05 2012-05-11 2012-05-30 2012-05-11 2012-05-30 2012-09-18 2012-09-18 2012-01-12 2012-02-08 2012-02-08 2012-02-27 2012-02-27 2012-03-28 2014-01-20 2014-01-26 ENGINES 1C-135(E)C-2-4-1, 1C-135-2-4-1, 1C-135(K)R-2-4JG-2 2J-F108-2-1, 1C-135-2-2 (-4,-10) PERFORM SERVICE 35961 003.008 35961 003.008.004 35961 TF-33 P5/P9 Engine Oil 003.008.004.001 35961 F-108 Engine oil 003.008.004.002 35961 004 GUIDANCE AND CONTROL ETM RC-2-11-2, ETM AN/ASN-121, 1C-135-2-9 (-11-2, -11-5) 35961 004.001 Apply range and slip markings 35961 004.002 Perform Basic MFD operation 35961 004.003 REMOVE AND INSTALL 35961 INS Battery 004.003.001 35961 006 CDC Volume Progression 35961 006.002 5 Level CDC Vol 1 AFI 36-2201 35961 006.003 5 Level CDC Vol 2 AFI 36-2201 35961 006.004 5 Level CDC Vol 3 AFI 36-2201 35961 007 OPLAN 8010 Alert Requirements ACCI 13-520 para 3.11.4 35961 007.001 Perform ADCC Alert Crew requirements: tow team member, refuel team member ACCI 13-501 para 3.11.4 RC-135V, T/N 64-14848, 30 April 2015 T-64 JOURNAL ENTRIES ENTRY SUBJECT DATE 2012-01-11 Conduct Orientation/Initial Evaluation SIGNATURE INFO REMARKS Within 60 days of assignment the Supervisor will conduct a Workcenter Orientation and Initial Evaluation of qualifications IAW AFI 36-2201 V3. 2015-04-02 90 day review I reviewed #s TBA entries today for accuracy and completion. There were no errors noted on this date 2015-04-02 90 day review for I reviewed #s TBA entries today for accuracy and completion. There were no errors noted on this date 2015-04-02 90 day review I reviewed #s TBA entries today for accuracy and completion. There were no errors noted on this date 2014-09-04 new supervisor I have been assisned as noted. I reviewed 2014-09-04 90 day review 2014-09-04 new supervisor 2014-04-22 90 Day Review I have been assisned as noted. I reviewed 2014-04-16 Role Request Requesting that 2014-03-27 temporary supervisor new supervisor. I was TDY from Mar-July. TBA was reviewed as of today. Zero defects s TBA entries today for accuracy and completion. There were no errors noted on this date new supervisor. I was TDY from Mar-July. TBA was reviewed as of today. Zero defects #s TBA entries today for accuracy and completion. There were no errors noted on this date has the Trainer Role added to his TBA. will be temporary supervisor until furture notice 2014-03-27 90 day review I reviewed #s TBA entries today for accuracy and completion. There were no errors noted on this date 2014-01-07 90 day review I reviewed #s TBA entries today for accuracy and completion. There were no errors noted on this date. 2013-09-16 90 day review I reviewed #s TBA entries today for accuracy and completion. There were no errors noted on this date. 2013-08-14 workcenter orientation 2013-06-10 90 day review A workcenter orientation was previously completed but was documented incorrectly. I conducted a workcenter orientation with on 20120112. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. I reviewed #s TBA entries today for accuracy and completion. There were no errors noted on this date. 2013-04-10 upgrade training 41 tasks started on 25 march and completed on 9 apr 2013-02-28 90 Day Review I have reviewed 2013-01-28 Recommendation for upgrade to 5 level Member has met all mandatory training requirements IAW AFI 36-2201 for award of his/her next higher skill level. MILPDS, IMDS, and TBA has been updated. 2013-01-23 Recommendation for upgrade to 5 level I am recommending to be upgraded to the skill level of journeyman. has met all mandatory training requirements IAW AFI 36-2201 for award of his 5 skill level. He understands the additional responsibilities that are required of the this new skill level, and I feel he is ready to handle the added responsibilities. I have reviewed their ITP and all tasks have been documented and completed. has completed all task and 100 percent qualified 2013-01-14 task completion 2012-12-18 30 day review 2012-11-28 30 day 2012-10-02 30 day entry TBA records for completeness and accuracy. No Defects 100% complete. is currently 8 months in upgrade training Task Qualified 257-263 = Task completion 98% CDC Status- Vol 3 of 3 completed 03/28. Training Status- Satisfactory Progress. Total Review of Trainee's record was conducted on 18 DEC 2012 is currently 8 months in upgrade training Task Qualified 256-263 = Task completion 97% CDC Status- Vol 3 of 3 completed 03/28. Training Status- Satisfactory Progress. Total Review of Trainee's record was conducted on 27 NOV 2012 is currently 7 months in upgrade training Task Qualified 256-263 = Task completion 97% CDC Status- Vol 3 of 3 completed 03/28. Training Status- Satisfactory Progress. Total Review of Trainee's record was conducted on 2 OCT 2012 2012-09-19 Tasks was signed off on 11 tasks on 20120918. He is encouraged to keep up the good work with his 5 level task progression. 2012-09-17 Tasks was signed off on 5 tasks on 20120917. He is encouraged to keep up the good work with his 5 level upgrade training. 2012-08-27 Tasks was signed off on 7 tasks. He has proven that he is competent and knowledgeable on all of these tasks. RC-135V, T/N 64-14848, 30 April 2015 T-65 JOURNAL ENTRIES ENTRY DATE SUBJECT SIGNATURE INFO REMARKS 2012-08-09 Comprehensive Review I have conducted a comprehensive review with review training have been reviewed. 2012-08-08 Pretest #2 Administered CDC 2A553A issued 07May12. Trainee was provided instructions for completing the pretests. Trainee scored a 90%. Areas missed: Fuel and corrosion. Review conducted on 07May12. 2012-08-08 Pretest #3 Administered CDC 2A553A pretest issued on 15May12. Trainee was provided instructions for completing the prestest. Trainee scored a 90%. Areas missed: Hyrdraulics and TOs. Review conducted on 15May12. 2012-08-08 Pretest #1 Administered CDC 2A553A pretest issued on 06May12. Trainee was provided instructions for completing the pretests. Trainee scored a 90%. Areas missed: Engines and TCTOs. Review conducted 06May12. 2012-08-07 CDC'S UPDATE has been counselled about his cdc's and has been put on 12 hr shifts for mandatory study until his EOC is completed his duty hours are 1200-0000 2012-07-25 July upgrade training entry is currently 7 months in upgrade training Task Qualified -192/263 = Task completion 73% CDC Status- Vol 3 of 3 completed 03/28. Training Status- Satisfactory Progress. Total Review of Trainee's record was conducted on 23 MAY 2012 As of 3 June 2012 will have as a temporary supervisor while notice. 2012-05-23 Deployed Supervisor 2012-05-23 June 30 day entry 2012-05-18 Tasks Completed 2012-05-15 upgrade training 2012-05-03 30 day records check 2012-04-03 5 LVL Upgrade Task Completion 2012-03-29 March monthly journel entry 2012-03-28 CDC VOLUME 3 COMPLETE 2012-03-28 30 Day review 2012-03-28 CDC VOLUME 3 COMPLETE 2012-03-28 30 Day review 2012-02-28 CDC Vol 3 issued 2012-02-28 CDC Vol 2 Complete 2012-02-28 CDC Vol 3 issued 2012-02-13 CDC Vol 1 Completed 2012-02-13 CDC Vol 2 issue 2012-02-13 CDC Vol 1 Completed 2012-01-25 B-Series Maintenance Stand Safety Brief 2012-01-12 UTM OJT Orientation . All volumes to include unit review questions, self test questions, and is deployed until further is currently 3 months in upgrade training Task Qualified -108/263 = Task completion 60% CDC Status- Vol 3 of 3 completed 03/28. Training Status- Satisfactory Progress. Total Review of Trainee's record was conducted on 23 MAY 2012 This review complies with APR Upgrade Journal entry. Another entry will be required the last week of June for upgrade journal entry was signed off on 12 tasks. I feel that he is showing great progress and is very competent on the tasks completed. was completed on 31 tasks towards his upgrade training is currently 3 months in upgrade training Task Qualified -108/263 = Task completion 41% CDC Status- Vol 3 of 3 completed 03/28. awaiting pretestest to order EOC Training Status- Satisfactory Progress. Total Review of Trainee's record was conducted on 3 MAY 2012 This review complies with APR Upgrade Journal entry. Another entry will be required the last week of this month for April upgrade journal entry has proven proficient in 22 task pertaining to maintenance practices and I feel confident in signing him off on these task. is currently 3 months in upgrade training Task Qualified -19/263 = Task completion 14% CDC Status- Vol 3 of 3 completed 03/28. awaiting pretestest to order EOC Training Status- Satisfactory Progress. Total Review of Trainee's record was conducted on 28 Mar 2012 This review complies with Mar Upgrade Journal entry. Another entry will be required the last week of this month for April upgrade journal entry CDC vol 3 completed on 28 Mar 12. ECI Form 34 bubble Sheets for Volume #3 has been completed on 28 Mar 12 and filed in the member green upgrade folder. Member received a score of 98% and all questions have been reviewed and corrected to 100% I have reviewed TBA. On schedule upgrade tasks. CDC vol 3 completed on 28 Mar 12. ECI Form 34 bubble Sheets for Volume #3 has been completed on 28 Mar 12 and filed in the member green upgrade folder. Member received a score of 98% and all questions have been reviewed and corrected to 100% I have reviewed TBA. On schedule upgrade tasks. 27 Feb 12 I issued volume 3 of his 2A553A CDCs. He was briefed on the CDC guidelines and he understands the responsibilities of the CDC program. He understands he has a maximum of 30 days to complete each volume and documentation will be completed accordingly. He understands that a comprehensive review must be completed upon competition of the last volume and he understands what constitutes a comprehensive review. He will follow the requirements as outlined in AFI 36-2201 CDC vol 1 completed on 27 feb 12. ECI Form 34 bubble Sheets for Volume #2 has been completed on 27 Feb 12 and filed in the member green upgrade folder. Member received a score of 99% and all questions have been reviewed and corrected to 100% 27 Feb 12 I issued volume 3 of his 2A553A CDCs. He was briefed on the CDC guidelines and he understands the responsibilities of the CDC program. He understands he has a maximum of 30 days to complete each volume and documentation will be completed accordingly. He understands that a comprehensive review must be completed upon competition of the last volume and he understands what constitutes a comprehensive review. He will follow the requirements as outlined in AFI 36-2201 CDC vol 1 completed on 8 feb 12. ECI Form 34 bubble Sheets for Volume #1 has been completed on 8 Feb 12 and filed in the member green upgrade folder. Member received a score of 94% and all questions have been reviewed and corrected to 100%. 8 Feb 12 I issued volume 2of his 2A553A CDCs. He was briefed on the CDC guidelines and he understands the responsibilities of the CDC program. He understands he has a maximum of 30 days to complete each volume and documentation will be completed accordingly. He understands that a comprehensive review must be completed upon competition of the last volume and he understands what constitutes a comprehensive review. He will follow the requirements as outlined in AFI 36-2201 CDC vol 1 completed on 8 feb 12. ECI Form 34 bubble Sheets for Volume #1 has been completed on 8 Feb 12 and filed in the member green upgrade folder. Member received a score of 94% and all questions have been reviewed and corrected to 100%. Air Force Safety Center has identified a discrepancy with all B-series maintenance stands. These stands do not have proper fall protection IAW regulation , 29 CFR 1910.23(a)(2). Fall hazard exists when using B-series stands (i.e. open area at b-5 stand ladder/platform access point and b-4 step/platform access point). The individual has been briefed and is aware of the risks when using all B series maintenance stands. Trainee Orientation RC-135V, T/N 64-14848, 30 April 2015 T-66 JOURNAL ENTRIES ENTRY DATE SUBJECT SIGNATURE INFO REMARKS 1. Purpose: To indoctrinate Personnel on the concept, scope and objective of OJT. 2. Definition of OJT: Describes all training received by an airman while performing duties within an Air Force specialty. A good OJT program will include an organized plan that is designed to qualify the trainee under supervised instruction. The trainee is required to learn through self-study as well as gain experience while actually working on-the-job. Two types of OJT are: a. Upgrade Training (UGT). Training to qualify airmen for the award of a skill level. UGT increases skills and knowledge beyond the levels previously acquired. b. Qualification Training (QT). Hands-on performance training designed to qualify a trainee in a specific duty position. This can be training in conjunction with UGT, it can occur after UGT completion, or at any other time training is necessary. 3. Duties of: a. Commander: AFI 36-2201, Chapter 4 b. Base Training Office: AFI 36-2201 , Chapter 3 c. Unit Training Manager, AFI 36-2201, Chapter 5 d. Supervisor: AFI 36-2201, Chapter 6 e. Trainer/Certifier: AFI 36-2201, Chapter 6 f. Trainee: AFI 36-2201, Chapter 6 4. Criteria for award of a skill level advancement: a. For award of the 3-skill level (Apprentice): Completion of AETC Formal Technical School (if available). b. For award of the 5-skill level (Journeyman): Completion of mandatory 5-level Career Development Course(s) (CDCs). Certification on all 5-skill level core tasks, duty position tasks identified by the supervisor. Complete a minimum of 15 months in UGT for initial award and 9 months for retrainees. Mandatory items listed on The Air Force Enlisted Classification Directory (AFECD) Recommended by supervisor. 2012-01-12 Initial Evaluation/Workcenter Orientation 2012-01-12 UTM CDC Breifing 2012-01-12 CDC Issue Vol 1 2012-01-12 UTM OJT Orientation c. For award of the 7-skill level (Craftsman): Completion of mandatory 7-level CDCs (if applicable). Possess the minimum grade of staff sergeant (upgrade begins first day of the promotion cycle, 01 Sept). Certification I conducted an initial evaluation with on 20120112. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he was briefed that his training is ultimately his responsibility, and he needs to ensure he reviews his training records at least once a week and actively pursues the training he needs to complete his upgrade. He has also been briefed that tasks should be signed off within 30 days of the start date, unless mission requirements prohibit the completion of the task within that time. I conducted a workcenter orientation with on 20120112. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. Member was issued their CDCs. Mbr was briefed on the CDC guidelines and understands the responsibilities of the CDC program. The CDCs will be completed in the specified time frame and documentation will be completed accordingly. Mbr understands that a comprehensive review must be completed upon competition of the last volume and also understands what constitutes a comprehensive review. Mbr will follow the requirements as outlined in AFI 36-2201 Today I issued volume 1 of his 2A551 CDCs. He was briefed on the CDC guidelines and he understands the responsibilities of the CDC program. He understands he has a maximum of 30 days to complete each volume and documentation will be completed accordingly. He understands that a comprehensive review must be completed upon competition of the last volume and he understands what constitutes a comprehensive review. He will follow the requirements as outlined in AFI 36-2201 Trainee Orientation 1. Purpose: To indoctrinate Personnel on the concept, scope and objective of OJT. 2. Definition of OJT: Describes all training received by an airman while performing duties within an Air Force specialty. A good OJT program will include an organized plan that is designed to qualify the trainee under supervised instruction. The trainee is required to learn through self-study as well as gain experience while actually working on-the-job. Two types of OJT are: a. Upgrade Training (UGT). Training to qualify airmen for the award of a skill level. UGT increases skills and knowledge beyond the levels previously acquired. b. Qualification Training (QT). Hands-on performance training designed to qualify a trainee in a specific duty position. This can be training in conjunction with UGT, it can occur after UGT completion, or at any other time training is necessary. 3. Duties of: a. Commander: AFI 36-2201, Chapter 4 b. Base Training Office: AFI 36-2201 , Chapter 3 c. Unit Training Manager, AFI 36-2201, Chapter 5 d. Supervisor: AFI 36-2201, Chapter 6 e. Trainer/Certifier: AFI 36-2201, Chapter 6 f. Trainee: AFI 36-2201, Chapter 6 4. Criteria for award of a skill level advancement: a. For award of the 3-skill level (Apprentice): Completion of AETC Formal Technical School (if available). b. For award of the 5-skill level (Journeyman): Completion of mandatory 5-level Career Development Course(s) (CDCs). Certification on all 5-skill level core tasks, duty position tasks identified by the supervisor. Complete a minimum of 15 months in UGT for initial award and 9 months for retrainees. Mandatory items listed on The Air Force Enlisted Classification Directory (AFECD) Recommended by supervisor. 2012-01-12 UTM CDC Breifing 2012-01-12 Initial Evaluation/Workcenter Orientation c. For award of the 7-skill level (Craftsman): Completion of mandatory 7-level CDCs (if applicable). Possess the minimum grade of staff sergeant (upgrade begins first day of the promotion cycle, 01 Sept). Certification Member was issued their CDCs. Mbr was briefed on the CDC guidelines and understands the responsibilities of the CDC program. The CDCs will be completed in the specified time frame and documentation will be completed accordingly. Mbr understands that a comprehensive review must be completed upon competition of the last volume and also understands what constitutes a comprehensive review. Mbr will follow the requirements as outlined in AFI 36-2201 I conducted an initial evaluation with on 20120112. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he was briefed that his training is ultimately his responsibility, and he needs to ensure he reviews his training records at least once a week and actively pursues the training he needs to complete his upgrade. He has also been briefed that tasks should be signed off within 30 days of the start date, unless mission requirements prohibit the completion of the task within that time. I conducted a workcenter orientation with on 20120112. Items covered include chain of command, duty locations and RC-135V, T/N 64-14848, 30 April 2015 T-67 JOURNAL ENTRIES ENTRY DATE SUBJECT 2012-01-12 CDC Issue Vol 1 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.008.005. 001 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.009.013. 001 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.003.002. 002 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.002.004. 001 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.002.003. 004 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.002.003. 003 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.002.003. 002 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.002.003. 001 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.001.003. 004.001 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.020.011. 001 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.015.002 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.011.003 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.009.013. 002 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.009.013. 001 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.008.005. 001 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.005.001 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.003.002. 002 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.002.004. 001 2012-03-02 Removed start date for task: CFETP- SIGNATURE INFO REMARKS hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. Today I issued volume 1 of his 2A551 CDCs. He was briefed on the CDC guidelines and he understands the responsibilities of the CDC program. He understands he has a maximum of 30 days to complete each volume and documentation will be completed accordingly. He understands that a comprehensive review must be completed upon competition of the last volume and he understands what constitutes a comprehensive review. He will follow the requirements as outlined in AFI 36-2201 Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.008.005.001 (2) Task Description: Team member (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.009.013.001 (2) Task Description: Purpose (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.003.002.002 (2) Task Description: Brakes (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.004.001 (2) Task Description: Cowling (F-108) (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.003.004 (2) Task Description: Wheel well doors (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.003.003 (2) Task Description: Emergency exit hatch (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.003.002 (2) Task Description: Cargo door (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.003.001 (2) Task Description: Crew entry door (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.001.003.004.001 (2) Task Description: Wing/tail walker (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.020.011.001 (2) Task Description: Perform pre-use inspection (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.015.002 (2) Task Description: Component identification (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.011.003 (2) Task Description: Safe aircraft for maintenance (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.009.013.002 (2) Task Description: Select and use ruler (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.009.013.001 (2) Task Description: Purpose (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.008.005.001 (2) Task Description: Team member (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.005.001 (2) Task Description: Flight control components and system operation (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.003.002.002 (2) Task Description: Brakes (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.004.001 (2) Task Description: Cowling (F-108) (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.003.004 RC-135V, T/N 64-14848, 30 April 2015 T-68 JOURNAL ENTRIES ENTRY DATE SUBJECT 2A5X1-006-001.001.002.003. 004 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.002.003. 003 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.002.003. 002 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.002.003. 001 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.001.003. 004.001 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.020.011. 001 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.015.002 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.011.003 2012-03-02 Removed start date for task: CFETP2A5X1-000-001.001.009.013. 002 2012-03-02 Removed start date for task: CFETP2A5X1-006-001.001.005.001 SIGNATURE INFO REMARKS (2) Task Description: Wheel well doors (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.003.003 (2) Task Description: Emergency exit hatch (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.003.002 (2) Task Description: Cargo door (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.002.003.001 (2) Task Description: Crew entry door (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.001.003.004.001 (2) Task Description: Wing/tail walker (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.020.011.001 (2) Task Description: Perform pre-use inspection (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.015.002 (2) Task Description: Component identification (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.011.003 (2) Task Description: Safe aircraft for maintenance (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-000-001.001.009.013.002 (2) Task Description: Select and use ruler (3) Reason: star date incorrect (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-006-001.001.005.001 (2) Task Description: Flight control components and system operation (3) Reason: star date incorrect (4) Removed By Employee: RC-135V, T/N 64-14848, 30 April 2015 T-69 CERTIFICATION I CERTIFY THAT THIS INDIVIDUAL TRAINING RECORD IS CURRENT AS OF 2015-05-04 _____________________________ TRAINEE SIGNATURE _____________________________ SUPERVISOR SIGNATURE RC-135V, T/N 64-14848, 30 April 2015 T-70 1. IDENTIFICATION DATA LAST NAME - FIRST NAME - MIDDLE INITIAL [Crew Chief 2] GRADE/RANK Staff Sergeant DAFSC/JOB SERIES 2A574 INDIVIDUAL TRAINING RECORD INDIVIDUAL'S SIGNATURE DATE 2015-05-04 Individual Training Record RC-135V, T/N 64-14848, 30 April 2015 T-71 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 001 Career Ladder Progression-1 Aug 12 TR: Air Force Enlisted Classification Directory (AFECD) 2A5X1 AND 2A5X4-000 001.001 Progression in career ladder 2A5X1 AND 2A5X4-000 001.002 Duties of AFSC 2A5X1 AND 2A5X4-000 003 AF OCCUPATIONAL SAFETY AND HEALTH (AFOSH) PROGRAM TR: AFIs 11-218, 21-101 and 91-301; applicable AFOSH STDs; TOs 00-25-172, 1-1-691, and applicable aircraft TOs 2A5X1 AND 2A5X4-000 003.001 Housekeeping consistent with safety of personnel and equipment 2A5X1 AND 2A5X4-000 003.002 Safety precautions pertaining to aircraft maintenance 2A5X1 AND 2A5X4-000 003.002.001 Engine air intake and exhaust 2A5X1 AND 2A5X4-000 003.002.002 High intensity sound 2A5X1 AND 2A5X4-000 003.002.003 Turbine, propeller, rotor plane of rotation 2A5X1 AND 2A5X4-000 003.002.004 Radio frequency radiation 2A5X1 AND 2A5X4-000 003.002.005 Ground handling of aircraft 2A5X1 AND 2A5X4-000 003.002.006 Hot brakes 2A5X1 AND 2A5X4-000 003.002.007 Use of tools and equipment 2A5X1 AND 2A5X4-000 003.002.008 Servicing aircraft systems 2A5X1 AND 2A5X4-000 003.002.009 Cleaning Agents 2A5X1 AND 2A5X4-000 003.002.010 Solvents 2A5X1 AND 2A5X4-000 003.002.011 Lubricants 2A5X1 AND 2A5X4-000 003.002.012 High pressure gasses 2A5X1 AND 2A5X4-000 003.002.013 Aircraft explosive equipment 2A5X1 AND 2A5X4-000 003.002.014 Composite materials 2A5X1 AND 2A5X4-000 003.002.015 Maintenance resource management TR: AFI 21-101; AFPAM 90-902 2A5X1 AND 2A5X4-000 003.002.016 Electrostatic hazards, static grounding and bonding TR: TOs 00-25-172 and 00-25-234 2A5X1 AND 2A5X4-000 003.003 Portable ground fire extinguishers TR: AFI 32-2001; TO 00-25-172 2A5X1 AND 2A5X4-000 003.003.001 Perform pre-use inspection 2A5X1 AND 2A5X4-000 003.003.002 Position 2A5X1 AND 2A5X4-000 003.003.003 Operate 2A5X1 AND 2A5X4-000 003.004 Foreign Object Damage (FOD) prevention program 2A5X1 AND 2A5X4-000 003.005 Dropped Object prevention program 2A5X1 AND 2A5X4-000 003.006 Hazardous chemicals TR: AFI 90-821 and applicable AFOSH STDs 2A5X1 AND 2A5X4-000 003.006.001 Use 2A5X1 AND 2A5X4-000 003.006.002 Disposal 2A5X1 AND 2A5X4-000 003.006.003 Hazard communication training program 2A5X1 AND 2A5X4-000 003.006.004 Hazardous material handling procedures 2A5X1 AND 2A5X4-000 003.007 AF Form 1492, Warning Tag TR: TO 00-20-1 2A5X1 AND 2A5X4-000 004 MAINTENANCE DIRECTIVES, REFERENCES, and INSTRUCTIONS TR: AFI 33-360 and TO 00-5 series as applicable 2A5X1 AND 2A5X4-000 004.001 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2010-04-09 2010-04-12 - A B - - - - 2010-04-09 2010-04-12 - A B - - - - - A - - - - - - A - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - 1b - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - - - - - - - - - - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - A B - - - - RC-135V, T/N 64-14848, 30 April 2015 T-72 1. Tasks Knowledge And Technical References TO system 2A5X1 AND 2A5X4-000 004.002 Air Force manuals and instructions 2A5X1 AND 2A5X4-000 004.003 Use technical orders 2A5X1 AND 2A5X4-000 004.004 TO improvement reporting 2A5X1 AND 2A5X4-000 005 SUPERVISION TR: AFIs 21-101, 36-2403, and AFTTP 3-3 2A5X1 AND 2A5X4-000 005.001 Plan work schedules 2A5X1 AND 2A5X4-000 005.002 Schedule maintenance 2A5X1 AND 2A5X4-000 005.003 Supervise personnel accomplishing maintenance 2A5X1 AND 2A5X4-000 005.004 Establish 2A5X1 AND 2A5X4-000 005.004.001 Work methods 2A5X1 AND 2A5X4-000 005.004.002 Work controls 2A5X1 AND 2A5X4-000 005.004.003 Performance standards 2A5X1 AND 2A5X4-000 005.005 Evaluate work performance of subordinate personnel 2A5X1 AND 2A5X4-000 006 TRAINING TR: AFIs 36-2201 and 36-2232 2A5X1 AND 2A5X4-000 006.001 Evaluate personnel for training 2A5X1 AND 2A5X4-000 006.002 Plan and supervise OJT 2A5X1 AND 2A5X4-000 006.003 Counsel trainees on training progress 2A5X1 AND 2A5X4-000 006.005 Document training records 2A5X1 AND 2A5X4-000 006.006 Purpose and use of Career Field Education and Training Plan (CFETP) 2A5X1 AND 2A5X4-000 007 MAINTENANCE MANAGEMENT TR: AFIs 21-101, 21-103, 21-118, 90-201 and AFMAN 23-110 2A5X1 AND 2A5X4-000 007.001 Basic functions within maintenance 2A5X1 AND 2A5X4-000 007.002 Resource management 2A5X1 AND 2A5X4-000 007.003 Personnel management 2A5X1 AND 2A5X4-000 007.004 Maintenance incident investigation and prevention 2A5X1 AND 2A5X4-000 007.005 Determine and report Aircraft Status 2A5X1 AND 2A5X4-000 008 MAINTENANCE DATA DOCUMENTATION (MDD) TR: AFI 21-101; TO 00-20 Series; applicable aircraft -06 Work Unit Code Manuals 2A5X1 AND 2A5X4-000 008.001 MDD Fundamentals 2A5X1 AND 2A5X4-000 008.002 Aircraft and supporting maintenance records 2A5X1 AND 2A5X4-000 008.002.001 Purpose 2A5X1 AND 2A5X4-000 008.002.002 Automated Forms 2A5X1 AND 2A5X4-000 008.002.007 Document other AFTO 781 series forms 2A5X1 AND 2A5X4-000 008.002.008 Document AFTO Form 244/245 2A5X1 AND 2A5X4-000 008.002.009 Document AFTO Form 350 2A5X1 AND 2A5X4-000 008.003 Maintenance Information Systems (MIS) 2A5X1 AND 2A5X4-000 008.003.001 Purpose 2A5X1 AND 2A5X4-000 008.003.002 Job data documentation (JDD) 2A5X1 AND 2A5X4-000 008.003.002.001 Purpose 2A5X1 AND 2A5X4-000 008.003.002.002 Access JDD 2A5X1 AND 2A5X4-000 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 1b - - - - - 2009-10-26 2009-10-26 - - B - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - A - - - - - - A - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - B - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - 1b - - - - - 2009-10-26 2009-10-26 - 1b - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-73 1. Tasks Knowledge And Technical References 008.003.002.003 Create maintenance event 2A5X1 AND 2A5X4-000 008.003.002.004 Defer maintenance event 2A5X1 AND 2A5X4-000 008.003.002.005 Schedule maintenance event 2A5X1 AND 2A5X4-000 008.003.002.006 Close maintenance event 2A5X1 AND 2A5X4-000 008.003.002.007 Use IMDS 2A5X1 AND 2A5X4-000 009 MAINTENANCE MATERIALS/ TOOLS TR:AFI 21-101, TOs 1-1A-8, 1-1A-14, 1-1-691 and 32- series TOs as applicable 2A5X1 AND 2A5X4-000 009.001 Tool control 2A5X1 AND 2A5X4-000 009.002 Select and use special tools 2A5X1 AND 2A5X4-000 009.003 Select/use restraint harness (e.g.; fall protection/prevention equipment) 2A5X1 AND 2A5X4-000 009.005 Hardware 2A5X1 AND 2A5X4-000 009.005.001 Purpose 2A5X1 AND 2A5X4-000 009.005.002 Remove/inspect/install 2A5X1 AND 2A5X4-000 009.006 Electrical connectors 2A5X1 AND 2A5X4-000 009.006.001 Purpose 2A5X1 AND 2A5X4-000 009.006.002 Connect/disconnect 2A5X1 AND 2A5X4-000 009.007 Securing devices 2A5X1 AND 2A5X4-000 009.007.001 Purpose 2A5X1 AND 2A5X4-000 009.007.002 Install/remove safety wire 2A5X1 AND 2A5X4-000 009.007.003 Install/remove cotter pins 2A5X1 AND 2A5X4-000 009.007.004 Safety cable 2A5X1 AND 2A5X4-000 009.008 Lubricants 2A5X1 AND 2A5X4-000 009.009 Sealants 2A5X1 AND 2A5X4-000 009.010 Adhesives 2A5X1 AND 2A5X4-000 009.011 Cleaning agents 2A5X1 AND 2A5X4-000 009.012 Hand tools 2A5X1 AND 2A5X4-000 009.012.001 Purpose 2A5X1 AND 2A5X4-000 009.012.002 Select, inspect and use 2A5X1 AND 2A5X4-000 009.013 Measuring tools 2A5X1 AND 2A5X4-000 009.013.001 Purpose 2A5X1 AND 2A5X4-000 009.013.002 Select and use ruler 2A5X1 AND 2A5X4-000 009.013.003 Select and use thickness gauge 2A5X1 AND 2A5X4-000 009.013.004 Use multi-meter 2A5X1 AND 2A5X4-000 009.013.005 Select, inspect and use torque wrench 2A5X1 AND 2A5X4-000 009.013.006 Select and use micrometer 2A5X1 AND 2A5X4-000 009.013.007 Use depth gauge 2A5X1 AND 2A5X4-000 010 RESPONSIBILITY FOR SUPPLY TR: AFIs 21-101 and 21-118, AFMAN 23-110, TOs 00-20-3 and 00-35D-54 2A5X1 AND 2A5X4-000 010.001 Maintenance supply concept 2A5X1 AND 2A5X4-000 010.003 Special requisition (GPC, Local purchase) 2A5X1 AND 2A5X4-000 010.004 Ordering parts 2A5X1 AND 2A5X4-000 010.006 Prepare repairable and serviceable parts for turn-in 2A5X1 AND 2A5X4-000 010.007 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - 2b - - - - - - A - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - 2b - - - - - - 2b - - - - - - 2b - - - - - - - - - - - - - 2b - - - - - 2009-10-26 2009-10-26 - A B - - - - 2012-01-16 2012-01-31 - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - B - - - - - - - - - - - 2009-10-26 2009-10-26 RC-135V, T/N 64-14848, 30 April 2015 T-74 1. Tasks Knowledge And Technical References Repair cycle assets 2A5X1 AND 2A5X4-000 010.008 DIFM Control 2A5X1 AND 2A5X4-000 010.009 Local manufacture of parts 2A5X1 AND 2A5X4-000 010.010 Equipment account management 2A5X1 AND 2A5X4-000 010.011 Deficiency reporting 2A5X1 AND 2A5X4-000 010.013 DD Forms 1574, 1575, 1576, 1577 and 1577-2 2A5X1 AND 2A5X4-000 011 AIRCRAFT GENERAL TR: AFI 11-218; applicable AFOSH STDs; TOs 00-20-1, 00-25-172, 1-1-691, 1-1B-50 and applicable aircraft TOs 2A5X1 AND 2A5X4-000 011.001 Weight and balance 2A5X1 AND 2A5X4-000 011.002 Determine weight and balance requirements 2A5X1 AND 2A5X4-000 011.003 Inventory aircraft equipment 2A5X1 AND 2A5X4-000 011.004 Safe aircraft for maintenance 2A5X1 AND 2A5X4-000 011.005 Corrosion control program 2A5X1 AND 2A5X4-000 011.005.001 Aircraft cleaning 2A5X1 AND 2A5X4-000 011.005.002 Corrosion identification 2A5X1 AND 2A5X4-000 011.005.004 Aircraft lubrication 2A5X1 AND 2A5X4-000 011.006 Aircraft inspections 2A5X1 AND 2A5X4-000 011.006.001 Cncepts and Types 2A5X1 AND 2A5X4-000 011.008 Aircraft marshalling signals 2A5X1 AND 2A5X4-000 011.011 Deice aircraft TR: TO 42C-1-2S-2; 14CFR121.629 section 121.629 2A5X1 AND 2A5X4-000 011.012 Debrief aircrews 2A5X1 AND 2A5X4-000 011.013 Aircraft guarded switches 2A5X1 AND 2A5X4-000 011.013.001 Design/function/proper identification 2A5X1 AND 2A5X4-000 011.013.002 Remove and replace covers 2A5X1 AND 2A5X4-000 011.013.003 Operational check 2A5X1 AND 2A5X4-000 012 AIRFRAME TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 012.002 Remove/inspect/install panels 2A5X1 AND 2A5X4-000 012.003 Inspect structural components 2A5X1 AND 2A5X4-000 013 LANDING GEAR TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 013.001 System fundamentals 2A5X1 AND 2A5X4-000 014 UTILITIES TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 014.001 System fundamentals 2A5X1 AND 2A5X4-000 014.001.001 Oxygen 2A5X1 AND 2A5X4-000 014.001.002 Bleed air 2A5X1 AND 2A5X4-000 014.001.003 Pressurization 2A5X1 AND 2A5X4-000 014.001.004 Air conditioning 2A5X1 AND 2A5X4-000 014.001.005 Fire/Overheat warning 2A5X1 AND 2A5X4-000 014.001.006 Fire suppression 2A5X1 AND 2A5X4-000 015 FLIGHT CONTROLS TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 015.001 Fundamentals of flight 2A5X1 AND 2A5X4-000 015.002 Primary flight control fundamentals 2A5X1 AND 2A5X4-000 015.003 Secondary flight control fundamentals 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-10-26 2009-10-26 - - B - - - - 2009-10-26 2009-10-26 - - - - - - - - - - - - - - 2009-10-26 2009-10-26 - - B - - - - 2009-10-26 2009-10-26 - - B - - - - - A B - - - - 2012-01-16 2012-01-31 - - - - - - - 2009-10-26 2009-10-26 - - A - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2007-10-04 2007-10-04 - 1b - - - - - 2007-10-04 2007-10-04 - - - - - - - 2007-10-04 2007-10-04 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - - A B - - - - - A B - - - - - A - - - - - - A - - - - - 2007-10-04 2007-10-04 RC-135V, T/N 64-14848, 30 April 2015 T-75 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 015.004 Component identification 2A5X1 AND 2A5X4-000 016 HYDRAULICS TR: TO 1-1A-8 and applicable aircraft TOs 2A5X1 AND 2A5X4-000 016.001 System fundamentals 2A5X1 AND 2A5X4-000 016.002 Remove/install components TR: TO 1-1A-8, Applicable aircraft TOs 2A5X1 AND 2A5X4-000 016.002.001 Tubing/hoses 2A5X1 AND 2A5X4-000 016.002.002 Fittings 2A5X1 AND 2A5X4-000 016.002.003 Filter elements 2A5X1 AND 2A5X4-000 016.003 Hydraulic Schematics /diagrams 2A5X1 AND 2A5X4-000 017 ENGINES TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 017.001 System fundamentals 2A5X1 AND 2A5X4-000 017.004 Joint Oil Analysis Program 2A5X1 AND 2A5X4-000 018 FUELS TR: TOs 00-25-172, 1-1-3, applicable AFOSH STDs and aircraft TOs 2A5X1 AND 2A5X4-000 018.001 System fundamentals 2A5X1 AND 2A5X4-000 018.002 Classify fuel leaks 2A5X1 AND 2A5X4-000 019 ELECTRICAL TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 019.001 AC Electrical system fundamentals 2A5X1 AND 2A5X4-000 019.002 DC electrical system fundamentals 2A5X1 AND 2A5X4-000 019.007 Electrical schematics/diagrams 2A5X1 AND 2A5X4-000 020 AEROSPACE GROUND EQUIPMENT TR: Applicable AFOSH STDs and TO 35A4 series as applicable 2A5X1 AND 2A5X4-000 020.001 Maintenance stands 2A5X1 AND 2A5X4-000 020.001.001 Purpose and description 2A5X1 AND 2A5X4-000 020.001.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.002 Self-propelled universal platforms 2A5X1 AND 2A5X4-000 020.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.002.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.003 Aircraft jacks TR: TO 35A2- series as applicable 2A5X1 AND 2A5X4-000 020.003.001 Purpose and description 2A5X1 AND 2A5X4-000 020.003.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.005 Oxygen servicing equipment TR: TO 15X-1-1, 37C2-8- as applicable 2A5X1 AND 2A5X4-000 020.005.001 Liquid oxygen (LOX) 2A5X1 AND 2A5X4-000 020.005.001.001 Purpose and description 2A5X1 AND 2A5X4-000 020.005.001.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.005.002 Gaseous oxygen (GOX) 2A5X1 AND 2A5X4-000 020.005.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.005.002.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.006 Diesel driven air compressors TR: TO 34Y1- series as applicable 2A5X1 AND 2A5X4-000 020.006.001 Purpose and description 2A5X1 AND 2A5X4-000 020.006.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.007 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2009-10-26 2009-10-26 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - A - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - - - - - - - - 2012-01-16 2012-01-31 - A - - - - - 2007-10-04 2007-10-04 - A B - - - - 2010-04-09 2010-06-01 - - B - - - - 2007-10-04 2007-10-04 - A B - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2010-04-09 2010-06-01 - A - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 2b - - - - - - A B - - - - - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - - - - - - 2010-04-09 2010-04-12 - A B - - - - 2010-04-09 2010-04-12 - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-76 1. Tasks Knowledge And Technical References Ground heaters TR: 35E7- series as applicable 2A5X1 AND 2A5X4-000 020.007.001 Purpose and description 2A5X1 AND 2A5X4-000 020.007.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.008 Lighting equipment TR: TO 35F5- series as applicable 2A5X1 AND 2A5X4-000 020.008.001 Purpose and description 2A5X1 AND 2A5X4-000 020.008.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.010 Air conditioning units TR: TO 35E9- Series as applicable 2A5X1 AND 2A5X4-000 020.010.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011 Ground generator sets/gas turbine compressors 2A5X1 AND 2A5X4-000 020.011.002 A/M32A-95 Gas turbine compressors TR: TO 35D12-series as applicable 2A5X1 AND 2A5X4-000 020.011.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011.003 Diesel driven generator sets TR: TO 35C2- series as applicable 2A5X1 AND 2A5X4-000 020.011.003.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011.003.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.012 Tow bar TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 020.012.001 Perform pre-use inspection 2A5X1 AND 2A5X4-000 020.012.002 Connect/disconnect 2A5X1 AND 2A5X4-000 020.013 Tow vehicles TR: TO 36A10 series as applicable 2A5X1 AND 2A5X4-000 020.013.001 Purpose and description 2A5X1 AND 2A5X4-000 020.013.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.014 Self-generating nitrogen equipment TR: TO 35D29-7-6-1 2A5X1 AND 2A5X4-000 020.014.001 Purpose and description 2A5X1 AND 2A5X4-000 020.014.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.015 Gaseous nitrogen servicing equipment TR: TO 35D3- series as applicable 2A5X1 AND 2A5X4-000 020.015.001 Purpose and description 2A5X1 AND 2A5X4-000 020.016 Engine stands and dollies TR: 35D3- series as applicable 2A5X1 AND 2A5X4-000 020.016.001 Purpose and description 2A5X1 AND 2A5X4-000 020.016.002 Perform pre-use inspection and operate 2A5X4-006 001 C-135 QUALITATIVE REQUIREMENTS AIRCRAFT GENERAL 2A5X4-006 001.001 Periodic/Isochronal inspection concept and inspection TR: TOs 00-20 series, Applicable -6 TOs 2A5X4-006 001.001.001 Periodic/Isochronal inspection concept 2A5X4-006 001.001.002 Perform inspections 2A5X4-006 001.001.002.001 Preflight 2A5X4-006 001.001.002.002 Alert 5A 2A5X4-006 001.001.002.003 Alert 5B 2A5X4-006 001.001.002.004 Thruflight 2A5X4-006 001.001.002.005 Quick Turn 2A5X4-006 001.001.002.006 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 5 7 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - - - B - - - - - - - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - A B - - - - 2009-10-26 2009-10-26 - - A - - - - 2010-04-09 2010-06-01 - - - - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - 2b - - - - - - - - - - - - - - - - - - - 2009-10-26 2009-11-03 - 2b - - - - - 2010-04-09 2010-06-01 - - - - - - - 2010-01-12 2010-01-12 - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-77 1. Tasks Knowledge And Technical References Hourly Post 2A5X4-006 001.001.002.009 Calendar 2A5X4-006 001.001.002.010 Special 2A5X4-006 001.001.002.011 900 Hr Insp 2A5X4-006 001.001.002.012 Time change item 2A5X4-006 001.001.002.013 Exterior panel/secondary structure inspection 2A5X4-006 001.002 Aircraft communications equipment TR: Applicable -2 TOs 2A5X4-006 001.002.001 Operate radio 2A5X4-006 001.002.002 Use interphone 2A5X4-006 001.003 Perform ground handling TR: AFI 11-218, TO 00-25-172, applicable AFOSH STDs, applicable -1 and -2 TOs 2A5X4-006 001.003.001 Aircraft launch 2A5X4-006 001.003.002 Call flight controls 2A5X4-006 001.003.003 Aircraft recovery 2A5X4-006 001.003.004 Tow aircraft 2A5X4-006 001.003.004.001 Wing/tail walker 2A5X4-006 001.003.004.002 Brake operator 2A5X4-006 001.003.004.003 Tow team supervisor 2A5X4-006 001.003.004.004 Tow vehicle operator 2A5X4-006 001.003.005 Jack and level aircraft 2A5X4-006 001.003.005.001 Jacking team member 2A5X4-006 001.003.005.005 Axle jacking 2A5X4-006 001.004 Compute center of gravity TR: Applicable aircraft -5 TOs 2A5X4-006 001.005 Install/remove ground safety devices TR: Applicable -2 TOs 2A5X4-006 001.005.001 Landing gear 2A5X4-006 001.005.002 Landing gear doors 2A5X4-006 001.006 Ground aircraft 2A5X4-006 001.007 Configure/reconfigure aircraft 2A5X4-006 001.007.002 Passenger/personnel 2A5X4-006 001.008 Maintain/store/configure/-21 equipment 2A5X4-006 001.010 Aircraft wash TR: TO - 6WC-3 2A5X4-006 001.010.001 Team member 2A5X4-006 001.010.002 Team supervisor 2A5X4-006 001.010.003 Post wash lube 2A5X4-006 001.011 Maintenance directives, references, & instructions TR: AFI 37-101 Vol 1 and TO 00-5-1 2A5X4-006 001.011.001 Use C-135 technical orders 2A5X4-006 001.012 Maintenance Data Documentation (MDD TR: AFI 21-101, TOs 00-20-1, 00-20-2, and applicable aircraft -06 Work Unit Code Manuals 2A5X4-006 001.012.001 Document AFTO Form 781H 2A5X4-006 001.012.002 Document AFTO Form 781A 2A5X4-006 001.012.003 Document AFTO Form 781J 2A5X4-006 001.012.004 Document AFTO Form 781K 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2010-04-09 2010-04-12 - - - - - - - 2010-04-09 2010-04-12 - - - - - - - 2010-04-09 2010-06-01 - - - - - - - 2012-01-16 2012-01-31 - - - - - - - 7 2009-10-26 2009-11-03 - - - - - - - 5 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 7 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 2012-09-24 2012-09-27 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 5 - 3c - - - - - 5 - 3c - - - - - 5 - 3c - - - - - 5 - 3c - - - - - 5 - 3c - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-78 1. Tasks Knowledge And Technical References 2A5X4-006 002 AIRFRAME SYSTEMS TR: Applicable -2 TOs 2A5X4-006 002.001 Airframe components and structure 2A5X4-006 002.002 Service cargo door reservoir 2A5X4-006 002.003 Operate 2A5X4-006 002.003.001 Crew entry door 2A5X4-006 002.003.002 Cargo door 2A5X4-006 002.003.003 Emergency exit hatch 2A5X4-006 002.003.004 Wheel well doors 2A5X4-006 002.004 Open and close 2A5X4-006 002.004.001 Cowling (F-108) 2A5X4-006 002.004.002 Cowling (TF-33) 2A5X4-006 002.004.003 Panels/doors 2A5X4-006 002.004.004 Windows 2A5X4-006 002.005 Remove and install 2A5X4-006 002.005.001 Cowling (F-108) 2A5X4-006 002.005.002 Cowling (TF-33) 2A5X4-006 002.005.003 Panels/doors 2A5X4-006 002.005.004 Non-explosive seats 2A5X4-006 002.005.005 Windows 2A5X4-006 002.005.007 Radomes 2A5X4-006 002.005.008 Door/hatch seals 2A5X4-006 002.005.009 Thermal curtains 2A5X4-006 002.005.013 Tail cone 2A5X4-006 002.006 Perform aircraft inclement weather procedures 2A5X4-006 002.007 Inspect crew/passenger comfort facilities TR: Applicable -6 TOs 2A5X4-006 002.008 Service crew/passenger comfort facilities 2A5X4-006 003 LANDING GEAR SYSTEMS TR: Applicable -2 TOs 2A5X4-006 003.001 Landing gear components and system operation 2A5X4-006 003.002 Troubleshoot 2A5X4-006 003.003 Operate 2A5X4-006 003.003.001 Landing gear 2A5X4-006 003.003.002 Brakes 2A5X4-006 003.003.003 Steering system 2A5X4-006 003.003.004 Anti skid system 2A5X4-006 003.004 Service 2A5X4-006 003.004.001 Snubber 2A5X4-006 003.004.002 Centering cylinder 2A5X4-006 003.004.003 Landing gear struts 2A5X4-006 003.004.003.001 Deflate 2A5X4-006 003.004.003.002 Drain 2A5X4-006 003.004.003.003 Fill 2A5X4-006 003.004.003.004 Inflate 2A5X4-006 003.004.004 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-10-26 2009-10-26 - A - - - - - 2012-09-24 2012-09-27 - b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - 2b/b - - - - - 2010-04-09 2010-04-12 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2012-01-16 2012-01-31 - - - - - - - 2009-11-17 2009-11-20 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2010-01-12 2010-01-12 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - - - - - - - - - - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2012-01-16 2012-01-31 - - - - - - - 2012-01-16 2012-01-31 - - - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-79 1. Tasks Knowledge And Technical References Tires 2A5X4-006 003.005 Lubricate landing gear components 2A5X4-006 003.006 Remove and Install 2A5X4-006 003.006.001 Snubbers 2A5X4-006 003.006.002 Centering cylinder 2A5X4-006 003.006.003 Wheel and tire assemblies 2A5X4-006 003.006.003.001 Nose 2A5X4-006 003.006.003.002 Main 2A5X4-006 003.006.004 Anti-skid transducer 2A5X4-006 003.006.005 Carbon brake assemblies 2A5X4-006 003.006.006 Bleed brake assembly (carbon) 2A5X4-006 003.007 Determine serviceability of aircraft tires TR: TO 4T-1-3 2A5X4-006 004 UTILITY SYSTEMS TR: TO 00-25-172, Applicable -2 TOs 2A5X4-006 004.001 Utility components and system operation 2A5X4-006 004.002 Troubleshoot 2A5X4-006 004.003 Operate 2A5X4-006 004.003.001 Bleed air system 2A5X4-006 004.003.002 Air conditioning system 2A5X4-006 004.003.003 Pressurization system 2A5X4-006 004.003.004 Anti-ice system 2A5X4-006 004.003.005 Fire/overheat warning system 2A5X4-006 004.003.006 Fire extinguishing system 2A5X4-006 004.003.007 Oxygen system 2A5X4-006 004.004 Oxygen system TR: Applicable -2, -3 TOs 2A5X4-006 004.004.001 Service gaseous oxygen 2A5X4-006 004.004.002 Service liquid oxygen 2A5X4-006 004.005 Inspect TR: Applicable -6 TOs 2A5X4-006 004.005.001 Bleed air system 2A5X4-006 004.005.002 Air conditioning system 2A5X4-006 004.005.003 Pressurization system 2A5X4-006 004.005.004 Anti-ice system 2A5X4-006 004.005.005 Fire/overheat warning system 2A5X4-006 004.005.006 Fire extinguisher system 2A5X4-006 004.005.007 Oxygen system 2A5X4-006 004.006 Air Cycle Machine (ACM) 2A5X4-006 004.006.001 Drain 2A5X4-006 004.006.002 Service 2A5X4-006 005 FLIGHT CONTROL SYSTEM TR: Applicable -2 TOs 2A5X4-006 005.001 Flight control components and system operation 2A5X4-006 005.002 Troubleshoot 2A5X4-006 005.003 Operate flight controls 2A5X4-006 005.003.001 Aileron system 2A5X4-006 005.003.002 Rudder system 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2007-10-04 2007-10-04 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-11-03 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 2010-01-12 2010-01-12 - A - - - - - - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2012-01-16 2012-01-31 - - - - - - - 2012-01-16 2012-01-31 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-11-17 2009-11-20 - 2b - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 2009-10-26 2009-10-26 - A - - - - - - - - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T-80 1. Tasks Knowledge And Technical References 2A5X4-006 005.003.003 Elevator system 2A5X4-006 005.003.004 Spoiler/Speed brake system 2A5X4-006 005.003.005 Stabilizer trim system 2A5X4-006 005.003.006 Flap system 2A5X4-006 005.004 Remove/install 2A5X4-006 005.004.001 Cove lip door 2A5X4-006 005.004.002 Cove lip door latch 2A5X4-006 005.004.005 Fore flap 2A5X4-006 005.004.006 Aileron snubber 2A5X4-006 005.004.007 Elevator snubber 2A5X4-006 005.004.013 Leading edge flaps 2A5X4-006 005.005 Lubricate flight controls 2A5X4-006 005.006 Service gearbox 2A5X4-006 006 HYDRAULIC SYSTEMS TR: Applicable -2 TOs 2A5X4-006 006.001 Hydraulic components and system operation 2A5X4-006 006.002 Troubleshoot 2A5X4-006 006.003 Service hydraulic system 2A5X4-006 006.003.001 Reservoir 2A5X4-006 006.003.002 Accumulator 2A5X4-006 006.003.003 Drain reservoir 2A5X4-006 006.004 Operate 2A5X4-006 006.004.001 Engine driven pump 2A5X4-006 006.004.002 Non-engine driven pump 2A5X4-006 006.005 Remove and install accumulator 2A5X4-006 007 ENGINES TR: AFI 11-218, applicable AFOSH STDs and -2 TOs 2A5X4-006 007.001 Engine and Auxiliary Power Unit (APU) components and system operation 2A5X4-006 007.003 Perform 2A5X4-006 007.003.001 Engine operational check 2A5X4-006 007.003.004 Engine motor wet 2A5X4-006 007.003.005 Engine motor dry 2A5X4-006 007.003.006 Audible ignition check 2A5X4-006 007.003.007 Alternate engine start 2A5X4-006 007.004 Operate 2A5X4-006 007.004.001 Engine and subsystems 2A5X4-006 007.005 Service 2A5X4-006 007.005.001 Oil system 2A5X4-006 007.005.002 Constant Speed Drive (CSD)/Integrated Drive Generator (IDG) 2A5X4-006 007.005.003 Gear box 2A5X4-006 007.005.004 Auxiliary Power Unit (if equipped) 2A5X4-006 007.006 Remove and install 2A5X4-006 007.006.001 Starter 2A5X4-006 007.006.002 Starter cartridge 2A5X4-006 007.007 Take engine oil sample 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2009-10-26 2009-10-26 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - 2b - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2008-04-02 2008-04-15 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - - - - - - - 2012-10-09 2012-10-16 - - - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - - - - - - - - A - - - - - 2012-10-09 2012-10-16 - - - - - - - 2012-10-09 2012-10-16 - - - - - - - 2012-10-09 2012-10-16 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - - - - - - - - - - - - - - - 2009-10-26 2009-10-26 - b - - - - - 2009-10-26 2009-10-26 - - - - - - - 2012-01-16 2012-01-31 - - - - - - - 2010-04-09 2010-04-12 - - - - - - - 2007-10-04 2007-10-04 - - - - - - - - - - - - - - - - - - - - - 2007-10-04 2007-10-04 5 5 2010-04-09 2010-04-12 RC-135V, T/N 64-14848, 30 April 2015 T-81 1. Tasks Knowledge And Technical References TR: TO 42B2-1-9, 33-1-37 2A5X4-006 007.008 Chip detectors 2A5X4-006 007.009 Inspect installed engine TR: Applicable -6 TOs 2A5X4-006 007.009.001 Turbine 2A5X4-006 007.010 Inspect Auxiliary Power Unit TR: Applicable -6 TOs 2A5X4-006 008 AIRCRAFT FUEL SYSTEMS TR: TO 00-25-172, applicable AFOSH STDs and -2 TOs 2A5X4-006 008.001 Fuel components and system operation 2A5X4-006 008.002 Inspect fuel filters 2A5X4-006 008.002.001 TF-33 TR: 1C-135E-2-4-1 2A5X4-006 008.002.002 F-108 TR: 2J-F-108-2-1 2A5X4-006 008.003 Ground transfer fuel 2A5X4-006 008.003.001 Wing tank transfer 2A5X4-006 008.003.002 Body tank transfer 2A5X4-006 008.004 Refuel aircraft 2A5X4-006 008.004.001 Team member 2A5X4-006 008.004.002 Team panel operator 2A5X4-006 008.004.003 Team supervisor 2A5X4-006 008.005 Defuel aircraft 2A5X4-006 008.005.001 Team member 2A5X4-006 008.005.002 Team panel operator 2A5X4-006 008.005.003 Team supervisor 2A5X4-006 008.006 Prepare aircraft for fuel cell maintenance 2A5X4-006 008.007 In-Flight Refueling (IFR) system 2A5X4-006 008.007.001 IFR receiver system 2A5X4-006 008.007.001.001 Inspect 2A5X4-006 008.007.001.002 Operate 2A5X4-006 009 ELECTRICAL SYSTEMS TR: Applicable -2 TOs 2A5X4-006 009.001 Electrical components and system operation 2A5X4-006 009.002 Switch guards 2A5X4-006 009.003 Perform operational check 2A5X4-006 009.003.002 Lighting system 2A5X4-006 009.003.003 Indicator warning lights 2A5X4-006 009.004 Remove and install 2A5X4-006 009.004.001 Light lenses 2A5X4-006 009.004.002 Light bulbs 2A5X4-006 009.004.003 Batteries 2A5X4-006 009.004.004 Connect/apply and disconnectexternal electrical power 2A5X4-006 010 EGRESS SYSTEM TR: Applicable -2 TOs 2A5X4-006 010.001 Egress components and system operation 2A5X4-006 010.003 Remove/install emergency escape slides (except RC-135) 2A5X4-006 011 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-10-26 2009-10-26 - A - - - - - 2009-10-26 2009-10-26 - 1b - - - - - 2010-04-09 2010-04-12 - 2b - - - - - 2009-10-26 2009-10-26 - A - - - - - - - - - - - - 2012-10-09 2012-10-16 - - - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 5/R 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 7 2010-01-12 2010-01-12 - - - - - - - 5 2009-10-26 2009-10-26 - b - - - - - 5/R 2009-10-26 2009-10-26 - b - - - - - 7/R 2010-01-12 2010-01-12 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - - - - - - - 2009-10-26 2009-10-26 - A - - - - - - A - - - - - 2009-10-26 2009-10-26 - 2b - - - - - 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - - - - - - - 5 2009-10-26 2009-10-26 - 2b - - - - - - 2b - - - - - 2010-04-09 2010-04-12 - A - - - - - 2010-04-09 2010-04-12 - - - - - - - 5 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-82 1. Tasks Knowledge And Technical References AEROSPACE GROUND EQUIPMENT TR: Applicable AFOSH STDs 2A5X4-006 011.001 Perform pre-use inspection and operate 2A5X4-006 011.001.002 Air conditioning units TR: TO 35E9-series as applicable 2A5X4-006 011.001.003 A/M32A-95 Gas turbine compressor TR: TO 35D12-series as applicable 2A5X4-006 011.001.004 Gaseous nitrogen servicing equipment TR: TO 35D3-series as applicable 2A5X4-006 011.001.005 Oil servicing carts TR: TO 35A17-series as applicable 2A5X4-006 011.001.006 Hydraulic servicing carts TR: TO 35A29-series as applicable 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-83 JOB QUALIFICATION STANDARD CONTINUATION/WJQS CRITICAL TASK NUMBER TASKS 35961 002 35961 002.001 35961 002.001.001 35961 002.001.002 35961 003 35961 003.002 35961 003.002.001 35961 003.005 35961 003.006 35961 003.008 35961 003.008.001 35961 003.008.002 35961 003.008.003 35961 003.008.004 35961 003.008.004.001 35961 003.008.004.002 35961 003.008.004.003 35961 003.008.004.004 35961 003.008.004.005 35961 003.008.004.005. 001 35961 003.008.004.005. 002 35961 004 35961 004.002 35961 004.003 35961 004.003.001 35961 005 35961 005.002 35961 005.003 35961 007 35961 007.001 35961 007.002 TASKS, KNOWLEDGE AND TECHNICAL REFERENCES CERTIFICATION START DATE COMPLETION DATE TRAINEE'S TRAINER'S CERTIFIER'S INITIALS INITIALS INITIALS HYDRAULICS 1C-135-2-2(-6,-7,-8-13) SERVICE Aircraft hydraulic system before TCTO-509 2010-04-09 2010-04-12 Aircraft hydraulic system after TCTO-509 2010-04-09 2010-04-12 ENGINES 1C-135(E)C-2-4-1, 1C-135-2-4-1, 1C-135(K)R-2-4JG-2 2J-F108-2-1, 1C-135-2-2 (-4,-10) Inspect F-108 Engine Components TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicableaircraft/ engine TOs Inspect F-108 engine acoustical panels TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicableaircraft/ engine TOs TF-33/P9 engine and subsystems F-108 engine and subsystems PERFORM TF-33 P5/P9 Inlets and exhaust inspection 2012-01-16 2012-01-31 F-108 Inlets and exhaust inspection 2012-01-16 2012-01-31 F-108 JFS operational check 2012-10-09 2012-10-16 TF-33 P5/P9 Engine Oil 2010-04-09 2010-04-12 F-108 Engine oil 2010-04-09 2010-04-12 TF-33 Pnuematic starter 2012-01-16 2012-01-31 F-108 Pnuematic starter 2012-01-16 2012-01-31 F-108 Fuel strainer 2012-01-16 2012-01-31 GUIDANCE AND CONTROL ETM RC-2-11-2, ETM AN/ASN-121, 1C-135-2-9 (-11-2, -11-5) Perform Basic MFD operation REMOVE AND INSTALL INS Battery 2012-09-24 2012-09-27 2010-04-09 2010-04-12 2012-01-16 2012-01-16 2012-01-31 2012-01-31 SERVICE REMOVE AND INSTALL TF-33 fuel strainer 1C-135-2-4-1 ELECT/ENVIROMENTAL 1C-135-2-2 (-3, -7, -10) Perform operational check of mark 2 anti-skid system Perform operational check of mark 3 anti-skid system OPLAN 8010 Alert Requirements ACCI 13-520 para 3.11.4 Perform ADCC Alert Crew requirements: tow team member, refuel team member ACCI 13-501 para 3.11.4 Perform DCC Alert Crew requirements: tow team supervisor, refuel team supervisor, engine run certified, red x orders ACCI 13-501 para 3.11.4 RC-135V, T/N 64-14848, 30 April 2015 T-84 JOURNAL ENTRIES ENTRY SUBJECT DATE 2015-04-13 Conduct Orientation/Initial Evaluation 2015-05-01 Certification To Sign Red X 2015-05-01 CAF Form 64 Submitted 2015-05-01 Certification to Sign Repeat/ Recur 2015-05-01 Certification to Sign NRTS 2015-05-01 Certification to Sign Off CND 2015-05-01 Certification to Sign All Condition Tags 2015-05-01 Certification to Sign NRTS 2015-05-01 Certification to Sign All Condition Tags 2015-05-01 Certification to Sign Off CND 2015-05-01 Certification to Sign Repeat/ Recur 2015-05-01 CAF Form 64 Submitted 2015-05-01 Certification To Sign Red X 2015-04-22 Tasks restored from archive on 2015-04-22 2015-04-22 Role Request 2015-04-22 Tasks restored from archive on 2015-04-22 2015-04-22 Initial Evaluation 2015-04-22 Role Request 2015-04-22 Workcenter Orientation 2015-04-22 Initial Evaluation 2015-04-22 Workcenter Orientation 2009-01-20 Removed start date for task: CFETP2A5X1-001.002.010.008 2009-01-20 Removed start date for task: CFETP2A5X1-001.002.010.010 2009-01-20 Removed start date for task: CFETP2A5X1-001.002.010.008 2009-01-20 Removed start date for task: CFETP2A5X1-001.002.010.010 2009-01-11 Removed start date for task: CFETP2A5X1-001.008.005.002.004 2009-01-11 Removed start date for task: CFETP2A5X1-001.008.005.002.001 2009-01-11 Removed start date for task: CFETP2A5X1-001.008.005.002.004 2009-01-11 Removed start date for task: CFETP- SIGNATURE INFO REMARKS Within 60 days of assignment the Supervisor will conduct a Workcenter Orientation and Initial Evaluation of qualifications IAW AFI 36-2201. I discussed Red X certification with . I interviewed him on a one-to-one basis and we went over the importance of always doing the right thing. I let him know that it will always be integrity first. We discussed how signing off a Red X means taking responsibility for the whole area and NOT just the part being inspected. An expensive aircraft and even more valuable lives depend on him making sure that everything is by the T.O. Guidance in signing of Red X is in 00-20-1 para 4.5. Submitted CAF Form 64. I have verified that he is qualified and signed off on the following tasks: Sign All Condition Tags and NTRS, Clear Red X and IPI, Sign Off CND, and Sign Off Repeat/Recur. I have interviewed on signing off Repeat/Recur. We discussed the guidance of finding how many times he can sign off a Repeat/Recur can be found in AFI 21-101 14.20.1 and the Offutt AFI 21-101 14.20.1.2. The guidance for signing it off can be found in 00-20-1. I have reviewed training records. He is signed off and qualified to be authorized to NRTS Documentation Guidance IAW TO 00-20-3. I have interviewed on signing off CNDs. We discussed the guidance of finding how many times he can sign off a CND can be found in AFI 21-101 14.20.2 and the Offutt AFI 21-101 chapter 14.20.2.4. The guidance for signing it off can be found in 00-20-1. I have reviewed training records. He is signed off and qualified to be authorized to Sign All Condition Tags IAW Documentation Guidance IAW TO 00-20-3 I have reviewed s training records. He is signed off and qualified to be authorized to NRTS Documentation Guidance IAW TO 00-20-3. I have reviewed training records. He is signed off and qualified to be authorized to Sign All Condition Tags IAW Documentation Guidance IAW TO 00-20-3 I have interviewed on signing off CNDs. We discussed the guidance of finding how many times he can sign off a CND can be found in AFI 21-101 14.20.2 and the Offutt AFI 21-101 chapter 14.20.2.4. The guidance for signing it off can be found in 00-20-1. I have interviewed on signing off Repeat/Recur. We discussed the guidance of finding how many times he can sign off a Repeat/Recur can be found in AFI 21-101 14.20.1 and the Offutt AFI 21-101 14.20.1.2. The guidance for signing it off can be found in 00-20-1. Submitted CAF Form 64. I have verified that he is qualified and signed off on the following tasks: Sign All Condition Tags and NTRS, Clear Red X and IPI, Sign Off CND, and Sign Off Repeat/Recur. I discussed Red X certification with . I interviewed him on a one-to-one basis and we went over the importance of always doing the right thing. I let him know that it will always be integrity first. We discussed how signing off a Red X means taking responsibility for the whole area and NOT just the part being inspected. An expensive aircraft and even more valuable lives depend on him making sure that everything is by the T.O. Guidance in signing of Red X is in 00-20-1 para 4.5. 305 Tasks were restored from archive on 2015-04-22 Request the roles Trainee, Trainer, Supervisor 305 Tasks were restored from archive on 2015-04-22 I conducted and documented an initial evaluation of trainee qualifications within 60 days of initial assignment (120 days for ARC), either PCS or PCA work center. Document the evaluation on AF Form 623a or automated version and file in the OJT record. As a minimum the evaluation should include: AFSC, duty position, core and HST, and deployment/UTC requirements. CDC requirements. Note: 30 days per volume. Formal/informal training requirements, such as skills, knowledge, or classroom instruction. Supervisors must evaluate technical school graduates on all tasks taught in the initial skills course as identified in the STS portion of the CFETP. Other local or unique training requirements. Supervisor and trainee responsibilities as outlined in this AFI and other governing directives, such as AFI 36-2101 and the CFETP. Supervisors are encouraged to allow trainees to complete course work during normal duty hours, if mission requirements allow. Supervisors will monitor trainee progress to ensure timely completion of CDCs or ADL course work. Request the roles Trainee, Trainer, Supervisor I conducted and documented work center orientations within 60 days of assignment (120 days for ARC). As a minimum, the orientation should include the following information: What the trainee will be doing. Duty hours and shifts, including periods of rest (non-duty time). Safety requirements found on the AF Form 55, Employee Safety and Health Record. All time and training requirements for upgrade and/or qualification training. Responsibilities of trainee, trainer, task certifier, and supervisor. I conducted and documented an initial evaluation of trainee qualifications within 60 days of initial assignment (120 days for ARC), either PCS or PCA work center. Document the evaluation on AF Form 623a or automated version and file in the OJT record. As a minimum the evaluation should include: AFSC, duty position, core and HST, and deployment/UTC requirements. CDC requirements. Note: 30 days per volume. Formal/informal training requirements, such as skills, knowledge, or classroom instruction. Supervisors must evaluate technical school graduates on all tasks taught in the initial skills course as identified in the STS portion of the CFETP. Other local or unique training requirements. Supervisor and trainee responsibilities as outlined in this AFI and other governing directives, such as AFI 36-2101 and the CFETP. Supervisors are encouraged to allow trainees to complete course work during normal duty hours, if mission requirements allow. Supervisors will monitor trainee progress to ensure timely completion of CDCs or ADL course work. I conducted and documented work center orientations within 60 days of assignment (120 days for ARC). As a minimum, the orientation should include the following information: What the trainee will be doing. Duty hours and shifts, including periods of rest (non-duty time). Safety requirements found on the AF Form 55, Employee Safety and Health Record. All time and training requirements for upgrade and/or qualification training. Responsibilities of trainee, trainer, task certifier, and supervisor. Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-001.002.010.008 (2) Task Description: Deficiency reporting (3) Reason: does not feel confident in getting signed off on This task without having the proper training information. (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-001.002.010.010 (2) Task Description: DD Forms 1574, 1575, 1576, 1577 and 1577-2 (3) Reason: does not feel confident in getting signed off on This task without having the proper training information. (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-001.002.010.008 (2) Task Description: Deficiency reporting (3) Reason: does not feel confident in getting signed off on This task without having the proper training information. (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-001.002.010.010 (2) Task Description: DD Forms 1574, 1575, 1576, 1577 and 1577-2 (3) Reason: does not feel confident in getting signed off on This task without having the proper training information. (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-001.008.005.002.004 (2) Task Description: Anti-ice system (3) Reason: Unable to get on aircraft for hands-on training. (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-001.008.005.002.001 (2) Task Description: Bleed air system (3) Reason: unable to get aircraft for hands-on training. (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-001.008.005.002.004 (2) Task Description: Anti-ice system (3) Reason: Unable to get on aircraft for hands-on training. (4) Removed By Employee: Journal Entry: Training start date was removed/reversed. (1) Task ID: CFETP-2A5X1-001.008.005.002.001 (2) Task Description: Bleed air system (3) Reason: unable to get aircraft for hands-on training. (4) Removed By Employee: RC-135V, T/N 64-14848, 30 April 2015 T-85 JOURNAL ENTRIES ENTRY DATE SUBJECT SIGNATURE INFO REMARKS 2A5X1-001.008.005.002.001 RC-135V, T/N 64-14848, 30 April 2015 T-86 CERTIFICATION I CERTIFY THAT THIS INDIVIDUAL TRAINING RECORD IS CURRENT AS OF 2015-05-04 _____________________________ TRAINEE SIGNATURE _____________________________ SUPERVISOR SIGNATURE RC-135V, T/N 64-14848, 30 April 2015 T-87 1. IDENTIFICATION DATA LAST NAME - FIRST NAME - MIDDLE INITIAL [Crew Chief 3] GRADE/RANK Staff Sergeant DAFSC/JOB SERIES 2A574 INDIVIDUAL TRAINING RECORD INDIVIDUAL'S SIGNATURE DATE 2015-05-04 Individual Training Record RC-135V, T/N 64-14848, 30 April 2015 T-88 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 001 Career Ladder Progression-1 Aug 12 TR: Air Force Enlisted Classification Directory (AFECD) 2A5X1 AND 2A5X4-000 001.001 Progression in career ladder 2A5X1 AND 2A5X4-000 001.002 Duties of AFSC 2A5X1 AND 2A5X4-000 003 AF OCCUPATIONAL SAFETY AND HEALTH (AFOSH) PROGRAM TR: AFIs 11-218, 21-101 and 91-301; applicable AFOSH STDs; TOs 00-25-172, 1-1-691, and applicable aircraft TOs 2A5X1 AND 2A5X4-000 003.001 Housekeeping consistent with safety of personnel and equipment 2A5X1 AND 2A5X4-000 003.002 Safety precautions pertaining to aircraft maintenance 2A5X1 AND 2A5X4-000 003.002.001 Engine air intake and exhaust 2A5X1 AND 2A5X4-000 003.002.002 High intensity sound 2A5X1 AND 2A5X4-000 003.002.003 Turbine, propeller, rotor plane of rotation 2A5X1 AND 2A5X4-000 003.002.004 Radio frequency radiation 2A5X1 AND 2A5X4-000 003.002.005 Ground handling of aircraft 2A5X1 AND 2A5X4-000 003.002.006 Hot brakes 2A5X1 AND 2A5X4-000 003.002.007 Use of tools and equipment 2A5X1 AND 2A5X4-000 003.002.008 Servicing aircraft systems 2A5X1 AND 2A5X4-000 003.002.009 Cleaning Agents 2A5X1 AND 2A5X4-000 003.002.010 Solvents 2A5X1 AND 2A5X4-000 003.002.011 Lubricants 2A5X1 AND 2A5X4-000 003.002.012 High pressure gasses 2A5X1 AND 2A5X4-000 003.002.013 Aircraft explosive equipment 2A5X1 AND 2A5X4-000 003.002.014 Composite materials 2A5X1 AND 2A5X4-000 003.002.015 Maintenance resource management TR: AFI 21-101; AFPAM 90-902 2A5X1 AND 2A5X4-000 003.002.016 Electrostatic hazards, static grounding and bonding TR: TOs 00-25-172 and 00-25-234 2A5X1 AND 2A5X4-000 003.003 Portable ground fire extinguishers TR: AFI 32-2001; TO 00-25-172 2A5X1 AND 2A5X4-000 003.003.001 Perform pre-use inspection 2A5X1 AND 2A5X4-000 003.003.002 Position 2A5X1 AND 2A5X4-000 003.003.003 Operate 2A5X1 AND 2A5X4-000 003.004 Foreign Object Damage (FOD) prevention program 2A5X1 AND 2A5X4-000 003.005 Dropped Object prevention program 2A5X1 AND 2A5X4-000 003.006 Hazardous chemicals TR: AFI 90-821 and applicable AFOSH STDs 2A5X1 AND 2A5X4-000 003.006.001 Use 2A5X1 AND 2A5X4-000 003.006.002 Disposal 2A5X1 AND 2A5X4-000 003.006.003 Hazard communication training program 2A5X1 AND 2A5X4-000 003.006.004 Hazardous material handling procedures 2A5X1 AND 2A5X4-000 003.007 AF Form 1492, Warning Tag TR: TO 00-20-1 2A5X1 AND 2A5X4-000 004 MAINTENANCE DIRECTIVES, REFERENCES, and INSTRUCTIONS TR: AFI 33-360 and TO 00-5 series as applicable 2A5X1 AND 2A5X4-000 004.001 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2007-10-12 2007-10-12 - A - - - - - 2007-10-12 2007-10-12 - A - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2013-03-01 2013-03-21 - A - - - - - 2013-03-01 2013-03-21 - A - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - 1b - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2010-02-08 2010-02-12 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2007-10-12 2007-10-12 - A - - - - - 2007-10-12 2007-10-12 - A B - - - - RC-135V, T/N 64-14848, 30 April 2015 T-89 1. Tasks Knowledge And Technical References TO system 2A5X1 AND 2A5X4-000 004.002 Air Force manuals and instructions 2A5X1 AND 2A5X4-000 004.003 Use technical orders 2A5X1 AND 2A5X4-000 004.004 TO improvement reporting 2A5X1 AND 2A5X4-000 005 SUPERVISION TR: AFIs 21-101, 36-2403, and AFTTP 3-3 2A5X1 AND 2A5X4-000 005.001 Plan work schedules 2A5X1 AND 2A5X4-000 005.002 Schedule maintenance 2A5X1 AND 2A5X4-000 005.003 Supervise personnel accomplishing maintenance 2A5X1 AND 2A5X4-000 005.004 Establish 2A5X1 AND 2A5X4-000 005.004.001 Work methods 2A5X1 AND 2A5X4-000 005.004.002 Work controls 2A5X1 AND 2A5X4-000 005.004.003 Performance standards 2A5X1 AND 2A5X4-000 005.005 Evaluate work performance of subordinate personnel 2A5X1 AND 2A5X4-000 006 TRAINING TR: AFIs 36-2201 and 36-2232 2A5X1 AND 2A5X4-000 006.001 Evaluate personnel for training 2A5X1 AND 2A5X4-000 006.002 Plan and supervise OJT 2A5X1 AND 2A5X4-000 006.003 Counsel trainees on training progress 2A5X1 AND 2A5X4-000 006.005 Document training records 2A5X1 AND 2A5X4-000 006.006 Purpose and use of Career Field Education and Training Plan (CFETP) 2A5X1 AND 2A5X4-000 007 MAINTENANCE MANAGEMENT TR: AFIs 21-101, 21-103, 21-118, 90-201 and AFMAN 23-110 2A5X1 AND 2A5X4-000 007.001 Basic functions within maintenance 2A5X1 AND 2A5X4-000 007.002 Resource management 2A5X1 AND 2A5X4-000 007.003 Personnel management 2A5X1 AND 2A5X4-000 007.004 Maintenance incident investigation and prevention 2A5X1 AND 2A5X4-000 007.005 Determine and report Aircraft Status 2A5X1 AND 2A5X4-000 008 MAINTENANCE DATA DOCUMENTATION (MDD) TR: AFI 21-101; TO 00-20 Series; applicable aircraft -06 Work Unit Code Manuals 2A5X1 AND 2A5X4-000 008.001 MDD Fundamentals 2A5X1 AND 2A5X4-000 008.002 Aircraft and supporting maintenance records 2A5X1 AND 2A5X4-000 008.002.001 Purpose 2A5X1 AND 2A5X4-000 008.002.002 Automated Forms 2A5X1 AND 2A5X4-000 008.002.007 Document other AFTO 781 series forms 2A5X1 AND 2A5X4-000 008.002.008 Document AFTO Form 244/245 2A5X1 AND 2A5X4-000 008.002.009 Document AFTO Form 350 2A5X1 AND 2A5X4-000 008.003 Maintenance Information Systems (MIS) 2A5X1 AND 2A5X4-000 008.003.001 Purpose 2A5X1 AND 2A5X4-000 008.003.002 Job data documentation (JDD) 2A5X1 AND 2A5X4-000 008.003.002.001 Purpose 2A5X1 AND 2A5X4-000 008.003.002.002 Access JDD 2A5X1 AND 2A5X4-000 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - 1b - - - - - 2010-03-16 2010-03-23 - - B - - - - 2010-03-16 2010-03-23 - - - - - - - 2010-03-16 2010-03-23 - - - - - - - 2010-03-16 2010-03-23 - - - - - - - 2010-03-16 2010-03-23 - - - - - - - 2010-03-16 2010-03-23 - - - - - - - 2010-03-16 2010-03-23 - - - - - - - 2010-03-16 2010-03-23 - - - - - - - 2010-03-16 2010-03-23 - - - - - - - 2010-03-16 2010-03-23 - - - - - - - 2010-03-16 2010-03-23 - - - - - - - 2007-10-12 2007-10-12 - - A - - - - 2013-03-01 2013-03-21 - - A - - - - 2007-10-12 2007-10-12 - A B - - - - 2010-03-23 2010-03-30 - - B - - - - 2010-03-23 2010-03-30 - - - - - - - 2010-03-23 2010-03-30 - - - - - - - 2010-03-23 2010-03-30 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A - - - - - 2010-02-01 2010-02-03 - - - - - - - 2007-10-12 2007-10-12 - 1b - - - - - 2007-10-12 2007-10-12 - 1b - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-90 1. Tasks Knowledge And Technical References 008.003.002.003 Create maintenance event 2A5X1 AND 2A5X4-000 008.003.002.004 Defer maintenance event 2A5X1 AND 2A5X4-000 008.003.002.005 Schedule maintenance event 2A5X1 AND 2A5X4-000 008.003.002.006 Close maintenance event 2A5X1 AND 2A5X4-000 008.003.002.007 Use IMDS 2A5X1 AND 2A5X4-000 009 MAINTENANCE MATERIALS/ TOOLS TR:AFI 21-101, TOs 1-1A-8, 1-1A-14, 1-1-691 and 32- series TOs as applicable 2A5X1 AND 2A5X4-000 009.001 Tool control 2A5X1 AND 2A5X4-000 009.002 Select and use special tools 2A5X1 AND 2A5X4-000 009.003 Select/use restraint harness (e.g.; fall protection/prevention equipment) 2A5X1 AND 2A5X4-000 009.005 Hardware 2A5X1 AND 2A5X4-000 009.005.001 Purpose 2A5X1 AND 2A5X4-000 009.005.002 Remove/inspect/install 2A5X1 AND 2A5X4-000 009.006 Electrical connectors 2A5X1 AND 2A5X4-000 009.006.001 Purpose 2A5X1 AND 2A5X4-000 009.006.002 Connect/disconnect 2A5X1 AND 2A5X4-000 009.007 Securing devices 2A5X1 AND 2A5X4-000 009.007.001 Purpose 2A5X1 AND 2A5X4-000 009.007.002 Install/remove safety wire 2A5X1 AND 2A5X4-000 009.007.003 Install/remove cotter pins 2A5X1 AND 2A5X4-000 009.007.004 Safety cable 2A5X1 AND 2A5X4-000 009.008 Lubricants 2A5X1 AND 2A5X4-000 009.009 Sealants 2A5X1 AND 2A5X4-000 009.010 Adhesives 2A5X1 AND 2A5X4-000 009.011 Cleaning agents 2A5X1 AND 2A5X4-000 009.012 Hand tools 2A5X1 AND 2A5X4-000 009.012.001 Purpose 2A5X1 AND 2A5X4-000 009.012.002 Select, inspect and use 2A5X1 AND 2A5X4-000 009.013 Measuring tools 2A5X1 AND 2A5X4-000 009.013.001 Purpose 2A5X1 AND 2A5X4-000 009.013.002 Select and use ruler 2A5X1 AND 2A5X4-000 009.013.003 Select and use thickness gauge 2A5X1 AND 2A5X4-000 009.013.004 Use multi-meter 2A5X1 AND 2A5X4-000 009.013.005 Select, inspect and use torque wrench 2A5X1 AND 2A5X4-000 009.013.006 Select and use micrometer 2A5X1 AND 2A5X4-000 009.013.007 Use depth gauge 2A5X1 AND 2A5X4-000 010 RESPONSIBILITY FOR SUPPLY TR: AFIs 21-101 and 21-118, AFMAN 23-110, TOs 00-20-3 and 00-35D-54 2A5X1 AND 2A5X4-000 010.001 Maintenance supply concept 2A5X1 AND 2A5X4-000 010.003 Special requisition (GPC, Local purchase) 2A5X1 AND 2A5X4-000 010.004 Ordering parts 2A5X1 AND 2A5X4-000 010.006 Prepare repairable and serviceable parts for turn-in 2A5X1 AND 2A5X4-000 010.007 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2013-02-12 2013-02-13 - A B - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2013-03-01 2013-03-21 - A - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2009-11-09 2009-11-13 - 2b - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - 2b - - - - - 2007-10-12 2007-10-12 - A B - - - - 2010-03-23 2010-03-30 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - - B - - - - 2014-08-02 2014-09-02 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-91 1. Tasks Knowledge And Technical References Repair cycle assets 2A5X1 AND 2A5X4-000 010.008 DIFM Control 2A5X1 AND 2A5X4-000 010.009 Local manufacture of parts 2A5X1 AND 2A5X4-000 010.010 Equipment account management 2A5X1 AND 2A5X4-000 010.011 Deficiency reporting 2A5X1 AND 2A5X4-000 010.013 DD Forms 1574, 1575, 1576, 1577 and 1577-2 2A5X1 AND 2A5X4-000 011 AIRCRAFT GENERAL TR: AFI 11-218; applicable AFOSH STDs; TOs 00-20-1, 00-25-172, 1-1-691, 1-1B-50 and applicable aircraft TOs 2A5X1 AND 2A5X4-000 011.001 Weight and balance 2A5X1 AND 2A5X4-000 011.002 Determine weight and balance requirements 2A5X1 AND 2A5X4-000 011.003 Inventory aircraft equipment 2A5X1 AND 2A5X4-000 011.004 Safe aircraft for maintenance 2A5X1 AND 2A5X4-000 011.005 Corrosion control program 2A5X1 AND 2A5X4-000 011.005.001 Aircraft cleaning 2A5X1 AND 2A5X4-000 011.005.002 Corrosion identification 2A5X1 AND 2A5X4-000 011.005.004 Aircraft lubrication 2A5X1 AND 2A5X4-000 011.006 Aircraft inspections 2A5X1 AND 2A5X4-000 011.006.001 Cncepts and Types 2A5X1 AND 2A5X4-000 011.008 Aircraft marshalling signals 2A5X1 AND 2A5X4-000 011.011 Deice aircraft TR: TO 42C-1-2S-2; 14CFR121.629 section 121.629 2A5X1 AND 2A5X4-000 011.012 Debrief aircrews 2A5X1 AND 2A5X4-000 011.013 Aircraft guarded switches 2A5X1 AND 2A5X4-000 011.013.001 Design/function/proper identification 2A5X1 AND 2A5X4-000 011.013.002 Remove and replace covers 2A5X1 AND 2A5X4-000 011.013.003 Operational check 2A5X1 AND 2A5X4-000 012 AIRFRAME TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 012.002 Remove/inspect/install panels 2A5X1 AND 2A5X4-000 012.003 Inspect structural components 2A5X1 AND 2A5X4-000 013 LANDING GEAR TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 013.001 System fundamentals 2A5X1 AND 2A5X4-000 014 UTILITIES TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 014.001 System fundamentals 2A5X1 AND 2A5X4-000 014.001.001 Oxygen 2A5X1 AND 2A5X4-000 014.001.002 Bleed air 2A5X1 AND 2A5X4-000 014.001.003 Pressurization 2A5X1 AND 2A5X4-000 014.001.004 Air conditioning 2A5X1 AND 2A5X4-000 014.001.005 Fire/Overheat warning 2A5X1 AND 2A5X4-000 014.001.006 Fire suppression 2A5X1 AND 2A5X4-000 015 FLIGHT CONTROLS TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 015.001 Fundamentals of flight 2A5X1 AND 2A5X4-000 015.002 Primary flight control fundamentals 2A5X1 AND 2A5X4-000 015.003 Secondary flight control fundamentals 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2010-03-23 2010-03-30 - - B - - - - 2010-03-23 2010-03-30 - - - - - - - 2010-03-23 2010-03-30 - - - - - - - 2010-03-23 2010-03-30 - - B - - - - 2010-03-23 2010-03-30 - - B - - - - 2013-03-01 2013-03-21 - A B - - - - 2010-02-15 2010-02-17 - - - - - - - 2010-02-15 2010-02-17 - - A - - - - 2007-10-12 2007-10-12 - A - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2010-02-15 2010-02-17 - A B - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - - - - - - - 2010-05-10 2010-05-12 - - - - - - - 2007-10-12 2007-10-12 - A - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2013-03-01 2013-03-21 - 1b - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - A B - - - - 2010-02-17 2010-02-19 - A B - - - - 2010-02-17 2010-02-19 - A B - - - - 2010-02-17 2010-02-19 - A B - - - - 2010-02-17 2010-02-19 - A B - - - - 2010-02-17 2010-02-19 - A B - - - - 2013-03-01 2013-03-21 - A B - - - - 2013-03-01 2013-03-21 - A B - - - - 2013-03-01 2013-03-21 - A - - - - - 2013-03-01 2013-03-21 - A - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-92 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 015.004 Component identification 2A5X1 AND 2A5X4-000 016 HYDRAULICS TR: TO 1-1A-8 and applicable aircraft TOs 2A5X1 AND 2A5X4-000 016.001 System fundamentals 2A5X1 AND 2A5X4-000 016.002 Remove/install components TR: TO 1-1A-8, Applicable aircraft TOs 2A5X1 AND 2A5X4-000 016.002.001 Tubing/hoses 2A5X1 AND 2A5X4-000 016.002.002 Fittings 2A5X1 AND 2A5X4-000 016.002.003 Filter elements 2A5X1 AND 2A5X4-000 016.003 Hydraulic Schematics /diagrams 2A5X1 AND 2A5X4-000 017 ENGINES TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 017.001 System fundamentals 2A5X1 AND 2A5X4-000 017.004 Joint Oil Analysis Program 2A5X1 AND 2A5X4-000 018 FUELS TR: TOs 00-25-172, 1-1-3, applicable AFOSH STDs and aircraft TOs 2A5X1 AND 2A5X4-000 018.001 System fundamentals 2A5X1 AND 2A5X4-000 018.002 Classify fuel leaks 2A5X1 AND 2A5X4-000 019 ELECTRICAL TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 019.001 AC Electrical system fundamentals 2A5X1 AND 2A5X4-000 019.002 DC electrical system fundamentals 2A5X1 AND 2A5X4-000 019.007 Electrical schematics/diagrams 2A5X1 AND 2A5X4-000 020 AEROSPACE GROUND EQUIPMENT TR: Applicable AFOSH STDs and TO 35A4 series as applicable 2A5X1 AND 2A5X4-000 020.001 Maintenance stands 2A5X1 AND 2A5X4-000 020.001.001 Purpose and description 2A5X1 AND 2A5X4-000 020.001.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.002 Self-propelled universal platforms 2A5X1 AND 2A5X4-000 020.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.002.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.003 Aircraft jacks TR: TO 35A2- series as applicable 2A5X1 AND 2A5X4-000 020.003.001 Purpose and description 2A5X1 AND 2A5X4-000 020.003.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.005 Oxygen servicing equipment TR: TO 15X-1-1, 37C2-8- as applicable 2A5X1 AND 2A5X4-000 020.005.001 Liquid oxygen (LOX) 2A5X1 AND 2A5X4-000 020.005.001.001 Purpose and description 2A5X1 AND 2A5X4-000 020.005.001.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.005.002 Gaseous oxygen (GOX) 2A5X1 AND 2A5X4-000 020.005.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.005.002.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.006 Diesel driven air compressors TR: TO 34Y1- series as applicable 2A5X1 AND 2A5X4-000 020.006.001 Purpose and description 2A5X1 AND 2A5X4-000 020.006.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.007 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2010-03-01 2010-03-03 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - A - - - - - 2010-03-23 2010-03-30 - A B - - - - 2010-03-23 2010-03-30 - - - - - - - 2010-03-23 2010-03-30 - - - - - - - 2013-08-23 2013-09-26 - - - - - - - 2010-03-23 2010-03-30 - A - - - - - 2013-03-01 2013-03-21 - A B - - - - 2009-05-12 2009-05-13 - - B - - - - 2013-03-01 2013-03-21 - A B - - - - 2007-10-12 2007-10-12 - A - - - - - 2010-03-30 2010-04-06 - A B - - - - 2010-03-30 2010-04-06 - A B - - - - 2010-03-30 2010-04-06 - A - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2013-03-01 2013-03-21 - A B - - - - 2013-03-01 2013-03-21 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-93 1. Tasks Knowledge And Technical References Ground heaters TR: 35E7- series as applicable 2A5X1 AND 2A5X4-000 020.007.001 Purpose and description 2A5X1 AND 2A5X4-000 020.007.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.008 Lighting equipment TR: TO 35F5- series as applicable 2A5X1 AND 2A5X4-000 020.008.001 Purpose and description 2A5X1 AND 2A5X4-000 020.008.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.010 Air conditioning units TR: TO 35E9- Series as applicable 2A5X1 AND 2A5X4-000 020.010.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011 Ground generator sets/gas turbine compressors 2A5X1 AND 2A5X4-000 020.011.002 A/M32A-95 Gas turbine compressors TR: TO 35D12-series as applicable 2A5X1 AND 2A5X4-000 020.011.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011.003 Diesel driven generator sets TR: TO 35C2- series as applicable 2A5X1 AND 2A5X4-000 020.011.003.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011.003.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.012 Tow bar TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 020.012.001 Perform pre-use inspection 2A5X1 AND 2A5X4-000 020.012.002 Connect/disconnect 2A5X1 AND 2A5X4-000 020.013 Tow vehicles TR: TO 36A10 series as applicable 2A5X1 AND 2A5X4-000 020.013.001 Purpose and description 2A5X1 AND 2A5X4-000 020.013.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.014 Self-generating nitrogen equipment TR: TO 35D29-7-6-1 2A5X1 AND 2A5X4-000 020.014.001 Purpose and description 2A5X1 AND 2A5X4-000 020.014.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.015 Gaseous nitrogen servicing equipment TR: TO 35D3- series as applicable 2A5X1 AND 2A5X4-000 020.015.001 Purpose and description 2A5X1 AND 2A5X4-000 020.016 Engine stands and dollies TR: 35D3- series as applicable 2A5X1 AND 2A5X4-000 020.016.001 Purpose and description 2A5X1 AND 2A5X4-000 020.016.002 Perform pre-use inspection and operate 2A5X4-006 001 C-135 QUALITATIVE REQUIREMENTS AIRCRAFT GENERAL 2A5X4-006 001.001 Periodic/Isochronal inspection concept and inspection TR: TOs 00-20 series, Applicable -6 TOs 2A5X4-006 001.001.001 Periodic/Isochronal inspection concept 2A5X4-006 001.001.002 Perform inspections 2A5X4-006 001.001.002.001 Preflight 2A5X4-006 001.001.002.002 Alert 5A 2A5X4-006 001.001.002.003 Alert 5B 2A5X4-006 001.001.002.004 Thruflight 2A5X4-006 001.001.002.005 Quick Turn 2A5X4-006 001.001.002.006 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 5 7 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2013-03-01 2013-03-21 - - B - - - - 2013-03-01 2013-03-21 - - - - - - - 2007-10-12 2007-10-12 - A B - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - A B - - - - 2009-05-12 2009-05-13 - - A - - - - 2009-05-12 2009-05-13 - - - - - - - 2007-10-12 2007-10-12 - A - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2009-05-12 2009-05-13 - 2b - - - - - 2009-05-12 2009-05-13 - - - - - - - 2010-01-12 2010-01-12 - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-94 1. Tasks Knowledge And Technical References Hourly Post 2A5X4-006 001.001.002.009 Calendar 2A5X4-006 001.001.002.010 Special 2A5X4-006 001.001.002.011 900 Hr Insp 2A5X4-006 001.001.002.012 Time change item 2A5X4-006 001.001.002.013 Exterior panel/secondary structure inspection 2A5X4-006 001.002 Aircraft communications equipment TR: Applicable -2 TOs 2A5X4-006 001.002.001 Operate radio 2A5X4-006 001.002.002 Use interphone 2A5X4-006 001.003 Perform ground handling TR: AFI 11-218, TO 00-25-172, applicable AFOSH STDs, applicable -1 and -2 TOs 2A5X4-006 001.003.001 Aircraft launch 2A5X4-006 001.003.002 Call flight controls 2A5X4-006 001.003.003 Aircraft recovery 2A5X4-006 001.003.004 Tow aircraft 2A5X4-006 001.003.004.001 Wing/tail walker 2A5X4-006 001.003.004.002 Brake operator 2A5X4-006 001.003.004.003 Tow team supervisor 2A5X4-006 001.003.004.004 Tow vehicle operator 2A5X4-006 001.003.005 Jack and level aircraft 2A5X4-006 001.003.005.001 Jacking team member 2A5X4-006 001.003.005.005 Axle jacking 2A5X4-006 001.004 Compute center of gravity TR: Applicable aircraft -5 TOs 2A5X4-006 001.005 Install/remove ground safety devices TR: Applicable -2 TOs 2A5X4-006 001.005.001 Landing gear 2A5X4-006 001.005.002 Landing gear doors 2A5X4-006 001.006 Ground aircraft 2A5X4-006 001.007 Configure/reconfigure aircraft 2A5X4-006 001.007.002 Passenger/personnel 2A5X4-006 001.008 Maintain/store/configure/-21 equipment 2A5X4-006 001.010 Aircraft wash TR: TO - 6WC-3 2A5X4-006 001.010.001 Team member 2A5X4-006 001.010.002 Team supervisor 2A5X4-006 001.010.003 Post wash lube 2A5X4-006 001.011 Maintenance directives, references, & instructions TR: AFI 37-101 Vol 1 and TO 00-5-1 2A5X4-006 001.011.001 Use C-135 technical orders 2A5X4-006 001.012 Maintenance Data Documentation (MDD TR: AFI 21-101, TOs 00-20-1, 00-20-2, and applicable aircraft -06 Work Unit Code Manuals 2A5X4-006 001.012.001 Document AFTO Form 781H 2A5X4-006 001.012.002 Document AFTO Form 781A 2A5X4-006 001.012.003 Document AFTO Form 781J 2A5X4-006 001.012.004 Document AFTO Form 781K 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2010-03-30 2010-04-06 - - - - - - - 2010-03-30 2010-04-06 - - - - - - - 2010-03-30 2010-04-06 - - - - - - - 2010-03-30 2010-04-06 - - - - - - - 7 2010-03-30 2010-04-06 - - - - - - - 5 2009-05-12 2009-05-13 - - - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 5 2010-01-12 2010-01-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 7 2010-03-30 2010-04-06 - - - - - - - 2008-08-11 2008-08-20 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 2009-05-12 2009-05-13 - - - - - - - 2010-03-30 2010-04-06 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2010-03-30 2010-04-06 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 5 2013-02-12 2013-02-13 - 3c - - - - - 5 2013-02-12 2013-02-13 - 3c - - - - - 5 2013-02-12 2013-02-13 - 3c - - - - - 5 2013-02-12 2013-02-13 - 3c - - - - - 5 2013-02-12 2013-02-13 - 3c - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-95 1. Tasks Knowledge And Technical References 2A5X4-006 002 AIRFRAME SYSTEMS TR: Applicable -2 TOs 2A5X4-006 002.001 Airframe components and structure 2A5X4-006 002.002 Service cargo door reservoir 2A5X4-006 002.003 Operate 2A5X4-006 002.003.001 Crew entry door 2A5X4-006 002.003.002 Cargo door 2A5X4-006 002.003.003 Emergency exit hatch 2A5X4-006 002.003.004 Wheel well doors 2A5X4-006 002.004 Open and close 2A5X4-006 002.004.001 Cowling (F-108) 2A5X4-006 002.004.002 Cowling (TF-33) 2A5X4-006 002.004.003 Panels/doors 2A5X4-006 002.004.004 Windows 2A5X4-006 002.005 Remove and install 2A5X4-006 002.005.001 Cowling (F-108) 2A5X4-006 002.005.002 Cowling (TF-33) 2A5X4-006 002.005.003 Panels/doors 2A5X4-006 002.005.004 Non-explosive seats 2A5X4-006 002.005.005 Windows 2A5X4-006 002.005.007 Radomes 2A5X4-006 002.005.008 Door/hatch seals 2A5X4-006 002.005.009 Thermal curtains 2A5X4-006 002.005.013 Tail cone 2A5X4-006 002.006 Perform aircraft inclement weather procedures 2A5X4-006 002.007 Inspect crew/passenger comfort facilities TR: Applicable -6 TOs 2A5X4-006 002.008 Service crew/passenger comfort facilities 2A5X4-006 003 LANDING GEAR SYSTEMS TR: Applicable -2 TOs 2A5X4-006 003.001 Landing gear components and system operation 2A5X4-006 003.002 Troubleshoot 2A5X4-006 003.003 Operate 2A5X4-006 003.003.001 Landing gear 2A5X4-006 003.003.002 Brakes 2A5X4-006 003.003.003 Steering system 2A5X4-006 003.003.004 Anti skid system 2A5X4-006 003.004 Service 2A5X4-006 003.004.001 Snubber 2A5X4-006 003.004.002 Centering cylinder 2A5X4-006 003.004.003 Landing gear struts 2A5X4-006 003.004.003.001 Deflate 2A5X4-006 003.004.003.002 Drain 2A5X4-006 003.004.003.003 Fill 2A5X4-006 003.004.003.004 Inflate 2A5X4-006 003.004.004 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2010-03-30 2010-04-06 - A - - - - - 2013-03-01 2013-03-21 - b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - 2b/b - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - A - - - - - 2010-04-06 2010-04-13 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2009-05-12 2009-05-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 2013-08-23 2013-09-26 5 2009-05-12 2009-05-13 - - - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-96 1. Tasks Knowledge And Technical References Tires 2A5X4-006 003.006 Remove and Install 2A5X4-006 003.006.001 Snubbers 2A5X4-006 003.006.002 Centering cylinder 2A5X4-006 003.006.003 Wheel and tire assemblies 2A5X4-006 003.006.003.001 Nose 2A5X4-006 003.006.003.002 Main 2A5X4-006 003.006.004 Anti-skid transducer 2A5X4-006 003.006.005 Carbon brake assemblies 2A5X4-006 003.006.006 Bleed brake assembly (carbon) 2A5X4-006 003.007 Determine serviceability of aircraft tires TR: TO 4T-1-3 2A5X4-006 004 UTILITY SYSTEMS TR: TO 00-25-172, Applicable -2 TOs 2A5X4-006 004.001 Utility components and system operation 2A5X4-006 004.002 Troubleshoot 2A5X4-006 004.003 Operate 2A5X4-006 004.003.001 Bleed air system 2A5X4-006 004.003.002 Air conditioning system 2A5X4-006 004.003.003 Pressurization system 2A5X4-006 004.003.004 Anti-ice system 2A5X4-006 004.003.005 Fire/overheat warning system 2A5X4-006 004.003.006 Fire extinguishing system 2A5X4-006 004.003.007 Oxygen system 2A5X4-006 004.004 Oxygen system TR: Applicable -2, -3 TOs 2A5X4-006 004.004.001 Service gaseous oxygen 2A5X4-006 004.004.002 Service liquid oxygen 2A5X4-006 004.005 Inspect TR: Applicable -6 TOs 2A5X4-006 004.005.001 Bleed air system 2A5X4-006 004.005.002 Air conditioning system 2A5X4-006 004.005.003 Pressurization system 2A5X4-006 004.005.004 Anti-ice system 2A5X4-006 004.005.005 Fire/overheat warning system 2A5X4-006 004.005.006 Fire extinguisher system 2A5X4-006 004.005.007 Oxygen system 2A5X4-006 004.006 Air Cycle Machine (ACM) 2A5X4-006 004.006.001 Drain 2A5X4-006 004.006.002 Service 2A5X4-006 005 FLIGHT CONTROL SYSTEM TR: Applicable -2 TOs 2A5X4-006 005.001 Flight control components and system operation 2A5X4-006 005.002 Troubleshoot 2A5X4-006 005.003 Operate flight controls 2A5X4-006 005.003.001 Aileron system 2A5X4-006 005.003.002 Rudder system 2A5X4-006 005.003.003 Elevator system 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2009-11-09 2009-11-13 - - - - - - - 2009-11-09 2009-11-13 - - - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2009-05-12 2009-05-13 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - A - - - - - 2013-08-23 2013-09-26 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 2007-10-12 2007-10-12 - A - - - - - 2010-04-06 2010-04-13 - - - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T-97 1. Tasks Knowledge And Technical References 2A5X4-006 005.003.004 Spoiler/Speed brake system 2A5X4-006 005.003.005 Stabilizer trim system 2A5X4-006 005.003.006 Flap system 2A5X4-006 005.004 Remove/install 2A5X4-006 005.004.001 Cove lip door 2A5X4-006 005.004.002 Cove lip door latch 2A5X4-006 005.004.005 Fore flap 2A5X4-006 005.004.006 Aileron snubber 2A5X4-006 005.004.007 Elevator snubber 2A5X4-006 005.004.013 Leading edge flaps 2A5X4-006 005.006 Service gearbox 2A5X4-006 006 HYDRAULIC SYSTEMS TR: Applicable -2 TOs 2A5X4-006 006.001 Hydraulic components and system operation 2A5X4-006 006.002 Troubleshoot 2A5X4-006 006.003 Service hydraulic system 2A5X4-006 006.003.001 Reservoir 2A5X4-006 006.003.002 Accumulator 2A5X4-006 006.003.003 Drain reservoir 2A5X4-006 006.004 Operate 2A5X4-006 006.004.001 Engine driven pump 2A5X4-006 006.004.002 Non-engine driven pump 2A5X4-006 006.005 Remove and install accumulator 2A5X4-006 007 ENGINES TR: AFI 11-218, applicable AFOSH STDs and -2 TOs 2A5X4-006 007.001 Engine and Auxiliary Power Unit (APU) components and system operation 2A5X4-006 007.003 Perform 2A5X4-006 007.003.001 Engine operational check 2A5X4-006 007.003.004 Engine motor wet 2A5X4-006 007.003.005 Engine motor dry 2A5X4-006 007.003.006 Audible ignition check 2A5X4-006 007.003.007 Alternate engine start 2A5X4-006 007.004 Operate 2A5X4-006 007.004.001 Engine and subsystems 2A5X4-006 007.005 Service 2A5X4-006 007.005.001 Oil system 2A5X4-006 007.005.002 Constant Speed Drive (CSD)/Integrated Drive Generator (IDG) 2A5X4-006 007.005.003 Gear box 2A5X4-006 007.005.004 Auxiliary Power Unit (if equipped) 2A5X4-006 007.006 Remove and install 2A5X4-006 007.006.001 Starter 2A5X4-006 007.006.002 Starter cartridge 2A5X4-006 007.007 Take engine oil sample TR: TO 42B2-1-9, 33-1-37 2A5X4-006 007.008 Chip detectors 2A5X4-006 007.009 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2007-10-12 2007-10-12 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - 2b - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2009-11-09 2009-11-13 - - - - - - - 2009-11-09 2009-11-13 - - - - - - - 2014-08-02 2014-09-02 - - - - - - - 2013-08-23 2013-09-26 - - - - - - - 2013-08-23 2013-09-26 - - - - - - - 2013-08-23 2013-09-26 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2007-10-12 2007-10-12 - A - - - - - 2010-04-06 2010-04-13 - - - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 2010-04-06 2010-04-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2010-04-06 2010-04-13 - - - - - - - 2007-10-12 2007-10-12 - A - - - - - 2008-10-01 2008-10-20 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2009-05-12 2009-05-13 - - - - - - - 2013-10-01 2013-11-01 - - - - - - - 2013-10-01 2013-11-01 - - - - - - - 2010-01-12 2010-01-12 - b - - - - - 2007-10-12 2007-10-12 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2013-10-01 2013-11-01 - - - - - - - 2010-04-06 2010-04-13 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - A - - - - - 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-98 1. Tasks Knowledge And Technical References Inspect installed engine TR: Applicable -6 TOs 2A5X4-006 007.009.001 Turbine 2A5X4-006 007.010 Inspect Auxiliary Power Unit TR: Applicable -6 TOs 2A5X4-006 008 AIRCRAFT FUEL SYSTEMS TR: TO 00-25-172, applicable AFOSH STDs and -2 TOs 2A5X4-006 008.001 Fuel components and system operation 2A5X4-006 008.002 Inspect fuel filters 2A5X4-006 008.002.001 TF-33 TR: 1C-135E-2-4-1 2A5X4-006 008.002.002 F-108 TR: 2J-F-108-2-1 2A5X4-006 008.003 Ground transfer fuel 2A5X4-006 008.003.001 Wing tank transfer 2A5X4-006 008.003.002 Body tank transfer 2A5X4-006 008.004 Refuel aircraft 2A5X4-006 008.004.001 Team member 2A5X4-006 008.004.002 Team panel operator 2A5X4-006 008.004.003 Team supervisor 2A5X4-006 008.005 Defuel aircraft 2A5X4-006 008.005.001 Team member 2A5X4-006 008.005.002 Team panel operator 2A5X4-006 008.005.003 Team supervisor 2A5X4-006 008.006 Prepare aircraft for fuel cell maintenance 2A5X4-006 008.007 In-Flight Refueling (IFR) system 2A5X4-006 008.007.001 IFR receiver system 2A5X4-006 008.007.001.001 Inspect 2A5X4-006 008.007.001.002 Operate 2A5X4-006 009 ELECTRICAL SYSTEMS TR: Applicable -2 TOs 2A5X4-006 009.001 Electrical components and system operation 2A5X4-006 009.002 Switch guards 2A5X4-006 009.003 Perform operational check 2A5X4-006 009.003.002 Lighting system 2A5X4-006 009.003.003 Indicator warning lights 2A5X4-006 009.004 Remove and install 2A5X4-006 009.004.001 Light lenses 2A5X4-006 009.004.002 Light bulbs 2A5X4-006 009.004.003 Batteries 2A5X4-006 009.004.004 Connect/apply and disconnectexternal electrical power 2A5X4-006 010 EGRESS SYSTEM TR: Applicable -2 TOs 2A5X4-006 010.001 Egress components and system operation 2A5X4-006 010.003 Remove/install emergency escape slides (except RC-135) 2A5X4-006 011 AEROSPACE GROUND EQUIPMENT TR: Applicable AFOSH STDs 2A5X4-006 011.001 Perform pre-use inspection and operate 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2007-10-12 2007-10-12 - 1b - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - A - - - - - 2013-10-01 2013-11-01 - - - - - - - 2013-10-01 2013-11-01 - - - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 5/R 2007-10-12 2007-10-12 - - - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 7 2010-01-12 2010-01-12 - - - - - - - 5 2007-10-12 2007-10-12 - b - - - - - 5/R 2007-10-12 2007-10-12 - b - - - - - 7/R 2010-01-12 2010-01-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - - - - - - - 2007-10-12 2007-10-12 - A - - - - - 2010-01-12 2010-01-12 - A - - - - - 2007-10-12 2007-10-12 - 2b - - - - - 2007-10-12 2007-10-12 - - - - - - - 5 2007-10-12 2007-10-12 - - - - - - - 5 2007-10-12 2007-10-12 - - - - - - - 5 2007-10-12 2007-10-12 - 2b - - - - - 5 2013-02-12 2013-02-13 - 2b - - - - - 2007-10-12 2007-10-12 - A - - - - - 2007-10-12 2007-10-12 - - - - - - - 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-99 1. Tasks Knowledge And Technical References 2A5X4-006 011.001.002 Air conditioning units TR: TO 35E9-series as applicable 2A5X4-006 011.001.003 A/M32A-95 Gas turbine compressor TR: TO 35D12-series as applicable 2A5X4-006 011.001.004 Gaseous nitrogen servicing equipment TR: TO 35D3-series as applicable 2A5X4-006 011.001.005 Oil servicing carts TR: TO 35A17-series as applicable 2A5X4-006 011.001.006 Hydraulic servicing carts TR: TO 35A29-series as applicable 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2013-03-01 2013-03-21 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-100 JOB QUALIFICATION STANDARD CONTINUATION/WJQS CRITICAL TASK NUMBER TASKS 35961 002 35961 002.001 35961 002.001.001 35961 002.001.002 35961 002.001.003 35961 002.001.003.001 35961 002.001.003.001. 001 35961 003 35961 003.002 35961 003.002.001 35961 003.004 35961 003.005 35961 003.006 35961 003.008 35961 003.008.001 35961 003.008.002 35961 003.008.003 35961 003.008.004 35961 003.008.004.001 35961 003.008.004.002 35961 003.008.004.003 35961 003.008.004.004 35961 003.008.004.005 35961 003.008.004.005. 001 35961 003.008.004.005. 002 35961 004 35961 004.001 35961 004.002 35961 004.003 35961 004.003.001 35961 005 35961 005.002 35961 005.003 35961 006 35961 006.005 35961 006.006 35961 007 35961 007.001 35961 007.002 TASKS, KNOWLEDGE AND TECHNICAL REFERENCES CERTIFICATION START DATE COMPLETION DATE TRAINEE'S TRAINER'S CERTIFIER'S INITIALS INITIALS INITIALS HYDRAULICS 1C-135-2-2(-6,-7,-8-13) SERVICE Aircraft hydraulic system before TCTO-509 2007-10-09 2007-10-17 Aircraft hydraulic system after TCTO-509 2007-10-09 2007-10-17 2010-04-20 2010-04-27 2013-10-01 2013-11-01 2008-10-01 2009-05-12 2009-07-24 2008-10-08 2009-05-13 2009-08-05 2008-10-01 2008-10-16 F-108 Inlets and exhaust inspection 2008-10-01 2008-10-16 F-108 JFS operational check 2010-04-20 2010-04-27 TF-33 P5/P9 Engine Oil 2007-10-09 2007-10-17 F-108 Engine oil 2007-10-09 2007-10-17 TF-33 Pnuematic starter 2010-04-13 2010-04-27 F-108 Pnuematic starter 2010-04-13 2010-04-27 TF-33 fuel strainer 1C-135-2-4-1 2010-04-13 2010-04-27 F-108 Fuel strainer 2009-05-12 2009-05-13 GUIDANCE AND CONTROL ETM RC-2-11-2, ETM AN/ASN-121, 1C-135-2-9 (-11-2, -11-5) Apply range and slip markings Perform Basic MFD operation REMOVE AND INSTALL INS Battery 2009-05-12 2007-10-09 2009-05-13 2007-10-17 2010-04-13 2010-04-27 2009-05-12 2009-05-12 2009-05-13 2009-05-13 2009-11-09 2009-12-10 2009-12-09 2010-01-09 2014-01-20 2014-01-27 2014-01-20 2014-01-27 REMOVE AND INSTALL OPERATE LANDING GEAR Position B ENGINES 1C-135(E)C-2-4-1, 1C-135-2-4-1, 1C-135(K)R-2-4JG-2 2J-F108-2-1, 1C-135-2-2 (-4,-10) Inspect F-108 Engine Components TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicableaircraft/ engine TOs Inspect F-108 engine acoustical panels TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicableaircraft/ engine TOs TF-33/P5 engine and subsystems TF-33/P9 engine and subsystems F-108 engine and subsystems PERFORM TF-33 P5/P9 Inlets and exhaust inspection SERVICE REMOVE AND INSTALL ELECT/ENVIROMENTAL 1C-135-2-2 (-3, -7, -10) Perform operational check of mark 2 anti-skid system Perform operational check of mark 3 anti-skid system CDC Volume Progression 7 Level CDC Vol 1 AFI 36-2201 7 Level CDC Vol 2 AFI 36-2201 OPLAN 8010 Alert Requirements ACCI 13-520 para 3.11.4 Perform ADCC Alert Crew requirements: tow team member, refuel team member ACCI 13-501 para 3.11.4 Perform DCC Alert Crew requirements: tow team supervisor, refuel team supervisor, engine run certified, red x orders ACCI 13-501 para 3.11.4 RC-135V, T/N 64-14848, 30 April 2015 T-101 JOURNAL ENTRIES ENTRY SUBJECT DATE 2015-03-11 APU CERTIFIER SIGNATURE INFO REMARKS HAS BEEN BRIEFED ON THE IMPORTANCE OF BEING AN APU CERTIFIER AND ALL THAT IS REQUIRED OF HIM. 2014-07-15 90 Day Review I reviewed 2014-03-24 90 day review I have reviewed records for completeness and accuracy. No discrepancies noted on this date. 2013-12-06 90 day review I have reviewed records for completeness and accuracy. No discrepancies noted on this date. 2013-08-19 quarterly review I have reviewed s TBA today and he has 18 tasks that need start dates loaded. He was previously signed off on these tasks, but due to the swap over to 2A5X4 these items were not signed off. I have spoken to about getting these tasks signed off and told him they need to be completed by 15 September 2013. All other items are up to date. 2013-08-15 workcenter orientation A workcenter orientation was previously completed but was not documented correctly. A workcenter orientation was conducted with on 20071101. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. I reviewed #s TBA entries today for accuracy and completion. There were no errors noted on this date. 2013-06-10 90 day review #s TBA entries today for accuracy and completion. There were no errors noted on this date. 2013-02-20 supervisor change I will be deploying soon leaving 4 March 2013 with an estimated return date of 15 June 2013. In my absence will be assuming supervisory duties for individuals I supervise. is currently a fully qualified 7 skill level and only requires quarterly journal entries. 2013-01-03 1/4 journal entry I have reviewed #s TBA today and all tasks are up to date. He continues to transfer into a technical expert in his career field and impresses me in his task knowledge. This NCO is an asset to the greatest Air Force in the World; I am proud to be his supervisor. 2012-10-12 90 Day TBA Review I reviewed TBA entries today for accuracy and completion. This review supersedes previous reviews. All records are accurate and current at this time. 2012-07-25 90 day TBA review/overdue review I reviewed TBA entries today for accuracy and completion. 90 Day review was missed in the Month of June. This review supersedes previous reviews. All records are accurate and current at this time. 2012-06-14 F108 comp review i have completed a comprehensive review of F108 eng run with P12 and recommend him for his test 2012-06-14 F-108 Eng run Pretests 2012-06-14 F108 comp review 2012-06-08 P-5 Eng run pretest has completed three pretests with the scores of 96%, 96% and 100% and is ready for the cert test i have completed a comprehensive review of F108 eng run with P12 and recommend him for his test took 5ea pretests and scored 100% on EA test. Also scored 100% on actual eng run test 2012-03-30 Quarterly Review I have reviewed s TBA today and everything looks great. He continues to become more proficient at his daily tasks. I will be departing the local area in a couple of days for a TDY and will report to for any supervisory questions he may have. This write-in is for the purpose of #s quarterly review and for me going TDY. 2012-02-27 returned from TDY I have just returned from the NCOA and I am resuming the position of supervisor of my subordinates. I will also be conducting an initial feedback in the very near future. 2012-01-25 B-Series Maintenance Stand Safety Brief Air Force Safety Center has identified a discrepancy with all B-series maintenance stands. These stands do not have proper fall protection IAW regulation , 29 CFR 1910.23(a)(2). Fall hazard exists when using B-series stands (i.e. open area at b-5 stand ladder/platform access point and b-4 step/platform access point). The individual has been briefed and is aware of the risks when using all B series maintenance stands. Today I performed TBA records quarterly review. All of his records are accurate and up to date. He remains a fully qualified 7 level. I will be TDY starting 5 January 2012 until 21 February 2012. does not require a temporary supervisor. 2012-01-03 Quarterly review 2011-11-23 Intial Eval. 2011-11-02 Records Review I conducted an initial evaluation with today. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he was briefed that his training is ultimately his responsibility, and he needs to ensure he reviews his training records at least once a week and actively pursues the training he needs to complete his upgrade. He has also been briefed that tasks should be signed off within 30 days of the start date, unless mission requirements prohibit the completion of the task within that time. Records Review C/W. is 100% completed with 5/7-Level tasks. 2011-09-27 90 Day Records Review Records Review C/W. is 100% completed with 5/7-Level tasks. 2011-09-07 Records Review Records Review C/W. is 100% completed with 5/7-Level tasks. 2011-07-20 Inital Eval/Orientation An initial evaluation has been conducted with on 20071102. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he was briefed that his training is ultimately his responsibility, and he needs to ensure he reviews his training records at least once a week and actively pursues the training he needs to complete his upgrade. He has also been briefed that tasks should be signed off within 30 days of the start date, unless mission requirements prohibit the completion of the task within that time A workcenter orientation was conducted with on 20071102. Items covered include chain of command, duty locations RC-135V, T/N 64-14848, 30 April 2015 T-102 JOURNAL ENTRIES ENTRY DATE SUBJECT SIGNATURE INFO REMARKS 2011-06-23 Records Review and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. Records Review C/W. is 100% completed with 5/7-Level tasks. 2011-05-08 Records Review Records Review C/W. 2011-04-14 90 Day review/ missed reviews I reviewed TBA entries today for accuracy and completion. 1 task was added to reflect MTP skill level requirements. Two 90-day reviews were missed from Sep'10-Apr '11. No other defects were noted. This review supersedes previous reviews. All items current and accurate. Another review will be conducted in 90 days IAW OI 36-01. 2011-03-30 APU Operation Qual 2010-09-27 Leave from 20100929-20101007 is 99% completed with 5/7-Level tasks. He knows what tasks he needs to focus on. has been qualified on C135 APU operation on 20 Feb 2011. will be going on leave from 20100929 thru 20101007 2010-09-14 Fomr 64 Brief Tow Super 3269 I interviewed on the responsibilities associated with being a Tow Team Supervisor. He is well aware that acft tow actions START & STOP under his command and IAW T.O. 1C-135-2-2CL-1. 2010-09-08 Red X Form 64 Brief 2704 I interviewed on his responsibilities as a 7-Level (Red X Certifier). He has proven his ability to take on This critical responsibility and has made it apparent he intends to comply with all standards required of him as a 7-Level Aerospace Maintenance Craftsman. (Guidance for the for signing off the Red X is listed in T.O. 00-20-1 para 4.5) 5102 I interviewed about the importance of an IPI and Clearing an IPI. I reminded him that an IPI is what it means, an In Progress Inspection, meaning that you do it while the task is in work and will be signed off at the job site. We also discussed the importance of the documentation of the IPI in the forms ( IAW 00-20-1 3.5.2 & AFI 21-101 14.20.3). I reminded him that an IPI is a Red X and the integrity must be the same as any other task, if not more important. 2110 I have interviewed on Cannot Duplicate (CND) corrective actions. We discussed what AFIs govern the CNDs (AFI 21-101 14.20.2 and the Offutt AFI 21-101 chapter 14.20.2.4). (The guidance for signing it off can be found in 00-20-1) 2111 I have interviewed on signing off Repeat/Recur. We discussed the guidance of finding how many times he can sign off a Repeat/Recur can be found in AFI 21-101 14.20.1 and the Offutt AFI 21-101 14.20.1.2. (The guidance for signing it off can be found in 00-20-1) 2099 I have reviewed training records and I verify that he is signed off and qualified to sign all NRTS Tags IAW T.O. 00-20-3 Documentation Guidance. 2093 I have reviewed training records and I verify that he is signed off and qualified to be sign all Condition Tags IAW T.O. 00-20-3 Documentation Guidance. Member has met all mandatory training requirements IAW AFI 36-2201 for award of his/her next higher skill level. MILPDS, IMDS, and TBA has been updated. 2010-09-07 7 Level Upgrade 2010-09-01 Entry Entered In Error The last entry for Skill level upgrade was entered in error the appropriate entry has been made. 2010-09-01 Skill Level Upgrade has completed all tasks required for his upgrade to 7-Level 2A571L as well as all volumes of his CDCs completed. He has been briefed on the expectations placed on him and the responsibilities he is to uphold. I reccomend he be upgraded at This time. has completed all tasks required for his upgrade to 7-Level 2A571L as well as all volumes of his CDCs completed. He has been briefed on the expectations placed on him and the responsibilities he is to uphold. I reccomend he be upgraded at This time. has completed all tasks required for his upgrade to 7-Level 2A571L as well as all volumes of his CDCs completed. He has been briefed on the expectations placed on him and the responsibilities he is to uphold. I reccomend he be upgraded at This time. The last entry for Skill level upgrade was entered in error the appropriate entry has been made. 2010-09-01 Skill Level Upgrade 2010-09-01 Skill Level Upgrade 2010-09-01 Entry Entered In Error 2010-09-01 Skill Level Upgrade 2010-08-27 TBA Review C/W has completed all tasks required for his upgrade to 7-Level 2A571L as well as all volumes of his CDCs completed. He has been briefed on the expectations placed on him and the responsibilities he is to uphold. I reccomend he be upgraded at This time. TBA review c/w keep up the good work 2010-07-14 30-Day Review 30-day review not completed since May records are up to date and review C/W at This time 2010-05-11 Review 30-day records check C/W 2010-04-15 Comprehensive Review C/W has completed a comprehensive review of his 7-level CDCs. His knowledge of This material was mind blowing. I personally believe he is 100% ready to take his EOC test. 2010-03-26 Pretest completed another pretest with a 97% 2010-03-09 Leave will be on leave from 20100311 thru 20100322 2010-03-04 Pretest Score 2010-03-04 30-Day Review 2010-03-04 Pretest Score 2010-03-04 30-Day Review 2010-03-02 7 Level Upgrade 2010-02-24 2nd Pretest score 100% on his pretest today. He has now had 2 consecutive scores above 90%. One more to go. He will continue to study, and will study while he is on leave after next week and we will set up a date to test after leave. I have reviewed tasks and have trained him on 2 tasks This week. Entry for 21 Feb was not entered and reviews will be continued every 30 days in the future until upgrade is complete. score 100% on his pretest today. He has now had 2 consecutive scores above 90%. One more to go. He will continue to study, and will study while he is on leave after next week and we will set up a date to test after leave. I have reviewed tasks and have trained him on 2 tasks This week. Entry for 21 Feb was not entered and reviews will be continued every 30 days in the future until upgrade is complete. took a pretest and scored a 97% will study and take another on Thursday. scored 75% on his pretest today. He will continue to study, and take another test on Friday This week. RC-135V, T/N 64-14848, 30 April 2015 T-103 JOURNAL ENTRIES ENTRY DATE SUBJECT SIGNATURE INFO REMARKS 2010-02-19 CDC Practice Test took a practice test today and scored 56%. He will study for his next test on 23 Feb. 2010-02-08 CDC Volume 2 has completed Vol. 2 of his 7-level CDCs scoring 100%. A comprehensive review was completed on 9 JAN 2010. He will now begin taking pretests until 3 consecutive 90% or above 2010-01-21 30-Day Review I have reviewed supervision of 2010-01-12 Tasks restored from archive on 2010-01-12 6 Tasks were restored from archive on 2010-01-12 2009-12-19 Leave 2009-12-15 Vol I Completed On Dec 10 records. He is currently TDY and we will resume training when he returns. I have just taken over and we will put together a plan of attack on his upgrade training upon return. will be on leave 21-22 Dec. has completed his VOL I of his 7-level CDCs. They were completed on Dec 10. He scored a 96%. A review was accomplished and his VOL II was issued with a completion date of 11 Jan 2010. 2009-11-30 Leave Will be on leave from 20091201 thru 20091204. CDC are on track 2009-11-14 30-Day Comprehensive Review A 30-Day Comprehensive Review was conducted on 2009-10-21 7 Level Upgrade, 30D Record Review Member started upgrade 1 September, 2009. has been is ALS and will soon be back to start his CDCs and to tackle the upgrade tasks. Records Reviewed, No defects noted, next due November 21, 2009 2009-10-21 New Task Groups Loaded New 5 and 7-level tasks groups were loaded due to the 38th and 45th AMUs merging. Please review the new tasks and complete as necessary. Also, The 7 Level CDC progression task group has been added to for the individual to annotate when a volume is completed. 2009-09-25 CDC Issue Today I issued his 2AX7X CDC#s. He was briefed on the CDC guidelines and he understands the responsibilities of the CDC program. The CDCs will be completed in the specified time frame and documentation will be completed accordingly. He understands that a comprehensive review must be completed upon completion of the last volume and he understands what constitutes a comprehensive review. He will follow the requirements as outlined in AFI 36-2201, Volume 3, Chapter 9, Table 9.1. will be at ALS until a projected date of 9 Nov 09. At that time he will begin his CDC upgrade training and will be issued Volume 1. With a 30-day completion req. 2009-09-22 ALS (CDCs) 2009-08-05 F108 Engine Run Cert 2009-08-04 TDY 2009-07-09 TF 33 P9 ENGINE RUN CERT 2009-06-05 Supervisor 2009-05-12 FDR 2009-05-08 New Task Groups Loaded I feel confident in training records. Upgrade has been started on 9 November 09. ability to run F108 engines. A form 64 is being submitted at This time. will be TDY from 20090806 thru 20090920 IS CERTIFIED TO RUN P9 ENGINES AT THIS TIME. FORM 64 IS BEING SUBMITTED has taken over as supervisor will is TDY from 6 June 2009 to 6 OCT 2009 completed FDR Class I loaded the updated 5/ADCC task groups to ITP. 2009-02-24 Sniffer TDY will be TDY with his jet from approxamately 26 FEB to March 12 2009-02-24 Sniffer TDY will be TDY with his jet from approxamately 26 FEB to March 12 2009-01-05 TDY GOING ON TDY FROM 20090105 THRU 20090120 2008-11-14 New Workcenter Requirements I have updated the workcenter requirements for all task groups and have applied those that pertain to 2008-10-29 Leave Will be on leave from 20081030 thru 20081108 2008-10-29 Training Reviewed all training tasks all up to date 2008-10-28 Eng run 64 has been trained on P-5 eng operation and inlets/exhaust inspection. He is fully-qualified/capable of performing these RC-135V, T/N 64-14848, 30 April 2015 T-104 JOURNAL ENTRIES ENTRY DATE SUBJECT SIGNATURE INFO REMARKS tasks. The importance of having Red X orders was also restressed to him. He understand and accepts the responsibility that comes with the task. A form 64 is being submitted. 2008-09-02 TDY Going TDY on the 20080905 2008-08-20 Leave Will be on leave from 20080822 thru 20080831. Not in upgrade training 2008-07-28 REFUEL/DEFUEL 64 HAS BEEN TRAINED AND IS QUALIFIED TO PERFORM REFUEL/DEFUEL SUPERVISOR. A FORM 64 HAS BEEN SUBMITTED. 2008-07-25 ADDITION TO SCR REQUEST ADDITION TO SCR FOR THE FOLLOWING COURSE CODES. ISFULLY QUALIFIED AND HAS MET ALL REQUIREMENTS AND REQUIRES ADDITION TO THE SCR TO PERFORM THIS TASK. HE WAS CERTIFIED BY 2008-07-01 Leave Taking leave from 20080704 thru 20080715 2008-06-20 Refuel/defuel supeRvisoR has been trained and signed off as a refuel/defuel supervisor. His 2426 has been submitted 2008-04-11 TDY Going TDY From 20080414 thru 20080510 2008-03-20 60-Day TBA Entry Reviewed training and TBA. On Track doing good. 2008-03-07 Leave Going on leave from 20080308 thru 20080316 2008-03-07 Leave Going on leave from 20080308 thru 20080316 2008-03-07 Leave Going on leave from 20080308 thru 20080316 2008-03-07 Leave Going on leave from 20080308 thru 20080316 2008-01-29 Leave Leave from Feb. 13, 2008 Thru Feb. 19, 2008 2007-10-12 Task(s) restored from archive on 2007-10-12 Task(s) Unarchived: CFETP - 2A5X1 - 001.002.001.001 Progression in career ladder 2A5X1, CFETP - 2A5X1 - 001.002.001.002 Duties of AFSC 2A5X1, CFETP - 2A5X1 - 001.002.002 OPERATIONS SECURITY (OPSEC) VULNERABILITY OF AFSC 2A5X1, CFETP - 2A5X1 - 001.002.003.001 Housekeeping consistent with safety of personnel and equipment, CFETP - 2A5X1 001.002.003.002.001 Engine air intake and exhaust, CFETP - 2A5X1 - 001.002.003.002.002 High intensity sound, CFETP - 2A5X1 001.002.003.002.003 Turbine plane of rotation, CFETP - 2A5X1 - 001.002.003.002.004 Radio frequency radiation, CFETP - 2A5X1 001.002.003.002.005 Ground handling of aircraft, CFETP - 2A5X1 - 001.002.003.002.006 Hot brakes, CFETP - 2A5X1 001.002.003.002.007 Use of tools and equipment, CFETP - 2A5X1 - 001.002.003.002.008 Servicing aircraft systems, CFETP - 2A5X1 - 001.002.003.002.009 Cleaning Agents, CFETP - 2A5X1 - 001.002.003.002.010 Solvents, CFETP - 2A5X1 - 001.002.003.002.011 Lubricants, CFETP - 2A5X1 - 001.002.003.002.012 High pressure gasses, CFETP - 2A5X1 - 001.002.003.002.013 Aircraft explosive equipment, CFETP - 2A5X1 - 001.002.003.002.014 Composite materials, CFETP - 2A5X1 - 001.002.003.003.001 Perform pre-use inspection, CFETP - 2A5X1 - 001.002.003.003.002 Position, CFETP - 2A5X1 - 001.002.003.003.003 Operate, CFETP - 2A5X1 001.002.003.004 Foreign Object Damage (FOD) prevention program, CFETP - 2A5X1 - 001.002.003.005 Dropped Object prevention program, CFETP - 2A5X1 - 001.002.003.006.001 Use, CFETP - 2A5X1 - 001.002.003.006.002 Disposal, CFETP - 2A5X1 001.002.003.007 Use AF Form 1492, CFETP - 2A5X1 - 001.002.004.001 TO system, CFETP - 2A5X1 - 001.002.004.002 Air Force manuals and instructions, CFETP - 2A5X1 - 001.002.004.003 Use technical orders, CFETP - 2A5X1 - 001.002.006.005 Document training records, CFETP - 2A5X1 - 001.002.007.001 Basic functions within maintenance, CFETP - 2A5X1 - 001.002.008.001 MDD Fundamentals, CFETP - 2A5X1 - 001.002.008.002.001 Purpose, I certify that the task information contained in This record has been transcribed and reflected in the active ITP. Action: 229 task(s) transcribed for product CFETP-2A5X1 2007-10-09 Transcription of AF 623 2009-05-26 Tasks restored from archive on 2009-05-26 Task was restored from archive on 2009-05-26 2013-02-05 Decertification for Task CFETP-2A5X1 AND 2A5X4-000-001.009.001 Member was decertified for improper tool control. Member will be recertified by a Section Chief within 30 days RC-135V, T/N 64-14848, 30 April 2015 T-105 CERTIFICATION I CERTIFY THAT THIS INDIVIDUAL TRAINING RECORD IS CURRENT AS OF 2015-05-04 _____________________________ TRAINEE SIGNATURE _____________________________ SUPERVISOR SIGNATURE RC-135V, T/N 64-14848, 30 April 2015 T-106 1. IDENTIFICATION DATA LAST NAME - FIRST NAME - MIDDLE INITIAL [Crew Chief 4] GRADE/RANK Staff Sergeant DAFSC/JOB SERIES 2A574 INDIVIDUAL TRAINING RECORD INDIVIDUAL'S SIGNATURE DATE 2015-05-04 Individual Training Record RC-135V, T/N 64-14848, 30 April 2015 T-107 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 001 Career Ladder Progression-1 Aug 12 TR: Air Force Enlisted Classification Directory (AFECD) 2A5X1 AND 2A5X4-000 001.001 Progression in career ladder 2A5X1 AND 2A5X4-000 001.002 Duties of AFSC 2A5X1 AND 2A5X4-000 003 AF OCCUPATIONAL SAFETY AND HEALTH (AFOSH) PROGRAM TR: AFIs 11-218, 21-101 and 91-301; applicable AFOSH STDs; TOs 00-25-172, 1-1-691, and applicable aircraft TOs 2A5X1 AND 2A5X4-000 003.001 Housekeeping consistent with safety of personnel and equipment 2A5X1 AND 2A5X4-000 003.002 Safety precautions pertaining to aircraft maintenance 2A5X1 AND 2A5X4-000 003.002.001 Engine air intake and exhaust 2A5X1 AND 2A5X4-000 003.002.002 High intensity sound 2A5X1 AND 2A5X4-000 003.002.003 Turbine, propeller, rotor plane of rotation 2A5X1 AND 2A5X4-000 003.002.004 Radio frequency radiation 2A5X1 AND 2A5X4-000 003.002.005 Ground handling of aircraft 2A5X1 AND 2A5X4-000 003.002.006 Hot brakes 2A5X1 AND 2A5X4-000 003.002.007 Use of tools and equipment 2A5X1 AND 2A5X4-000 003.002.008 Servicing aircraft systems 2A5X1 AND 2A5X4-000 003.002.009 Cleaning Agents 2A5X1 AND 2A5X4-000 003.002.010 Solvents 2A5X1 AND 2A5X4-000 003.002.011 Lubricants 2A5X1 AND 2A5X4-000 003.002.012 High pressure gasses 2A5X1 AND 2A5X4-000 003.002.013 Aircraft explosive equipment 2A5X1 AND 2A5X4-000 003.002.014 Composite materials 2A5X1 AND 2A5X4-000 003.002.015 Maintenance resource management TR: AFI 21-101; AFPAM 90-902 2A5X1 AND 2A5X4-000 003.002.016 Electrostatic hazards, static grounding and bonding TR: TOs 00-25-172 and 00-25-234 2A5X1 AND 2A5X4-000 003.003 Portable ground fire extinguishers TR: AFI 32-2001; TO 00-25-172 2A5X1 AND 2A5X4-000 003.003.001 Perform pre-use inspection 2A5X1 AND 2A5X4-000 003.003.002 Position 2A5X1 AND 2A5X4-000 003.003.003 Operate 2A5X1 AND 2A5X4-000 003.004 Foreign Object Damage (FOD) prevention program 2A5X1 AND 2A5X4-000 003.005 Dropped Object prevention program 2A5X1 AND 2A5X4-000 003.006 Hazardous chemicals TR: AFI 90-821 and applicable AFOSH STDs 2A5X1 AND 2A5X4-000 003.006.001 Use 2A5X1 AND 2A5X4-000 003.006.002 Disposal 2A5X1 AND 2A5X4-000 003.006.003 Hazard communication training program 2A5X1 AND 2A5X4-000 003.006.004 Hazardous material handling procedures 2A5X1 AND 2A5X4-000 003.007 AF Form 1492, Warning Tag TR: TO 00-20-1 2A5X1 AND 2A5X4-000 004 MAINTENANCE DIRECTIVES, REFERENCES, and INSTRUCTIONS TR: AFI 33-360 and TO 00-5 series as applicable 2A5X1 AND 2A5X4-000 004.001 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2011-10-17 2011-10-17 - A - - - - - 2011-10-17 2011-10-17 - A - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2013-03-01 2013-03-21 - A - - - - - 2013-03-01 2013-03-21 - A - - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - 1b - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2011-10-17 2011-10-17 - A - - - - - 2011-10-17 2011-10-17 - A B - - - - RC-135V, T/N 64-14848, 30 April 2015 T-108 1. Tasks Knowledge And Technical References TO system 2A5X1 AND 2A5X4-000 004.002 Air Force manuals and instructions 2A5X1 AND 2A5X4-000 004.003 Use technical orders 2A5X1 AND 2A5X4-000 004.004 TO improvement reporting 2A5X1 AND 2A5X4-000 005 SUPERVISION TR: AFIs 21-101, 36-2403, and AFTTP 3-3 2A5X1 AND 2A5X4-000 005.001 Plan work schedules 2A5X1 AND 2A5X4-000 005.002 Schedule maintenance 2A5X1 AND 2A5X4-000 005.003 Supervise personnel accomplishing maintenance 2A5X1 AND 2A5X4-000 005.004 Establish 2A5X1 AND 2A5X4-000 005.004.001 Work methods 2A5X1 AND 2A5X4-000 005.004.002 Work controls 2A5X1 AND 2A5X4-000 005.004.003 Performance standards 2A5X1 AND 2A5X4-000 005.005 Evaluate work performance of subordinate personnel 2A5X1 AND 2A5X4-000 006 TRAINING TR: AFIs 36-2201 and 36-2232 2A5X1 AND 2A5X4-000 006.001 Evaluate personnel for training 2A5X1 AND 2A5X4-000 006.002 Plan and supervise OJT 2A5X1 AND 2A5X4-000 006.003 Counsel trainees on training progress 2A5X1 AND 2A5X4-000 006.005 Document training records 2A5X1 AND 2A5X4-000 006.006 Purpose and use of Career Field Education and Training Plan (CFETP) 2A5X1 AND 2A5X4-000 007 MAINTENANCE MANAGEMENT TR: AFIs 21-101, 21-103, 21-118, 90-201 and AFMAN 23-110 2A5X1 AND 2A5X4-000 007.001 Basic functions within maintenance 2A5X1 AND 2A5X4-000 007.002 Resource management 2A5X1 AND 2A5X4-000 007.003 Personnel management 2A5X1 AND 2A5X4-000 007.004 Maintenance incident investigation and prevention 2A5X1 AND 2A5X4-000 007.005 Determine and report Aircraft Status 2A5X1 AND 2A5X4-000 008 MAINTENANCE DATA DOCUMENTATION (MDD) TR: AFI 21-101; TO 00-20 Series; applicable aircraft -06 Work Unit Code Manuals 2A5X1 AND 2A5X4-000 008.001 MDD Fundamentals 2A5X1 AND 2A5X4-000 008.002 Aircraft and supporting maintenance records 2A5X1 AND 2A5X4-000 008.002.001 Purpose 2A5X1 AND 2A5X4-000 008.002.002 Automated Forms 2A5X1 AND 2A5X4-000 008.002.007 Document other AFTO 781 series forms 2A5X1 AND 2A5X4-000 008.002.008 Document AFTO Form 244/245 2A5X1 AND 2A5X4-000 008.002.009 Document AFTO Form 350 2A5X1 AND 2A5X4-000 008.003 Maintenance Information Systems (MIS) 2A5X1 AND 2A5X4-000 008.003.001 Purpose 2A5X1 AND 2A5X4-000 008.003.002 Job data documentation (JDD) 2A5X1 AND 2A5X4-000 008.003.002.001 Purpose 2A5X1 AND 2A5X4-000 008.003.002.002 Access JDD 2A5X1 AND 2A5X4-000 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 1b - - - - - 2011-10-17 2011-10-17 - - B - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-17 2011-10-17 - - A - - - - 2013-03-01 2013-03-21 - - A - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - B - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - 1b - - - - - 2011-10-17 2011-10-17 - 1b - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-109 1. Tasks Knowledge And Technical References 008.003.002.003 Create maintenance event 2A5X1 AND 2A5X4-000 008.003.002.004 Defer maintenance event 2A5X1 AND 2A5X4-000 008.003.002.005 Schedule maintenance event 2A5X1 AND 2A5X4-000 008.003.002.006 Close maintenance event 2A5X1 AND 2A5X4-000 008.003.002.007 Use IMDS 2A5X1 AND 2A5X4-000 009 MAINTENANCE MATERIALS/ TOOLS TR:AFI 21-101, TOs 1-1A-8, 1-1A-14, 1-1-691 and 32- series TOs as applicable 2A5X1 AND 2A5X4-000 009.001 Tool control 2A5X1 AND 2A5X4-000 009.002 Select and use special tools 2A5X1 AND 2A5X4-000 009.003 Select/use restraint harness (e.g.; fall protection/prevention equipment) 2A5X1 AND 2A5X4-000 009.005 Hardware 2A5X1 AND 2A5X4-000 009.005.001 Purpose 2A5X1 AND 2A5X4-000 009.005.002 Remove/inspect/install 2A5X1 AND 2A5X4-000 009.006 Electrical connectors 2A5X1 AND 2A5X4-000 009.006.001 Purpose 2A5X1 AND 2A5X4-000 009.006.002 Connect/disconnect 2A5X1 AND 2A5X4-000 009.007 Securing devices 2A5X1 AND 2A5X4-000 009.007.001 Purpose 2A5X1 AND 2A5X4-000 009.007.002 Install/remove safety wire 2A5X1 AND 2A5X4-000 009.007.003 Install/remove cotter pins 2A5X1 AND 2A5X4-000 009.007.004 Safety cable 2A5X1 AND 2A5X4-000 009.008 Lubricants 2A5X1 AND 2A5X4-000 009.009 Sealants 2A5X1 AND 2A5X4-000 009.010 Adhesives 2A5X1 AND 2A5X4-000 009.011 Cleaning agents 2A5X1 AND 2A5X4-000 009.012 Hand tools 2A5X1 AND 2A5X4-000 009.012.001 Purpose 2A5X1 AND 2A5X4-000 009.012.002 Select, inspect and use 2A5X1 AND 2A5X4-000 009.013 Measuring tools 2A5X1 AND 2A5X4-000 009.013.001 Purpose 2A5X1 AND 2A5X4-000 009.013.002 Select and use ruler 2A5X1 AND 2A5X4-000 009.013.003 Select and use thickness gauge 2A5X1 AND 2A5X4-000 009.013.004 Use multi-meter 2A5X1 AND 2A5X4-000 009.013.005 Select, inspect and use torque wrench 2A5X1 AND 2A5X4-000 009.013.006 Select and use micrometer 2A5X1 AND 2A5X4-000 009.013.007 Use depth gauge 2A5X1 AND 2A5X4-000 010 RESPONSIBILITY FOR SUPPLY TR: AFIs 21-101 and 21-118, AFMAN 23-110, TOs 00-20-3 and 00-35D-54 2A5X1 AND 2A5X4-000 010.001 Maintenance supply concept 2A5X1 AND 2A5X4-000 010.003 Special requisition (GPC, Local purchase) 2A5X1 AND 2A5X4-000 010.004 Ordering parts 2A5X1 AND 2A5X4-000 010.006 Prepare repairable and serviceable parts for turn-in 2A5X1 AND 2A5X4-000 010.007 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2013-04-02 2013-04-11 - A - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A - - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - 2b - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - B - - - - 2014-04-22 2014-04-23 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-110 1. Tasks Knowledge And Technical References Repair cycle assets 2A5X1 AND 2A5X4-000 010.008 DIFM Control 2A5X1 AND 2A5X4-000 010.009 Local manufacture of parts 2A5X1 AND 2A5X4-000 010.010 Equipment account management 2A5X1 AND 2A5X4-000 010.011 Deficiency reporting 2A5X1 AND 2A5X4-000 010.013 DD Forms 1574, 1575, 1576, 1577 and 1577-2 2A5X1 AND 2A5X4-000 011 AIRCRAFT GENERAL TR: AFI 11-218; applicable AFOSH STDs; TOs 00-20-1, 00-25-172, 1-1-691, 1-1B-50 and applicable aircraft TOs 2A5X1 AND 2A5X4-000 011.001 Weight and balance 2A5X1 AND 2A5X4-000 011.002 Determine weight and balance requirements 2A5X1 AND 2A5X4-000 011.003 Inventory aircraft equipment 2A5X1 AND 2A5X4-000 011.004 Safe aircraft for maintenance 2A5X1 AND 2A5X4-000 011.005 Corrosion control program 2A5X1 AND 2A5X4-000 011.005.001 Aircraft cleaning 2A5X1 AND 2A5X4-000 011.005.002 Corrosion identification 2A5X1 AND 2A5X4-000 011.005.004 Aircraft lubrication 2A5X1 AND 2A5X4-000 011.006 Aircraft inspections 2A5X1 AND 2A5X4-000 011.006.001 Cncepts and Types 2A5X1 AND 2A5X4-000 011.008 Aircraft marshalling signals 2A5X1 AND 2A5X4-000 011.011 Deice aircraft TR: TO 42C-1-2S-2; 14CFR121.629 section 121.629 2A5X1 AND 2A5X4-000 011.012 Debrief aircrews 2A5X1 AND 2A5X4-000 011.013 Aircraft guarded switches 2A5X1 AND 2A5X4-000 011.013.001 Design/function/proper identification 2A5X1 AND 2A5X4-000 011.013.002 Remove and replace covers 2A5X1 AND 2A5X4-000 011.013.003 Operational check 2A5X1 AND 2A5X4-000 014 UTILITIES TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 014.001 System fundamentals 2A5X1 AND 2A5X4-000 014.001.001 Oxygen 2A5X1 AND 2A5X4-000 014.001.002 Bleed air 2A5X1 AND 2A5X4-000 014.001.003 Pressurization 2A5X1 AND 2A5X4-000 014.001.004 Air conditioning 2A5X1 AND 2A5X4-000 014.001.005 Fire/Overheat warning 2A5X1 AND 2A5X4-000 014.001.006 Fire suppression 2A5X1 AND 2A5X4-000 015 FLIGHT CONTROLS TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 015.002 Primary flight control fundamentals 2A5X1 AND 2A5X4-000 015.003 Secondary flight control fundamentals 2A5X1 AND 2A5X4-000 015.004 Component identification 2A5X1 AND 2A5X4-000 016 HYDRAULICS TR: TO 1-1A-8 and applicable aircraft TOs 2A5X1 AND 2A5X4-000 016.001 System fundamentals 2A5X1 AND 2A5X4-000 016.002 Remove/install components TR: TO 1-1A-8, Applicable aircraft TOs 2A5X1 AND 2A5X4-000 016.002.001 Tubing/hoses 2A5X1 AND 2A5X4-000 016.002.002 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start 5 B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2011-10-17 2011-10-17 - - B - - - - 2011-10-17 2011-10-17 - - - - - - - 2014-04-22 2014-04-23 - - - - - - - 2011-10-17 2011-10-17 - - B - - - - 2011-10-17 2011-10-17 - - B - - - - 2013-03-01 2013-03-21 - A B - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - - A - - - - 2011-10-17 2011-10-17 - A - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-17 2011-10-17 - A - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2013-03-01 2013-03-21 - A B - - - - 2013-03-01 2013-03-21 - A - - - - - 2013-03-01 2013-03-21 - A - - - - - 2011-10-17 2011-10-17 - A - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-24 2011-10-28 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-111 1. Tasks Knowledge And Technical References Fittings 2A5X1 AND 2A5X4-000 016.002.003 Filter elements 2A5X1 AND 2A5X4-000 016.003 Hydraulic Schematics /diagrams 2A5X1 AND 2A5X4-000 017 ENGINES TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 017.004 Joint Oil Analysis Program 2A5X1 AND 2A5X4-000 018 FUELS TR: TOs 00-25-172, 1-1-3, applicable AFOSH STDs and aircraft TOs 2A5X1 AND 2A5X4-000 018.002 Classify fuel leaks 2A5X1 AND 2A5X4-000 019 ELECTRICAL TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 019.001 AC Electrical system fundamentals 2A5X1 AND 2A5X4-000 019.002 DC electrical system fundamentals 2A5X1 AND 2A5X4-000 019.007 Electrical schematics/diagrams 2A5X1 AND 2A5X4-000 020 AEROSPACE GROUND EQUIPMENT TR: Applicable AFOSH STDs and TO 35A4 series as applicable 2A5X1 AND 2A5X4-000 020.001 Maintenance stands 2A5X1 AND 2A5X4-000 020.001.001 Purpose and description 2A5X1 AND 2A5X4-000 020.001.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.002 Self-propelled universal platforms 2A5X1 AND 2A5X4-000 020.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.002.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.003 Aircraft jacks TR: TO 35A2- series as applicable 2A5X1 AND 2A5X4-000 020.003.001 Purpose and description 2A5X1 AND 2A5X4-000 020.003.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.005 Oxygen servicing equipment TR: TO 15X-1-1, 37C2-8- as applicable 2A5X1 AND 2A5X4-000 020.005.001 Liquid oxygen (LOX) 2A5X1 AND 2A5X4-000 020.005.001.001 Purpose and description 2A5X1 AND 2A5X4-000 020.005.001.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.005.002 Gaseous oxygen (GOX) 2A5X1 AND 2A5X4-000 020.005.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.005.002.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.006 Diesel driven air compressors TR: TO 34Y1- series as applicable 2A5X1 AND 2A5X4-000 020.006.001 Purpose and description 2A5X1 AND 2A5X4-000 020.006.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.007 Ground heaters TR: 35E7- series as applicable 2A5X1 AND 2A5X4-000 020.007.001 Purpose and description 2A5X1 AND 2A5X4-000 020.007.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.008 Lighting equipment TR: TO 35F5- series as applicable 2A5X1 AND 2A5X4-000 020.008.001 Purpose and description 2A5X1 AND 2A5X4-000 020.008.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.010 Air conditioning units TR: TO 35E9- Series as applicable 2A5X1 AND 2A5X4-000 020.010.001 Purpose and description 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2014-04-22 2014-04-23 - - - - - - - 2011-10-24 2011-10-28 - A - - - - - 2011-10-17 2011-10-17 - - B - - - - 2011-10-24 2011-10-28 - A - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-24 2011-10-28 - A - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2013-04-02 2013-04-11 - A B - - - - 2013-04-02 2013-04-11 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-24 2011-10-28 - A B - - - - 2012-01-03 2012-02-02 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - RC-135V, T/N 64-14848, 30 April 2015 T-112 1. Tasks Knowledge And Technical References 2A5X1 AND 2A5X4-000 020.011 Ground generator sets/gas turbine compressors 2A5X1 AND 2A5X4-000 020.011.002 A/M32A-95 Gas turbine compressors TR: TO 35D12-series as applicable 2A5X1 AND 2A5X4-000 020.011.002.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011.003 Diesel driven generator sets TR: TO 35C2- series as applicable 2A5X1 AND 2A5X4-000 020.011.003.001 Purpose and description 2A5X1 AND 2A5X4-000 020.011.003.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.012 Tow bar TR: Applicable aircraft TOs 2A5X1 AND 2A5X4-000 020.012.001 Perform pre-use inspection 2A5X1 AND 2A5X4-000 020.012.002 Connect/disconnect 2A5X1 AND 2A5X4-000 020.013 Tow vehicles TR: TO 36A10 series as applicable 2A5X1 AND 2A5X4-000 020.013.001 Purpose and description 2A5X1 AND 2A5X4-000 020.013.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.014 Self-generating nitrogen equipment TR: TO 35D29-7-6-1 2A5X1 AND 2A5X4-000 020.014.001 Purpose and description 2A5X1 AND 2A5X4-000 020.014.002 Perform pre-use inspection and operate 2A5X1 AND 2A5X4-000 020.015 Gaseous nitrogen servicing equipment TR: TO 35D3- series as applicable 2A5X1 AND 2A5X4-000 020.015.001 Purpose and description 2A5X1 AND 2A5X4-000 020.016 Engine stands and dollies TR: 35D3- series as applicable 2A5X1 AND 2A5X4-000 020.016.001 Purpose and description 2A5X1 AND 2A5X4-000 020.016.002 Perform pre-use inspection and operate 2A5X4-006 001 C-135 QUALITATIVE REQUIREMENTS AIRCRAFT GENERAL 2A5X4-006 001.001 Periodic/Isochronal inspection concept and inspection TR: TOs 00-20 series, Applicable -6 TOs 2A5X4-006 001.001.001 Periodic/Isochronal inspection concept 2A5X4-006 001.001.002 Perform inspections 2A5X4-006 001.001.002.001 Preflight 2A5X4-006 001.001.002.002 Alert 5A 2A5X4-006 001.001.002.003 Alert 5B 2A5X4-006 001.001.002.004 Thruflight 2A5X4-006 001.001.002.005 Quick Turn 2A5X4-006 001.001.002.006 Hourly Post 2A5X4-006 001.001.002.009 Calendar 2A5X4-006 001.001.002.010 Special 2A5X4-006 001.001.002.011 900 Hr Insp 2A5X4-006 001.001.002.012 Time change item 2A5X4-006 001.001.002.013 Exterior panel/secondary structure inspection 2A5X4-006 001.002 Aircraft communications equipment TR: Applicable -2 TOs 2A5X4-006 001.002.001 Operate radio 2A5X4-006 001.002.002 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-10-17 2011-10-17 - - - - - - - 2013-03-01 2013-03-21 - - B - - - - 2013-03-01 2013-03-21 - - - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - 2b - - - - - 2011-10-17 2011-10-17 - A B - - - - 2011-10-17 2011-10-17 - - A - - - - 2011-10-17 2011-10-17 - - - - - - - 2011-11-16 2011-12-13 - A - - - - - 2011-11-16 2011-12-13 - 2b - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2011-11-16 2011-12-13 - 2b - - - - - 2011-11-16 2011-12-13 - - - - - - - 2012-01-03 2012-03-14 - 2b - - - - - 2012-04-09 2012-04-23 - - - - - - - 2012-04-09 2012-04-23 - - - - - - - 2012-04-09 2012-04-23 - - - - - - - 2012-04-09 2012-04-23 - - - - - - - 7 2011-11-16 2011-12-13 - - - - - - - 5 2012-01-02 2012-01-19 - - - - - - - 5 2011-11-16 2011-12-13 - 2b - - - - - 5 5 7 RC-135V, T/N 64-14848, 30 April 2015 T-113 1. Tasks Knowledge And Technical References Use interphone 2A5X4-006 001.003 Perform ground handling TR: AFI 11-218, TO 00-25-172, applicable AFOSH STDs, applicable -1 and -2 TOs 2A5X4-006 001.003.001 Aircraft launch 2A5X4-006 001.003.002 Call flight controls 2A5X4-006 001.003.003 Aircraft recovery 2A5X4-006 001.003.004 Tow aircraft 2A5X4-006 001.003.004.001 Wing/tail walker 2A5X4-006 001.003.004.002 Brake operator 2A5X4-006 001.003.004.003 Tow team supervisor 2A5X4-006 001.003.004.004 Tow vehicle operator 2A5X4-006 001.003.005 Jack and level aircraft 2A5X4-006 001.003.005.001 Jacking team member 2A5X4-006 001.003.005.005 Axle jacking 2A5X4-006 001.004 Compute center of gravity TR: Applicable aircraft -5 TOs 2A5X4-006 001.005 Install/remove ground safety devices TR: Applicable -2 TOs 2A5X4-006 001.005.001 Landing gear 2A5X4-006 001.005.002 Landing gear doors 2A5X4-006 001.006 Ground aircraft 2A5X4-006 001.007 Configure/reconfigure aircraft 2A5X4-006 001.007.002 Passenger/personnel 2A5X4-006 001.008 Maintain/store/configure/-21 equipment 2A5X4-006 001.010 Aircraft wash TR: TO - 6WC-3 2A5X4-006 001.010.001 Team member 2A5X4-006 001.010.002 Team supervisor 2A5X4-006 001.010.003 Post wash lube 2A5X4-006 001.011 Maintenance directives, references, & instructions TR: AFI 37-101 Vol 1 and TO 00-5-1 2A5X4-006 001.011.001 Use C-135 technical orders 2A5X4-006 001.012 Maintenance Data Documentation (MDD TR: AFI 21-101, TOs 00-20-1, 00-20-2, and applicable aircraft -06 Work Unit Code Manuals 2A5X4-006 001.012.001 Document AFTO Form 781H 2A5X4-006 001.012.002 Document AFTO Form 781A 2A5X4-006 001.012.003 Document AFTO Form 781J 2A5X4-006 001.012.004 Document AFTO Form 781K 2A5X4-006 002 AIRFRAME SYSTEMS TR: Applicable -2 TOs 2A5X4-006 002.001 Airframe components and structure 2A5X4-006 002.002 Service cargo door reservoir 2A5X4-006 002.003 Operate 2A5X4-006 002.003.001 Crew entry door 2A5X4-006 002.003.002 Cargo door 2A5X4-006 002.003.003 Emergency exit hatch 2A5X4-006 002.003.004 Wheel well doors 2A5X4-006 002.004 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 5 2011-11-16 2012-01-19 - b - - - - - 5 2012-01-02 2012-01-19 - 2b - - - - - 5 2011-11-16 2012-01-19 - b - - - - - 5 2011-10-24 2011-10-28 - b - - - - - 5 2012-01-02 2012-01-19 - b - - - - - 7 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 5 2011-10-24 2011-10-28 - 2b - - - - - 5 2012-01-02 2012-01-19 - 2b - - - - - 5 2011-11-16 2011-12-13 - 2b - - - - - 5 2011-11-16 2011-12-13 - 2b - - - - - 5 2011-10-24 2011-10-28 - 2b - - - - - 2013-03-01 2013-03-21 - - - - - - - 2011-11-16 2012-01-19 - - - - - - - 2011-10-24 2011-10-28 - - - - - - - 2012-04-09 2012-04-23 - - - - - - - 2012-02-15 2012-03-14 - - - - - - - 5 2013-02-01 2013-02-13 - 3c - - - - - 5 2013-02-01 2013-02-13 - 3c - - - - - 5 2013-02-01 2013-02-13 - 3c - - - - - 5 2013-02-01 2013-02-13 - 3c - - - - - 5 2013-02-01 2013-02-13 - 3c - - - - - 2011-10-24 2011-10-28 - A - - - - - 2013-03-01 2013-03-21 - b - - - - - 5 2011-10-24 2011-10-28 - 2b - - - - - 5 2011-11-16 2011-12-13 - 2b - - - - - 5 2011-11-16 2011-12-13 - 2b - - - - - 5 2011-11-16 2011-12-13 - 2b - - - - - RC-135V, T/N 64-14848, 30 April 2015 T-114 1. Tasks Knowledge And Technical References Open and close 2A5X4-006 002.004.001 Cowling (F-108) 2A5X4-006 002.004.002 Cowling (TF-33) 2A5X4-006 002.004.003 Panels/doors 2A5X4-006 002.004.004 Windows 2A5X4-006 002.005 Remove and install 2A5X4-006 002.005.001 Cowling (F-108) 2A5X4-006 002.005.002 Cowling (TF-33) 2A5X4-006 002.005.003 Panels/doors 2A5X4-006 002.005.004 Non-explosive seats 2A5X4-006 002.005.005 Windows 2A5X4-006 002.005.007 Radomes 2A5X4-006 002.005.008 Door/hatch seals 2A5X4-006 002.005.009 Thermal curtains 2A5X4-006 002.005.013 Tail cone 2A5X4-006 002.006 Perform aircraft inclement weather procedures 2A5X4-006 002.007 Inspect crew/passenger comfort facilities TR: Applicable -6 TOs 2A5X4-006 002.008 Service crew/passenger comfort facilities 2A5X4-006 003 LANDING GEAR SYSTEMS TR: Applicable -2 TOs 2A5X4-006 003.001 Landing gear components and system operation 2A5X4-006 003.002 Troubleshoot 2A5X4-006 003.003 Operate 2A5X4-006 003.003.001 Landing gear 2A5X4-006 003.003.002 Brakes 2A5X4-006 003.003.003 Steering system 2A5X4-006 003.003.004 Anti skid system 2A5X4-006 003.004 Service 2A5X4-006 003.004.001 Snubber 2A5X4-006 003.004.002 Centering cylinder 2A5X4-006 003.004.003 Landing gear struts 2A5X4-006 003.004.003.001 Deflate 2A5X4-006 003.004.003.002 Drain 2A5X4-006 003.004.003.003 Fill 2A5X4-006 003.004.003.004 Inflate 2A5X4-006 003.004.004 Tires 2A5X4-006 003.005 Lubricate landing gear components 2A5X4-006 003.006 Remove and Install 2A5X4-006 003.006.001 Snubbers 2A5X4-006 003.006.002 Centering cylinder 2A5X4-006 003.006.003 Wheel and tire assemblies 2A5X4-006 003.006.003.001 Nose 2A5X4-006 003.006.003.002 Main 2A5X4-006 003.006.004 Anti-skid transducer 2A5X4-006 003.006.005 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 2012-01-02 2012-01-19 - 2b/b - - - - - 2012-01-02 2012-01-19 - - - - - - - 2011-11-16 2011-12-13 - - - - - - - 2011-11-16 2011-12-13 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2011-11-16 2011-12-13 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - A - - - - - 2012-01-02 2012-01-19 - - - - - - - 2014-04-22 2014-04-23 - - - - - - - 2011-11-16 2012-01-19 - 2b - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-02-20 2012-03-21 - - - - - - - 5 2012-01-02 2012-01-19 - 2b - - - - - 5 2012-01-02 2012-01-19 - 2b - - - - - 5 2011-11-03 2011-11-10 - 2b - - - - - 2011-11-03 2011-11-10 - - - - - - - 5 2011-11-03 2011-11-10 - 2b - - - - - 5 2011-11-03 2011-11-10 - 2b - - - - - 5 2011-11-03 2011-11-10 - 2b - - - - - 2013-03-01 2013-03-21 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 5 2012-01-02 2012-01-19 - 2b - - - - - 5 2011-11-16 2012-01-19 - 2b - - - - - 5 2012-01-02 2012-01-19 - 2b - - - - - 5 2011-11-16 2012-01-19 - 2b - - - - - 2014-04-22 2014-04-23 5 RC-135V, T/N 64-14848, 30 April 2015 T-115 1. Tasks Knowledge And Technical References Carbon brake assemblies 2A5X4-006 003.006.006 Bleed brake assembly (carbon) 2A5X4-006 003.007 Determine serviceability of aircraft tires TR: TO 4T-1-3 2A5X4-006 004 UTILITY SYSTEMS TR: TO 00-25-172, Applicable -2 TOs 2A5X4-006 004.001 Utility components and system operation 2A5X4-006 004.002 Troubleshoot 2A5X4-006 004.003 Operate 2A5X4-006 004.003.001 Bleed air system 2A5X4-006 004.003.002 Air conditioning system 2A5X4-006 004.003.003 Pressurization system 2A5X4-006 004.003.004 Anti-ice system 2A5X4-006 004.003.005 Fire/overheat warning system 2A5X4-006 004.003.006 Fire extinguishing system 2A5X4-006 004.003.007 Oxygen system 2A5X4-006 004.004 Oxygen system TR: Applicable -2, -3 TOs 2A5X4-006 004.004.001 Service gaseous oxygen 2A5X4-006 004.004.002 Service liquid oxygen 2A5X4-006 004.005 Inspect TR: Applicable -6 TOs 2A5X4-006 004.005.001 Bleed air system 2A5X4-006 004.005.002 Air conditioning system 2A5X4-006 004.005.003 Pressurization system 2A5X4-006 004.005.004 Anti-ice system 2A5X4-006 004.005.005 Fire/overheat warning system 2A5X4-006 004.005.006 Fire extinguisher system 2A5X4-006 004.005.007 Oxygen system 2A5X4-006 004.006 Air Cycle Machine (ACM) 2A5X4-006 004.006.001 Drain 2A5X4-006 004.006.002 Service 2A5X4-006 005 FLIGHT CONTROL SYSTEM TR: Applicable -2 TOs 2A5X4-006 005.001 Flight control components and system operation 2A5X4-006 005.002 Troubleshoot 2A5X4-006 005.003 Operate flight controls 2A5X4-006 005.003.001 Aileron system 2A5X4-006 005.003.002 Rudder system 2A5X4-006 005.003.003 Elevator system 2A5X4-006 005.003.004 Spoiler/Speed brake system 2A5X4-006 005.003.005 Stabilizer trim system 2A5X4-006 005.003.006 Flap system 2A5X4-006 005.004 Remove/install 2A5X4-006 005.004.001 Cove lip door 2A5X4-006 005.004.002 Cove lip door latch 2A5X4-006 005.004.005 Fore flap 2A5X4-006 005.004.006 Aileron snubber 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A Tng Start B Tng Complete C D Trainee Initialst Trainer Initials E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC 5 2012-01-02 2012-01-19 - 2b - - - - - 5 2011-10-24 2011-10-28 - 2b - - - - - 2012-01-02 2012-01-19 - A - - - - - 2014-04-22 2014-04-23 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2011-11-16 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - 2b - - - - - 2011-11-16 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2011-11-16 2012-01-19 - - - - - - - 5 2012-01-02 2012-01-19 - b - - - - - 5 2012-01-02 2012-01-19 - b - - - - - 2012-01-02 2012-01-19 - A - - - - - 2014-04-22 2014-04-23 - - - - - - - 2012-01-02 2012-01-19 - 2b - - - - - 2012-01-02 2012-01-19 - 2b - - - - - 2012-01-02 2012-01-19 - 2b - - - - - 2012-01-02 2012-01-19 - 2b - - - - - 2012-01-02 2012-01-19 - 2b - - - - - 2011-11-16 2012-01-19 - 2b - - - - - 2012-02-20 2012-03-21 - - - - - - - 2012-02-20 2012-03-21 - - - - - - - 2014-04-22 2014-04-23 - - - - - - - 2014-04-22 2014-04-23 - - - - - - - 5 RC-135V, T/N 64-14848, 30 April 2015 T-116 1. Tasks Knowledge And Technical References 2A5X4-006 005.004.007 Elevator snubber 2A5X4-006 005.004.013 Leading edge flaps 2A5X4-006 005.005 Lubricate flight controls 2A5X4-006 005.006 Service gearbox 2A5X4-006 006 HYDRAULIC SYSTEMS TR: Applicable -2 TOs 2A5X4-006 006.001 Hydraulic components and system operation 2A5X4-006 006.002 Troubleshoot 2A5X4-006 006.003 Service hydraulic system 2A5X4-006 006.003.001 Reservoir 2A5X4-006 006.003.002 Accumulator 2A5X4-006 006.003.003 Drain reservoir 2A5X4-006 006.004 Operate 2A5X4-006 006.004.001 Engine driven pump 2A5X4-006 006.004.002 Non-engine driven pump 2A5X4-006 006.005 Remove and install accumulator 2A5X4-006 007 ENGINES TR: AFI 11-218, applicable AFOSH STDs and -2 TOs 2A5X4-006 007.001 Engine and Auxiliary Power Unit (APU) components and system operation 2A5X4-006 007.003 Perform 2A5X4-006 007.003.001 Engine operational check 2A5X4-006 007.003.004 Engine motor wet 2A5X4-006 007.003.005 Engine motor dry 2A5X4-006 007.003.006 Audible ignition check 2A5X4-006 007.003.007 Alternate engine start 2A5X4-006 007.004 Operate 2A5X4-006 007.004.001 Engine and subsystems 2A5X4-006 007.005 Service 2A5X4-006 007.005.001 Oil system 2A5X4-006 007.005.002 Constant Speed Drive (CSD)/Integrated Drive Generator (IDG) 2A5X4-006 007.005.003 Gear box 2A5X4-006 007.005.004 Auxiliary Power Unit (if equipped) 2A5X4-006 007.006 Remove and install 2A5X4-006 007.006.001 Starter 2A5X4-006 007.006.002 Starter cartridge 2A5X4-006 007.007 Take engine oil sample TR: TO 42B2-1-9, 33-1-37 2A5X4-006 007.008 Chip detectors 2A5X4-006 007.009 Inspect installed engine TR: Applicable -6 TOs 2A5X4-006 007.009.001 Turbine 2A5X4-006 007.010 Inspect Auxiliary Power Unit TR: Applicable -6 TOs 2A5X4-006 008 AIRCRAFT FUEL SYSTEMS TR: TO 00-25-172, applicable AFOSH STDs and -2 TOs 2A5X4-006 008.001 Fuel components and system operation 2A5X4-006 008.002 Inspect fuel filters 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2014-04-22 2014-04-23 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - - - - - - - 2014-04-22 2014-04-23 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2012-01-02 2012-01-19 - A - - - - - 2012-01-02 2012-01-19 - - - - - - - 5 2011-11-16 2011-12-13 - 2b - - - - - 5 2011-11-16 2011-12-13 - 2b - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - 2b - - - - - 2012-01-02 2012-01-19 - - - - - - - 2013-03-01 2013-03-21 - A - - - - - 2013-01-29 2013-04-29 - - - - - - - 2013-01-29 2013-04-29 - - - - - - - 2013-01-29 2013-04-29 - - - - - - - 2013-01-29 2013-04-29 - - - - - - - 2014-04-22 2014-04-23 - - - - - - - 2014-04-22 2014-04-23 - - - - - - - 2011-11-16 2011-12-13 - b - - - - - 2013-01-29 2013-04-29 - - - - - - - 2013-01-29 2013-04-29 - - - - - - - 2012-09-24 2012-09-27 - - - - - - - 2014-04-22 2014-04-23 - - - - - - - 2012-04-09 2012-06-18 - - - - - - - 2012-04-09 2012-04-23 - - - - - - - 2012-01-03 2012-02-02 - A - - - - - 2013-01-29 2013-04-29 - 1b - - - - - 2013-01-29 2013-04-29 - 2b - - - - - 2012-02-20 2012-03-21 - A - - - - - 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-117 1. Tasks Knowledge And Technical References 2A5X4-006 008.002.001 TF-33 TR: 1C-135E-2-4-1 2A5X4-006 008.002.002 F-108 TR: 2J-F-108-2-1 2A5X4-006 008.003 Ground transfer fuel 2A5X4-006 008.003.001 Wing tank transfer 2A5X4-006 008.003.002 Body tank transfer 2A5X4-006 008.004 Refuel aircraft 2A5X4-006 008.004.001 Team member 2A5X4-006 008.004.002 Team panel operator 2A5X4-006 008.004.003 Team supervisor 2A5X4-006 008.005 Defuel aircraft 2A5X4-006 008.005.001 Team member 2A5X4-006 008.005.002 Team panel operator 2A5X4-006 008.005.003 Team supervisor 2A5X4-006 008.006 Prepare aircraft for fuel cell maintenance 2A5X4-006 008.007 In-Flight Refueling (IFR) system 2A5X4-006 008.007.001 IFR receiver system 2A5X4-006 008.007.001.001 Inspect 2A5X4-006 008.007.001.002 Operate 2A5X4-006 009 ELECTRICAL SYSTEMS TR: Applicable -2 TOs 2A5X4-006 009.001 Electrical components and system operation 2A5X4-006 009.002 Switch guards 2A5X4-006 009.003 Perform operational check 2A5X4-006 009.003.002 Lighting system 2A5X4-006 009.003.003 Indicator warning lights 2A5X4-006 009.004 Remove and install 2A5X4-006 009.004.001 Light lenses 2A5X4-006 009.004.002 Light bulbs 2A5X4-006 009.004.003 Batteries 2A5X4-006 009.004.004 Connect/apply and disconnectexternal electrical power 2A5X4-006 010 EGRESS SYSTEM TR: Applicable -2 TOs 2A5X4-006 010.001 Egress components and system operation 2A5X4-006 010.003 Remove/install emergency escape slides (except RC-135) 2A5X4-006 011 AEROSPACE GROUND EQUIPMENT TR: Applicable AFOSH STDs 2A5X4-006 011.001 Perform pre-use inspection and operate 2A5X4-006 011.001.002 Air conditioning units TR: TO 35E9-series as applicable 2A5X4-006 011.001.003 A/M32A-95 Gas turbine compressor TR: TO 35D12-series as applicable 2A5X4-006 011.001.004 Gaseous nitrogen servicing equipment TR: TO 35D3-series as applicable 2A5X4-006 011.001.005 Oil servicing carts TR: TO 35A17-series as applicable 2A5X4-006 011.001.006 Hydraulic servicing carts TR: TO 35A29-series as applicable 2. Core Tasks Career Field Education and Training Plan (CFETP) 3. Certification for OJT 4. Proficiency Codes Used to Indicate Training A C D Tng Trainee Complete Initialst 2014-04-22 2014-04-23 B Trainer Initials Tng Start E Certifier Initials A 3-Skill Level (1) Crse (2) CDC B 5-Skill Level (1) Crse (2) CDC C 7-Skill Level QTP (1) Crse (2) CDC - - - - - - - 2014-04-22 2014-04-23 - - - - - - - 5 2012-01-03 2012-02-02 - b - - - - - 5/R 2012-01-03 2012-02-02 - - - - - - - 5 2011-10-24 2011-10-28 - b - - - - - 5 2012-01-02 2012-01-19 - b - - - - - 7 2011-11-16 2012-01-19 - - - - - - - 5 2011-10-24 2011-10-28 - b - - - - - 5/R 2012-01-02 2012-01-19 - b - - - - - 7/R 2012-01-02 2012-01-19 - - - - - - - 2012-01-02 2012-01-19 - - - - - - - 2012-02-20 2012-03-21 - - - - - - - 2012-02-20 2012-03-21 - - - - - - - 2012-02-15 2012-03-14 - A - - - - - 2013-03-01 2013-03-21 - A - - - - - 2011-11-16 2011-12-13 - 2b - - - - - 2013-03-01 2013-03-21 - - - - - - - 5 2011-10-24 2011-10-28 - - - - - - - 5 2011-10-24 2011-10-28 - - - - - - - 5 2012-01-02 2012-01-19 - 2b - - - - - 5 2013-02-01 2013-02-13 - 2b - - - - - 2012-01-02 2012-01-19 - A - - - - - 2012-01-02 2012-01-19 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - - - - - - - 2013-03-01 2013-03-21 - 2b - - - - - 5 5 RC-135V, T/N 64-14848, 30 April 2015 T-118 JOB QUALIFICATION STANDARD CONTINUATION/WJQS CRITICAL TASK NUMBER TASKS 35961 002 35961 002.001 35961 002.001.001 35961 002.001.002 35961 003 35961 003.002 35961 003.002.001 35961 003.004 35961 003.005 35961 003.006 35961 003.008 35961 003.008.001 35961 003.008.002 35961 003.008.003 35961 003.008.004 35961 003.008.004.001 35961 003.008.004.002 35961 003.008.004.003 35961 003.008.004.004 35961 003.008.004.005 35961 003.008.004.005. 001 35961 003.008.004.005. 002 35961 004 35961 004.001 35961 004.002 35961 004.003 35961 004.003.001 35961 005 35961 005.002 35961 005.003 35961 006 35961 006.005 35961 006.006 35961 007 35961 007.001 35961 007.002 TASKS, KNOWLEDGE AND TECHNICAL REFERENCES CERTIFICATION START DATE COMPLETION DATE TRAINEE'S TRAINER'S CERTIFIER'S INITIALS INITIALS INITIALS HYDRAULICS 1C-135-2-2(-6,-7,-8-13) SERVICE Aircraft hydraulic system before TCTO-509 2012-01-02 2012-01-19 Aircraft hydraulic system after TCTO-509 2012-01-02 2012-01-19 2014-04-22 2014-04-23 2013-04-29 2013-04-29 2013-04-29 2013-04-29 2013-04-29 2013-04-29 2012-04-09 2012-04-23 F-108 Inlets and exhaust inspection 2012-04-09 2012-04-23 F-108 JFS operational check 2013-04-29 2013-04-29 TF-33 P5/P9 Engine Oil 2012-01-02 2012-01-19 F-108 Engine oil 2012-01-02 2012-01-19 TF-33 Pnuematic starter 2012-01-02 2012-01-19 F-108 Pnuematic starter 2012-01-02 2012-01-19 TF-33 fuel strainer 1C-135-2-4-1 2012-01-02 2012-01-19 F-108 Fuel strainer 2012-01-02 2012-01-19 GUIDANCE AND CONTROL ETM RC-2-11-2, ETM AN/ASN-121, 1C-135-2-9 (-11-2, -11-5) Apply range and slip markings Perform Basic MFD operation REMOVE AND INSTALL INS Battery 2012-01-02 2012-01-19 2012-01-02 2012-01-02 2012-01-19 2012-01-19 2014-04-22 2014-04-23 2014-04-22 2014-04-23 2014-01-14 2014-01-27 2014-01-14 2014-01-27 ENGINES 1C-135(E)C-2-4-1, 1C-135-2-4-1, 1C-135(K)R-2-4JG-2 2J-F108-2-1, 1C-135-2-2 (-4,-10) Inspect F-108 Engine Components TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicableaircraft/ engine TOs Inspect F-108 engine acoustical panels TOs 00-20-1, 00-35D-54,1-1A-8, 2J-1-13, 2-1-111, and applicableaircraft/ engine TOs TF-33/P5 engine and subsystems TF-33/P9 engine and subsystems F-108 engine and subsystems PERFORM TF-33 P5/P9 Inlets and exhaust inspection SERVICE REMOVE AND INSTALL ELECT/ENVIROMENTAL 1C-135-2-2 (-3, -7, -10) Perform operational check of mark 2 anti-skid system Perform operational check of mark 3 anti-skid system CDC Volume Progression 7 Level CDC Vol 1 AFI 36-2201 7 Level CDC Vol 2 AFI 36-2201 OPLAN 8010 Alert Requirements ACCI 13-520 para 3.11.4 Perform ADCC Alert Crew requirements: tow team member, refuel team member ACCI 13-501 para 3.11.4 Perform DCC Alert Crew requirements: tow team supervisor, refuel team supervisor, engine run certified, red x orders ACCI 13-501 para 3.11.4 RC-135V, T/N 64-14848, 30 April 2015 T-119 JOURNAL ENTRIES ENTRY SUBJECT DATE 2011-10-12 Conduct Orientation/Initial Evaluation 2014-05-02 90 day review SIGNATURE INFO REMARKS Within 60 days of assignment the Supervisor will conduct a Workcenter Orientation and Initial Evaluation of qualifications IAW AFI 36-2201 V3. 90 day review c/w. 2014-05-02 Temp Supervisor is 100% task-qualified. Reviewed ITP 20140502, no discrepancies found will be on leave 17-28 May. will be temporary supervisor for 2014-05-02 90 day review 90 day review c/w. 2014-04-09 Temporary Supervisor I will ge going TDY to NCOA from 11 Apr thru 29 May and 2014-04-07 Temporary Supervisor I am Going TDY to NCOA from 11 Apr thru 29 May 2014-01-24 90 Day Review I reviewed 2013-11-18 TDY is 100% task-qualified. Reviewed ITP 20140502, no discrepancies found wil be your Temporary Supervisor will be your Temporary Supervisor TBA entries today for accuracy and completion. There were no errors noted on this date. will be TDY from 4 December 2014 to 15 March 2014 2013-10-16 90 day review 90 review has been C/W 2013-10-01 Temporary supervisor I 2013-09-26 F-108 cert ENG RUN Course code 3250, F-108 Eng Run 3252, F-108 Eng Run 4228, F-108 Eng Run 3248 performed all steps to run eng without flaw. Also discussed the importance of always using the applicable TOs while running eng as this is a critical task, and he has demonstrated that he will follow these guidelines 2013-09-24 Engine run pretest 2013-08-15 workcenter orientation 2013-07-31 90 Day review Missing For will be Deploying and I am assigning as a Temporary supervisor untill my return... scored 3 consecutive 100's on Engine Run F108 practice tests. Is ready for Engine Run test. A workcenter orientation was previously completed but was not documented correctly. A workcenter orientation was conducted with on 20110117. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. I reviewed TBA entries today for accuracy and completion. 90 Day review was missed in the Month of Jan and April. This review supersedes previous reviews. All records are accurate and current at this time. 2013-02-14 SSgt Wilkinson's CAF Form 64 I have verified that he is qualified and signed off on the following tasks: Tow team mbr, Tow brake rider, Tow Super, Tow vehicle Operator 2012-10-15 90 Day TBA Review A records review was conducted on records. There are 12 tasks remaining to meet his 7 level requirements for the C-135 airframe. He is encouraged to continue his retraining progress. No discrepancies noted at this time. All records are current and accurate. 2012-08-24 F108 Pretest I have taken 3 F108 engine run pretests and scored a 90%,96%,96%. I am ready to take my engine run test. 2012-07-17 90 Day Review A records review was conducted on records. There are 14 tasks remaining to meet his 7 level requirements for the c-135 airframe all that is left are engine related tasks, which some of them are engine run related awaiting time and class space. He is encouraged to continue his retraining progress. No discrepancies noted at this time. All records are current and accurate. 2012-06-04 Certification to Sign NRTS I have reviewed training records. He is signed off and qualified to be Authorized to NRTS Documentation Guidance IAW TO 00-20-3. I have reviewed training records. He is signed off and qualified to be authorized to Sign All Condition Tags IAW Documentation Guidance IAW TO 00-20-3. I discussed Red X certification with . I interviewed him on a one-to-one basis and we went over the importance of always doing the right thing. I let him know that it will always be integrity first. We discussed how signing off a Red X means taking responsibility for the whole area and NOT just the part being inspected. An expensive aircraft and even more valuable lives depend on him making sure that everything is by the T.O. Guidance in signing of Red X is in 00-20-1 para 4.5. I have interviewed on signing off Repeat/Recur. We discussed the guidance of finding how many times he can sign off a Repeat/Recur can be found in AFI 21-101 14.20.1 and the Offutt AFI 21-101 14.20.1.2. The guidance for signing it off can be found in 00-20-1. I am recommending to be upgraded to the skill level of craftsman. has met all mandatory training requirements IAW AFI 36-2201 for award of his 7 skill level. He understands the additional responsibilities that are required of this new skill level, and I feel he is ready to handle the added responsibilities. I have reviewed their ITP and all tasks have been documented and completed. Submitted CAF Form 64. I have verified that he is qualified and signed off on the following tasks: Sign All Condition Tags and NTRS, Clear Red X in 2A5X3A, Sign Off CND, and Sign Off Repeat/Recur. I have interviewed on signing off CNDs. We discussed the guidance of finding how many times he can sign off a CND can be found in AFI 21-101 14.20.2 and the Offutt AFI 21-101 chapter 14.20.2.4. The guidance for signing it off can be found in 00-20-1. Submitted CAF Form 64. I have verified that he is qualified and signed off on the following tasks: Sign All Condition Tags and NTRS, Clear Red X in 2A5X3A, Sign Off CND, and Sign Off Repeat/Recur. I am recommending to be upgraded to the skill level of craftsman. has met all mandatory training requirements IAW AFI 36-2201 for award of his 7 skill level. He understands the additional responsibilities that are required of this new skill level, and I feel he is ready to handle the added responsibilities. I have reviewed their ITP and all tasks have been documented and completed. I have interviewed on signing off CNDs. We discussed the guidance of finding how many times he can sign off a CND can be found in AFI 21-101 14.20.2 and the Offutt AFI 21-101 chapter 14.20.2.4. The guidance for signing it off can be found in 00-20-1. 2012-06-04 Certification to Sign All Condition Tags 2012-06-04 Certification To Sign Red X In 2A5X3A 2012-06-04 Certification to Sign Repeat/ Recur 2012-06-04 Recommendation for upgrade to 7 level 2012-06-04 CAF Form 64 Submitted 2012-06-04 Certification to Sign Off CND 2012-06-04 CAF Form 64 Submitted 2012-06-04 Recommendation for upgrade to 7 level 2012-06-04 Certification to Sign Off CND RC-135V, T/N 64-14848, 30 April 2015 T-120 JOURNAL ENTRIES ENTRY SUBJECT DATE 2012-06-04 Certification to Sign Repeat/ Recur 2012-06-04 Certification To Sign Red X In 2A5X3A 2012-06-04 Certification to Sign All Condition Tags 2012-06-04 Certification to Sign NRTS 2012-04-23 90 Day Review SIGNATURE INFO REMARKS I have interviewed on signing off Repeat/Recur. We discussed the guidance of finding how many times he can sign off a Repeat/Recur can be found in AFI 21-101 14.20.1 and the Offutt AFI 21-101 14.20.1.2. The guidance for signing it off can be found in 00-20-1. I discussed Red X certification with . I interviewed him on a one-to-one basis and we went over the importance of always doing the right thing. I let him know that it will always be integrity first. We discussed how signing off a Red X means taking responsibility for the whole area and NOT just the part being inspected. An expensive aircraft and even more valuable lives depend on him making sure that everything is by the T.O. Guidance in signing of Red X is in 00-20-1 para 4.5. I have reviewed training records. He is signed off and qualified to be authorized to Sign All Condition Tags IAW Documentation Guidance IAW TO 00-20-3. I have reviewed training records. He is signed off and qualified to be Authorized to NRTS Documentation Guidance IAW TO 00-20-3. A records review was conducted on records. There are 22 tasks remaining to meet his 7 level requirements for the c-135 airframe. He is encouraged to continue his retraining progress. No discrepancies noted at this time. All records are current and accurate. 2012-02-09 135 Inlets and Exhaust 135 Inlets and Exhaust class was completed on 23 Jan 2012. 2012-01-25 B-Series Maintenance Stand Safety Brief Air Force Safety Center has identified a discrepancy with all B-series maintenance stands. These stands do not have proper fall protection IAW regulation , 29 CFR 1910.23(a)(2). Fall hazard exists when using B-series stands (i.e. open area at b-5 stand ladder/platform access point and b-4 step/platform access point). The individual has been briefed and is aware of the risks when using all B series maintenance stands. A records review was conducted on records. There are 38 of 350 open tasks remaining to meet his 7 level requirements for the c-135 airframe. He is encouraged to continue his satisfactory retraining progress. No discrepancies noted at this time. All records are current and accurate. 2012-01-21 90 Day review 2011-11-21 Supervisor Deployed will be deployed from 5 December 2011 to 15 March 2012. he is deployed. 2011-10-28 30 day review I reviewed TBA entries today for accuracy and completion. There were no errors noted on this date. Signed off on 38 tasks during this time will review remaining tasks with and create a training plan. 2011-10-17 Tasks restored from archive on 2011-10-17 2011-10-17 Initial Evaluation/Workcenter Orientation 152 Tasks were restored from archive on 2011-10-17 2011-10-17 Tasks restored from archive on 2011-10-17 2012-03-02 In progress 2011-10-17 Tasks restored from archive on 2011-10-17 will be interim supervisor while I conducted an initial evaluation with on 20111017. We reviewed his current level of competency and current qualifications, and also discussed the level which he needs to progress to. In addition, we identified his AFSC, duty position and wartime/UTC training requirement listed in the workcenter Master Training Plan. Additionally, he was briefed that his training is ultimately his responsibility, and he needs to ensure he reviews his training records at least once a week and actively pursues the training he needs to complete his upgrade. He has also been briefed that tasks should be signed off within 30 days of the start date, unless mission requirements prohibit the completion of the task within that time. I conducted a workcenter orientation with on 20111017. Items covered include chain of command, duty locations and hours, office symbol, phone number, and proper work habits. In addition, we covered workcenter safety and base specific security directives and the importance of good communication both up and down the chain. We also covered recall policies and procedures and mobility requirements. Finally, we discussed off duty employment and educational opportunities. 152 Tasks were restored from archive on 2011-10-17 CFETP - 2A5X1-006 - 001.001.001.001.002.008 is still in training on this task as not very many opportunitys have presented itself to get complete training on this major inspection. Task was restored from archive on 2011-10-17 RC-135V, T/N 64-14848, 30 April 2015 T-121 CERTIFICATION I CERTIFY THAT THIS INDIVIDUAL TRAINING RECORD IS CURRENT AS OF 2015-05-04 _____________________________ TRAINEE SIGNATURE _____________________________ SUPERVISOR SIGNATURE RC-135V, T/N 64-14848, 30 April 2015 T-122 TECHNICAL PROCESS SPECIFICATION 3-100 DEPOT WORK DIRECTIVE ....... U-4 DEPOT WORK ORDER TICKET ................................................................................. U-10 4848 INTEGRATE MAINTENANCE DATA SYSTEM HISTORY ............................ U-15 U2. U3. U4. RC-135V, T/N 64-14848, 30 April 2015 1 AIR FORCE TECHNICAL ORDER FORM 95 .............................................................. U-3 U1. AIRCRAFT MAINTENANCE RECORDS, NOT INCLUDED IN TAB H OR O TAB U INTENTIONALLY LEFT BLANK 64-14848, 30 April 2015 2 DATE 2014171 SN 01 * TCTO NUMBER/NARRATIVE * 1RC-TC135-1154 LCS VALVE REDUCTION DATA CODE *STAT* ACC BY *HMC* *P/F* 0104809 22 796 ~ DATE 2014171 T P * TCTO NUMBER/NARRATIVE * DATA CODE *STAT* ACC BY *HMC* *P/F* 1RC-TC135-1134 0103441 22 796 REPLACEMENT OF APC P/N C-09335-5 WITH C- * TCTO NUMBER/NARRATIVE * DATA CODE *STAT* ACC BY *HMC* *P/F* L551403 L551403 03 D 798 OTI OF AIRCRAFT ACTUATOR CARTRIDGE INSTA I I RC-135V, T/N 64-14848, 30 April 2015 U-3 Https ://imds-octf. csd. disa.mil/txl/fs 6/19/2015 VERSION DATE: 052115 SN DESGN-P/N (ITEM INST) S/N NHA'S TIME AC LOGS ITEM'S TIME 03 206090-4-1 0000060831 39061.7 7420 0.0 CONF LOC/POS: LEFT WUC/LCN: 4123P SN LINE*[--------- NARRATIVE DATA----------] 02 00 ON THIS DATE A4848 RETURNED TO OFFUTT AFB FROM PDM. SN 01 SN DESGN-P/N (ITEM INST) S/N NHA'S TIME AC LOGS ITEM'S TIME 03 ON389698-1 0000017873 38734.6 7327 0 CONF LOC/POS: WUC/LCN: 65BBC TRANSACTION PROCESSED DATE 2014170 L/N: DATE 2014170 P DATE 2014170 DATE 2014171 L/N: T P J SN 02 ------------------------------------------------------------------------------ T P - LCS VALVE REPLACEMENT ------------------------------------------------------------------------------ T P - ;~;::~~i~:--~~--~:~~~~:~~~~~~~~~;;;.;~;~-:--~~i~:~~~~-:~~~;:-~~~-;~-:~~~:-:;;;:-- I ~ T~P t Page 6of6 IE REV ND loflS DATE ISSUED DWU NO 22 May 2014 TP53-100 TITLE ?annel-Inna Rue-{me OXYGEN SYSTEMS. INSTALLATION OF Each portiOn Of the de?nition data set is at the same revision sIaIus. See page i for notes. revision history. and approvals. 3.1 3.1.1 3.2 3.2.1 3.2.2 3.2.3 3.2.4 3.2.5 3.2.6 3.2.7 3.2.8 3.2.9 3.2.10 3.2.11 3.2.12 3.2.13 3.2.14 3.2.15 3.2.16 3.2.17 3.2.18 3.2.19 3.2.21} TECHNICAL PROCESS SPECIFICATION TABLE OF CONTENTS ORDER OF PEEGEOENCE. APPLICABLE GOVERNMENT NON-GOVERNMENT DOCUMENTS. EQUIPMENT, OXYGEN TANKS. NON-BREATHING BREATHING FLEXIBLE IIOSES. HOSES. TUBING. THREAD SEAL TAPE GASEOUS OXYGEN. ..6 LIQUID GROMMET CAPS AND PLUGS. ..6 TEST STRINGER CLIP. WASHERVquNDSCREW CONICAL PLASTIC BAGS AND SLEEVES. .u 3-52215-HMay 201-11 45h ?hull rum-.qu Ils-L' mun-Ilium In uJII-Inulimgm I lhIL' (ref. I urn-n mush-nu: or Ito-mums nrnulluq ?mocking: u1l11 L'lfl'll'l'uJU' il uh nu "ulnluny. and on! ulnl'lII'?Ilml Ilr wulgl -1 :nl-quLI-nn I?Lll :runmu - nl 64-14848, 30 April 2015 U-4 '19 DATE ISSLI ED 22 May 2014 DING NO REV TPS3- 00 PAGE m: 2 of 15 TITLE Racial-n: OXYGEN SYSTEMS, INSTALLATION OF 3.3 3.3.1 3.3.2 3.3.3 3.3.4 3.3.5 3.3.5 3.3.7 3.3.7.1 3.3.3 3.3.91I 3.3.10 3.3.11 3.3.12 3.3.13 3.3.14 3.3.15 3.3.16 3.3.18 3.3.19 3.3.20 3.3.21 3.3.21.1 3.3.21.2 3.3.21.3 3.3.21.4 3.3.21.5 3.3.21.6 3.3.22 3.3.22.1 3.3.22.2 3.3.22.3 3.3.23 3.3.24 3.3.25 GENERAL SAFETY AND CHEMICAL HANDLING. PERSONNEL TRAINING. HANDLING OF CLEANED TOOLS. PRESSURE CLEANING REQUIREMENTS. . CONTAMINATION INSPECTION BY BRIGHT WHITE LIGHT METHOD. . ELECTRICAL GROUNDING. OPENING OF SYSTEM. OXYGEN SYSTEM STORAGE OF TIME LIMITATIONS. CONVERSION HIGH PRESSURE FLEXIBLE . LOW PRESSURE TUBE .. . ORIENTATION AND SEPARATION REQUIREMENTS. CABLE. I-IOSES. AND MOVING PARTS ELECTRICAL COMPONENT E: WIRING . . FUEL. OIL. AND HYDRAULIC FLUID PIPING HEATED COMPONENT SEPARATION. RIGID PARTS CLEARANCE. MAINE AND DISCONNECT CLEARANCE. MOUNTING OF OXYGEN LINES AND BREATHING .. CLAMPS AND SUPPORTS. VIBRATION AND FITTING INSTALLATION OF HOSES. . . . If] ..10 . ?17' . 2014) (ref. CSF-WI-ZI 9] shall manual- cun?duulalng nl' In Ihum I13 nnlpany. Indian:- atlm cunl'IdmLuI abaul Lh: Comping. 01':an when dliclosuru II uulhomcd 0t IcyaIIy mnndalud. shaII meL-cl L4 dammit-ms and In transmitting and L-J Inlarmahnn All al' or pfcm'mury 51m? be atcurdancc ?'Ilh applicable palm. RC-135V, 64-14848, 30 April 2015 U-5 REV PAGE NO 3 DUE DATE ISSUED DWG ND 22 May 2014 TITLE Aerospace Systems OXYGEN SYSTEM 5. INSTALLATION OF 3.3.25.1 3.3.25.2 3.4 3.4.1 3.4.2 3.5 3.5.1 3.5.2 -1 J. 3.6.1 3A2 3.6.3 4. 4.2 4.3 5.1 6. ELI 6.3 (3.2.1 6.2.2 6.2.3 6.2.4 6.2.5 6.3 CONNECTION TO 5204-05A-S9 12 CONNECTION TO ALUMINUM FITTINGS. INSTALLATION USING CONE AND SEAL FITTINGS. I2 INITIAL TORGUING. FINAL TORQUING. INSTALLATION USING FLARE AND FLARELESS TYPE INITIAL FINAL TOROUING. INSTALLATION USING PIPE THREAD FITTINGS. THREAD SEALING. QUALITY ASSURANCE RESPONSIBILITY FOR INSPECTION MONITORING PROCEDURES FOR EQUIPMENT USED IN l3 MONITORING PROCEDURES FOR MATERIALS USED IN l3 OXYGEN SYSTEM TESTING. LEAKAGE LOX SYSTEM PRESSURE DECAY. GOX SYSTEM PRESSURE LOX EYAPORATION LOSS FUNCTIONAL TESTS. PREPARATION FOR DELIVERY. AIRCRAFT NOTES. SURFACE .. l5 HIGH PRESSURE GASEOUS OXYGEN SYSTEM PRESSURE GASEOUS OXYGEN DRAWING NOTE Il{May 2014} (ref. CSP-WI-2 i9} unplumcs shall mmnlaln '1ch ol' In lug. Campus. and any :unhdumul Inl'mmamq .1me the ?ha-n aulhot-ch a legally mandaud pr 1,3,15 Emu [mum documunu' :1rul L15l'.? Ln ruimamg L-I- inrmnuIImI. All arranJIdanInl or propncury Shall be In ucurdancc :nmpang. pniIcI RC-135V, 64-14848, 30 April 2015 U-6 i3 - ISSUED DING VD REV PAGE NO 22 Mag,r 20H TPSS-I 00 12 of 15 Aerospace Systems OXYGEN SYSTEMS. INSTALLATION OF 3.3.22.3 3.3.23 3.3.24 3.3.25 3.3.25.1 3.3.25.2 3.4 3.4.1 3.4.2 3.5 3.5.2 Vibration and cha?ng. All tubing shall be mounted to prevent 1vibration and cha?ng by using rubberized or cushioning clamps. Oxygen system components shall not strike against the aircraft structure or other components during aircraft vibration and shock encountered during normal use ol'the aircraft. Insulation. ll'requircd by the engineering drawing due to proximity to electrical or heat sources. the oxygen lines shall be insulated per l?l?hj- I '42 Type I or Type 2. Fla reless ?tting installationi?assembly. Flareless ?ttings shall be fabricated per 1 l?hE- 1 ill. Installation of hoses. Connection to coupling. When connecting hoses to Parker-Hannitin 5204-USA-59 quicl-t disconnect couplings. a lit conical washer shall be installed between the hose and the coupling. Connection to Silo? aluminum ?ttings. ll' leaks are present after connecting hoses to Silo" aluminum ?ttings tea. ASID34DUSDS. ASIGBSDUSUSUS. ASID36DUSUSUSUS. A554UGDUS. conical washers may be installed between the hose and the ?tting where the leak exists. Installation using cone and seal type ?ttings. initial torquing. lland tighten while pressing the cone and seal ?rmly together. The nut shall not be used to align the tubing or to draw the cone and seal into contact. The out shall have an initial torque ot'50 lit lit-lb. prior to pressure testing. Final torquing. It~ leakage occurs after testing per 4.5.l, depi'essurizc the system and examine seal and cone for nicks. eccentricity. or other defects and cancel as necessary. Repeat tightening. and retnrque to eliminate leaks while not exceeding Ills-lb. ll'leaks occur. repair or replace as necessary. Installation using ?are and ?areless type ?ttings. The following requirements apply to all sizes. Initial torquing. Hand tighten while pressing the sealing surfaces ?rmly together. The nut shall not be used to align the tubing or to draw the ?are to the ?tting. The nut shall have an initial minimum torque value as specified in I it prior to checking l'or leaks. Final torquing. ll" leakage occurs alter testing per depressurixe the system and increase torque required to stop the leakage. Do not exceed the maximum torque 1value given in .hltl I II. If leakage cannot be repair or replace as necessary. lrel' 9i Lat-'15 mealtimes Ill-ill maintain the ol'mfiirrniilitm entrusted to them l:i_i the Company. and ting. ntlte-t connection: about (cunning. ciccpi itlim ducleauin: Ii a; lean", mama tnfornution shall protect L-J dot: Litticnts and use dime on In and rel-hum; InfrIHIialtni-i All ol confidential or pttipxuinrt infant-taint" shall be "1 accordance ii applicable COII'l-pill'l'. poliei. RC-135V, 64-14848, 30 April 2015 U-7 DATE ISSUED DWG ND REV PAGE NO 22 May 2014 TP53-100 13 or 15 l'th.E Aerospace Systems PO BOX (1051': GREENVILLE. TEXAS TS-IliIi-l'rtlin OXYGEN SYSTEMS, INSTALLATION OF 3.6 3.6.1 3.6.2 3.6.3 4.2 4.3 TABLE II TORQUE VALUES FDR FLARE AND FLARELESS TYPE FITTINGS Tubing 0.0. {in} AME 4071 Aluminum AMS 5560 CRES {in-1b.] tin.-ib.] Min. Max. Min. MaxI35 150 53?16 [[10 125 [1?0 200 ISIS 200 ?431') 500 855 9-45 1 'Flt} 790 140 1260 Installation using pipe thread ?ttings. Torquing. The ?ttings shall be torqued to the minimum value necessary to eliminate leakage after testing per 4.5.I and be within the torque values of TABLE TORQUE VALUES FOR PIPE THREAD TYPE FITTINGS Tubing 0. D. tin.) Min. (in. th.) Max. (in. 113.} [1'8 4? 15h U4 60 200 3f8 1th 400 Thread sealing. Seal pipe threads using tape per A-A-58092. When applying the tape. skip the first two rows of threads to prevent contamination of the oxygen space. Do not apply more than two layers of tape to the pipe threads. Pu rging. The system shall be purged per the appropriate Technical Order. Aircrall Maintenance Manual or established industry procedures. Only trained personnel per 4A and those directly involved with the purging procedure shall be permitted on or around the aircraft while purging 1with oxygen. QUALITY ASSURANCE PROVISIONS. Responsibility for inspection. Organizationally assigned personnel responsible for performing the requirements described herein are also primarily responsible liar ensuring the quality of the process activities. Other personnel within the operating department. or others as deemed appropriate by management may be assigned to verify compliance with requirements listed herein. Quality Assuranco departments may perform inspections or audits as necessary to provide adequate oversight of process controls. Monitoring procedures for equipment used in process. The process owner or department performing the procesa shall verify by process audits or inspection that all equipment used in this process are per the requirements speci?ed herein. Monitoring procedures for materials used in process. The process owner or department performing the process shall verify by process audits or inspection that all materials used in this process are per the requirements speci?ed herein and are within any applicable shelf life limits. 20141 (ref. employces. stall the t?If Inlittmalmn to them in the Comping and an}. other :onfldentlol about the Compnni ?hm disclosure 15 unthorucd a: legally mummy. of information sit-Ill protect documents and use in trummluulg and relating 1,-5 Informalmn All at mummy}. mfoqnuunn slmu ht- neemdnm: comp?, plig} RC-135V, 64-14848, 30 April 2015 U-8 l9 22 May 2014 N0 REV TFSS- 1 00 FAGENO l4 TITLE Aerospace Systems Po. toss TEXAS 75403-6055 OXYGEN SYSTEMS. INSTALLATION OF 4.4 4.5 4.5.1 4.5.2 4.5.3 Training. Personnel performing work per this Specification shall be trained and designated as qualified personnel by the Manufacturing or Production Department Supervisor. Trainedrquali?ed status shall be conferred on personnel who successfully demonstrate a knowledge and pro?ciency of the process and who are able to produce satisfactory work per this speci?cation. Retraining of personnel shall be performed when deemed necessary by the supervisor and-"or when there is documented evidence that substantiates unacceptable proficiency or workmanship. Oxygen system testing. when required by contract. drawing. or other governing document. tests tor system leakage. pressure decay, and evaporation loss shall be performed per the Engineering drawing. established industry procedures. or as speci?ed below. Leakage test. The oxygen system. excluding cylinders and converters. personal mounted regulators. seat pan. mask. and hard line relief valve. shall be maintained at the operating pressure while ail ?ttings. and connections are examined for leaks. All leak testing is to be done with leak test compound per All leaks should be within requirements. Proper procedures shall accompany leakage elimination. Wipe off all leak test compound after testing. LOX system pressure decay. The oxygen system shall he charged with gaseous oxygen to the Operating pressure. A?er 5 minutes. the ?rst recording of oxygen pressure is to be recorded. ?ne-half hour should elapse before the second reading of oxygen pressure. The system shall not have a pressure loss greater than what is speci?ed in Ali! .I lit. TABLE HI HOUR SYSTEM PRESSURE LOSS Liquid Oxygen System Converter Capacity - [Literal System Pressure Loss {pate} COX system pressure decay. The oxygen system shall he charged with gaseous oxygen or nitrogen to the design pressure. Alter 5 minutes. the ?rst recording of oxygen pressure. distribution line temperature. and the time are to be recorded. Four hours should elapse betiore the second reading of oxygen pressure and distribution line temperature is recorded. The system should not have a pressure loss greater than what is specified in equation P1 ?rst pressure reading {psi} P2 second pressure reading (psi) PC corrected Pi reading (Equation {1 1] TI T2 second temperature reading ?rst temperature reading t= time [in hours} between and T2 readings. Equation ll PC Pl (Pl Tlln'Tl +4601] Equation - Pclitf-?C t} is less than or equal to U.UU5 3?527IS-itMay 20h? (ref. pans umpmyui shall maintain the con?de-main: eulrusted to them by the t'nntpany and any other confidential udatmnuen about tht: C'tunpmn alum disclosure ti nuthctued cl leg-:11} amid-Ital Recipients or L115 mfmmaum ,hall t.-3 and use tn and rebuttal; 1.in All tr?nsnus?lon of con?dential or mammary utten'nmltun slutli bl: in accordance policy RC-135V, 64-14848, 30 April 2015 emu-nun. .Iu 1 II I [i'l?l'llt?l running-n TS7580R1]R 12168-11201-51 LI EA EA EA 30 1 1 1 1 1 0038 .- 0036 I Should Cost ---.····~----·· x B ~ ... ~ - '--.. ~. T T 0 0 0 7 Text item Text item Local Fabrication Local Fabrication Local Fabrication Existing: Obtain Mod/lnslall Teio:t item UC ftem Category Dffc. T I UID PAGE ~~1(-: '~ . CLOCK 76596949 11111111111 © 76596949 lnspectioh Copy W/O Number MDUQN/DRINRDRIRWK IQRC I Budget Substitute Part Number PAGE Resp. Doc. RC-135V, T/N 64-14848, 30 April 2015 U-10 / AN824-50 TEE PART OF 12168-11.270-611 Reference Item F.A June 06, 2013 04:13 PM AN815-5D PART OF 12168-11270-5611 Reference Item EA ·--·-~ OXY TUBE ASSY 12168-11201-53 0012 0011 I OXYGEN TUBE ASSY Material Reference 0008 0001 12168-11201-21 I Engineering TAPE IDENTIFICATION 12168-11270-611KT OXY R/S CLEANING KIT Item I Plamed Start Finish Date 07/2512013 10/22/2013IPaae1of5 CLOCK Planner 0010 GJ90 l.5290 !WC OXY TUBE ASSY TS7580R1 Reference Item EA Rev_ Component Description 1 SL.oc MDUQNJDR/NRDRIRWK QTY UIM Component PAGE - - Ord T11 CLOCK ~ ~"TECO 225 Diiie Prinll!d I 06/0612013 IPP01 MOUQNJDRINRDR/RWK Rs ~ !2168-11270 - 11000-0 1G12272.01.02.HABL --- WBS Description I 64-14848 I MRP Clrl Pnl Clrl I WllS - ·~ AlrcrMt Sartal I# Material Dascription CREW REST OXY SYS ISNTL Material Number 12168-11270-611M 12168-11270-611M Illllll lllll lllll lllll l~l llll lllHI 111111111 ~I ~11111 Hiii Hll Hll ~101111 H .... Serial II Prd c1r1 EA EA EA EA 1 1 2 3 EA EA 12168-11270-5611 12168-11270-5611]R BACS38Y3 BACS38Y3]R NAS623-3-14 NAS623-3-14)R NAS623-3-3 NAS623-3-3)R NAS43DD3-32 NAS43DD3-32]R NAS114900322J NAS114900332J]R MS21919WDG6 MS21919WDG6]R MS21919WDG5 MS21919WDG5]R M26626-5-25 M26626-5-25]R Reference Item AN97Q..3 AN970-3]R June 06, 2013 04:13 PM DEA 3 DEA DEA 2 l~_J_:A EA 4 QTY U/M Co~nt Debt Printed Ty1 I 06/0612013 lordPP01 GJ90 I Sloe 0056 0055 0045 0044 0043 Item Planner I I I I I Finish Daw I QRC I Should Cost Budget Subatltute 19art Number I I0501 I Iooa9 I loon I0014 0070 I ~--·---------···--·--·--·----- ·1--~sJ ---· I I I I L5290 swc Planned Start 07/2512013 10/22/2013 I Page 2 of 5 RC-135V, T/N 64-14848, 30 April 2015 U-11 I Engineering Material Reference OXY R/S CLEANING KIT I Engineering Material Reference SUPPORT, WIRE HARNESS ASSY I Engineering Material Reference SCREW PAN HEAD I Engineering Material Reference SCREW PAN HEAD I Engineering Material Reference SPACER SLEEVE-SCR&BOLT I Engineering Material Reference WASHER FLAT I Engineering Material Reference CLAMP LOOP,SUPPORT I Engineering Material Reference CLAMP LOOP,SUPPORT I Engineering Materlal Reference HOSE ASSEMBLY OXYGEN AS440700505 PART OF 12168-11270-5611 I Engineering Material Reference WASHER FLAT Rev Component Description 11000- Oxvaen Svstem, RJ1 MRP I 225Ctrll WBS Description 64-14848 Aircraft 1G12272.01.02.HABL Aircraft Tail I WBS 1100 I 64-14848 12168-1127Q..611M Plant Matarlal Deac:rlption CREW REST OXY SYS ISNTL Mat.rial Number 12168-11270-611 M IllH ~~111111Hll111 ~II HI~ llll llll II lllll llll l~~l II lllll l~I ~ 1111 7 7 7 7 7 7 7 7 T 7 IExisting: Obtain Mod/Install IExi:sting: Obtain Mod/Install Existing: Obtain Mod/Install Existing: Obtain Mod/Install - Existing: Obtain Mod/Install Existing: Obtain Mod/lnstaR Existing: Obtain Modllns1all Existing: Obtain Mod/lnstan Tex.titem ExisHng: Obtain Modllns1all UtD IX I1 I, Existing: Obtain Mod/~nstall __L x x x x x x x x x B l/C Item Category Deec. 76596949 11111111111 W/O Number 76596949 Inspection Copy .... ~·~- I Work *000276596949* *000176596949* *000976596949* L5290 swc I I Planner ]R ITEMS EXIST IN THE -G11KT COORDINATE WITH APPLICABLE CORRESPONDING INSTALLATIONS *********************************************************** ENSURE COMPLIANCE WITH ALL DRAWING NOTES AND APPLICABLE FLAGNOTBS FOR SPECIFIED FS STATIONS WHEN PERFORMING THIS INSTALLATION *********************************************************** **************************************************** THIS TICKET TO BE WORKED BY OXYGEN CERTIFIED PERSONNEL ONLY •••*******************•*******.******.************** Time P l _ $Wt GJ90 ' Budget Inspection Copy Qty C....tlcn Cullrlmer ·o.t. 11111111111 76596949 W/O Number 76596949 Preductton lmpection IQRC 1Should Cast Finish Data RC-135V, T/N 64-14848, 30 April 2015 U-12 >>>>>>>> Operation continued on next page «<««< I 07/25/2013 10/22/2013 I Page 3 of 5 IN THE PRECEDING BOM, THE CHARACTER ] IS USED TO SEPARATE THE BASE PART NUMBER FROM THE SOURCE OF SUPPLY/USAGE CODE. THE COMBINATION OF BASE PN AND USAGE CODE IS FOR COMPUTER SYSTEM FUNCTION ONLY. PART IDENTIFICATION SHOULD CONSIST OF THE BASE PART NUMBER ONLY. CODE DEFINITION ]C CUSTOMER FURNISHED (CFE) TO BE STOCKED AND ISSUED ]R EXISTING MATERIAL REMOVED FROM AN ASSEMBLY OR AIRCAAFT TO TO BE STOCKED AND ISSUED 111111111111111111~1111 June 06, 2013 04:13 PM 0009 1111111 0003 ' O.,.,...on PRT Sl.oc: *********************************************************** 111111111I111111111111111111111111111111 •000376596949* 0002 D... Prlnlacl I 06/06/2013 Drawing Revision Level 1 1 1 1 1~ I 111111m11111~ m11111~111~ ~~111 0001 111~1111! l~Hlll~H~lll~llB [ 11000-0x ·bOp 10~;1ber WBS DeKrlpflon 64-14848 MAP Clr1 Prd Clr1 I 225 I 1G12272.01.02.HABL Aircraft Tall I was Plant Airerafl Serial t CREW REST OXY SYS ISNTl.. 12168-11270-611 M I 1100 64-14848 Materi.i Description Mal8rtal Number 12168-11270-611M IllH ~~1111111~1 Ull llll llll~ n1101111111m~II~1111111111111111111111 ... WOftc Center l L5290 INSTALL SUPPORTS AS SHOWN IN ZN2G12. *002076596949* L5290 June 06, 2013 04:13 PM 0030 *003076596949* L5290 L5290 swc I l Planner LOCATE AND INSTALL OXYGEN HOSE ASSEMBLIES AND OXYGEN TUBE ASSEMBLIES AS SHOWN WITH REQUIRED RAW STOCK. GJOO Tim• Budget l~f) Qty Com!llletian c........ 76596949 ' 1.1f.t1i 1 ~ti1/f3 '1~J I Date llllllllWllll 76596949 Inspection Copy W/O Number In~ ';.J::) '. . _~:s t ,.~~.-u:\i"""-!\ ; u .~!) G. • ~....:o!>,,., l t.'il':. (!J -·· PreduclOn I QRC I Should Cost Finish Date RC-135V, T/N 64-14848, 30 April 2015 U-13 VERIFY BEFORE CLOSEOUT OF THIS TICKET THE CURRENT REVISION LEVEL & APPLICABLE ECO'S VERSUS ENGINEER.ING DRAWING & PARTS LIST (IF APPLICABLE) Ilml 1 ~1 ~II~~ 11111~1 ~~~~I~~ 1~1111 ~I~ 0020 Operation PRT I &Loe I 07/25/2013 10/2212013 I PaQe 4 of 5 Planned Start GOVERNMENT FURNISHED MATERIAL (GFE) TO BE STOCKED AND ISSUED MATERIAL ITEM IDENTIFIED IN THE SOW, GSOOO OR OTHER EQUIPMENT LIST TO BE STOCKED AND ISSUED. ]P ANY PART THAT J:S TO BE BUILT :IN-HOUSE FROM OEM DRAWINGS. NOT LIMITED TO, BUT TYPICALLY USED BY PDM PLANNING. JR REFERENCE MATERIAL THAT DOES NOT GENERATE AN ORDER OR REQUIRE ISSUE ]V ENGINEER.ING DESIGNED PART NUMBER NORMALLY FABRICATED IN-HOUSE BUT CODED TO PURCHASE ]U EXISTING MATERIAL NOT IN STOCK, BUT REQUIRED FOR NEXT ASSEMBLY TICKET ]X MATERIAL IDENTIFIED AS EXCESS/INACTIVE MOVED TC NEW ACCOUNT:ING VALUATION CLASS XOOO ]T SPECIAL TOOL REQUIRED FOR FABRICATION OR INSTALLATION ]G ]L 1~11~111111111111111111111111 0010 ·00107~ DatePrintad I 06/0612013 1on1rv1 PP01 »>>>>» Operation continued from previous page <<<<<<<< 111111111111111111111 0 l =Pl 11000 - OxVQen Svslem. RJ1 IMRPCtrtlPnlCtrl 225 WBS Description 64-14848 AircraftSerial# 1G122i'2.01.02.HABL Aircraft Tail t WBS 1100 I64-14848 CREW REST OXY SYS ISNTL 1216S..i1270-611M Plant Material Description Material Number 12168-11270-611M 1111111111111111111111111111111111~ IHI 1111111111 HI 111111111111111111111111111111111 12168-11270-611M WBS Description 11000 - OxVQel'l System, RJ 1 1G12272.01.02.HABL 1111 Work··· Center I ·004076596949* L5290 June 06, 2013 04:13 PM 0050 *005076596949* L5290 DalePrintlld ·Grcup#/Counter .. ·- - Operation PRT Sloe INSPBC'l' - VERIFY INS~ALLATION COMPLBTB AND SATISl!"AC'.l'ORY I SWC L5290 Time l I ...... -- Plan- I I Sub.Doc. GJ90 RC-135V, T/N 64-14848, 30 April 2015 U-14 Inspect - Verify FOD Free IAW GOP 2 111111 1111111111111 0040 I 11111111111 er ~ Op loplhbo1 225 Aircraft!klrlal# IMRPCtrllPrclClrl 64-14848 Aircraft Tall # WBS Plant I 06/0612013 1on1Typl PP01 51394288 /1 CREW REST OXY SYS ISNTl. 12168-11270-611 M I 1100 64-14848 Matllrial O...crlpllon Malarial Number Illllll lllll lllll lllll lllll llll llllll lllll lllll lllll llll llll lllll lllll lllll llllH ~ 1111 ." ' ~- :~J> ~· ·"' ··v~) ' (!) ·:~ "')' C; tw!'\i Qty ! ........ ~ CuMcinwr 76596949 1'1/(j ~/13 0.- - 111111111111111~11 W/O Number 76596949 lnspecDon I Should Collt PNduclion QRC Budgat Inspection Copy WCE DDR Discrepancy 151200078 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151196406 002 001 28 DAY FMS UPDATE REQ 151190101 004 001 FWD URINAL INOP 151190102 004 001 NOTICABLE RIGHT ROLL WHEN SPEED BRAKES RAISED DURING LANDING ROLL 151190102 019 001 NOTICABLE RIGHT ROLL WHEN SPEED BRAKES RAISED DURING LANDING ROLL 151190098 001 001 DSS RPU #2 WILL NOT APPLY OR DISPLAY 3.3V, 5V, + OR - 12V, A ND FAN POWER 151190099 001 001 ONE SLICE IN EAP 131 FAILED RFD CALL TEST 151190065 001 001 A/C REQ'D SUPPORT FOR LAUNCH 151190096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151190096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151190096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151190096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151190096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151190096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151190096 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151190096 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151180207 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 151180290 003 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180291 003 001 INFLT THE ANTISKID ONLY SHOWED RELEASES ON THE OUTBOARDS ONL Y. INBRDS WERE BLANK. TESTE 151180307 003 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180307 003 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180311 003 001 INFLT THE ANTISKID ONLY SHOWED RELEASES ON THE OUTBOARDS ONL Y. INBRDS WERE BLANK. TESTE 151180307 004 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180307 004 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180290 019 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180292 001 001 DMCA5 RCVR 8, TUNER 1 CAUSES SPIKES IN PAN 500 MHZ- 2-5GHZ 151180308 001 001 DMCA5 RCVR 8, TUNER 1 CAUSES SPIKES IN PAN 500MGZ-2.5 GHZ 151180307 004 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180288 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151180288 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151180288 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151180288 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS RC-135V, T/N 64-14848, 30 April 2015 U-15 JCN WCE DDR Discrepancy 151180288 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151180288 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151180288 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151180307 009 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180290 003 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180290 003 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180290 003 001 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION 151180288 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151170085 003 001 MANIFOLD VALVE LIGHT ON AR PANEL WON'T ILLUMINATE WHEN PLACE IN THE REFUEL POSITION 151170087 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151170087 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151170087 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151170087 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151170087 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151170087 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151170087 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151170087 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151150047 019 001 #4 PMC INDICATED SPLIT N2 & DEMAND POINTER; #4 ENG 5% LOWERN 2 W/ THROTTLES ALLIGNED; PM 151150047 019 001 #4 PMC INDICATED SPLIT N2 & DEMAND POINTER; #4 ENG 5% LOWERN 2 W/ THROTTLES ALLIGNED; PM 151150047 003 001 #4 PMC INDICATED SPLIT N2 & DEMAND POINTER; #4 ENG 5% LOWERN 2 W/ THROTTLES ALLIGNED; PM 151150047 003 001 #4 PMC INDICATED SPLIT N2 & DEMAND POINTER; #4 ENG 5% LOWERN 2 W/ THROTTLES ALLIGNED; PM 151150047 003 001 #4 PMC INDICATED SPLIT N2 & DEMAND POINTER; #4 ENG 5% LOWERN 2 W/ THROTTLES ALLIGNED; PM 151140180 003 001 LEFT HAND PACK OVERPRESSURIZES GIVES UUUU ERROR ON FLOW CONT ROLLER 151140180 003 001 LEFT HAND PACK OVERPRESSURIZES GIVES UUUU ERROR ON FLOW CONT ROLLER 151140180 003 001 LEFT HAND PACK OVERPRESSURIZES GIVES UUUU ERROR ON FLOW CONT ROLLER 151140180 003 001 LEFT HAND PACK OVERPRESSURIZES GIVES UUUU ERROR ON FLOW CONT ROLLER 151140180 003 001 LEFT HAND PACK OVERPRESSURIZES GIVES UUUU ERROR ON FLOW CONT ROLLER 151140180 003 001 LEFT HAND PACK OVERPRESSURIZES GIVES UUUU ERROR ON FLOW CONT ROLLER 151140180 004 001 LEFT HAND PACK OVERPRESSURIZES GIVES UUUU ERROR ON FLOW CONT ROLLER 151130110 002 001 RADAR INSTRUMENTATION NOT DISPLAYING. BLINKED AT FIRST THEN BLACKED OUT COMPLETELY. SCOP 151130110 002 001 RADAR INSTRUMENTATION NOT DISPLAYING. BLINKED AT FIRST THEN BLACKED OUT COMPLETELY. SCOP 151130114 003 001 LH LANDING LIGHT C/B POPPED IN FLIGHT RC-135V, T/N 64-14848, 30 April 2015 U-16 JCN WCE DDR Discrepancy 151130114 003 001 LH LANDING LIGHT C/B POPPED IN FLIGHT 151130107 001 001 DFS-3 (DMCA 5A) FAILS RADIATED BITE FOR NOT HAVING UPDATED B ORESIGHT 151130108 001 001 ES822 #4 RCVR 1 FAILS ]CRS FOR AUDIO 151130109 001 001 UHF #4 WILL NOT TX 151130106 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151130106 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151130106 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151130106 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151130106 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151130106 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151130106 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151130106 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151120014 004 001 E2 ANTENNA MOUNT LOOSE POSSIBLY CRACKED 151120014 004 001 E2 ANTENNA MOUNT LOOSE POSSIBLY CRACKED 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120014 001 001 E2 ANTENNA MOUNT LOOSE POSSIBLY CRACKED 151120059 001 001 A/C REQ'D SUPPORT FOR LAUNCH 151120012 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151120012 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151120012 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151120012 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS RC-135V, T/N 64-14848, 30 April 2015 U-17 JCN WCE DDR Discrepancy 151120012 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151120012 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151120014 008 001 E2 ANTENNA MOUNT LOOSE POSSIBLY CRACKED 151120012 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120006 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 151120007 003 001 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION IAW 1-C135-6 2-A-03 151120008 003 001 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO FREQ 000060H DUE 39383.3HR PSN OWC 151120012 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151110028 002 001 WATER SUSPECTED IN RADAR PRESSURE LINES 151110030 002 001 RADAR REQS IFOC. SEE JCN 151100193 WCE 001 FOR ORIGINAL DISC REPANCY 151110162 001 001 IFCD #6 ISSUES 0006/0086 TYPE MISMATCH FOUND 151110164 001 001 DMCA #4B UNABLE TO ALLOCATE SIG APP 151110037 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110037 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110037 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110038 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110038 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110038 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 RC-135V, T/N 64-14848, 30 April 2015 U-18 JCN WCE DDR Discrepancy 151110039 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110039 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110039 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110040 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110040 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151110040 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 151100175 002 001 TCAS FAIL IN CHOCKS. MX ATTEMPTED TO CORRECT, BUT PROBLEM CO RRECTED ITSELF. AFTER FLIGHT, 151100175 002 001 TCAS FAIL IN CHOCKS. MX ATTEMPTED TO CORRECT, BUT PROBLEM CO RRECTED ITSELF. AFTER FLIGHT, 151100175 002 001 TCAS FAIL IN CHOCKS. MX ATTEMPTED TO CORRECT, BUT PROBLEM CO RRECTED ITSELF. AFTER FLIGHT, 151100193 002 001 RADAR MAG FAIL DURING FLIGHT MULTI TIMES. NO SWEEP, FAULT CO DES 0209 AND 0202 AND MAG FAI 151100216 002 001 7 LEVEL INSPECTION REQUIRED FOR RECUR SEE JCN 151100193 151100009 003 001 7 DAY LCS INSP DUE IAW ETM-RC135-6 151100177 004 001 FUEL DUMPED 25K INFLT 151100188 001 001 ENCOUNTERED HEAVY SMOKE AND BURNING SMELL FROM THE PCA AND/O R MONITOR PANEL IN THE CO 151100188 001 001 ENCOUNTERED HEAVY SMOKE AND BURNING SMELL FROM THE PCA AND/O R MONITOR PANEL IN THE CO 151100182 001 001 SPARE INTERPHONE FCD DROPS CONNECTION TO SYSTEM 151100183 001 001 E10 FAILS RADIATED BITE AT FREQ 348.01 MHZ ACROSS ALL DF'S 151109615 001 001 *REDBALL* ELINT RAID NOT CONNECTING TO LAN 151100173 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151100173 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151100173 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151100173 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151100173 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151100173 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151100173 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151100173 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151086420 002 001 RADAR PRESSURE DEHYDRATOR WAS PINK UPON PHYSICAL INSPECTION, SILICA REQUIRES REPLACEMEN 151070070 008 001 SECONDARY STRUCTURE/PANEL INSP DUE PRIOR TO NEXT FLIGHT IAW OAFBI 21-100 PARA 7.2.1 151070070 008 001 SECONDARY STRUCTURE/PANEL INSP DUE PRIOR TO NEXT FLIGHT IAW OAFBI 21-100 PARA 7.2.1 151060153 002 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O 151060153 002 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O 151060153 002 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O RC-135V, T/N 64-14848, 30 April 2015 U-19 JCN WCE DDR Discrepancy 151060153 002 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O 151060153 002 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O 151060153 002 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O 151060153 002 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O 151060153 002 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O 151060154 002 001 TCAS INOP DURING DESCENT- KNOWN TRAFFIC WITHIN NORMAL OPERAT ING ENVELOPE NOT DISPLAYE 151066407 002 001 RADAR SYSTEM INTERMITTENTLY BLANKS WHEN RADAR PRESSURE PLACE D IN NORMAL ON AT 34 PSI 151066407 002 001 RADAR SYSTEM INTERMITTENTLY BLANKS WHEN RADAR PRESSURE PLACE D IN NORMAL ON AT 34 PSI 151060156 004 001 #1 ENG COWLING OPEN TO FOM 151065420 017 001 A/P J1 CANNON PLUG REQUIRES RELOCATION 151065420 017 001 A/P J1 CANNON PLUG REQUIRES RELOCATION 151065420 017 001 A/P J1 CANNON PLUG REQUIRES RELOCATION 151065420 017 001 A/P J1 CANNON PLUG REQUIRES RELOCATION 151060153 001 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O 151060153 001 001 RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS O 151060155 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151060155 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151060155 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151060155 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151060155 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151060155 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151065410 008 001 ALL INSP ERQ. C/W PRIOR TO NEXT FLIGHT 151065410 008 001 ALL INSP ERQ. C/W PRIOR TO NEXT FLIGHT 151065410 008 001 ALL INSP ERQ. C/W PRIOR TO NEXT FLIGHT 151065410 008 001 ALL INSP ERQ. C/W PRIOR TO NEXT FLIGHT 151060155 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151060155 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151050109 002 001 RADAR INOP SHORTLY AFTER TAKEOFF. MAGNETRON FAIL .05- EVEN A FTER MULTIPLE RESTARTS 151054510 002 001 UPPER LEFT NUTPLATE BROKEN ON NAV RADAR MONITOR. SCREW REMOV ED TO PREVENT FOD. 151050108 003 001 LT PACK OVER PRESSURIZES, GIVES "UUUU" INDICATION W/LOUD RUS H OF WIND 151050108 003 001 LT PACK OVER PRESSURIZES, GIVES "UUUU" INDICATION W/LOUD RUS H OF WIND 151050107 001 001 MIDS WOULD NOT LOAD CRYPTO IN LOC 1 & 2 RC-135V, T/N 64-14848, 30 April 2015 U-20 JCN WCE DDR Discrepancy 151050105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151050105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151050105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151050105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151050105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151050105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151050105 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151050105 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151040007 008 001 30 DAY WASTE SYSTEM SANITIZING FREQ 000030D DUE 2015106 PSN 151030133 002 001 RADAR PRESSURIZATION WAS OVER PRESSURIZING THE UNIT TO 35-37 OVER THE LIMIT AT 34. THIS CA 151036410 002 001 NAV RADAR VIDEO MONITOR ETR'D FROM A4131 TO A4848 FOR TROUBL ESHOOTING SEE JCN 151030133 151036411 002 001 RADAR REQ'S OP CHK IAW ETM-RC135-2-11 PG 2-41 PARA 2.4.3A SE E JCN 151036410 151030037 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 151030090 004 001 2EA FWD URINAL VALVES REQUIRE REPLACEMENT 151030094 001 001 SUPPORT REQUIRED FOR A/C LAUNCH 151030130 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151030130 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151030130 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151030130 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151030130 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151030130 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151030130 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151030130 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151030086 001 001 BL11 TQS MOUNT REPLACEMENT TCTO NBR 1RC-TC135-1180 GRND DATE= 17331 151000169 002 001 WHEN RADAR PRESSURIZATION PUMP STARTED & STOPPED, RADAR DISP LAY BLANKED OUT COMPLETEL 151000166 004 001 # 1 MLG WHEEL AND TIRE WORN OUT OF LIMITS REQUIRES CHANGE 151000166 004 001 # 1 MLG WHEEL AND TIRE WORN OUT OF LIMITS REQUIRES CHANGE 151000166 004 001 # 1 MLG WHEEL AND TIRE WORN OUT OF LIMITS REQUIRES CHANGE 151000166 004 001 # 1 MLG WHEEL AND TIRE WORN OUT OF LIMITS REQUIRES CHANGE 151000170 017 001 MFD/PFD SCREEN AT NAV STATION WOULD BLUR FOR A FEW MINUTES A T A TIME RANDOMLY THROUGH 151000171 004 001 LEFT HYDRAULIC QUANTITY DROPPED TO 2.0 IN FLT. UPON DESCENT, LEFT HYDRO QUANTITY CAME BAC 151000168 001 001 SPARE OWS JLAN1 PORT WON'T CONNECT TO LAN SWITCH RC-135V, T/N 64-14848, 30 April 2015 U-21 JCN WCE DDR Discrepancy 151000094 001 001 SUPPORT REQUIRED FOR A/C LAUNCH 151000164 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151000164 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151000164 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151000164 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151000164 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151000164 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151000164 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 151000166 003 001 # 1 MLG WHEEL AND TIRE WORN OUT OF LIMITS REQUIRES CHANGE 151000164 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150980029 004 001 TAWS REQ IFOC DUE TO CALL OUTS SEE JCN 150970158 WCE 004 150980119 001 001 AIRCRAFT GENERATION PROFILE (SIOP)REENGINED ACFT 150980119 004 001 AIRCRAFT GENERATION PROFILE (SIOP)REENGINED ACFT 150980119 008 001 AIRCRAFT GENERATION PROFILE (SIOP)REENGINED ACFT 150980119 008 001 AIRCRAFT GENERATION PROFILE (SIOP)REENGINED ACFT 150980119 003 001 AIRCRAFT GENERATION PROFILE (SIOP)REENGINED ACFT 150980119 003 001 AIRCRAFT GENERATION PROFILE (SIOP)REENGINED ACFT 150980119 003 001 AIRCRAFT GENERATION PROFILE (SIOP)REENGINED ACFT 150980119 005 001 AIRCRAFT GENERATION PROFILE (SIOP)REENGINED ACFT 150970158 002 001 RADIO ALT #2 FDR DATA SHOWS BLIP AT 17000 FT 150970158 002 001 RADIO ALT #2 FDR DATA SHOWS BLIP AT 17000 FT 150970158 002 001 RADIO ALT #2 FDR DATA SHOWS BLIP AT 17000 FT 150970158 002 001 RADIO ALT #2 FDR DATA SHOWS BLIP AT 17000 FT 150970005 001 001 60D MODE IV/MODE C CHECK DUE IAW AFI 21-101 (RC, TC, WC SERIES ONLY) FREQ 000060D DUE 201510 150970004 008 001 60 DAY AIRCRAFT RECORDS CHECK DUE IAW AFI 21-101 FREQ 000060D DUE 2015097 PSN OWC: A83SU L 150960130 002 001 AISLE MAINT BL 10 STOPPED WORKING 150960125 004 001 WHEEL WELL DOOR LIGHT IS BURNED OUT 150960128 004 001 CARGO DOOR HANDLE FOR CAM #2 (FROM THE FRONT) A LITTLE LOOSE . 150960126 017 001 WIND SHEAR WARNING AT 17,000' FROZE WARNING ON FLIGHT DIRECT OR FOR 90 MIN. REQUIRED ALL 150960129 001 001 SPARE KEYBOARD CAPS LOCK KEY DOES NOT WORK 150960131 001 001 DMCA #4B SIG APP WILL NOT ALLOCATE 150960124 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS RC-135V, T/N 64-14848, 30 April 2015 U-22 JCN WCE DDR Discrepancy 150960124 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150960124 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150960124 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150960124 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150960124 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150960124 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150960124 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150945424 002 001 IFOC REQUIRED FOR RADAR. PER AIRCREW-1. SEE JCN 150930097 WC E 001 150945425 003 001 7 DAY LCS INSPECTION DUE 150940032 017 001 28 DAY TAWS UPDATE REQ'D 150930097 002 001 RADAR HAD NO RETURNS;SHOWED FAULT MOD PWR FAIL AND FAULT COD E 0204. TURNED OFF RADAR A 150930098 002 001 TAWS CALLED "TERRAIN" AND "PULL UP" DESCENDING THROUGH 26,00 0 FEET AND 14,000 FEET 150930098 002 001 TAWS CALLED "TERRAIN" AND "PULL UP" DESCENDING THROUGH 26,00 0 FEET AND 14,000 FEET 150930095 001 001 DF-M FAILS RADIATED BITE ON ALL ARRAYS AND ALL FREQS 150930096 001 001 EP ISSUES ERROR "CUT REPORT NAV TIME MONOTONICALLY INCREASIN G" 150930047 001 001 A/C REQ SUPPORT FOR LAUNCH 150930094 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150930094 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150930094 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150930094 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150930094 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150930094 008 002 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150930094 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150930094 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150920084 003 001 LH PACK OVER PRESSURIZED WHEN SET TO COND AIR ON CLIMBOUT AN D CRUISE ALTITUDE 150920084 003 001 LH PACK OVER PRESSURIZED WHEN SET TO COND AIR ON CLIMBOUT AN D CRUISE ALTITUDE 150920084 003 001 LH PACK OVER PRESSURIZED WHEN SET TO COND AIR ON CLIMBOUT AN D CRUISE ALTITUDE 150920084 003 001 LH PACK OVER PRESSURIZED WHEN SET TO COND AIR ON CLIMBOUT AN D CRUISE ALTITUDE 150920084 003 001 LH PACK OVER PRESSURIZED WHEN SET TO COND AIR ON CLIMBOUT AN D CRUISE ALTITUDE 150920084 003 001 LH PACK OVER PRESSURIZED WHEN SET TO COND AIR ON CLIMBOUT AN D CRUISE ALTITUDE 150920095 004 001 RIGHT SIGHT WINDOW IS DIRTY AND IS TOUGH TO SEE THROUGH 150920098 004 001 FRONT URINAL IS DRAINING A LOT SLOWER THAN NORMAL. TOOK 15- 20 MIN TO DRAIN PER USE. RC-135V, T/N 64-14848, 30 April 2015 U-23 JCN WCE DDR Discrepancy 150920047 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920089 001 001 DF-M CH 6 HAD EXCESSIVE DRIFT, CAUSED RFD BS FAILURE 150920145 001 001 A/C REQ'D SUPPORT FOR LAUNCH 150920084 004 001 LH PACK OVER PRESSURIZED WHEN SET TO COND AIR ON CLIMBOUT AN D CRUISE ALTITUDE 150920105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150920105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150920105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150920105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150920105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150920105 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150920105 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920047 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150920048 003 001 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION IAW 1-C135-6 2-A-03 150920049 003 001 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO FREQ 000060H DUE 39325.4HR PSN OWC 150920105 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150910025 002 001 RAD ALT #1 AND #2 REQUIRE SWAP FOR TROUBLE SHOOTING. SEE JCN 150900121 WCE 001 RC-135V, T/N 64-14848, 30 April 2015 U-24 JCN WCE DDR Discrepancy 150910133 008 001 INLETS AND EXHAUST REQ INSP PRIOR TO FLIGHT 150910133 008 001 INLETS AND EXHAUST REQ INSP PRIOR TO FLIGHT 150900124 002 001 AIR DATA LOADER NOT READING DISKS #005 150900121 017 001 REPEATED TAWS WARNING AFTER TAKEOFF (UP TO5 PER MINUTE). WAR NING CEASED WHEN RAD ACT W 150900089 001 001 A/C REQUIRES SUPPORT FOR LAUNCH 150900125 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150900125 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150900125 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150900125 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150900125 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150900125 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150900125 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150900125 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150896405 002 001 28D FMS UPDATE REQUIRED 150895411 003 001 7 DAY LCS INSP DUE IAW ETM-RC135-6 150895411 003 001 7 DAY LCS INSP DUE IAW ETM-RC135-6 150860056 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150860056 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150860056 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150860056 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150860056 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150860056 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150860056 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150860100 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860100 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860100 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860101 003 001 120HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR TOPCOAT CONTAMINATION IAW 1C-135-6 PG 2-A-03 150860101 003 001 120HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR TOPCOAT CONTAMINATION IAW 1C-135-6 PG 2-A-03 150860102 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860102 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860102 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860103 003 001 120HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR TOPCOAT CONTAMINATION IAW 1C-135-6 PG 2-A-03 RC-135V, T/N 64-14848, 30 April 2015 U-25 JCN WCE DDR Discrepancy 150860103 003 001 120HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR TOPCOAT CONTAMINATION IAW 1C-135-6 PG 2-A-03 150860104 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860104 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860104 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860105 003 001 120HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR TOPCOAT CONTAMINATION IAW 1C-135-6 PG 2-A-03 150860105 003 001 120HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR TOPCOAT CONTAMINATION IAW 1C-135-6 PG 2-A-03 150860106 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860106 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860106 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150860107 003 001 120HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR TOPCOAT CONTAMINATION IAW 1C-135-6 PG 2-A-03 150860107 003 001 120HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR TOPCOAT CONTAMINATION IAW 1C-135-6 PG 2-A-03 150860056 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150845410 004 001 1 EA FIRST AID KIT IN FLIGHT DECK OPENED FOR TRAINING / BROK EN ZIPPER REMOVED FROM ACFT 150830019 001 001 HDP REQUIRES CALL TEST 150830020 001 001 DMCA 2B FAILS CALL TEST 150830021 001 001 DMCA 2A FAILS CALL TEST 150830022 001 001 DMCA 4B FAILS CALL TEST 150830023 001 001 DMCA 5A FAILS CALL TEST 150830024 001 001 DMCA 5B FAILS CALL TEST 150830145 001 001 CE #1 DOES NOT GENERATE BANDSCAN WHEN SCAN TASKING ENTRY IS SET TO A BANDWIDTH OF 80 MH 150830146 001 001 DMCA 5 RXCR 1 CAUSES RFD BORESIGHT TO RAIL 20-30 MHZ 150830147 001 001 HDP FREEZES WHILE BOOTING 150830148 001 001 SI9105 #3 SHOWS POWER FAULT 150830149 001 001 HSDC-D GIVES ERROR: MOUNTING FAILED UNABLE TO FIND REQUIRED DISKS RETUAL:1 150830136 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150830136 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150830136 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150830136 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150830136 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150830136 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150830136 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150830136 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS RC-135V, T/N 64-14848, 30 April 2015 U-26 JCN WCE DDR Discrepancy 150825410 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150825410 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150820046 004 001 LT WHEEL WELL UPPER TORQUE TUBE BRACKET BROKEN REQUIRES R2 150820052 004 001 3EA LIGHTNING PATCHES REQUIRES INSTALLATION 150820053 004 001 #4 OUTBOARD WING FLAP REQUIRES MOHAIR 150820002 008 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 150820002 008 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 150820002 003 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 150820002 005 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 150810036 004 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 004 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 004 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 004 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 017 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 017 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 017 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 017 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 017 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 017 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 017 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 017 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 019 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 008 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 008 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 008 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 008 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 008 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 008 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 008 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 008 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 004 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 009 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV RC-135V, T/N 64-14848, 30 April 2015 U-27 JCN WCE DDR Discrepancy 150810036 009 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 003 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 003 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 003 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 003 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150810036 003 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150790097 002 001 TACAN #1 STAYED IN TEST MODE FROM T/O TILL LANDING 150795427 002 001 HF COUPLER ACCESS PANEL REMOVED TO FOM REMOVED PER MB 1RC/TC 135-1175 150795427 002 001 HF COUPLER ACCESS PANEL REMOVED TO FOM REMOVED PER MB 1RC/TC 135-1175 150790094 001 001 SI9105 #3 SHOWS POWER FAULT 150790095 001 001 SPARE KEYBOARD INOP 150790096 001 001 POS 1/2 LIGHT CONTROL CB INTERMITENT 150790063 001 001 A/C REQ SUPPORT FOR LAUNCH 150790092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150790092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150790092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150790092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150790092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150790092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150790092 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150790092 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150789615 002 001 *REDBALL* RADAR DISPLAY INOP 150789616 002 001 *REDBALL* RADAR INOP 150780131 001 001 CANNOT CONFIGURE SHAWNA W/TS LOAD RAID SET 9 150780097 001 001 A/C REQ SUPPORT FOR LAUNCH 150780132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150780132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150780132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150780132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150780132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150780132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150780132 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS RC-135V, T/N 64-14848, 30 April 2015 U-28 JCN WCE DDR Discrepancy 150780132 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150770079 004 001 LEFT OVER WING HATCH REQUIRES REPLACEMENT 150770079 004 001 LEFT OVER WING HATCH REQUIRES REPLACEMENT 150770079 004 001 LEFT OVER WING HATCH REQUIRES REPLACEMENT 150770146 004 001 # 3 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150770146 004 001 # 3 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150770146 004 001 # 3 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150770153 004 001 FORWARD FWD BODY PUMP VIBRATES AND MAKES LOUD NOISES WHILE R UNNING 150770153 019 001 FORWARD FWD BODY PUMP VIBRATES AND MAKES LOUD NOISES WHILE R UNNING 150770120 001 001 A/C REQ SUPPORT FOR LAUNCH 150770146 008 001 # 3 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150770146 008 001 # 3 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150770149 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150770149 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150770149 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150770149 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150770149 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150770149 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150770149 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150770153 009 001 FORWARD FWD BODY PUMP VIBRATES AND MAKES LOUD NOISES WHILE R UNNING 150770149 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150760009 008 001 30 DAY WASTE SYSTEM SANITIIZING FREQ 000030D DUE 2015078 PSN OWC: A83SU LOC OPT: POSITION: 150750155 002 001 ADL AT NAV1 STATION DID NOT LOAD AFTER MULTIPLE ATTEMPTS 150750016 003 001 7 DAY LCS INSPECTION DUE IAW TO ETM-RC135-2-3 150750016 003 001 7 DAY LCS INSPECTION DUE IAW TO ETM-RC135-2-3 150750154 017 001 TAWS PRODUCED FALSE TERRAIN WARNINGS AT FL190 AT KLNK WITH R ADIO ALTIMETER IN RAD ALT. O 150750148 001 001 AEP DOES NOT INITIALIZE 150750144 001 001 NDU WILL NOT SEND OUT NAV DATA TO COLLECTION SYSTEM 150750146 001 001 NDU A WILL NOT BOOT NDU CONFIGURED TO B SIDE 150750150 001 001 DMCA #5 RX 4 CH 1 DOWNED TO HCP ON RESET 150750152 001 001 DMCA #1 RX7 CH1 DOWNED TO HCP ON RESET 150750153 001 001 AIRCRAFT CONFIGURED FOR NDU-B RC-135V, T/N 64-14848, 30 April 2015 U-29 JCN WCE DDR Discrepancy 150750121 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150750121 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150750121 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150750121 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150750121 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150750121 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150750121 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150750121 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150750121 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150740013 008 001 PREP FOR FLIGHT 150740013 008 001 PREP FOR FLIGHT 150740013 008 001 PREP FOR FLIGHT 150730018 017 001 COPILOTS MFD REQUIRES R2 150730018 017 001 COPILOTS MFD REQUIRES R2 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 004 001 MLG STRUT REPACK 150700056 004 001 MLG STRUT REPACK 150700056 004 001 MLG STRUT REPACK 150700056 004 001 MLG STRUT REPACK 150700056 004 001 MLG STRUT REPACK 150700056 004 001 MLG STRUT REPACK 150700132 004 001 ENGINE COWL OPEN TO FOM 150700132 004 002 ENGINE COWL OPEN TO FOM 150709615 004 001 *REDBALL* RT STRUT DEFLATED RC-135V, T/N 64-14848, 30 April 2015 U-30 JCN WCE DDR Discrepancy 150709615 004 001 *REDBALL* RT STRUT DEFLATED 150700056 019 001 MLG STRUT REPACK 150700056 019 001 MLG STRUT REPACK 150700056 008 001 MLG STRUT REPACK 150700078 008 001 FUEL NOT CONFIGURED FOR FLIGHT 150700056 009 001 MLG STRUT REPACK 150700056 009 001 MLG STRUT REPACK 150700056 009 001 MLG STRUT REPACK 150700056 009 001 MLG STRUT REPACK 150700056 009 001 MLG STRUT REPACK 150700056 009 001 MLG STRUT REPACK 150700056 009 001 MLG STRUT REPACK 150700130 009 001 HYDRO MULE CONNECTED FOR DEFUEL 150700130 009 002 HYDRO MULE CONNECTED FOR DEFUEL 150700011 003 001 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO FREQ 000060H DUE 39270.8HR PSN OWC 150700012 003 001 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION IAW 1-C135-6 2-A-03 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150700056 003 001 MLG STRUT REPACK 150690195 004 001 AUX SEAT WALK AROUND BOTTLE BRACKET BROKEN 150690174 004 001 RT HYD SYSTEM WILL NOT BUILD PAST 2500 PSI WITH AUXILIARY PU 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES RC-135V, T/N 64-14848, 30 April 2015 U-31 JCN WCE DDR Discrepancy 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690145 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES 150690033 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150690033 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150690033 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150690033 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150690033 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150690033 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150690033 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150690174 009 001 RT HYD SYSTEM WILL NOT BUILD PAST 2500 PSI WITH AUXILIARY PU MP 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690145 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150690033 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150680158 001 001 ALASKA CONSTANTLY SCROLLING. DISK FREE SPACE QUERY FAILED ER RORS. 150680159 001 001 JTT LAN 49 ISSUE. 150680159 001 002 JTT LAN 49 ISSUE. 150685425 001 001 STAMPEDING SEROW QRC INSTALLED. SEE 781C 150656414 003 001 IFOC DUE ON IMP BOX CHANNEL 8 150640006 004 001 #2 WHEEL AND TIRE WORN OOL REQ R2 RC-135V, T/N 64-14848, 30 April 2015 U-32 JCN WCE DDR Discrepancy 150640006 004 001 #2 WHEEL AND TIRE WORN OOL REQ R2 150640006 004 001 #2 WHEEL AND TIRE WORN OOL REQ R2 150640006 008 001 #2 WHEEL AND TIRE WORN OOL REQ R2 150640006 008 001 #2 WHEEL AND TIRE WORN OOL REQ R2 150646405 003 001 STATIC BOOM STICK BROKEN REMOVED FOR REMANUFACTURE 150635425 003 001 A/R DOOR LIGHT PANELS REMOVED FOR T/S 150635425 003 001 A/R DOOR LIGHT PANELS REMOVED FOR T/S 150635425 003 001 A/R DOOR LIGHT PANELS REMOVED FOR T/S 150635425 004 001 A/R DOOR LIGHT PANELS REMOVED FOR T/S 150635425 004 001 A/R DOOR LIGHT PANELS REMOVED FOR T/S 150625415 002 001 28 DAY FMS UPDATE REQUIRED 150616420 003 001 IFOC DUE ON IMP BOX CH 7 SENSORS 8,9,10,11,12 PER AIRCREW -1 SEE JCN 142510082,142510083,1425 150610111 004 001 TEAR IN SKIN OF LEADING EDGE ON RIGHT A/R SLIPWAY DOOR 150610111 004 001 TEAR IN SKIN OF LEADING EDGE ON RIGHT A/R SLIPWAY DOOR 150610111 019 001 TEAR IN SKIN OF LEADING EDGE ON RIGHT A/R SLIPWAY DOOR 150610111 019 001 TEAR IN SKIN OF LEADING EDGE ON RIGHT A/R SLIPWAY DOOR 150610111 001 001 TEAR IN SKIN OF LEADING EDGE ON RIGHT A/R SLIPWAY DOOR 150610084 001 001 A/C REQUIRED SUPPORT FOR LAUCNH 150610111 004 001 TEAR IN SKIN OF LEADING EDGE ON RIGHT A/R SLIPWAY DOOR 150610110 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150610110 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150610110 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150610110 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150610110 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150610110 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150610110 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150610111 003 001 TEAR IN SKIN OF LEADING EDGE ON RIGHT A/R SLIPWAY DOOR 150610111 003 001 TEAR IN SKIN OF LEADING EDGE ON RIGHT A/R SLIPWAY DOOR 150610110 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150580031 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580031 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580031 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 RC-135V, T/N 64-14848, 30 April 2015 U-33 JCN WCE DDR Discrepancy 150580032 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580032 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580032 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580033 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580033 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580033 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580034 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580034 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150580034 003 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150579615 019 001 *REDBALL*: RT OVERWING HATCH EMER LIGHT MISSING MIRROR 150570088 001 001 ASE1 SPARE KEYBOARD BAD; KEYS LOCK UP 150570089 001 001 UHF 4 WOULD NOT LOAD CRYPTO 150570089 001 001 UHF 4 WOULD NOT LOAD CRYPTO 150570070 001 001 A/C REQUIRED SUPPORT FOR LAUNCH 150570086 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150570086 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150570086 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150570086 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150570086 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150570086 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150570086 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150570086 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150560094 002 001 VALIDATION OF PN/SN FOR SIRU 150560104 002 001 LN-120 "SIRU ALERT" SYSTEM PROCESSOR FAIL ATTEMPTED AIRBORNE ALIGNMENT UNABLE TO REALIGN 150560059 001 001 A/C REQUIRED SUPPORT FOR LAUNCH 150560103 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150560103 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150560103 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150560103 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150560103 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150560103 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150560103 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS RC-135V, T/N 64-14848, 30 April 2015 U-34 JCN WCE DDR Discrepancy 150560103 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150550026 003 001 # 6 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150550030 003 001 LH 35 DEG CONTROL VALVE INDICATOR INOP (VALVE ACTUATES CORRE CTLY) 150550030 003 001 LH 35 DEG CONTROL VALVE INDICATOR INOP (VALVE ACTUATES CORRE CTLY) 150550030 003 001 LH 35 DEG CONTROL VALVE INDICATOR INOP (VALVE ACTUATES CORRE CTLY) 150550026 004 001 # 6 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150550026 004 001 # 6 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150550026 004 001 # 6 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150550026 004 001 # 6 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150550026 008 001 # 6 WHEEL AND TIRE WORN OUT OF LIMITS REQUIRE R2 150550036 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150550036 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150550036 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150550036 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150550036 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150550036 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150550036 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150550036 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150540025 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150540025 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150540025 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150540142 003 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN 150540142 003 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN 150540142 003 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN 150540142 003 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN 150540142 003 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN 150540142 003 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN 150540142 003 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN 150540142 003 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN 150540142 003 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN 150540143 001 001 BP6 WOULD NOT POWER ON 150540142 004 001 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN RC-135V, T/N 64-14848, 30 April 2015 U-35 JCN WCE DDR Discrepancy 150510091 004 001 LEFT OVERWING HATCH PIVOT HOOK NEEDS TO BE ADJUSTED. WHILE I N FLIGHT, DOES NOT ENGAGE. 150510090 001 001 KESTREL B DOES NOT RECOGNIZE A/D DEMOD CARD 150510092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150510092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150510092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150510092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150510092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150510092 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150510092 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150510092 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150505411 017 001 # 1 KDU INOP 150500087 008 001 SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OA FBI 21-100 PARA 7.2.1 150500087 008 001 SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OA FBI 21-100 PARA 7.2.1 150499615 003 001 *REDBALL* #4 GEN LOW RPM LIGHT ILLUMINATED 150499615 003 001 *REDBALL* #4 GEN LOW RPM LIGHT ILLUMINATED 150490167 001 001 PLP INTERMITTENTLY GIVES MORPH-B 100MHZ INPUT ERRORS WHEN SW ITCHING ANTENNA INPUTS. 150490172 001 001 FDP WILL NOT BOOT, WORKS FINE WITH BP2 IS CONFIGURED. 150490154 001 001 A/C REQUIRED SUPPORT FOR LAUNCH 150490004 008 001 30 DAY WASTE SYSTEM SANITIIZING FREQ 000030D DUE 2015048 PSN OWC: A83SU LOC OPT: POSITION: 150490160 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150490160 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150490160 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150490160 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150490160 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150490160 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150490160 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150490018 003 001 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO FREQ 000060H DUE 39211.8HR PSN OWC 150490019 003 001 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION IAW 1-C135-6 2-A-03 150490160 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150480195 003 001 LH FLOW CONTROLLER SHOWED "UUUU" LASTED LONGER THAN 30SECOND S. FELT AND HEARD RUSH OF 150480197 004 001 PILOT SEAT RAILS-- REQUEST LUBRICATION FOR SLIDING FORE + AF T 150480196 017 001 #3 ENG FUEL FLOW SENSOR/TRANSMITTER SEEMS TO BE LAGGING. FUE L GAUGE READING + FMS FUEL RC-135V, T/N 64-14848, 30 April 2015 U-36 JCN WCE DDR Discrepancy 150480189 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 019 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480031 001 001 LT OB FLAP UPPER OB SURFACE GOUGED AND REQUIRES SHEET METAL EVAL NEXT DOWNTIME 150480032 001 001 LT FLAP UPPER SURFACE SKIN HAS RUB SPOTS AND REQUIRES SHEETM ETAL REPAIR NEXT DOWNTIME 150480153 001 001 A/C REQD SUPPORT FOR LAUNCH 150480192 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150480192 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150480192 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150480192 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150480192 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150480192 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150480192 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480189 003 001 60 HOUR INSPECTION DUE FOR F108 ENGINES 150480192 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150430026 001 001 60D MODE IV/MODE C CHECK DUE IAW AFI 21-101 (RC, TC, WC SERIES ONLY) FREQ 000060D DUE 201504 150430025 004 001 12 MTH HOT GAS PURGE OF LOX CONVERTERS IAW T.O. 1C-135-6 FREQ 000012M DUE 2015044 PSN OWC 150430025 008 001 12 MTH HOT GAS PURGE OF LOX CONVERTERS IAW T.O. 1C-135-6 FREQ 000012M DUE 2015044 PSN OWC RC-135V, T/N 64-14848, 30 April 2015 U-37 JCN WCE DDR Discrepancy 150430024 004 001 12M PERFORM PITOT-STATIC SYSTEM AND ADC CHECKOUT PER ETM-RC135-2-11, CHAPTER 5 FREQ 00001 150430024 004 001 12M PERFORM PITOT-STATIC SYSTEM AND ADC CHECKOUT PER ETM-RC135-2-11, CHAPTER 5 FREQ 00001 150430024 004 001 12M PERFORM PITOT-STATIC SYSTEM AND ADC CHECKOUT PER ETM-RC135-2-11, CHAPTER 5 FREQ 00001 150430024 004 001 12M PERFORM PITOT-STATIC SYSTEM AND ADC CHECKOUT PER ETM-RC135-2-11, CHAPTER 5 FREQ 00001 150430024 004 001 12M PERFORM PITOT-STATIC SYSTEM AND ADC CHECKOUT PER ETM-RC135-2-11, CHAPTER 5 FREQ 00001 150430024 004 001 12M PERFORM PITOT-STATIC SYSTEM AND ADC CHECKOUT PER ETM-RC135-2-11, CHAPTER 5 FREQ 00001 150430024 004 001 12M PERFORM PITOT-STATIC SYSTEM AND ADC CHECKOUT PER ETM-RC135-2-11, CHAPTER 5 FREQ 00001 150430023 003 001 12M SINCE LAST PE PERFORM HOURLY INSP (F108)(EXCLUDING TC-135 SERIES) FREQ 000012M DUE 2015 150426405 003 001 3EA LOX CONVERTERS DRAINED FOR HOT GAS PURGE SEE JCN 1504300 25 WCE 001 150410077 019 001 AT QD CHUCK ASSY 1/4" OF WIRE EXPOSED 150410079 019 001 TENSION READS LOW (59 LBS) ON 14379 SETTING (HOWEVER, IT REA DS 72LBS ON 6370-1 SETTING), PA 150410082 019 001 QD ONLY HAS 2 THREADS SHOWING IN CENTER BODY 150410030 019 001 HYD TEST STAND HT05 CONNECTED TO #1 & #4 ENGINES 150410076 019 001 CHUCK ASSEMBLY AT QD, THE SLEEVE NEEDS REPLACED AND GLUED ON WITH XL8 (WORN IN 2 SPOTS 150400026 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150400026 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150400076 004 001 LT MLG FWD DOOR SEALS TORN IN MULTIPLE PLACES (M) 150400076 004 001 LT MLG FWD DOOR SEALS TORN IN MULTIPLE PLACES (M) 150400086 004 001 LEFT AND RIGHT ACM REQUIRES SERVICING 150400086 004 001 LEFT AND RIGHT ACM REQUIRES SERVICING 150400086 004 001 LEFT AND RIGHT ACM REQUIRES SERVICING 150400086 004 001 LEFT AND RIGHT ACM REQUIRES SERVICING 150400123 004 001 LT OB FLAP UPPER OB SURFACE GOUGED. REQUIRES SHEET METAL EVA L 150400125 004 001 LT FLAP UPPER SURFACE SKIN HAS RUB SPOTS, POSSIBLE CORROSION . REQUIRES SHEET METAL EVAL 150400104 019 001 #4 ENGINE FUEL PUMP QUAD BOLT RETAINER MISSING. NO FOD 150400104 019 001 #4 ENGINE FUEL PUMP QUAD BOLT RETAINER MISSING. NO FOD 150400065 019 001 DENT IN CENTERWING CAVITY DRAIN LINE BY RT WHEEL WELL AFT DO OR PADDLE. 150400105 019 001 LT OB AIL TAB MIDDLE HINGE PIN NOT IN SEGMENT 150400078 019 001 HF LONGWIRE TENSION QUESTIONABLE, WIRE 14379 INSTALLED ON JE T READS 59LBS WITH TENSIOME 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 RC-135V, T/N 64-14848, 30 April 2015 U-38 JCN WCE DDR Discrepancy 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 019 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT RC-135V, T/N 64-14848, 30 April 2015 U-39 JCN WCE DDR Discrepancy 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 019 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400153 019 001 #3 MEC VBV CABLE BRACKET BENT, MEC REQUIRES REPLACEMENT. 150400153 019 001 #3 MEC VBV CABLE BRACKET BENT, MEC REQUIRES REPLACEMENT. 150400040 004 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400039 003 001 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT RC-135V, T/N 64-14848, 30 April 2015 U-40 JCN WCE DDR Discrepancy 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150400040 003 001 ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 150370114 002 001 AISLE MAINT COMM CORD REQUIRES REPAIR. 150370003 008 001 60 DAY AIRCRAFT RECORDS CHECK DUE IAW ACCI 21-101 FREQ 000060D DUE 2015037 PSN OWC: A83SU 150366420 002 001 28 DAY FMS UPDATE REQUIRED 150360128 017 001 TAWS ALERT @5000 FEET IN THE CLIMB, STAYED ON THROUGH 11,000 UNTIL TURNED OFF. CB PULLED A 150366405 017 001 28 DAY TAWS UPDATE REQUIRED 150369615 019 001 *REDBALL* #4 LOW OIL PRESSURE LIGHT ILLUMINATED 150369615 019 001 *REDBALL* #4 LOW OIL PRESSURE LIGHT ILLUMINATED 150369615 019 001 *REDBALL* #4 LOW OIL PRESSURE LIGHT ILLUMINATED 150360130 001 002 UHF 4 HAS VSWR ERRORS IN LINE-OF-SIGHT AND SATCOM 150360132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150360132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150360132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150360132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150360132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150360132 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150360132 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150360132 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150340139 002 001 IRS1 GPS NO SIGNAL. RED W/ "--" 150340142 002 001 EIN BUS A FAIL ON LN-120. 150340043 004 001 2 EA FIRST AID KITS FORWARD OF GALLEY OVER DUE INSPECTION/ R 150340164 004 001 LEFT WING LANDING LIGHT PANEL RMVD TO RESET TAXI CIRCUIT BRE AKER 150340138 017 001 NAV CLOCK INOP. 150340141 017 001 TAWS WARNING WENT OFF AT 5000FT AND AGAIN AT FL320 WHEN TEST ED. WOULD NOT STOP UNTIL W 150340134 001 001 DMCS #2 VHF TUNERS FAIL, MULTIPLE P/C AND RESETS NO GOOD. 150340135 001 001 E9 FAIL RFD BITE TEST 150340136 001 001 POS 23 KEYBOARD HAS INTERMITTENT CONNECTIVITY. 150340137 001 001 CV131 DOWNCONVERTER COMES UP DOWN. RC-135V, T/N 64-14848, 30 April 2015 U-41 JCN WCE DDR Discrepancy 150340142 001 001 EIN BUS A FAIL ON LN-120. 150340142 001 001 EIN BUS A FAIL ON LN-120. 150340133 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150340133 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150340133 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150340133 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150340133 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150340133 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150340133 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150340133 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150330013 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150330013 003 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150330076 004 001 MAIN ACFT BATT DEAD REQ R2 150330076 004 001 MAIN ACFT BATT DEAD REQ R2 150306408 001 001 12 HOUR CURE CHK NEEDED ON GPS 1 ANTENNA. APPLIED AT 2130 150306408 002 001 12 HOUR CURE CHK NEEDED ON GPS 1 ANTENNA. APPLIED AT 2130 150306407 001 001 SCREW STRIPPED ON FMS GPS 1 ANTENNA 150300099 001 001 UHF 4 SHOWS VSWR FAULT WHEN TX 150300102 001 001 CE 4 FAILED TO CONNECT ESP GUI INTERFACE WHEN TRANSFERING PA U BUFFER TO ER 150300052 001 001 SUPPORT REQUIRED FOR A/C LAUNCH 150300096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150300096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150300096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150300096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150300096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150300096 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150300096 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150300096 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150290145 001 001 FWD BODY AFT PUMP LEAKING REQUIRES HYDRO EVAL 150290145 004 001 FWD BODY AFT PUMP LEAKING REQUIRES HYDRO EVAL 150290140 001 001 UNABLE TO RESET SSD EDAS WITH SYSTEM STATUS 150290141 001 001 E6 FAIL MULT RFD BORESIGHT TEST RC-135V, T/N 64-14848, 30 April 2015 U-42 JCN WCE DDR Discrepancy 150290111 001 001 SUPPORT REQUIRED FOR A/C LAUNCH 150290133 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150290133 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150290133 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150290133 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150290133 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150290133 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150290133 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150290145 002 001 FWD BODY AFT PUMP LEAKING REQUIRES HYDRO EVAL 150290145 003 001 FWD BODY AFT PUMP LEAKING REQUIRES HYDRO EVAL 150290133 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150280271 001 001 GPS 1 NO NAV ALL FLIGHT. NO SATS OR INTEG. FMS 1 COULD NOTBE USED FOR ANY GPS BASED NAVIGA 150280271 002 001 GPS 1 NO NAV ALL FLIGHT. NO SATS OR INTEG. FMS 1 COULD NOTBE USED FOR ANY GPS BASED NAVIGA 150284848 001 001 FWD BDY FWD A/R PUMP PRESS LINE LEAKING 150284848 002 001 FWD BDY FWD A/R PUMP PRESS LINE LEAKING 150284848 005 001 FWD BDY FWD A/R PUMP PRESS LINE LEAKING 150284848 006 001 FWD BDY FWD A/R PUMP PRESS LINE LEAKING 150284848 007 001 FWD BDY FWD A/R PUMP PRESS LINE LEAKING 150284848 008 001 FWD BDY FWD A/R PUMP PRESS LINE LEAKING 150284848 009 001 FWD BDY FWD A/R PUMP PRESS LINE LEAKING 150280273 001 001 CANNOT CONFIGURE FOR SHAWNA WITH ANY CE 150280230 001 001 SUPPORT REQUIRED FOR A/C LAUNCH 150280268 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150280268 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150280268 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150280268 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150280268 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150280268 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150280268 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150284848 003 001 FWD BDY FWD A/R PUMP PRESS LINE LEAKING 150284848 004 001 FWD BDY FWD A/R PUMP PRESS LINE LEAKING 150280268 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS RC-135V, T/N 64-14848, 30 April 2015 U-43 JCN WCE DDR Discrepancy 150270042 001 001 RH S-DUCT REMOVED FOR INSPECTION 150270042 002 001 RH S-DUCT REMOVED FOR INSPECTION 150270042 003 001 RH S-DUCT REMOVED FOR INSPECTION 150270007 001 001 120 DAY AN/ASN-121 BATTERY CAP CHECK & INSP IAW 1C-135-6 (NOT ON OC/WC-135 SERIES) FREQ 000 150270008 004 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 150270042 004 001 RH S-DUCT REMOVED FOR INSPECTION 150270008 001 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 150270008 003 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 150270008 002 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 150265410 001 001 AN/ASN-121 BATTERY REQUIRES REPLACEMENT 150260016 001 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150260016 002 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150260124 024 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 025 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260071 001 001 FRONT URINAL EXTREMELY SLOW TO DRAIN 150260124 001 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 004 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 010 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 011 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 012 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 013 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 014 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 015 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 016 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 017 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 019 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260059 001 001 DMCA# 2B FAILS RFD BORESIGHT ALL CHANNELS 150260064 001 001 DMCA2 ISSUES DMCA2 10 GIGE NOT RESPONDING TO PING CHECK CABL E 150260069 001 001 NO TX OR RX UHF #4 150260061 001 001 SUPPORT REQUIRED FOR A/C LAUNCH 150260124 027 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 028 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV RC-135V, T/N 64-14848, 30 April 2015 U-44 JCN WCE DDR Discrepancy 150260124 029 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 030 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260058 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150260058 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150260058 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150260058 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150260058 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150260058 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150260124 002 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 003 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 005 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 006 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 007 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260058 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150260124 018 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 008 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 009 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 020 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 021 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 022 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 023 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260124 026 001 (83FL) F108 HPO INSP IAW 1C-135-6WC-1 SECTION IV 150260058 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150240016 001 001 EXT RECON POWER DOES NOT WORK IN EXTERNAL BUT DOES IN APPLIE D 150239615 001 001 **REDBALL** FMS NO RAIM 150230116 001 001 POSN 1 KEYBOARD SHIFT KEY INOP 150230117 001 001 DMCA 1B FAILS RFD BORESIGHT 150230117 001 002 DMCA 1B FAILS RFD BORESIGHT 150230117 001 003 DMCA 1B FAILS RFD BORESIGHT 150230118 001 001 CAN 105 FAILS ]RFA 150230006 001 001 30 DAY WASTE SYSTEM SANITIIZING FREQ 000030D DUE 2015021 PSN OWC: A83SU LOC OPT: POSITION: 150230007 001 001 72M HALON 1211 FIRE EXTING BOTTLES DUE COMPLETE MAINT IAW T.O. 1C-135-6 FREQ 000072M DUE 2 RC-135V, T/N 64-14848, 30 April 2015 U-45 JCN WCE DDR Discrepancy 150230115 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150230115 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150230115 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150230115 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150230115 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150230115 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150230115 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150230061 001 001 60HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 FRE 150230061 001 001 60HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 FRE 150230062 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230062 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230062 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230063 001 001 60HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 FRE 150230063 001 001 60HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 FRE 150230064 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230064 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230064 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230065 001 001 60HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 FRE 150230065 001 001 60HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 FRE 150230066 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230066 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230066 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230067 001 001 60HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 FRE 150230067 001 001 60HR (+6, - AS REQ'D)INSP MAIN FUEL FILTER FOR CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 FRE 150230068 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230068 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230068 001 001 60HR (+6, - AS REQ'D) STARTER SYSTEM OIL LEVEL CHECK IAW 1C-135-6 PG 2-A-030A PARA 22A FREQ 00 150230115 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150220107 008 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 009 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 010 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 011 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 RC-135V, T/N 64-14848, 30 April 2015 U-46 JCN WCE DDR Discrepancy 150220107 015 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 016 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 017 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 018 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 021 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 022 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 023 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 024 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220043 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150220043 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150220043 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150220043 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150220043 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150220043 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150220107 026 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 027 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220043 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150220043 004 002 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150220107 001 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 002 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 004 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 005 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 006 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 007 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 012 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 013 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 014 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 020 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220107 025 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 150220126 001 001 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION IAW 1-C135-6 2-A-03 RC-135V, T/N 64-14848, 30 April 2015 U-47 JCN WCE DDR Discrepancy 150220127 001 001 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO FREQ 000060H DUE 39158.3HR PSN OWC 150220043 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150210169 001 001 LEFT AR RECEPTACLE LIGHT BURNED OUT 150219616 001 001 **REDBALL** NOSE WHEEL WELL INSP LIGHT INOP 150210165 001 001 DSS CE#7 SHOWS OFFLINE FOR WB 150210166 001 001 DSS DISPLAYS "SHAWNA DIGRX VERSION 01.001.037 IS NOT COMPATI BLE. SEE DSS.COMPATIBILITYXML" 150210167 001 001 XMP NO.1 WILL NOT PROCESS SIGNALS OF INTEREST WHILE TV IS RU NNING 150210168 001 001 XMP NO.2 WILL NOT PROCESS SIGNALS OF INTEREST WHILE TV IS RU NNING 150210169 002 001 LEFT AR RECEPTACLE LIGHT BURNED OUT 150200146 001 001 GPS INTEG WARNING ON FMS 1-GPS 1 FOR THE MAJORITY OF THE FLI GHT. CAUSES RAIM ISSUES FOR G 150200142 002 001 'OVHD PANEL LIGHTS' LIGHT STAYED ON THE ENTIRE FLIGHT WITH N O ASSOCIATED OVHD PANEL FAULT 150206420 001 001 AUX HEAT PANEL READS 8 DEGREES WHEN VALVE IS IN THE FULL COL D POSITION 150200142 001 001 'OVHD PANEL LIGHTS' LIGHT STAYED ON THE ENTIRE FLIGHT WITH N O ASSOCIATED OVHD PANEL FAULT 150200141 001 001 CORPUS SHOWS RF PHASE BORESIGHT ERRORS 150200143 001 001 EAN 105 AL WOULD NOT GO GREEN IN HCP. 150200144 001 001 EAN 105 BR WOULD NOT GO GREEN IN HCP 150200145 001 001 RACAL WOULD NOT ALLOW SIGNAL ROUTING IN MAINT. SWITCHING PAN EL. RACAL TIMEOUT. 150200171 001 001 STAMPEDING SEROW QRC INSTALLED 150200172 001 001 TEAPARTY QRC INSTALLED 150200114 001 001 A/C REQUIRES SUPPORT FOR LAUNCH 150200147 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150200147 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150200147 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150200147 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150200147 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150200147 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150200147 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150200147 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150190023 001 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150190023 002 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150160036 001 001 PRE INLETS AND EXHAUST INSP REQ PRIOR TO ENG FUNTION 150160036 002 001 PRE INLETS AND EXHAUST INSP REQ PRIOR TO ENG FUNTION RC-135V, T/N 64-14848, 30 April 2015 U-48 JCN WCE DDR Discrepancy 150155411 001 001 FWD GAP WAVEGUIDE REMOVED TO F.O.M. SEE JCN 150140118 FOR OR IGINAL DISCREPANCY 150140118 001 001 NAV RADAR WILL NOT DISPLAY CURRENT RADAR PICTURE WHILE IN SR CH/BCN/WARN. RADAR INOPERA 150140118 002 001 NAV RADAR WILL NOT DISPLAY CURRENT RADAR PICTURE WHILE IN SR CH/BCN/WARN. RADAR INOPERA 150140118 003 001 NAV RADAR WILL NOT DISPLAY CURRENT RADAR PICTURE WHILE IN SR CH/BCN/WARN. RADAR INOPERA 150140119 001 001 INS-1 GPS ANTENNA CONNECTOR PIN IS WEARING BADLY AND NEEDS R EPLACEMENT. HINDERS FUNCTIO 150140129 001 001 GPS APPROACH ON PILOT'S PFD DROPPED DURING FINAL APPROACH (S WITCHED TO COPILOT'S SIG GEN 150140123 001 001 COPILOT FLOOD LIGHT INOP 150140124 001 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 002 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 003 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 011 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 012 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 013 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 014 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 015 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 016 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 017 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 018 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140125 001 001 MULTIPLE C/B'S POPPED INFLIGHT: #2 FWD BOOST PUMP PHASE B,C #3 AFT BOOST PUMP PHASE B,C RH 150140126 001 001 SEVERAL SYSTEMS INOP W/ C/B POPS: SYD INOP (REENGAGING CAUSE D A/P TO UNCOUPLE), Q-INLET PO 150140127 001 001 ASSYMETRIC THRUST AND Q-INLET POWER LIGHTS FLICKER DURING ST AB TRIM ACTUATION 150140128 002 001 EXCESSIVE WHISTLING SOUND FROM FLIGHT DECK WHEN THROTTLES BR OUGHT BACK TO IDLE 150140128 003 001 EXCESSIVE WHISTLING SOUND FROM FLIGHT DECK WHEN THROTTLES BR OUGHT BACK TO IDLE 150140128 001 001 EXCESSIVE WHISTLING SOUND FROM FLIGHT DECK WHEN THROTTLES BR OUGHT BACK TO IDLE 150140014 001 001 FORWARD BODY FUEL TANK BLANKING OUT 150149615 001 001 *REDBALL* FWD BODY TANK BLANKS OUT 150140117 001 001 #10 AND #11 SPOILER SWIVEL LEAKING REQS RESEAL 150140117 004 001 #10 AND #11 SPOILER SWIVEL LEAKING REQS RESEAL 150140124 006 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 007 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 008 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140120 001 001 ES822 #5 WILL NOT RESET TO HCP RC-135V, T/N 64-14848, 30 April 2015 U-49 JCN WCE DDR Discrepancy 150140121 001 001 KESTREL A WILL NOT BOOT 150140122 001 001 DSS CE #9 SHOWS OFFFLINE FOR WIDEBAND 150140037 001 001 SUPPORT REQD FOR A/C LAUNCH 150140128 004 001 EXCESSIVE WHISTLING SOUND FROM FLIGHT DECK WHEN THROTTLES BR OUGHT BACK TO IDLE 150140115 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150140115 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150140115 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150140115 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150140115 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150140115 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150140115 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150140117 002 001 #10 AND #11 SPOILER SWIVEL LEAKING REQS RESEAL 150140117 003 001 #10 AND #11 SPOILER SWIVEL LEAKING REQS RESEAL 150140124 004 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 005 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 009 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140124 010 001 LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. 150140125 002 001 MULTIPLE C/B'S POPPED INFLIGHT: #2 FWD BOOST PUMP PHASE B,C #3 AFT BOOST PUMP PHASE B,C RH 150140125 003 001 MULTIPLE C/B'S POPPED INFLIGHT: #2 FWD BOOST PUMP PHASE B,C #3 AFT BOOST PUMP PHASE B,C RH 150140115 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150130155 001 001 DMCA 5 HAS STRIPPED SCREW AT 5 O-CLOCK POSITION 150130155 002 001 DMCA 5 HAS STRIPPED SCREW AT 5 O-CLOCK POSITION 150130083 001 001 MODEL3050 HOUSING POWER CABLE INSPECTION TCTO NBR 1RC-TC135-1148 GRND DATE= 17259 150120131 001 001 GPS 1 WOULD NOT ACQUIRE. FMS DISPLAY WOULD DISPLACE RED. IRS RATE >1.45 150120027 001 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150120027 002 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150120128 001 001 LEFT ACM PACK OVERPRESSURIZES WHEN GROUND MAINTENANCE CAME U P TO CHECK OUT GRAVEL NO 150120128 002 001 LEFT ACM PACK OVERPRESSURIZES WHEN GROUND MAINTENANCE CAME U P TO CHECK OUT GRAVEL NO 150120128 004 001 LEFT ACM PACK OVERPRESSURIZES WHEN GROUND MAINTENANCE CAME U P TO CHECK OUT GRAVEL NO 150120128 005 001 LEFT ACM PACK OVERPRESSURIZES WHEN GROUND MAINTENANCE CAME U P TO CHECK OUT GRAVEL NO 150120128 006 001 LEFT ACM PACK OVERPRESSURIZES WHEN GROUND MAINTENANCE CAME U P TO CHECK OUT GRAVEL NO 150120129 001 001 LEFT ACM PACK HAS GRAVEL SOUND. NOTICED ON 1ST TOUCH AND GOA ND GOT WORSE ON 2ND T&G. T RC-135V, T/N 64-14848, 30 April 2015 U-50 JCN WCE DDR Discrepancy 150120129 002 001 LEFT ACM PACK HAS GRAVEL SOUND. NOTICED ON 1ST TOUCH AND GOA ND GOT WORSE ON 2ND T&G. T 150120129 003 001 LEFT ACM PACK HAS GRAVEL SOUND. NOTICED ON 1ST TOUCH AND GOA ND GOT WORSE ON 2ND T&G. T 150120129 004 001 LEFT ACM PACK HAS GRAVEL SOUND. NOTICED ON 1ST TOUCH AND GOA ND GOT WORSE ON 2ND T&G. T 150120129 005 001 LEFT ACM PACK HAS GRAVEL SOUND. NOTICED ON 1ST TOUCH AND GOA ND GOT WORSE ON 2ND T&G. T 150120129 006 001 LEFT ACM PACK HAS GRAVEL SOUND. NOTICED ON 1ST TOUCH AND GOA ND GOT WORSE ON 2ND T&G. T 150120129 007 001 LEFT ACM PACK HAS GRAVEL SOUND. NOTICED ON 1ST TOUCH AND GOA ND GOT WORSE ON 2ND T&G. T 150120129 008 001 LEFT ACM PACK HAS GRAVEL SOUND. NOTICED ON 1ST TOUCH AND GOA ND GOT WORSE ON 2ND T&G. T 150120130 001 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120130 002 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120130 003 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120130 004 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120130 005 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120130 006 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120130 007 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120130 008 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120130 009 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120137 001 001 AEP WILL NOT LOAD RCS 150120132 001 001 HOOKDET CHANNELS 1+2 NOT RECIEVING FROM IF SWITCH 150120132 001 002 HOOKDET CHANNELS 1+2 NOT RECIEVING FROM IF SWITCH 150120133 001 001 DMCA 4 RXR4/RXR5/RXR7 PPS REFERENCE UNLOCKED 150120134 001 001 DFS3 CH5 RCVR 3 TUNER #1 FAILS TUNER BS 150120135 001 001 SINGLE CHNL PWR SUPPLY CAUSES SCROLLING "NO RESPONSE" ERRORS 150120136 001 001 HLP-C WOULD NOT BOOT. BP2 CONFIGURED AS HLP-C 150120095 001 001 A/C REQUIRES SUPPORT FOR LAUNCH 150120128 003 001 LEFT ACM PACK OVERPRESSURIZES WHEN GROUND MAINTENANCE CAME U P TO CHECK OUT GRAVEL NO 150120130 010 001 LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF 150120127 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150120127 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150120127 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150120127 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150120127 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150120127 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS RC-135V, T/N 64-14848, 30 April 2015 U-51 JCN WCE DDR Discrepancy 150120127 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150120127 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150120127 005 002 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 150090043 001 001 CURE CHECK DUE ON PILOTS NUMBER 3 CHECK AT 1530 150080138 001 001 PILOTS #3 WINDOW DELAM REQ R2 150086405 001 001 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP PRIOR TO ENG R UN 150086405 002 001 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP PRIOR TO ENG R UN 150076410 001 001 28 DAY FMS UPDATE REQ 150070072 001 001 ABIT RADOME PAINT CHIPPED 150070072 002 001 ABIT RADOME PAINT CHIPPED 150060007 001 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150060007 002 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 150060087 003 001 SHARKBYTE II ANTENNA INST TCTO NBR 1RC-TC135-1175 GRND DATE= 17269 150060087 002 001 SHARKBYTE II ANTENNA INST TCTO NBR 1RC-TC135-1175 GRND DATE= 17269 150060087 001 001 SHARKBYTE II ANTENNA INST TCTO NBR 1RC-TC135-1175 GRND DATE= 17269 150050003 001 001 1800 HR PERFORM OPS CHECKOUT OF GRAVITY FEED CONFIG (SUCTION) PER 2-5 SERIES TO FREQ 00180 150050005 001 001 ALL 4 ENG DUE GRAVITY FEED OPS CHECK 150050005 002 001 ALL 4 ENG DUE GRAVITY FEED OPS CHECK 150050005 003 001 ALL 4 ENG DUE GRAVITY FEED OPS CHECK 150050024 001 001 ROUTINE INSP OF LEFT AND RIGHT HAND MLG ACTUATORS TCTO NBR 1C-135-WA-1-1892 GRND DATE= 1 143636410 001 001 7 DAY LCS INSP DUE IAW ETM-RC135-6 143636410 002 001 7 DAY LCS INSP DUE IAW ETM-RC135-6 143630091 001 001 LEFT STATIC BOOM TAPED TO FOM SEE JCN 143500059 143630091 002 001 LEFT STATIC BOOM TAPED TO FOM SEE JCN 143500059 143630007 001 001 24M LN120 SIRU GPS INTERNAL BATTERY REPLACEMENT PER ETM-RC135-2-11 FREQ 000024M DUE 20150 143630007 002 001 24M LN120 SIRU GPS INTERNAL BATTERY REPLACEMENT PER ETM-RC135-2-11 FREQ 000024M DUE 20150 143570145 001 001 A/C REQUIRES SUPPORT FOR LAUNCH 143570123 002 001 AFT CARGO JUMP SEAT C/B CANNOT BE PUSHED IN. 143570125 001 001 ES922 #5 WOULD NOT RESET TO HCP. 143570128 001 001 SI9105 #3 WOULD NOT RESET TO HCP. 143570130 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143570130 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS RC-135V, T/N 64-14848, 30 April 2015 U-52 JCN WCE DDR Discrepancy 143570130 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143570130 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143570130 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143570130 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143570130 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143570130 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143560029 001 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 143560029 002 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 143530020 001 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 005 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 008 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 011 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 014 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 015 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 016 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 017 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 019 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530001 001 001 30 DAY WASTE SYSTEM SANITIIZING FREQ 000030D DUE 2014353 PSN 143530020 002 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 003 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 004 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 006 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 007 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 009 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 010 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 012 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 013 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143530020 018 001 #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING 143520148 001 001 WEATHER DOOR REQ REMOVAL TO FOM 143520164 001 001 MAIN ACFT BATT DISCONNECTED FOR FUEL CELL MAINT 143500059 001 001 NAVIGATOR ALTIMETER REPLACEMENT TCTO NBR 1RC-TC135-1160 GRND DATE= 17183 143500059 002 001 NAVIGATOR ALTIMETER REPLACEMENT TCTO NBR 1RC-TC135-1160 GRND DATE= 17183 RC-135V, T/N 64-14848, 30 April 2015 U-53 JCN WCE DDR Discrepancy 143500059 003 001 NAVIGATOR ALTIMETER REPLACEMENT TCTO NBR 1RC-TC135-1160 GRND DATE= 17183 143490011 001 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 143490011 002 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 143496500 001 001 SWITCH ACTUATOR ROLLER CANNED FROM A4848 TO A4131 PER / PROCESSED BY 143496500 002 001 SWITCH ACTUATOR ROLLER CANNED FROM A4848 TO A4131 PER / PROCESSED BY 143490163 001 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 002 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 005 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 009 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 011 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 012 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 013 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 014 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 015 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 016 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 017 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 018 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 020 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 021 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 022 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 023 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 023 002 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 024 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 025 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 026 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 027 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 028 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 003 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 004 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 006 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 007 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 008 001 (83FL) F-108 ACFT PREPARED FOR WASH RC-135V, T/N 64-14848, 30 April 2015 U-54 JCN WCE DDR Discrepancy 143490163 010 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 019 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 029 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 030 001 (83FL) F-108 ACFT PREPARED FOR WASH 143490163 031 001 (83FL) F-108 ACFT PREPARED FOR WASH 143480003 003 001 ACFT A&D JACKED FOR NLG SWING 143480003 005 001 ACFT A&D JACKED FOR NLG SWING 143480025 001 001 180 DAY CORROSION INSPECTION WCE 004 ONLY FOR MAJOR CCI DURING PE INSPECTION FREQ 000180 143480025 002 001 180 DAY CORROSION INSPECTION WCE 004 ONLY FOR MAJOR CCI DURING PE INSPECTION FREQ 000180 143480025 003 001 180 DAY CORROSION INSPECTION WCE 004 ONLY FOR MAJOR CCI DURING PE INSPECTION FREQ 000180 143480003 001 001 ACFT A&D JACKED FOR NLG SWING 143480003 002 001 ACFT A&D JACKED FOR NLG SWING 143480003 004 001 ACFT A&D JACKED FOR NLG SWING 143456410 001 001 28DAY FMS UPDATE REQUIRED 143440100 001 001 RT OVER WING HATCH SEAL WORN OUT OF LIMITS REQ REPLACEMENT 143440100 002 001 RT OVER WING HATCH SEAL WORN OUT OF LIMITS REQ REPLACEMENT 143440079 001 001 ACFT ON JACKS 143440079 002 001 ACFT ON JACKS 143440119 001 001 ANTENNA LEADING EDGE TAPE REPLACEMENT TCTO NBR 1RC-TC135-1170 GRND DATE= 17245 143436405 001 001 LK AND OPS CK DUE NLG LOCK RETENTION ACT IAW 1C-135-2-7-1 PG 7-87 PARA 7.15.4 143436405 002 001 LK AND OPS CK DUE NLG LOCK RETENTION ACT IAW 1C-135-2-7-1 PG 7-87 PARA 7.15.4 143436405 003 001 LK AND OPS CK DUE NLG LOCK RETENTION ACT IAW 1C-135-2-7-1 PG 7-87 PARA 7.15.4 143436405 004 001 LK AND OPS CK DUE NLG LOCK RETENTION ACT IAW 1C-135-2-7-1 PG 7-87 PARA 7.15.4 143420007 001 001 60D MODE IV/MODE C CHECK DUE IAW AFI 21-101 (RC, TC, WC SERIES ONLY) FREQ 000060D DUE 201434 143420008 001 001 60 DAY AIRCRAFT RECORDS CHECK DUE IAW ACCI 21-101 FREQ 000060D DUE 2014350 PSN OWC: A83SU 143385413 001 001 LN-120 BATT DISCONNECTED TO FOM. SEE JCN 143380016 WCE 001. SEE THIS JCN WCE 2 FOR WARNING 143385413 002 001 LN-120 BATT DISCONNECTED TO FOM. SEE JCN 143380016 WCE 001. SEE THIS JCN WCE 2 FOR WARNING 143380016 010 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 011 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 012 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 013 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 042 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION RC-135V, T/N 64-14848, 30 April 2015 U-55 JCN WCE DDR Discrepancy 143380016 043 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 044 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 048 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 049 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 050 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 051 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380036 001 001 LCS DRAIN LINE DUST COVER FWD OF FUEL CELL 1 BROKEN REMOVED 143380016 007 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 008 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 040 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 045 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 046 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380028 001 001 NLG LOCK RETENTION ACT CANN'D TO A4127 (JCN 143389615) 143386500 001 001 NLG LOCK RETENTION ACTUATOR CANNED FROM A4848 TO A4127 PER / PROCESSED BY S 143386500 002 001 NLG LOCK RETENTION ACTUATOR CANNED FROM A4848 TO A4127 PER / PROCESSED BY S 143380016 001 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 002 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 003 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 004 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 015 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 018 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 021 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 024 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 025 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 026 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 027 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 028 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 029 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 030 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 031 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 032 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 033 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION RC-135V, T/N 64-14848, 30 April 2015 U-56 JCN WCE DDR Discrepancy 143380016 036 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 037 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 038 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 041 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 035 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 039 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 034 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 005 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 014 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 006 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 009 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 047 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380028 002 001 NLG LOCK RETENTION ACT CANN'D TO A4127 (JCN 143389615) 143380016 016 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 017 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 019 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 020 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 022 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143380016 023 001 CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION 143370146 001 001 POSITION 23 FOOT SWITCH REQUIRES SCREW 143370151 001 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370151 004 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370151 005 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370151 006 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370151 007 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370151 008 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370151 009 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370151 010 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370151 011 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370155 001 001 CO PILOT MAP LIGHT INOP 143370154 006 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 007 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB RC-135V, T/N 64-14848, 30 April 2015 U-57 JCN WCE DDR Discrepancy 143379615 001 001 **REDBALL** COPILOT APC INOP 143370154 014 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 017 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 019 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 021 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 001 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 002 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 010 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 016 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 018 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370019 001 001 TEAPARTY QRC INSTALLED REQ'S REMOVAL AFTER FLIGHT 143370020 001 001 STAMPEDING SEROW QRC INSTALLED REQ'S REMOVAL AFTER FLIGHT 143370147 001 001 DRP SCREWS ARE STRIPPED THEY NEED TO BE REPLACED 143370085 001 001 SUPPORT REQD FOR A/C LAUNCH 143370145 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143370145 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143370145 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143370145 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143370145 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143370145 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143370145 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143370154 015 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 020 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370151 002 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370151 003 001 LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. 143370154 003 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 004 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 005 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 008 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 009 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 011 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370154 012 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB RC-135V, T/N 64-14848, 30 April 2015 U-58 JCN WCE DDR Discrepancy 143370154 013 001 FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIB 143370145 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143360013 001 001 FUEL LEAKING FROM CENTER WING CAVITY DRAIN. REQUIRES EVALUAT ION 143360013 002 001 FUEL LEAKING FROM CENTER WING CAVITY DRAIN. REQUIRES EVALUAT ION 143360013 003 001 FUEL LEAKING FROM CENTER WING CAVITY DRAIN. REQUIRES EVALUAT ION 143360003 008 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 008 002 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 014 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 015 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 016 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 017 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 018 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 020 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 021 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 025 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 026 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 027 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 028 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 029 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 030 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 031 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 032 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 033 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 034 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 035 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 001 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 004 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 005 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 006 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 007 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 009 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 010 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA RC-135V, T/N 64-14848, 30 April 2015 U-59 JCN WCE DDR Discrepancy 143360003 011 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 012 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 013 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 019 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 022 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 023 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 024 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 003 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143360003 002 001 60 DAY HOURLY POST-FLT INSP DUE IAW 1C-135-6WC-1 & ETM-RC135-6WC-1 (BL10 OR BL 9) AS APPLICA 143365411 001 001 55 ISS COMPLY WITH 60 DAY HPO IAW ETM RC135-6WC-1 CARD 4-001 AND 5-001 143350163 001 001 PILOT'S YOKE TRANSMIT BUTTON NEEDS PRESSED TWICE IN ORDER TO TRANSMIT OUT ON FD'S. 143359615 001 001 **REDBALL** LN100 #1 INOP 143359616 001 001 **REDBALL** LN-120 W/N TIE INTO FMS 143350197 001 001 #1 ENG HAS SINGLE IGNITION.(LT SIDE NOT WORKING) 143350197 002 001 #1 ENG HAS SINGLE IGNITION.(LT SIDE NOT WORKING) 143350197 003 001 #1 ENG HAS SINGLE IGNITION.(LT SIDE NOT WORKING) 143350159 001 001 DENT ON LFT ELEVATOR BALANCE BAY PANEL REQ. SHEETMETAL EVAL 143350096 001 001 A/C REQ'S SUPPORT FOR LAUNCH 143350164 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143350164 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143350164 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143350164 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143350164 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143350164 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143350164 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143350197 004 001 #1 ENG HAS SINGLE IGNITION.(LT SIDE NOT WORKING) 143350197 005 001 #1 ENG HAS SINGLE IGNITION.(LT SIDE NOT WORKING) 143350164 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143350162 001 001 S29105-3 WILL NOT RESET TO HCP 143346420 001 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 143346420 002 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 143296410 001 001 RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 14 3280206 RC-135V, T/N 64-14848, 30 April 2015 U-60 JCN WCE DDR Discrepancy 143296410 002 001 RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 14 3280206 143296410 003 001 RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 14 3280206 143296410 004 001 RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 14 3280206 143296410 006 001 RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 14 3280206 143296410 007 001 RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 14 3280206 143295415 001 001 DRT RCVR TOP LEFT AND BOTTOM RIGHT SCREWS REQUIRE INSTALL 143296410 005 001 RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 14 3280206 143280028 001 001 TR#2 SHOWED FLUCTUATING VOLTAGE IN FLIGHT LOAD DROPPED TO ZE RO. LOAD DISTRIBUTION CB 50 143280031 001 001 #2 MAIN TANK FWD BOOST PUMP,#3 MAIN TANK AFT BOOST PUMP, AND CENTER WING RIGHT OVERRID 143280032 001 001 Q- INLET HEAT INOP 143280033 001 001 DC POWER AMMETER/ VOLTMETER KNOB FELL OFF DURING FLIGHT. PLA CED IN NAV DESK DRAWER 143280063 001 001 2 EA AFT A/R PUMP PANELS REMOVED FOR FUEL CELL 143280063 002 001 2 EA AFT A/R PUMP PANELS REMOVED FOR FUEL CELL 143280063 003 001 2 EA AFT A/R PUMP PANELS REMOVED FOR FUEL CELL 143280212 001 001 MAIN AND JFS BATTERIES DISCONNECTED FOR FUEL CELL MAINT. 143285410 001 001 SERIES YAW DAMPER WILL NOT ENGAGE 143280208 002 001 HYD MULE HT CONNECTED TO #2 ENG FOR DEFUEL 143280021 008 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 009 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 010 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 011 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 015 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 016 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 017 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 018 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 021 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 022 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 023 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 024 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280079 001 001 FUEL LEAK AFT OF MLG DOORS REQ EVAL 143280108 001 001 8 HR LEAK CHECK REQUIRE AT 1930 ON CWG TANK 143280108 002 001 8 HR LEAK CHECK REQUIRE AT 1930 ON CWG TANK RC-135V, T/N 64-14848, 30 April 2015 U-61 JCN WCE DDR Discrepancy 143280206 001 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 005 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 008 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 009 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 014 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 015 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 016 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 017 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 018 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280037 001 001 AWG 7122C HARD DRIVE CHASSIS IS INSTALLED UPSIDE DOWN 143280038 001 001 ES822 #5 WILL NOT RESET TO HCP 143280024 001 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143280024 002 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143280024 003 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143280024 006 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143280024 007 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143280024 008 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143280063 004 001 2 EA AFT A/R PUMP PANELS REMOVED FOR FUEL CELL 143280212 002 001 MAIN AND JFS BATTERIES DISCONNECTED FOR FUEL CELL MAINT. 143280024 004 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143280208 001 001 HYD MULE HT CONNECTED TO #2 ENG FOR DEFUEL 143280021 001 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 002 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 003 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 004 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 005 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 006 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 007 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 012 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 013 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 014 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 019 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 RC-135V, T/N 64-14848, 30 April 2015 U-62 JCN WCE DDR Discrepancy 143280021 020 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 025 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 026 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280021 027 001 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 143280022 001 001 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION IAW 1-C135-6 2-A-03 143280023 001 001 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO FREQ 000060H DUE 39102.8HR PSN OWC 143280206 002 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 003 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 004 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 006 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 007 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 010 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 011 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 012 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 013 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280206 019 001 CTR WING #6 CELL LEAKING SEE JCN 143280108 143280024 005 001 REQUIRED THROUGH FLIGHT INSPECTION ITEMS 143276414 001 001 28 DAY FMS UPDATE REQUIRED 143270046 001 001 MICROWAVE INOP REQ REPLACEMENT AFTER FLIGHT 143270052 001 001 SUPPORT REQUIRED FOR A/C LAUNCH 143260025 001 001 NABRE CONFIGURED FOR FIRE BAT 143230065 001 001 SECONDARY SUPERVISORY MODULE W/N BOOT 143230066 001 001 HSDC A SHOWS NO VIDEO 143220191 003 001 # 2 ENG LOW OIL PRESSURE SWITCH CANNED TO A4132 # 2 ENG SEE JCN 143226503 143220191 001 001 # 2 ENG LOW OIL PRESSURE SWITCH CANNED TO A4132 # 2 ENG SEE JCN 143226503 143226503 001 001 LOW OIL PRESSURE SWITCH CANNED FROM A4848 TO A4132 PER / 143226503 002 001 LOW OIL PRESSURE SWITCH CANNED FROM A4848 TO A4132 PER / 143220065 001 001 CLASS A F/L ON RT JACK PAD 143220065 002 001 CLASS A F/L ON RT JACK PAD 143220065 003 001 CLASS A F/L ON RT JACK PAD 143220065 004 001 CLASS A F/L ON RT JACK PAD 143220065 005 001 CLASS A F/L ON RT JACK PAD RC-135V, T/N 64-14848, 30 April 2015 U-63 JCN WCE DDR Discrepancy 143226502 001 001 BOLT CAN FROM A4848 TO A4132 PER / PROCESSED BY / CANNIBALIZAT 143226502 002 001 BOLT CAN FROM A4848 TO A4132 PER / PROCESSED BY / CANNIBALIZAT 143220007 001 001 30 DAY WASTE SYSTEM SANITIIZING FREQ 000030D DUE 2014323 PSN OWC: A83SU LOC OPT: POSITION: 143220191 004 001 # 2 ENG LOW OIL PRESSURE SWITCH CANNED TO A4132 # 2 ENG SEE JCN 143226503 143220191 005 001 # 2 ENG LOW OIL PRESSURE SWITCH CANNED TO A4132 # 2 ENG SEE JCN 143226503 143220191 006 001 # 2 ENG LOW OIL PRESSURE SWITCH CANNED TO A4132 # 2 ENG SEE JCN 143226503 143220191 002 001 # 2 ENG LOW OIL PRESSURE SWITCH CANNED TO A4132 # 2 ENG SEE JCN 143226503 143210092 001 001 IRIDIUM REQUIRES OP CHECK DUE TO R2/REGISTRATION OF TRANSCEI VER 143215410 001 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 143215410 002 001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 143216500 001 001 PANEL ASSEMBLY CANNED FROM A4848 TO A4135 PER CANNIBALIZATION FOR A4135 UNIT 143216500 002 001 PANEL ASSEMBLY CANNED FROM A4848 TO A4135 PER CANNIBALIZATION FOR A4135 UNIT 143180090 001 001 #5 C/L/D LATCH REM TO SHEET METAL FOR PRIMER 143180090 002 001 #5 C/L/D LATCH REM TO SHEET METAL FOR PRIMER 143170183 001 001 # 5 MOST INBOARD COVE LIP DOOR REQS. R2 DUE TO CHAFFING ON F LAP TRACK 143170183 003 001 # 5 MOST INBOARD COVE LIP DOOR REQS. R2 DUE TO CHAFFING ON F LAP TRACK 143170183 009 001 # 5 MOST INBOARD COVE LIP DOOR REQS. R2 DUE TO CHAFFING ON F LAP TRACK 143170183 010 001 # 5 MOST INBOARD COVE LIP DOOR REQS. R2 DUE TO CHAFFING ON F LAP TRACK 143170183 013 001 # 5 MOST INBOARD COVE LIP DOOR REQS. R2 DUE TO CHAFFING ON F LAP TRACK 143170183 014 001 # 5 MOST INBOARD COVE LIP DOOR REQS. R2 DUE TO CHAFFING ON F LAP TRACK 143170183 016 001 # 5 MOST INBOARD COVE LIP DOOR REQS. R2 DUE TO CHAFFING ON F LAP TRACK 143170183 004 001 # 5 MOST INBOARD COVE LIP DOOR REQS. R2 DUE TO CHAFFING ON F LAP TRACK RC-135V, T/N 64-14848, 30 April 2015 U-64 JCN WC Event Narrative LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 28 DAY FMS UPDATE REQ FWD URINAL INOP NOTICABLE RIGHT ROLL WHEN SPEED BRAKES RAISED DURING LANDING ROLL COMBINE SPOILER SPEED BRAKE CHECK REQUIRED FOR TROUBLESHOOTI NG THIS WCE 001 THIS JCN DSS RPU #2 WILL NOT APPLY OR DISPLAY 3.3V, 5V, + OR - 12V, A ND FAN POWER ONE SLICE IN EAP 131 FAILED RFD CALL TEST A/C REQ'D SUPPORT FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION INFLT THE ANTISKID ONLY SHOWED RELEASES ON THE OUTBOARDS ONL Y. INBRDS WERE BLANK. TESTED FORWARD +AFT POSITION SHOWE LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION OPS CHK DUE ON TRUCK LEVEL SW IAW 1C-135-2-7-1 SEE THIS JCN WCE 001 INFLT THE ANTISKID ONLY SHOWED RELEASES ON THE OUTBOARDS ONL Y. INBRDS WERE BLANK. TESTED FORWARD +AFT POSITION SHOWE ACFT REQUIRES GEAR SWING FOR TROUBLE SHOOTING #2 ENGINE COWL OPENED TO CONNECT HYDRAULIC MULE 4EA PANELS REMOVED FOR JACKING OPS SEE JCN 151180290002 DMCA5 RCVR 8, TUNER 1 CAUSES SPIKES IN PAN 500 MHZ- 2-5GHZ DMCA5 RCVR 8, TUNER 1 CAUSES SPIKES IN PAN 500MGZ-2.5 GHZ ***IPI*** ENSURE LANDING GEAR CONTROL LEVER IS RETURNED TO T HE DOWN AND LOCKED POSITION SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 RC-135V, T/N 64-14848, 30 April 2015 U-65 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION WC Event Narrative ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY HYD MULE HTO8 CONNECTED TO #2 ENG TO FOM ACFT ON JACKS FOR TROUBLESHOOTING SEE JCN 151180290001 5EA JACK PADS AND 1EA PLUMB BOB INSTALLED FOR JACKING OPS SE E JCN 151190290002 ENSURE LANDING GEAR LEVER IS IN DOWN AND LOCKED POSITION PRI OR TO DOWN JACK SEE JCN 151180290002 LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 MANIFOLD VALVE LIGHT ON AR PANEL WON'T ILLUMINATE WHEN PLACE D IN THE REFUEL POSITION ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 #4 PMC INDICATED SPLIT N2 & DEMAND POINTER; #4 ENG 5% LOWERN 2 W/ THROTTLES ALLIGNED; PMC CUT-OUT FOR LANDING # 4 ENG COWLING OPEN TO FOM PLA TESTER INSTALLED ON # 4 ENG. FOR ADJUSTMENT I'S AND E'S INSP REQUIRED PRIOR TO ENGINE RUN I'S AND E'S INSP REQUIRED AFTER ENGINE RUN LEFT HAND PACK OVERPRESSURIZES GIVES UUUU ERROR ON FLOW CONT ROLLER CENTER WING ACCESS DOOR OPENED TO FOM LH KEEL BEAM BAY DOOR OPENED TO FOM LH AIRFLOW CONTROLLER REMOVED FOR REPLACEMENT LH S-DUCT REMOVED TO FOM T-DUCT REMOVED TO FOM 2 EACH WARNING TAGS INSTALLED MX IN PROGRESS 1OF2 ENGINE THR OTTLES NOTE: DONT ADVANCE THROTTLES 2OF2 EXT BLEED AIR REC RADAR INSTRUMENTATION NOT DISPLAYING. BLINKED AT FIRST THEN BLACKED OUT COMPLETELY. SCOPE STILL DISPLAYED RADAR RETURNS RADAR IFOC REQUIRED SEE THIS JCN WCE 001 LH LANDING LIGHT C/B POPPED IN FLIGHT RC-135V, T/N 64-14848, 30 April 2015 U-66 SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 WC Event Narrative LH LANDING LIGHT PANEL REMOVED TO FOM SEE THIS JCN WCE 001 DFS-3 (DMCA 5A) FAILS RADIATED BITE FOR NOT HAVING UPDATED B ORESIGHT ES822 #4 RCVR 1 FAILS ]CRS FOR AUDIO UHF #4 WILL NOT TX SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 E2 ANTENNA MOUNT LOOSE POSSIBLY CRACKED E2 ANTENNA PANEL REMOVED FOR LOOSE ANTENNA #1 ENG FAN COWL OPEN TO FOM #2 ENG FAN COWL OPEN TO FOM #3 ENG FAN COWL OPEN TO FOM #4 ENG FAN COWL OPEN TO FOM #1 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #2 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #3 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #4 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #1 ENG FUEL STRAINER REMOVED FOR INSP #2 ENG FUEL STRAINER REMOVED FOR INSP #3 ENG FUEL STRAINER REMOVED FOR INSP #4 ENG FUEL STRAINER REMOVED FOR INSP E2 ANTENNA REMOVED TO FOM SEE WCE 001 A/C REQ'D SUPPORT FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 RC-135V, T/N 64-14848, 30 April 2015 U-67 ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 WC Event Narrative ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 E2 MOUNTING BOLTS SEALED REQ. CURE CHECK @ 0630 15113 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 ENG'S 1,2,3,4 T-HANDLES PULLED ENG STARTER C/B'S P ULLED FIRE SPRSN C/B'S PULLED FIRE SHUTOFF PULLED 4 EACH WARNING TAGS INSTALLED ON #1 ENG STARTER C/ B,FIRE SPRN C/B,T-HANDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #2 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #3 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 2 EACH WARNING TAGS INSTALLED ON: ACFT BATT SWITCH AND EXTERNAL POWER RECEPTACLE INSP ALL 4 ENG TRANS GEARBOXES FOR LEAKS,LOOSE OR MISSING HARDWARE IAW 1C-135-6 PG.S-A-031 STEP 22 ALL FOUR ENG STARTERS DUE OIL CHECK IAW 1C-135(K)R -2-4JG-6 TASK 6-29-1 PG 6-136 INSPECT ALL FOUR ENG CHIP DETECTORS 1AW IAW 1C-135-6 PG S-A-031 STEP 22 ITEM C INSP DIFFERENTIAL OIL PRESSURE INDICATOR(DPI) FOR POPPED INDICATION. ON#1,2,4 IDG'S IAW 1C-135-6 INSP ALL 4 MAIN FUEL STRAINER FOR TOP-COAT C ONTAMINATION IAW 1C-135-6 PG 2-A-032 UTEN 30STEP A ALL 4 ENG DUE IDLE RUN LEAK CHECK ON OIL AND FUEL SYSTEMS IAW 1C-135(K)R-2-4JG-5 TASK 5-12-1 PG.5-28 INLETS AND EXHAUSTS INSP DUE PRIOR TO ENG RUN INLETS AND EXHAUSTS INSP DUE POST TO ENG RUN C/W 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION C/W 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 WATER SUSPECTED IN RADAR PRESSURE LINES RADAR REQS IFOC. SEE JCN 151100193 WCE 001 FOR ORIGINAL DISC REPANCY IFCD #6 ISSUES 0006/0086 TYPE MISMATCH FOUND DMCA #4B UNABLE TO ALLOCATE SIG APP CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 RC-135V, T/N 64-14848, 30 April 2015 U-68 4 EACH WARNING TAGS INSTALLED ON: #4 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B WC Event Narrative CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 TCAS FAIL IN CHOCKS. MX ATTEMPTED TO CORRECT, BUT PROBLEM CO RRECTED ITSELF. AFTER FLIGHT, DURING LDG ROLLOUT, TCAS FAIL R TCAS FAIL. PROCESSOR SUSPECTED BAD OUT OF SUPPLY TCAS FAIL. HEADING & ATTITUDE BIT FAIL W/ MX PC 7 LEVEL INSPECTION REQUIRED FOR RECUR SEE JCN 151100193 7 DAY LCS INSP DUE IAW ETM-RC135-6 FUEL DUMPED 25K INFLT ENCOUNTERED HEAVY SMOKE AND BURNING SMELL FROM THE PCA AND/O R MONITOR PANEL IN THE CORVUS RAC 28 VDC POWER SUPPLY REMOVED. UNIT REQUIRES REPLACEMENT. DON OT OPERATE CORVUS SYSTEM UNTIL REPLACEMENT IS COMPLETE. TR SPARE INTERPHONE FCD DROPS CONNECTION TO SYSTEM E10 FAILS RADIATED BITE AT FREQ 348.01 MHZ ACROSS ALL DF'S *REDBALL* ELINT RAID NOT CONNECTING TO LAN SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 RADAR PRESSURE DEHYDRATOR WAS PINK UPON PHYSICAL INSPECTION, SILICA REQUIRES REPLACEMENT. SECONDARY STRUCTURE/PANEL INSP DUE PRIOR TO NEXT FLIGHT IAW OAFBI 21-100 PARA 7.2.1 INLETS AND EXHAUST INSP DUE PRIOR TO NEXT FLIGHT RADAR INOP 40 MIN AFTER TAKEOFF MAGNETRON FAIL .05. MALFUNCT ION OCCURRED ON BOTH LEGS OF MAXWELL OUT AND BACK 7 LVL INSP REQ FOR RECURR WRITE-UP RADOME ACCESS PANEL REMOVED TO FOM SEE THIS JCN WCE 001 RC-135V, T/N 64-14848, 30 April 2015 U-69 RADAR MAG FAIL DURING FLIGHT MULTI TIMES. NO SWEEP, FAULT CO DES 0209 AND 0202 AND MAG FAIL 0.05 WC Event Narrative RADAR FAILS WITH 118, 119, 115 FAULTS. NOSE RADOME REMOVED TO FOM. SEE THIS JCN WCE 001 NOSE RADOM ACCESS PANEL REMOVED TO FOM SEE THIS JCN WCE 001 OUT OF DOCKS CHECK REQUIRED ON WEATHER RADAR IAW ETM-RC135-2 -11 SEE THIS JCN WCE 001 RADAR REQ IFOC FOR MAG FAIL IAW AIRCREW -1 TCAS INOP DURING DESCENT- KNOWN TRAFFIC WITHIN NORMAL OPERAT RADAR SYSTEM INTERMITTENTLY BLANKS WHEN RADAR PRESSURE PLACE D IN NORMAL ON AT 34 PSI NAV RADAR MONITOR INTERMITTENTLY FLICKERS WHEN RADAR PRESSUR IZES IN NORMAL ON POSITION #1 ENG COWLING OPEN TO FOM A/P J2 CANNON PLUG REQUIRES RELOCATION A/P PROCESSOR REMOVED TO FOM SEE THIS JCN WCE 001 & 002 A/P SYSTEM OPS CHECK DUE IAW ETM-RC135-2-11 PG 3-19 PARA 3.4 .4 SEE THIS JCN WCE 001 & 002 FWD GAP ANTENNA WAVEGUIDE DISCONNECTED TO FOM SEE THIS JCN W CE 005 5 EA WARNING TAGS INSTALLED 1/5 SRCH RDR(T9) 2/5SRCH RDR(AX7 ) 3/5 SRCH RDR(AX8) 4/5 PRESS. KIT(BD8) 5/5 PRESS. KIT(BD9)S EE TH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 ALL SECONDARY STRUCTURE/PANEL REQ. INSP. PRIOR TO NEXT FLIGH T ALL FOUR ENGINE INLET AND EXHAUST REQ. INSP. FOR FOD PRIOR T O NEXT ENGINE FUNCTION ALL SECONDARY STRUCTURE/PANEL REQ. INSP IAW OAFBI 21-100 PAR A 7.2.1 PRIOR TO NEXT FLIGHT ALL FOUR ENGINES INLETS AND EXHAUST REQ. INSP FOR FOD PRIOR TO NEXT ENGINE FUNCTION TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 RADAR INOP SHORTLY AFTER TAKEOFF. MAGNETRON FAIL .05- EVEN A FTER MULTIPLE RESTARTS UPPER LEFT NUT PLATE BROKE. SCREW REMOVED. LT PACK OVER PRESSURIZES, GIVES "UUUU" INDICATION W/LOUD RUS H OF WIND IFOC DUE ON LH PACK MIDS WOULD NOT LOAD CRYPTO IN LOC 1 & 2 RC-135V, T/N 64-14848, 30 April 2015 U-70 A/P J1 CANNON PLUG REQUIRES RELOCATION WC Event Narrative SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 PERFORM WASTE SYS SANITIZING FOR THE ACFT WASTE TA & LAV SVC CART IAW ETM-RC135V/W-2. NAV RADAR VIDEO MONITOR ETR'D FROM A4131 TO A4848 FOR TROUBL ESHOOTING SEE JCN 151030133 AND JCN 151036490 RADAR REQ'S OP CHK IAW ETM-RC135-2-11 PG 2-41 PARA 2.4.3A SE E JCN 151036410 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 2EA FWD URINAL VALVES REQUIRE REPLACEMENT SUPPORTED A/C LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 ACCOMPLISH BL11 TQS MOUNT REPLACEMENT WHEN RADAR PRESSURIZATION PUMP STARTED & STOPPED, RADAR DISP LAY BLANKED OUT COMPLETELY #1 WHEEL DUST COVER REMOVED FOR WHEEL & TIRECHANGE IPI REQU IRED 1C-135-2-7-1 # 1 WHEEL SPEED TRANSDUCER REMOVED IPI REQ1C-135-2-7-1 #1 WHEEL SPEED TRANSDUCER REQUIRES REQ OPS CHECKIAW 1C-135-2 -7-1 #1 TIRE WORN OUT OF LIMITS REQUIRES CHANGE IPI REQUIRED 1C-1 35-2-7-1 MFD/PFD SCREEN AT NAV STATION WOULD BLUR FOR A FEW MINUTES A T A TIME RANDOMLY THROUGHOUT THE FLT LEFT HYDRAULIC QUANTITY DROPPED TO 2.0 IN FLT. UPON DESCENT, LEFT HYDRO QUANTITY CAME BACK UP TO 3.5 AFTER GR LOWERED SPARE OWS JLAN1 PORT WON'T CONNECT TO LAN SWITCH RC-135V, T/N 64-14848, 30 April 2015 U-71 RADAR PRESSURIZATION WAS OVER PRESSURIZING THE UNIT TO 35-37 OVER THE LIMIT AT 34. THIS CAUSED THE RADAR SCREEN TO GO BL WC Event Narrative SUPPORT REQUIRED FOR A/C LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION LT MLG ON AXLE JACK FOR WHEEL AND TIRE CHANGE TAWS REQ IFOC DUE TO CALL OUTS SEE JCN 150970158 WCE 004 MODE IV CHECK REQUIRED FOR EXERCISE PLTZ GOGGLE POWER CHECK REQUIRED THERMAL CURTAINS REQ INSTALL/INSP "NOTE" AFTER INSTALLATIONS OF CURTAINS UPLOAD ACFT FOR EXERCISE COMMITMENT OPEN & CLOSE #3 ENGINE COWL SERVICE JFS OIL LIFE SUPPORT UPLOAD FL 15 CHECKLIST (55 ISS/HLGNJ) RADIO ALT #2 FDR DATA SHOWS BLIP AT 17000 FT RADIO ALT #2 FDR DATA SHOWS BLIP AT 17000 FT SEE THIS JCN WC REMOVED FUEL CELL # 1 ACCESS PANEL TO FOM SEE THIS JCN WCE 0 01 RADIO ALT #2 FDR DATA SHOWS BLIP AT 17000 FT SEE THIS JCN WC E 002 C/W MODE IV/MODE C CHECK IAW ACCI 21-101. COMPLY WITH ACFT RECORDS CHECK IAW AFI 21-101. AISLE MAINT BL 10 STOPPED WORKING WHEEL WELL DOOR LIGHT IS BURNED OUT CARGO DOOR HANDLE FOR CAM #2 (FROM THE FRONT) A LITTLE LOOSE . WIND SHEAR WARNING AT 17,000' FROZE WARNING ON FLIGHT DIRECT OR FOR 90 MIN. REQUIRED ALL APC RESET IN FLIGHT. SPARE KEYBOARD CAPS LOCK KEY DOES NOT WORK DMCA #4B SIG APP WILL NOT ALLOCATE SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 RC-135V, T/N 64-14848, 30 April 2015 U-72 LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 WC Event Narrative ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 IFOC REQUIRED FOR RADAR. PER AIRCREW-1. SEE JCN 150930097 WC E 001 7 DAY LCS INSPECTION DUE RADAR HAD NO RETURNS;SHOWED FAULT MOD PWR FAIL AND FAULT COD E 0204. TURNED OFF RADAR AND PULLED CIRCUIT BREAKERS, TUR TAWS CALLED "TERRAIN" AND "PULL UP" DESCENDING THROUGH 26,00 0 FEET AND 14,000 FEET 7 LVL INSP REQ FOR RECURR WRITE-UP DF-M FAILS RADIATED BITE ON ALL ARRAYS AND ALL FREQS EP ISSUES ERROR "CUT REPORT NAV TIME MONOTONICALLY INCREASIN G" A/C REQ SUPPORT FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 LH PACK OVER PRESSURIZED WHEN SET TO COND AIR ON CLIMBOUT AN D CRUISE ALTITUDE CENTER WING ACCESS DOOR OPENED TO FOM LEFT KEEL BEAM BAY DOOR OPENED TO FOM LH AIRFLOW CONTROLLER REMOVED FOR REPLACEMENT LEFT S-DUCT REMOVED TO FOM T-DUCT REMOVED TO FOM RIGHT SIGHT WINDOW IS DIRTY AND IS TOUGH TO SEE THROUGH FRONT URINAL IS DRAINING A LOT SLOWER THAN NORMAL. TOOK 15- 20 MIN TO DRAIN PER USE. RC-135V, T/N 64-14848, 30 April 2015 U-73 28 DAY TAWS UPDATE REQ'D WC Event Narrative #1 ENGINE FAN COWL OPEN TO FOM #2 ENGINE FAN COWL OPEN TO FOM #3 ENGINE FAN COWL OPEN TO FOM #4 ENGINE FAN COWL OPEN TO FOM #1 ENGINE CHIP DETECTORS (4 EACH) REMOVED FOR INSPECTION #2 ENGINE CHIP DETECTORS (4 EACH) REMOVED FOR INSPECTION #3 ENGINE CHIP DETECTORS (4 EACH) REMOVED FOR INSPECTION #4 ENGINE CHIP DETECTORS (4 EACH) REMOVED FOR INSPECTION DF-M CH 6 HAD EXCESSIVE DRIFT, CAUSED RFD BS FAILURE 2 EACH WARNING TAGS INSTALLED MX IN PROGRESS 1OF2 ENGINE THR OTTLES NOTE: DONT ADVANCE THROTTLES 2OF2 EXT BLEED AIR REC SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY 60HR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 PAGE 2-A-30A PARA 22 60HR INSP IN PROGRESS:#1,2,3,&4 C/B'S PULLED. NOTE STARTER SERVICING BEING PERFORMED.DONT RESET START INSP ALL 4 ENG TRANS GEARBOES FOR LEAKS,LOOSE OR ALL FOUR ENGINES STARTERS DUE OIL CHECK IAW 1C-135(K)R-2-4JG-6 TASK 6-28-1 PARA 6-127 INSP ALL 4 ENGINE CHIP DETECTORS 1AW IAW 1C-135-6 PG S-A-031 STEP 22 ITEM C INSPECT OIL LEVELS ON #1,2,4 ENGINE IDG'S IAW 1C-135-6 PG 2 S-A-032A ITEM 3 STEP B ALL FOUR ENGINES DUE IDLE RUN & LEAK CHECK ON OIL SYSTEM IAW 1C-135(K)R-2-4JG-5 TASK 5-12-1 PG 5-28 INLES & EXHAUST INSPEC DUE PRIOR ENGINE FUNCTION IAW 1C-135(K)R-2-4JG-2 TASK 2-14-1 PAGE 2-36 INLES & EXHAUST INSPEC DUE POST ENGINE FUNCTION IAW 1C-135(K)R-2-4JG-2 TASK 2-15-8 PAGE 2-154 INSP DIFFERENTIAL OIL PRESSURE INDICATOR(DPI) FOR POPPED INDICATION. ON#1,2,4 IDG'S IAW 1C-135-6 C/W 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION C/W 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 RAD ALT #1 AND #2 REQUIRE SWAP FOR TROUBLE SHOOTING. SEE JCN 150900121 WCE 001 RC-135V, T/N 64-14848, 30 April 2015 U-74 A/C REQ'D SUPPORT FOR LAUNCH WC Event Narrative INLETS AND EXHAUST REQ INSP PRIOR TO FLIGHT PANELS REQ INSP INSP PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7 .2.1 AIR DATA LOADER NOT READING DISKS #005 REPEATED TAWS WARNING AFTER TAKEOFF (UP TO5 PER MINUTE). WAR NING CEASED WHEN RAD ACT WAS SELECTED "OFF" A/C REQUIRES SUPPORT FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 28D FMS UPDATE REQUIRED 7 DAY LCS INSP DUE IAW ETM-RC135-6 FUEL CELL 0 ACCESS PANEL OPENED FOR LCS INSP SEE THIS JCN WC E 1 SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 REMOVE AND INSPECT MAIN ENGINE FUEL FILTER FOR TOPCOAT CONTAMINATION IAW T.O. 1C-135-6 WITH FILTERS REMOVED INSP ALL HELICOIL INSERTS FOR PROPER INSTALL/CONDITION IAW T.O. 1C-135-6 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 REMOVE AND INSPECT MAIN ENGINE FUEL FILTER FOR TOPCOAT CONTAMINATION IAW T.O. 1C-135-6 RC-135V, T/N 64-14848, 30 April 2015 U-75 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION WC Event Narrative WITH FILTERS REMOVED INSP ALL HELICOIL INSERTS FOR PROPER INSTALL/CONDITION IAW T.O. 1C-135-6 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 REMOVE AND INSPECT MAIN ENGINE FUEL FILTER FOR TOPCOAT CONTAMINATION IAW T.O. 1C-135-6 WITH FILTERS REMOVED INSP ALL HELICOIL INSERTS FOR PROPER INSTALL/CONDITION IAW T.O. 1C-135-6 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 WITH FILTERS REMOVED INSP ALL HELICOIL INSERTS FOR PROPER INSTALL/CONDITION IAW T.O. 1C-135-6 LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 1 EA FIRST AID KIT IN FLIGHT DECK OPENED FOR TRAINING / BROK EN ZIPPER REMOVED FROM ACFT HDP REQUIRES CALL TEST DMCA 2B FAILS CALL TEST DMCA 2A FAILS CALL TEST DMCA 4B FAILS CALL TEST DMCA 5A FAILS CALL TEST DMCA 5B FAILS CALL TEST CE #1 DOES NOT GENERATE BANDSCAN WHEN SCAN TASKING ENTRY IS SET TO A BANDWIDTH OF 80 MHZ OR BELOW DMCA 5 RXCR 1 CAUSES RFD BORESIGHT TO RAIL 20-30 MHZ HDP FREEZES WHILE BOOTING SI9105 #3 SHOWS POWER FAULT HSDC-D GIVES ERROR: MOUNTING FAILED UNABLE TO FIND REQUIRED DISKS RETUAL:1 SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 RC-135V, T/N 64-14848, 30 April 2015 U-76 REMOVE AND INSPECT MAIN ENGINE FUEL FILTER FOR TOPCOAT CONTAMINATION IAW T.O. 1C-135-6 WC Event Narrative 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 ACCESS PNL REMOVED FOR INSPECTION LT WHEEL WELL UPPER TORQUE TUBE BRACKET BROKEN REQUIRES R2 3EA LIGHTNING PATCHES REQUIRES INSTALLATION #4 OUTBOARD WING FLAP REQUIRES MOHAIR COMPLY WITH 60 DAY HPO CARDS IAW 1C-135-6WC-1 COMPLY WITH 60 DAY HPO CARD IAW ETM-RC135-6WC-1 CARD 7-001 COMPLY WITH 60 DAY HPO CARD IAW ETM-RC135-6WC-1 CARD 6-001 55ISS COMPLY WITH 60 DAY HPO IAW ETM-RC135-6WC-1 CARD 4-001, 5-001 STAB TRIM ACCESS PANEL REMOVED FOR HPO 2EA WARNING TAGS INST ALLED IAW 1C-135-2-8-1 PARA 15.10.3 STEP 10 RT KEEL BEAM BAY DOOR LOWERED FOR HPO CLOSE IAW 1C-135-2-2-2 PARA 15.95.2 STEP 8 LT KEEL BEAM BAY DOOR LOWERED FOR HPO CLOSE IAW 1C-135-2-2-2 PARA 15.95.2 STEP 8 #1 ENG FAN COWL OPEN FOR HPO CLOSE IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 #2 ENG FAN COWL OPEN FOR HPO CLOSE IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 #3 ENG FAN COWL OPEN FOR HPO CLOSE IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 #4 ENG FAN COWL OPEN FOR HPO CLOSE IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 #1 ENG DUCT COWL OPEN FOR HPO CLOSE IAW 1C-135-2-2-2 PG 20-2 1 PARA 20.8 #2 ENG DUCT COWL OPEN FOR HPO CLOSE IAW 1C-135-2-2-2 PG 20-2 1 PARA 20.8 #3 ENG DUCT COWL OPEN FOR HPO CLOSE IAW 1C-135-2-2-2 PG 20-2 1 PARA 20.8 #4 ENG DUCT COWL OPEN FOR HPO CLOSE IAW 1C-135-2-2-2 PG 20-2 1 PARA 20.8 JFS TURBINE OIL DRAINED 1EA WARNING TAGS INSTALLED 1OF1 JFS STARTER C/B NOTE: DO NOT RESET 8 EA SPOILER LOCKS INSTALL FOR HPO 3EA WARN TAGS INSTALL TAG 1/3 INBRD SPOILER CUTOUT SWTCH TAG 2/3 OUTBRD SPOILER CUTOU 8EA L/E FLAP LOCKS INSTALLED 1EA WARNING TAG INSTALLED 1OF1 FLAP HANDLE NOTE: DO NOT OPERATE STAB TRIM LOCK INSTALLED 2EA WARNING TAGS INSTALLED TAG 1OF2 STAB PWR SWITCH TAG 2OF2 FCS POWER SWITCH NOTE: DO N OT OP (83FL) C/W 1C-135-6WC-1 CARDS 4-002 THRU4-011, 4-015,4-016 ITEMS 1 THRU 5,4-020 THRU 4-22 (83FL) C/W IPI INSP IAW LPS MXG-1C-135-6WC-1-OFC1 CARD 4-022 ITEM 1 C/W CARD 4-012IAW 1C-135-6WC-1 RT ACM DRAINED FOR HPO IAW 1C-135-6WC-1 CARD 4-012 LT ACM DRAINED FOR HPO IAW 1C-135-6WC-1 CARD 4-012 (83GC)C/W INSP 1C-135-6WC-1 CARD 4-016 ITEM 8 A/R DOOR LOCK INSTALLED 1EA WARNING TAG INSTALLED RC-135V, T/N 64-14848, 30 April 2015 U-77 10EA COVE LIP DOORS LOWERED FOR HPO (RAISE) IAW 1C-135-2-8-1 PG 5-220 PAR 5.15.9 STP 11 WC Event Narrative (83HY)COMPLY WITH 1C-135-6WC-1 CARD 4-019 ITEMS 2 THRU 4 ALL FOUR ENG FIRE SUPPRESSION C/B S PULLED FOR HPO HPO 4 EA WARNING TAGS INSTALLED NOTE: DO NOT RESET ALL FOUR ENG T-HANDLES PULLED 4EA WARNING TAGS INSTALLED NOTE: DO NOT RESET ALL FOUR ENG FIRE SHUTOFF C/B S PULLED FOR HPO HPO 4EA WARNING TAGS INSTALLED NOTE: DO NOT RESET SHOP NARRATIVE: (83JE)C/W 1C-135-6WC-1 CARD 4-016 ITEM 7 ALL FOUR ENGINES DUE AUDIBLE IGNITION CHK FOR HPO TACAN #1 STAYED IN TEST MODE FROM T/O TILL LANDING HF COUPLER ACCESS PANEL REMOVED TO FOM REMOVED PER MB 1RC/TC 135-1175 HF COUPLER ACCESS PANEL REMOVED TO FOM REMOVED PER MB 1RC/TC 135-1175 SPARE KEYBOARD INOP POS 1/2 LIGHT CONTROL CB INTERMITENT SUPPORTED A/C FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 *REDBALL* RADAR DISPLAY INOP *REDBALL* RADAR INOP CANNOT CONFIGURE SHAWNA W/TS LOAD RAID SET 9 SUPPORTED A/C LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY RC-135V, T/N 64-14848, 30 April 2015 U-78 SI9105 #3 SHOWS POWER FAULT WC Event Narrative LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 LEFT OVER WING HATCH REQUIRES REPLACEMENT HATCH REQS. REPLACEMENT TEMP. HATCH INSTALLED FROM -21 AWAIT ING PARTS THIS IS THE INSTALLATION WCE CREATED BY JCN 150770079002 # 3 W/T WORN OUT OF LIMITS REQ R2 IPI REQ IAW 1C-135-2-7-1 PARA 6.13.2STEP 3, STEP 3, 6.13.3 STEPS 1,5, 6 & 6.13.2. # 3 WHL DUST CVR REM FOR W/T CHG IPI REQ IAW 1C-135-2-7-1 PA RA 9-13.4 STEP 6(OC/WC), STEP 27(RC/TC) # 3 WHL SPD TRN REM FOR W/T CHG IPI REQ IAW1C-135-2-1 PARA 6 .13.3 STEPS 9, 11 & PARA 9.12.2. #2 ENG COWLING OPENED TO FOM FORWARD FWD BODY PUMP VIBRATES AND MAKES LOUD NOISES WHILE R UNNING RIGHT MLG AXLE ON JACKS # 3 WHEEL AND TIRE ANTI-SKID SYS REQUIRES OPS CHECK IAW 1C-1 35-2-7-1PARA 9-13 FOR OC/WC, PARA 9.14 FOR RC/RC. SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY HYD MULE HT03 CONNECTED TO #2 ENG TO FOM LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 PERFORM WASTE SYS SANITIZING FOR THE ACFT WASTE TA & LAV SVC CART IAW ETM-RC135V/W-2. ADL AT NAV1 STATION DID NOT LOAD AFTER MULTIPLE ATTEMPTS 7 DAY LCS INSPECTION DUE IAW TO ETM-RC135-2-3 FUEL CELL 0 OPENED TO FOM TAWS PRODUCED FALSE TERRAIN WARNINGS AT FL190 AT KLNK WITH R ADIO ALTIMETER IN RAD ALT. ON FINAL AT KOFF TO LOW TERRAIN @ AEP DOES NOT INITIALIZE NDU WILL NOT SEND OUT NAV DATA TO COLLECTION SYSTEM NDU A WILL NOT BOOT NDU CONFIGURED TO B SIDE DMCA #5 RX 4 CH 1 DOWNED TO HCP ON RESET DMCA #1 RX7 CH1 DOWNED TO HCP ON RESET AIRCRAFT CONFIGURED FOR NDU-B RC-135V, T/N 64-14848, 30 April 2015 U-79 SUPPORTED A/C LAUNCH WC Event Narrative SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1 -001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE BEFORE CREW SHOW COPILOTS MFD REQUIRES R2 COPILOTS MFD REMOVED FOR R2 RT MLG WIRE HARNESS REMOVED TO F.O.M ANTI-SKID SYSTEM DUE OPS CHECK WHEEL #3 DUST COVER REMOVED IPI REQ IAW1C-135-2-7 PARA 5-56D .1 STEP 23 WHEEL #4 DUST COVER REMOVED IPI REQ IAW1C-135-2-7 PARA 5-56D .1 STEP 23 WHEEL #7 DUST COVER REMOVED IPI REQ IAW1C-135-2-7 PARA 5-56D .1 STEP 23 WHEEL #8 DUST COVER REMOVED IPI REQ IAW1C-135-2-7 PARA 5-56D .1 STEP 23 RT TRUCK LEVEL SWITCH OPS CK DUE RT SAFTEY SWITCH OPS CHECK DUE RH TRUCK LEVEL SWITCH REQUIRES R2 RT MLG STRUT LEAKING OUT OF LIMITS RT MLG TRUNNION TO DRAG BRACE BRAKE LINES REMOVED TOF.O.M AFTER STRUT CONFIG 4 HR LK CHK ON RT MLG STRUT DUEIAW 1C-135 -2-7 TABLE 1-8 MLG BRAKES DUE BLEED RT LK CK DUE ON MLG TRUNNION TO DRAG BRACE BRAKELINES #2 ENG COWLING OPENED TO FOM #1 ENGINE COWL OPEN TO FOM #1 ENGINE COWL OPEN TO FOM *REDBALL* RT STRUT DEFLATED RC-135V, T/N 64-14848, 30 April 2015 U-80 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO NEXT FLIGH T IAW OAFBI 21-100 PARA 7.2.1 WC Event Narrative 4 HOUR LEAK CHECK ON RT MLG SHOCK STRUT STARTED AT 1045 RT MLG REMOVED FOR STRUT RE-PACK RT MLG REQUIRES SAFETY RT MLG STRUT NOT CONFIGURED FOR FLIGHT FUEL NOT CONFIGURED FOR FLIGHT 2EA WARN TAGS INTALLED TO F.O.M 1OF2 INSTALL ON LT HYD DP SWITCH 2OF2 INST ON RT HYD DP SWITCH RT MLG REQ NITROGEN SERVICING PRIOR TO DOWN JACK RT MLG STRUT REQUIRES HYDRAULIC SERVICING PRIOR TOINSTALL PERFORM LANDING GEAR CHECK OUT PER 1C-135-2-7-1 PG 6-1 PARA 6.4 IPI DUE TO ENSURE INNER CYLINDER IS FREE OF FOD PRIOR TO ASS EMBLY IAW 1C-135-2-7-1 PRAR6.98.7 PRIOR TO STEP 1. HYD MULE HT03 CONNECTED TO #2 ENG HYDRO MULE CONNECTED TO #1 ENGINE FOR DEFUEL HYDRO MULE CONNECTED TO #1 ENGINE FOR DEFUEL C/W 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO C/W 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION 4 EA JACK PANELS REMOVED FOR AIRCRAFT JACK 5 EA JACK PADS INSTALLED FOR AIRCRAFT JACK 1 EA PLUMB BOB INSTALLED FOR AIRCRAFT JACK AIRCRAFT ON JACKS FOR MLG STRUT RE-PACK AUX SEAT WALK AROUND BOTTLE BRACKET BROKEN RT HYD SYSTEM WILL NOT BUILD PAST 2500 PSI WITH AUXILIARY PU MP #1 ENG FAN COWL OPEN TO FOM #2 ENG FAN COWL OPEN TO FOM #3 ENG FAN COWL OPEN TO FOM #4 ENG FAN COWL OPEN TO FOM #1 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #2 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #3 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #4 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #1 ENG FUEL STRAINER REMOVED FOR INSP #2 ENG FUEL STRAINER REMOVED FOR INSP RC-135V, T/N 64-14848, 30 April 2015 U-81 IPI REQ FOR STRUT REPACK IAW 1C-135-2-7 PARA 2-200A STEP 48 WC Event Narrative #3 ENG FUEL STRAINER REMOVED FOR INSP #4 ENG FUEL STRAINER REMOVED FOR INSP SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 ENG'S 1,2,3,4 T-HANDLES PULLED ENG STARTER C/B'S P ULLED FIRE SPRSN C/B'S PULLED FIRE SHUTOFF PULLED 4 EACH WARNING TAGS INSTALLED ON #1 ENG STARTER C/ B,FIRE SPRN C/B,T-HANDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #2 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #3 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #4 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 2 EACH WARNING TAGS INSTALLED ON: ACFT BATT SWITCH AND EXTERNAL POWER RECEPTACLE INSP ALL 4 ENG TRANS GEARBOXES FOR LEAKS,LOOSE OR MISSING HARDWARE IAW 1C-135-6 PG.S-A-031 STEP 22 ALL FOUR ENG STARTERS DUE OIL CHECK IAW 1C-135(K)R -2-4JG-6 TASK 6-29-1 PG 6-136 INSPECT ALL FOUR ENG CHIP DETECTORS 1AW IAW 1C-135-6 PG S-A-031 STEP 22 ITEM C INSP DIFFERENTIAL OIL PRESSURE INDICATOR(DPI) FOR POPPED INDICATION. ON#1,2,4 IDG'S IAW 1C-135-6 INSP ALL 4 MAIN FUEL STRAINER FOR TOP-COAT C ONTAMINATION IAW 1C-135-6 PG 2-A-032 UTEN 30STEP A ALL 4 ENG DUE IDLE RUN LEAK CHECK ON OIL AND FUEL SYSTEMS IAW 1C-135(K)R-2-4JG-5 TASK 5-12-1 PG.5-28 INLETS AND EXHAUSTS INSP DUE PRIOR TO ENG RUN INLETS AND EXHAUSTS INSP DUE POST TO ENG RUN LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 ALASKA CONSTANTLY SCROLLING. DISK FREE SPACE QUERY FAILED ER RORS. JTT LAN 49 ISSUE. JTT LAN 49 ISSUE. STAMPEDING SEROW QRC INSTALLED. SEE 781C IFOC DUE ON IMP BOX CHANNEL 8 #2 W/T REQ R2 IPI REQ IAW 1C-135-2-7-1 PARA 6.13.2STEP 3, ST EP 3, 6.13.3 STEPS 1,5, 6 & 6.13.2. RC-135V, T/N 64-14848, 30 April 2015 U-82 1 EA WARNING TAG INSTALLED 1OF1 RT HYDRO PRESS S/W SEE THISJ CN WCE 001 WC Event Narrative #2 WHL DUST CVR REM FOR W/T CHG IPI REQ IAW 1C-135-2-7-1 PAR A 9-13.4 STEP 6(OC/WC), STEP 27(RC/TC) #2 WHL SPD TRN REM FOR W/T CHG IPI REQ IAW1C-135-2-1 PARA 6. 13.3 STEPS 9, 11 & PARA 9.12.2. LT MLG AXLE ON JACKS ANTI-SKID SYS REQUIRES OPS CHECK IAW 1C-135-2-7-1PARA 9-13 F OR OC/WC, PARA 9.14 FOR RC/RC. STATIC BOOM STICK BROKEN REMOVED FOR REMANUFACTURE A/R DOOR LIGHT PANELS REMOVED FOR T/S A/R DOOR LIGHTS INOP ARR SLIPWAY DOOR LIGHTS INOP 1 EA WARNING TAG INSTALLED. 1 OF 1 INSTALLED ON A/R MASTER R EFUEL SWITCH. NOTE: DO NOT OPERATE SWITCH. 28 DAY FMS UPDATE REQUIRED IFOC DUE ON IMP BOX CH 7 SENSORS 8,9,10,11,12 PER AIRCREW -1 SEE JCN 142510082,142510083,142510084,142510085,142510089 TEAR IN SKIN OF LEADING EDGE ON RIGHT A/R SLIPWAY DOOR THIS IS THE INSTALLATION WCE CREATED BY JCN 150610111001 REMOVED UPPER A/R MANIFOLD LK CK DUE ON UPPER A/R MANIFOLD RT SIDE OF SLIPWAY NEAR RECEPTICLE REQUIRES EVAL A/C REQUIRED SUPPORT FOR LAUNCH 2 EA WARNING TAGS INSTALLED: 1OF2-RT HYD PUMP SWITCH 2OF2-SL IPWAY DOOR LIGHT C/B. DO NOT OPERATE. SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY 2 EA WARNING TAGS INSTALLED NOTE OPEN FUEL LINE 1 OF 2 EXT P WR-DO NOT APPLY 2 OF 2 BATT PWR SWITCHES- DO NOT CYCLE IPI DUE PRIOR TO INSTALLATION OF UPPER A/R MANIFOLD LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 RC-135V, T/N 64-14848, 30 April 2015 U-83 A/R/R SLIPWAY DOOR LOCK INSTALLED TO FOM WC Event Narrative CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 ASE1 SPARE KEYBOARD BAD; KEYS LOCK UP UHF 4 WOULD NOT LOAD CRYPTO UHF 4 REQ OPS CHECK IAW ETM-RC135V/W-2 VOL 2 PG 56-31 PARA 5 6.1.4.3 A/C REQUIRED SUPPORT FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 VALIDATE THE CURRENT PN/SN INSTALLED ON A4848 AND UPDATE IMD S CONFIGURATION WUC 72XNO AS REQUIRED IAW AFO 21-101 CHAPT LN-120 "SIRU ALERT" SYSTEM PROCESSOR FAIL ATTEMPTED AIRBORNE ALIGNMENT UNABLE TO REALIGN A/C REQUIRED SUPPORT FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY RC-135V, T/N 64-14848, 30 April 2015 U-84 *REDBALL*: RT OVERWING HATCH EMER LIGHT MISSING MIRROR WC Event Narrative LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 # 6 WHL DUST CVR REM FOR W/T CHG IPI REQ IAW 1C-135-2-7-1 PA RA 9-13.4 STEP 6(OC/WC), STEP 27(RC/TC) LH 35 DEG CONTROL VALVE INDICATOR INOP (VALVE ACTUATES CORRE CTLY) LH KEEL BEAM BAY DOOR OPENED TO FOM CENTER WING ACCESS DOOR OPENED TO FOM # 6 W/T WORN OUT OF LMITS REQ R2 IPI REQ IAW 1C-135-2-7-1 P ARA 6.13.2STEP 3, STEP 3, 6.13.3 STEPS 1,5, 6 & 6.13.2. # 6 WHL SPD TRN REM FOR W/T CHG IPI REQ IAW1C-135-2-1 PARA 6 .13.3 STEPS 9, 11 & PARA 9.12.2. THIS IS THE INSTALLATION WCE CREATED BY JCN 150550026001 # 6 W&T ANTI-SKID SYS REQUIRES OPS CHECK IAW 1C-135-2-7-1PAR A 9-13 FOR OC/WC, PARA 9.14 FOR RC/RC. SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 OPENED FOR LCS INSPECTION 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 L.H. PACK OVERPRESSURIZES WHEN TURNED ON. FLOW CONTROLLER SH OWS "UUUU" JUST AFTER 44 IN H2O AND LOUD RUSH OF AIR RH KEEL BEAM BAY DOOR OPENED TO FOM LH KEEL BEAM BAY DOOR OPENED TO FOM CENTER WING ACCESS DOOR OPENED TO FOM LH WATER SEPARATOR REMOVED TO FOM LH TORQUE MOTOR REMOVED FOR REPLACEMENT LH 35DEG TEMP SENSOR REMOVED FOR REPLACEMENT LH 35DEG CONTROL VALVE REMOVED FOR TS RH 35DEG CONTROL VALVE REMOVED FOR TS BP6 WOULD NOT POWER ON 5 EA WARN TAGS INATLLED 1OF5 TOW BAR REC 2OF5 PLUMB BOB INDI CATION 3OF5 BLEED AIR RECPT 4OF5 THROTTLES 5OF5 FUEL CONTRO RC-135V, T/N 64-14848, 30 April 2015 U-85 LFT MLG AXLE ON JACKS WC Event Narrative LEFT OVERWING HATCH PIVOT HOOK NEEDS TO BE ADJUSTED. WHILE I KESTREL B DOES NOT RECOGNIZE A/D DEMOD CARD SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY # 1 KDU INOP SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OA FBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE F *REDBALL* #4 GEN LOW RPM LIGHT ILLUMINATED #4 ENG FAN COWL OPENED TO FOM. PLP INTERMITTENTLY GIVES MORPH-B 100MHZ INPUT ERRORS WHEN SW ITCHING ANTENNA INPUTS. FDP WILL NOT BOOT, WORKS FINE WITH BP2 IS CONFIGURED. A/C REQUIRED SUPPORT FOR LAUNCH PERFORM WASTE SYS SANITIZING FOR THE ACFT WASTE TA & LAV SVC CART IAW ETM-RC135V/W-2. SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY C/W 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO C/W 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 LH FLOW CONTROLLER SHOWED "UUUU" LASTED LONGER THAN 30SECOND S. FELT AND HEARD RUSH OF AIR. ATTEMPTED TO ADD HEAT BUT PILOT SEAT RAILS-- REQUEST LUBRICATION FOR SLIDING FORE + AF T #3 ENG FUEL FLOW SENSOR/TRANSMITTER SEEMS TO BE LAGGING. FUE L GAUGE READING + FMS FUEL PAGE FLOW READING LAG BEHIND OT RC-135V, T/N 64-14848, 30 April 2015 U-86 LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 WC Event Narrative #1 ENGINE FAN COWL OPEN TO FOM #2 ENGINE FAN COWL OPEN TO FOM #3 ENGINE FAN COWL OPEN TO FOM #4 ENGINE FAN COWL OPEN TO FOM #1 ENGINE CHIP DETECTORS (4 EACH) REMOVED FOR INSPECTION #2 ENGINE CHIP DETECTORS (4 EACH) REMOVED FOR INSPECTION #3 ENGINE CHIP DETECTORS (4 EACH) REMOVED FOR INSPECTION #4 ENGINE CHIP DETECTORS (4 EACH) REMOVED FOR INSPECTION LT OB FLAP UPPER OB SURFACE GOUGED AND REQUIRES SHEET METAL EVAL NEXT DOWNTIME A/C REQD SUPPORT FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY 60HR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 PAGE 2-A-30A PARA 22 60HR INSP IN PROGRESS:#1,2,3,&4 C/B'S PULLED. NOTE STARTER SERVICING BEING PERFORMED.DONT RESET START INSP ALL 4 ENG TRANS GEARBOES FOR LEAKS,LOOSE OR MISSING HARDWARE IAW 1C-135-6 PGS-A-031 STEP22 B ALL FOUR ENGINES STARTERS DUE OIL CHECK IAW 1C-135(K)R-2-4JG-6 TASK 6-28-1 PARA 6-127 INSP ALL 4 ENGINE CHIP DETECTORS 1AW IAW 1C-135-6 PG S-A-031 STEP 22 ITEM C INSPECT OIL LEVELS ON #1,2,4 ENGINE IDG'S IAW 1C-135-6 PG 2 S-A-032A ITEM 3 STEP B ALL FOUR ENGINES DUE IDLE RUN & LEAK CHECK ON OIL SYSTEM IAW 1C-135(K)R-2-4JG-5 TASK 5-12-1 PG 5-28 INLES & EXHAUST INSPEC DUE PRIOR ENGINE FUNCTION IAW 1C-135(K)R-2-4JG-2 TASK 2-14-1 PAGE 2-36 INLES & EXHAUST INSPEC DUE POST ENGINE FUNCTION IAW 1C-135(K)R-2-4JG-2 TASK 2-15-8 PAGE 2-154 INSP DIFFERENTIAL OIL PRESSURE INDICATOR(DPI) FOR POPPED INDICATION. ON#1,2,4 IDG'S IAW 1C-135-6 LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 C/W MODE IV/MODE C CHECK IAW ACCI 21-101 SEC 22F C/W 12 MTH HOT GAS PURGE OF LOX CONVERTERS IAW1C-135-2-3-2 P ARA 10.2.5.1 SERVICE LOX AFTER HOT GAS PURGE RC-135V, T/N 64-14848, 30 April 2015 U-87 LT FLAP UPPER SURFACE SKIN HAS RUB SPOTS AND REQUIRES SHEETM ETAL REPAIR NEXT DOWNTIME WC Event Narrative PERFORM PITOT-STATIC SYSTEM & ADC CHECKOUT PER ETM-RC135-2-11, CHAPTER 5. PERFORM ADC CHECKOUT PER ETM-RC135-2-11, CHAPTER 5 PILOT'S PITOT TUBE TAPED TO FOM. SEE WCE 1 COPILOT'S PITOT TUBE TAPED TO FOM. SEE WCE 1 PILOT'S STATIC BOOM TAPED TO FOM. SEE WCE 1 COPILOT'S STATIC BOOM TAPED TO FOM. SEE WCE 1 TTU-205 CONNECTED TO A/C TO FOM. SEE WCE 1 C/W 12M SINCE LAST PE PERFORM HOURLY(F108)(EXCLUDING TC-135 SERIES) SEE JCN 150400039 FOR COMPLETION 3EA LOX CONVERTERS DRAINED FOR HOT GAS PURGE SEE JCN 1504300 25 WCE 001 TENSION READS LOW (59 LBS) ON 14379 SETTING (HOWEVER, IT REA QD ONLY HAS 2 THREADS SHOWING IN CENTER BODY HYD TEST STAND HT05 CONNECTED TO #1 & #4 ENGINES CHUCK ASSEMBLY AT QD, THE SLEEVE NEEDS REPLACED AND GLUED ON WITH XL8 (WORN IN 2 SPOTS 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 PANEL OPENED FOR LCS INSPECTION LT MLG FWD DOOR SEALS TORN IN MULTIPLE PLACES (M) RT AFT MLG FWD DOOR SEALS TORN IN MULTIPLE PLACES (M) LEFT AND RIGHT ACM REQUIRES SERVICING LEFT KEEL BEAM BAY DOORS OPEN TO FOM RIGHT KEEL BEAM BAY DOOR OPEN TO FOM LT AND RT ACM REQUIRE DRAIN AND SERVICED LT OB FLAP UPPER OB SURFACE GOUGED. REQUIRES SHEET METAL EVA L LT FLAP UPPER SURFACE SKIN HAS RUB SPOTS, POSSIBLE CORROSION . REQUIRES SHEET METAL EVAL #4 ENGINE FUEL PUMP QUAD BOLT RETAINER MISSING. NO FOD #4 ENG COWLING OPENED TO FOM DENT IN CENTERWING CAVITY DRAIN LINE BY RT WHEEL AFT DOOR PA DDLE. LT OB AIL TAB MIDDLE HINGE PIN NOT IN SEGMENT HF LONGWIRE TENSION QUESTIONABLE, WIRE 14379 INSTALLED ON JE T READS 59LBS WITH TENSIOMETER SETTING AT 14379 AND READS 7 INSPECTION INPROGRESS IN & AROUND MAIN & LEADING EDGE FLAPS DO NOT OPERATE LT WING O/B LEADING EDGE FLAP REMOVED FOR #1 ENG FAN DUCT OPENING RT WING O/B LEADING EDGE FLAP REMOVED FOR #4 ENG FAN DUCT OPENING RC-135V, T/N 64-14848, 30 April 2015 U-88 AT QD CHUCK ASSY 1/4" OF WIRE EXPOSED WC Event Narrative REMOVE,CLEAN & INSPECT LT HYD BLEED ORIFICE LT HYD BLEED ORIFICE REQUIRES LEAK CHECK REMOVE,CLEAN & INSPECT RT HYD BLEED ORIFICE RT HYD BLEED ORIFICE REQUIRES LEAK CHECK REMOVE,CLEAN,REPLACE LT HYD RETURN FILTER LT HYD RETURN FILTER REQUIRES LEAK CHECK REMOVE,CLEAN,REPLACE RT HYD RETURN FILTER RT HYD RETURN FILTER REQUIRES LEAK CHECK ALL FOUR ENGINE REQUIRES TCTO 566 FUEL PUMP REPLACEMENT 2 WA RNING TAGS INSTALLED 1.EXT PWR RECPT 2.ACFT BATT SW. NOTE: D RT WING OTBD LEADING EDGE FLAP REQUIRES REMOVAL DUE TO #4 ENG INBD FAN DUCT BEING OPEN FOR TCTO ALL FOUR ENG T-HANDLES PULLED FOR ENGINE MAINT DO NOT PUSH IN #1 FUEL PUMP REQUIRES REPLACEMENT FOR TCTO IPI REQURED DURING INSTALLATION IAW 2J-F108-2-1 #1 VSV STATIC RIG CHECK REQUIRED IAW 2J-F108-2-1 WP73-21-10-501 FIG 502 PARA C #1 VBV STATIC RIG CHECK REQUIRED IAW 2J-F108-2-1 WP73-21-10-501,FIG505 PARA C #1 PERFORM PLA GAIN CHECK IAW 1C-135-2-4-1-1 PG6-74 PARA 6.28.2 #1 ENG REQUIRES WET MOTOR DUE TO FUEL PUMP CHG IAW 1C-135-2-4-1-1 PG 3-205 PARA 3.13 #1 ENG PERFORM IDLE LEAK CHECKS IAW 1C-135-2-4-1-1 PG3-300 PARA 3-14.2 #2 FUEL PUMP REQUIRES REPLACEMENT FOR TCTO. IPI REQUIRED DURING INSTALLATION IAW 2J-F108-2-1 #2 VSV STATIC RIG CHECK REQUIRED IAW 2J-F108-2-1 WP73-21-10-501 FIG202 PARA C #2 VBV STATIC RIG CHECK REQUIRED IAW 2J-F108-2-1 WP73-21-10-501 FIG 505 PARA C #2 ENG PERFORM PLA GAIN CHECK IAW 1C-135-2-4-1-1 P6-74 PARA6.28.2 #2 ENG REQUIRES WET MOTOR DUE TO FUEL PUMP CHG IAW 1C-135-2-4-1-1 PG 3-205 PARA3.13 #2 ENG PERFORM IDLE LEAK CHECKS IAW 1C-135-2-4-1-1 PG3-300 PARA3-14.2 #3 FUEL PUMP REQUIRES REPLACEMENT FOR TCTO. IPI REQUIRED DURING INSTALLATION IAW 2J-F108-2-1 #3 VSV STATIC RIG CHECK REQUIRED IAW 2J-F108-2-1 WP73-21-10-501 FIG 502 PARA C #3 VBV STATIC RIG CHECK REQUIRED IAW 2J-F108-2-1 WP73-21-10-501 FIG 505 PARA C #3 ENG PERFORM PLA GAIN CHECK IAW 1C-135-2-4-1-1 PG6-74 PARA6.28.2 #3 ENG REQUIRES WET MOTOR DUE TO FUEL PUMP CHG IAW 1C-135-2-4-1-1 PG3-205 PARA3.13 #3 ENG PERFORM IDLE LEAK CHECKS IAW 1C-135-2-4-1-1 PG3-300 PARA3-14.2 #4 FUEL PUMP REQUIRES REPLACEMENT FOR TCTO. IPI REQUIRED DURING INSTALLATION IAW 2J-F108-2-1 #4 VSV STATIC RIG CHECK REQUIRED IAW 2J-F108-2-1 WP73-21-10-501 FIG 502 PARA C RC-135V, T/N 64-14848, 30 April 2015 U-89 LT WING OTBD LEADING EDGE FLAP REQUIRES REMOVAL DUE TO #1 ENG INBD FAN DUCT BEING OPEN FOR TCTO WC Event Narrative #4 VBV STATIC RIG CHECK REQUIRED IAW 2J-F108-2-1 WP73-21-10-501 FIG 505 PARA C #4 ENG PERFORM PLA GAIN CHECK IAW 1C-135-2-4-1-1 PG6-74 PARA6.28.2 #4 ENG REQUIRES WET MOTOR DUE TO FUEL PUMP CHG IAW 1C-135-2-4-1-1 PG3-205 PARA3.13 #4 ENG PERFORM IDLE LEAK CHECKS IAW 1C-135-2-4-1-1 PG3-300 PARA 3.14.2 #3 MEC VBV CABLE BRACKET BENT, MEC REQUIRES REPLACEMENT. #3 ENG THROTTLE QUADRANT DISC'D FROM MEC TEMS OF FDR REQUIRES DOWN LOAD DUE TO FUEL PUMP CHANGE AND TRIM RUNS 12 M SINCE LAST PE PERFORM 900 HOURLY INSP DUE IAW T.O 1C-13 5-6 PANEL SHEET IN USE FOR 900 HOUR INSPECTION IAW 00-20-1 PG5-7PARA5.7.3.16.3.3.1 8 EA SPOILER LOCKS INSTALLED FOR INSPECTION 1EA WARN TAG 1OF1 INSTALLED ON FLAP HANDLE. NOTE: DO NOT OPERATE FLAPS. 900 HR INSP INPROGRESS 8 EA LEADING EDGE FLAP LOCKS INSTALLED FOR 900 HOUR INSPECTION 2EA WARN TAGS 1OF2 STAB TRIM CUTOUT SW;2OF2 FCS PER SWITCH, NOTE DO NOT OPERATE STAB TRIM LOCK INSTALLED. 3EA C/B SAFETY LOCKS INSTALLED ANTENNA COVERS INSTALLED FOR 900 HR INSP 3EA WARNTAGS 1OF1LTHYD DP SW,2OF3 RTHYD DPSW;3OF3 BLEEDAIR DOOR. NOTE:DON'T MOVE SWITCHES/APPLY AIR 2 EA WARNING TAGS 1 OF 2 PILOTS YOKE STAB TRIM SWITCH; 2 OF2 CO-PILOT YOKE STAB TRIM SWITCH. NOTE: DO NOT OPERATE. LT HYDRAULIC RESERVOIR DRAINED FOR RETURN FILTER MAINTENANCE RT HYDRAULIC RESERVOIR DRAINED FOR RETURN FILTER MAINTENANCE CIRCUIT BREAKER SAFTEY LOCKS INSTALLED 1EA-1,2,3, 4 FIRE SUPPRESSION C/B'S CIRCUIT BREAKER SAFETY LOCKS INSTALLED 1EA-1,2,3, 4 FIRE SHUTOFF ENG C/B'S 4EA WARNTAGS #1T-HANDLE,#2THANDLE,#3THANDLE,#4THAN DLE, NOTE DO NOT PUSH IN ENG MAINT INPROGRESS # 1 ENG PERFORM THROTTLE RIG CHECK IAW 1C-135-2-4 -1-1 PG 6-78 PARA 6.31 #1 ENGINE TRIM TOOL INSTALLED #1 ENGINE REQUIRES TRIM RUN IAW 1C-135- 2-4-1-1 PG 3-246 PARA 3.17 #2 ENG PERFORM THROTTLE RIG CHECK IAW 1C-135-2-4-1 -1 PG 6-78 PARA 6.31 #2 ENG TRIM TOOL INSTALLED #2 ENG REQUIRES TRIM RUN IAW 1C-135-2-4-1-1 PG 3-246 PARA3.17 #3 ENG PERFORM THROTTLE RIG CHECK IAW 1C-135-2-4- -1 PG 6-78 PARA6.31 #3 ENGINE TRIM TOOL INSTALLED #3 ENGINE REQUIRES TRIM RUN IAW 1C-135-2-4-1-1 PG 3-246 PARA 3.17 RC-135V, T/N 64-14848, 30 April 2015 U-90 3EA WARNTAGS 1OF3 I/B CUTOUT SW,2OF3 O/B CUTOUT SW,3OF3 SPOILER HANDLE,NOTE DO NOT RESET /MOVE WC Event Narrative #4 ENG PERFORM THROTTLE RIG CHECK IAW 1C-135-2-4- -1 PG 6-78 PARA 6.31 #4 ENG TRIM TOOL INSTALLED #4 ENG REQUIRES TRIM RUN 1C-135-2-4-1-1 PG 3-246 PARA 3.17 PRE INLET AND EXHAUST INSPECTION PRIOR TO ENG RUN FOR FUEL PUMP TCTO 566 ALL 4 ENGINES POST INLET AND EXHAUST INSPECTION PRIOR TO ENG RUN FOR FUEL PUMP TCTO ALL 4 ENGINES AISLE MAINT COMM CORD REQUIRES REPAIR. COMPLY WITH ACFT RECORDS CHECK IAW ACCI 21-101, OA FBS1 28 DAY FMS UPDATE REQUIRED TAWS ALERT @5000 FEET IN THE CLIMB, STAYED ON THROUGH 11,000 UNTIL TURNED OFF. CB PULLED AND RADIO ALTIMETER TURNED OFF. *REDBALL* #4 LOW OIL PRESSURE LIGHT ILLUMINATED #4 ENG COWLING OPEN TO FOM #4 ENG DUE LEAK AND OPS CHECK UHF 4 HAS VSWR ERRORS IN LINE-OF-SIGHT AND SITCOM SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 IRS1 GPS NO SIGNAL. RED W/ "--" EIN BUS A FAIL ON LN-120. 2 EA FIRST AID KITS FORWARD OF GALLEY OVER DUE INSPECTION/ R EQUIRE REPLACEMENT LEFT WING LANDING LIGHT PANEL RMVD TO RESET TAXI CIRCUIT BRE AKER NAV CLOCK INOP. TAWS WARNING WENT OFF AT 5000FT AND AGAIN AT FL320 WHEN TEST ED. WOULD NOT STOP UNTIL WE TURNED IT TO OVERIDE. DMCS #2 VHF TUNERS FAIL, MULTIPLE P/C AND RESETS NO GOOD. E9 FAIL RFD BITE TEST POS 23 KEYBOARD HAS INTERMITTENT CONNECTIVITY. CV131 DOWNCONVERTER COMES UP DOWN. RC-135V, T/N 64-14848, 30 April 2015 U-91 28 DAY TAWS UPDATE REQUIRED WC Event Narrative EIN BUS A FAIL ON LN-120. SEE THIS JCN WCE 001 FOR ORIGINALW RITE UP NDU BUS A FOR LN-120 REQ. OPS CHECK IAW ETM-RC135V/W-2 VOL 2 PARA 40.1.4 SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 PANEL OPENED FOR LCS INSPECTION MAIN ACFT BATT DEAD REQ R2 THIS IS THE INSTALLATION WCE CREATED BY JCN 150330076001 12 HOUR CURE CHK NEEDED ON GPS 1 ANTENNA. APPLIED AT 2130 6 HR CURE CHECK NEEDED ON GPS 1 ANTENNA @ 1600. SEE THIS JCN WCE 001. SCREW STRIPPED ON FMS GPS 1 ANTENNA UHF 4 SHOWS VSWR FAULT WHEN TX CE 4 FAILED TO CONNECT ESP GUI INTERFACE WHEN TRANSFERING PA SUPPORT REQUIRED FOR A/C LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 FWD BODY AFT PUMP LEAKING REQUIRES HYDRO EVAL FWD FWD AR PUMP ACCESS PANEL AND FWD AFT AR PUMP ACCESS PANE L REMOVED TO FOM UNABLE TO RESET SSD EDAS WITH SYSTEM STATUS E6 FAIL MULT RFD BORESIGHT TEST RC-135V, T/N 64-14848, 30 April 2015 U-92 LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 WC Event Narrative SUPPORT REQUIRED FOR A/C LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY I'S AND E'S INSP REQUIRED PRIOR TO ENGINE RUN LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 GPS 1 NO NAV ALL FLIGHT. NO SATS OR INTEG. FMS 1 COULD NOTBE USED FOR ANY GPS BASED NAVIGATION FMS 1 REQUIRES OUT OF DOCK CHK FWD BDY FWD A/R PUMP PRESS LINE LEAKING FWD BDY FWD A/R PUMP PANEL REMOVED TO FOM LEAK AND OPS CHECK DUE ON FORWARDS BODY FORWARD AR PUMP FORWARD BODY FUEL CELL ACCESS PANEL REMOVED FOR FOM #2 ENGINE FAN COWL OPENED TO FOM HYDRAULIC TEST STAND HT08 CONNECTED TO #2 ENGINE. 1 OF 1 WARNING TAG INSTALLED. 1 OF 1 LEFT HYDRAULIC PRESSURE SWITCH. CANNOT CONFIGURE FOR SHAWNA WITH ANY CE SUPPORT REQUIRED FOR A/C LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY INLET & EXHAUST INSP DUE PRIOR TO ENG RUN INLET & EXHUAST INSP DUE POST ENG RUN LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 RC-135V, T/N 64-14848, 30 April 2015 U-93 I'S AND E'S INSP REQUIRED AFTER ENGINE RUN WC Event Narrative RH S-DUCT REMOVED FOR INSPECTION A/C T-DUCT REMOVED FOR INSPECTION CENTER WING ACCESS PANEL REMOVED TO FOM 120 DAY AN/ASN-121 BATTERY CAP CHECK & INSP IAW 1C-135-6 COMPLY WITH 60 DAY HPO CARD IAW ETM-RC135-6WC-1 CARD 7-001 5EA WARN TAGS INSRTALLED 1OF5 EXT AIR RECPT 2OF5 ENG THROTTL ES 3OF5 TOW RECPT 4OF5 PLUMB BOB INDICATION 5OF5 REFUEL PNL COMPLY WITH 60 DAY HPO CARDS IAW 1C-135-6WC-1 COMPLY WITH 60 DAY HPO CARD IAW ETM-RC135-6WC-1 CARD 6-001 55ISS COMPLY WITH 60 DAY HPO IAW ETM-RC135-6WC-1 CARD 4-001, 5-001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 PANEL OPENED FOR LCS INSPECTION RT KEEL BEAM BAY DOOR LOWERED FOR HPO (CLOSE IAW 1C-135-2-2, PG 3-181, PARA 3-145, STEP 5) LT KEEL BEAM BAY DOOR LOWERED FOR HPO (CLOSE IAW 1C-135-2-2, PG 3-181, PARA 3-145, STEP 5) FRONT URINAL EXTREMELY SLOW TO DRAIN 10EA COVE LIP DOORS LOWERED FOR HPO, (RAISE) IAW 1C-135-2-8, PG 5-220, PARA 5-159, STEP 11 STAB TRIM ACCESS PANEL REMOVED(INSTALL IAW 2-8,PG 6-7,PARA 6-21 STEP5)1EA WARNING TAGS INSTALLED #4 ENG FAN COWL OPEN FOR HPO(CLOSE IAW 1C-135-2-2, PG 5-16H, PARA, STEP 5) #3 ENG FAN COWL OPEN FOR HPO(CLOSE IAW 1C-135-2-2, PG 5-16H, PARA, STEP 5) #2 ENG FAN COWL OPEN FOR HPO(CLOSE IAW 1C-135-2-2, PG 5-16H, PARA, STEP 5) #1 ENG FAN COWL OPEN FOR HPO(CLOSE IAW 1C-135-2-2, PG 5-16H, PARA, STEP 5) #1 ENG DUCT COWL OPEN FOR HPO (CLOSE IAW 1C-135-2 -2 PG 5-16H, PARA 5-28G) #2 ENG DUCT COWL OPEN FOR HPO (CLOSE IAW 1C-135-2 -2 PG 5-16H, PARA 5-28G) #3 ENG DUCT COWL OPEN FOR HPO (CLOSE IAW 1C-135-2 -2 PG 5-16H, PARA 5-28G) #4 ENG DUCT COWL OPEN FOR HPO (CLOSE IAW 1C-135-2 -2 PG 5-16H, PARA 5-28G) JFS TURBINE OIL DRAINED 1EA WARNING TAGS INSTALLED 1OF1 JFS STARTER C/B NOTE: DO NOT RESET DMCA# 2B FAILS RFD BORESIGHT ALL CHANNELS DMCA2 ISSUES DMCA2 10 GIGE NOT RESPONDING TO PING CHECK CABL E NO TX OR RX UHF #4 SUPPORT REQUIRED FOR A/C LAUNCH C/W CARD 4-012IAW 1C-135-6WC-1 RT ACM DRAINED FOR HPO IAW 1C-135-6WC-1 CARD 4-012 RC-135V, T/N 64-14848, 30 April 2015 U-94 AN/ASN-121 BATTERY REQUIRES REPLACEMENT SEE JCN 150270007 FO R ORIGINAL DISCREPANCY. WC Event Narrative LT ACM DRAINED FOR HPO IAW 1C-135-6WC-1 CARD 4-012 C/W 1C-135-6WC-1 CARD 4-006 ITEM 1 AND 2 SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 8 EA SPOILER LOCKS INSTALLED FOR HPO. 3 EA WARNING TAGS INSTALLED.SEE PG BLK NOTE: DO NOT OPERATE 6EA WARN TAGS INST 1/6 SPOIL CONT HNDL2/6IB SPOIL CO3/6OB SPOIL CO4/6STAB TRIM CO5/6FLAP HNDL6/6A/R (83FL) C/W 1C-135-6WC-1 CARDS 4-002 THRU4-011, 4-015,4-016 ITEMS 1 THRU 5,4-020 THRU 4-22 (83FL) C/W IPI INSP IAW LPS MXG-1C-135-6WC-1-OFC1 CARD 4-022 ITEM 1 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY (83GC)C/W INSP 1C-135-6WC-1 CARD 4-016 ITEM 8 A/R DOOR LOCK INSTALLED 1EA WARNING TAG INSTALLED (83HY)COMPLY WITH 1C-135-6WC-1 CARD 4-019 ITEMS 2 THRU 4 ALL FOUR ENG FIRE SUPPRESSION C/B S PULLED FOR HPO HPO 4 EA WARNING TAGS INSTALLED NOTE: DO NOT RESET ALL FOUR ENG T-HANDLES PULLED 4EA WARNING TAGS INSTALLED NOTE: DO NOT RESET ALL FOUR ENG FIRE SHUTOFF C/B S PULLED FOR HPO HPO 4EA WARNING TAGS INSTALLED NOTE: DO NOT RESET SHOP NARRATIVE: (83JE)C/W 1C-135-6WC-1 CARD 4-016 ITEM 7 ALL FOUR ENGINES DUE AUDIBLE IGNITION CHK FOR HPO LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 EXT RECON POWER DOES NOT WORK IN EXTERNAL BUT DOES IN APPLIE D **REDBALL** FMS NO RAIM POSN 1 KEYBOARD SHIFT KEY INOP DMCA 1B FAILS RFD BORESIGHT (TEMP CABLE INSTALLED FROM ESW11 6 TO EAP132) DMCA 1B FAILS RFD BORESIGHT (TEMP CABLE INSTALLED FROM ESW11 6 TO EAP132) DMCA 1B FAILS RFD BORESIGHT (TEMP CABLE INSTALLED FROM ESW11 6 TO EAP132) CAN 105 FAILS ]RFA PERFORM WASTE SYS SANITIZING FOR THE ACFT WASTE TA & LAV SVC CART IAW ETM-RC135V/W-2. REMOVE HALON 1211 FIRE EXTING FOR COMPLETE MAINT RC-135V, T/N 64-14848, 30 April 2015 U-95 8EA L/E FLAP LOCKS INSTALLED 1EA WARNING TAG INSTALLED 1OF1 FLAP HANDLE NOTE: DO NOT OPERATE WC Event Narrative SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY REMOVE AND INSPECT MAIN ENGINE FUEL FILTER FOR TOPCOAT CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 WITH FILTERS REMOVED INSP ALL HELICOIL INSERTS FOR PROPERINSTALL/CONDITION IAW LPS-55MXG-1C-135-6OFC1 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 REMOVE AND INSPECT MAIN ENGINE FUEL FILTER FOR TOPCOAT CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 WITH FILTERS REMOVED INSP ALL HELICOIL INSERTS FOR PROPERINSTALL/CONDITION IAW LPS-55MXG-1C-135-6OFC1 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 REMOVE AND INSPECT MAIN ENGINE FUEL FILTER FOR TOPCOAT CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 WITH FILTERS REMOVED INSP ALL HELICOIL INSERTS FOR PROPERINSTALL/CONDITION IAW LPS-55MXG-1C-135-6OFC1 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 REMOVE AND INSPECT MAIN ENGINE FUEL FILTER FOR TOPCOAT CONTAMINATION IAW LPS-55MXG-1C-135-6-OFC1 WITH FILTERS REMOVED INSP ALL HELICOIL INSERTS FOR PROPERINSTALL/CONDITION IAW LPS-55MXG-1C-135-6OFC1 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 VISUALLY INSP, WITHOUT REMOVAL, TRANSFER GEAR BOX, CLEVIS MOUNT BRACKET IAW T.O. 2J-F108-2-1 VISUALLY INSP ENGINE OIL CHIP DETECTORS FOR WEAR INDICATIONS. IAW T.O. 2J-F108-2-1 LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 #1 ENG FAN COWL OPEN TO FOM #2 ENG FAN COWL OPEN TO FOM #3 ENG FAN COWL OPEN TO FOM #4 ENG FAN COWL OPEN TO FOM RC-135V, T/N 64-14848, 30 April 2015 U-96 CHECK STARTER SYSTEM OIL LEVEL IAW T.O. 1C-135(K)R-2-4JG-6 WC Event Narrative #1 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #2 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #3 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #4 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #1 ENG FUEL STRAINER REMOVED FOR INSP #2 ENG FUEL STRAINER REMOVED FOR INSP #3 ENG FUEL STRAINER REMOVED FOR INSP #4 ENG FUEL STRAINER REMOVED FOR INSP SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 INLETS AND EXHAUSTS INSP DUE PRIOR TO ENG RUN INLETS AND EXHAUSTS INSP DUE POST TO ENG RUN TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 ENG'S 1,2,3,4 T-HANDLES PULLED ENG STARTER C/B'S P ULLED FIRE SPRSN C/B'S PULLED FIRE SHUTOFF PULLED 4 EACH WARNING TAGS INSTALLED ON #1 ENG STARTER C/ B,FIRE SPRN C/B,T-HANDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #2 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #3 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #4 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 2 EACH WARNING TAGS INSTALLED ON: ACFT BATT SWITCH INSP ALL 4 ENG TRANS GEARBOXES FOR LEAKS,LOOSE OR MISSING HARDWARE IAW 1C-135-6 PG.S-A-031 STEP 22 ALL FOUR ENG STARTERS DUE OIL CHECK IAW 1C-135(K)R -2-4JG-6 TASK 6-29-1 PG 6-136 INSPECT ALL FOUR ENG CHIP DETECTORS 1AW IAW 1C-135-6 PG S-A-031 STEP 22 ITEM C INSP DIFFERENTIAL OIL PRESSURE INDICATOR(DPI) FOR POPPED INDICATION. ON#1,2,4 IDG'S IAW 1C-135-6 INSP ALL 4 MAIN FUEL STRAINER FOR TOP-COAT C ONTAMINATION IAW 1C-135-6 PG 2-A-032 UTEN 30STEP A ALL 4 ENG DUE IDLE RUN LEAK CHECK ON OIL AND FUEL SYSTEMS IAW 1C-135(K)R-2-4JG-5 TASK 5-12-1 PG.5-28 C/W 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION RC-135V, T/N 64-14848, 30 April 2015 U-97 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION WC Event Narrative C/W 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 LEFT AR RECEPTACLE LIGHT BURNED OUT **REDBALL** NOSE WHEEL WELL INSP LIGHT INOP DSS CE#7 SHOWS OFFLINE FOR WB DSS DISPLAYS "SHAWNA DIGRX VERSION 01.001.037 IS NOT COMPATI BLE. SEE DSS.COMPATIBILITYXML" WHEN ATTEMPTING TO USE SHAWN XMP NO.1 WILL NOT PROCESS SIGNALS OF INTEREST WHILE TV IS RU NNING XMP NO.2 WILL NOT PROCESS SIGNALS OF INTEREST WHILE TV IS RU NNING A/R DOORS LOCK INSTALLED FOR LIGHTBULB R2 SEE THIS JCN WCE 0 01 'OVHD PANEL LIGHTS' LIGHT STAYED ON THE ENTIRE FLIGHT WITH N O ASSOCIATED OVHD PANEL FAULT. COULD NOT PRESS TO RE-SET. AUX HEAT PANEL READS 8 DEGREES WHEN VALVE IS IN THE FULL COL D POSITION OPS CHK DUE ON 'OVERHEAD PANEL LIGHTS' LIGHT CORPUS SHOWS RF PHASE BORESIGHT ERRORS EAN 105 AL WOULD NOT GO GREEN IN HCP. EAN 105 BR WOULD NOT GO GREEN IN HCP RACAL WOULD NOT ALLOW SIGNAL ROUTING IN MAINT. SWITCHING PAN STAMPEDING SEROW QRC INSTALLED TEAPARTY QRC INSTALLED A/C REQUIRES SUPPORT FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL ZERO ACCESS PNL REMOVED FOR INSPECTION PRE INLETS AND EXHAUST INSP REQ PRIOR TO ENG FUNTION POST INLETS AND EXHAUST INSP REQ AFTER ENG FUNCTION RC-135V, T/N 64-14848, 30 April 2015 U-98 GPS INTEG WARNING ON FMS 1-GPS 1 FOR THE MAJORITY OF THE FLI GHT. CAUSES RAIM ISSUES FOR GPS APPROACHES. SATELLITES WERE B WC Event Narrative FWD GAP WAVEGUIDE REMOVED TO F.O.M. SEE JCN 150140118 FOR OR IGINAL DISCREPANCY NAV RADAR WILL NOT DISPLAY CURRENT RADAR PICTURE WHILE IN SR CH/BCN/WARN. RADAR INOPERABLE. SCAN KNOB NEEDS TO BE TIGHT NOSE RADOME REMOVED TO F.O.M. SEE THIS JCN WCE 001 FOR ORIGI NAL DISCREPANCY RADAR OPS CHECK REQ IAW ETM-RC135-2-11 PG 2-40A PARA 2.4.2A SEE THIS JCN WCE 001 FOR ORIGINAL DISCREPANCY INS-1 GPS ANTENNA CONNECTOR PIN IS WEARING BADLY AND NEEDS R EPLACEMENT. HINDERS FUNCTION OF GPS ON INS-1. GPS APPROACH ON PILOT'S PFD DROPPED DURING FINAL APPROACH (S WITCHED TO COPILOT'S SIG GEN) COPILOT FLOOD LIGHT INOP LOW RPM LIGHTS ON IDG'S CONTINUOUSLY FLICKERED AFTER ENGINE START. OVERHEAD ANN CONTROL UNIT REQ'S R2 #1 ENGINE COWLING OPENED UP FOR FOM IAW 1C-135-2-10-1 SEE T HIS JCN 150140124001 #2 ENGINE COWLING OPENED UP FOR FOM IAW 1C-135-2-10-1 SEE T HIS JCN 150140124001 #4 ENGINE COWLING OPENED UP FOR FOM IAW 1C-135-2-10-1 SEE T HIS JCN 150140124 WCE 001 #1 IDG DISCONNECT FOR OPS CHECK SEE THIS JCN 150140124001 #2 IDG DISCONNECT FOR OPS CHECK SEE THIS JCN 150140124001 #4 IDG REQ'S SERVICING IAW 1C-135-2-10-1 SEE THIS JCN 150140 124001 #4 IDG OVERHEAT LIGHT BULB BURNT OUT #4 IDG DISCONNECT FOR OPS CHK SEE THIS JCN 150140124001 MULTIPLE C/B'S POPPED INFLIGHT: #2 FWD BOOST PUMP PHASE B,C #3 AFT BOOST PUMP PHASE B,C RH OVERRIDE PUMP B,C PHASE A DIS T SEVERAL SYSTEMS INOP W/ C/B POPS: SYD INOP (REENGAGING CAUSE D A/P TO UNCOUPLE), Q-INLET POWER OFF, COPILOT WINDOW HEAT I ASSYMETRIC THRUST AND Q-INLET POWER LIGHTS FLICKER DURING ST AB TRIM ACTUATION CABIN PRESSURE TEST GAUGE CONNECTED TO AICRAFT IN NOSE WHEEL WELL CABIN PRESSURE ALTIMETER UNMOUNTED FOR CABIN PRESSURIZATION OPS CHECK EXCESSIVE WHISTLING SOUND FROM FLIGHT DECK WHEN THROTTLES BR OUGHT BACK TO IDLE FORWARD BODY FUEL TANK BLANKING OUT *REDBALL* FWD BODY TANK BLANKS OUT #10 AND #11 SPOILER SWIVEL LEAKING REQS RESEAL #6 AND #7 COVE LIP DOORS LOWERED TO FOM #1 ENG COWLING OPEN TO FOM #2 ENG COWLING OPEN TO FOM #4 ENG COWLING OPEN TO FOM ES822 #5 WILL NOT RESET TO HCP RC-135V, T/N 64-14848, 30 April 2015 U-99 OPS CHECK DUE ON OVERHEAD ANN CONT UNIT IAW 1C-135-2-10-1 WC Event Narrative KESTREL A WILL NOT BOOT DSS CE #9 SHOWS OFFFLINE FOR WIDEBAND SUPPORT REQD FOR A/C LAUNCH 1 EACH PLUG INSTALLED IN BACK OF PRESSURE ALTIMETER 1 EACH W ARNING TAG INSTALLED 1OF1 CABIN PRESSURE ALTIMETER NOTE: PLU SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY 2 EA WARNING TAGS INSTALLED TO FOM 1 OF 2 ON RT AUX PUMP S/W 2 OF 2 ON LT AUX PUMP S/W MAINTENANCE IN PROGRESS NOTE: DON SPOILER LOCK INSTALLED ON #6 SPOILER TO FOM I'S & E'S DUE BEFORE ENGINE OPERATION. I'S & E'S DUE POST ENGINE OPERATION I'S & E'S DUE BEFORE ENGINE OPERATION. I'S & E'S DUE POST ENGINE OPERATION I'S AND E'S INSP REQUIRED PRIOR TO ENGINE RUN I'S AND E'S INSP REQUIRED AFTER ENGINE LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 DMCA 5 HAS STRIPPED SCREW AT 5 O-CLOCK POSITION DMCA 5 HAS STRIPPED SCREW AT 11 O-CLOCK POSITION INSPECT MODEL3050 HOUSING POWER CABLE GPS 1 WOULD NOT ACQUIRE. FMS DISPLAY WOULD DISPLACE RED. IRS RATE >1.45 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 PANEL OPENED FOR LCS INSPECTION LEFT ACM PACK OVERPRESSURIZES WHEN GROUND MAINTENANCE CAME U P TO CHECK OUT GRAVEL NOISE CENTER WING ACCESS PANEL OPENED TO FOM IAW 1C-135-2-3-2 (TEM P INSTALLED) SEE WCE 001 LH FLOW CONT. REQ R2 (TEMP INSTALLED) LH "S" DUCT REMOVED TO FOM (TEMP INSTALLED "T" DUCT REMOVED TO FOM LEFT ACM PACK HAS GRAVEL SOUND. NOTICED ON 1ST TOUCH AND GOA ND GOT WORSE ON 2ND T&G. THE PACK WAS SHUTDOWN IMMEDIAT RC-135V, T/N 64-14848, 30 April 2015 U-100 ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 WC Event Narrative LH WATER SEPARATOR SOCK REQ REPLACEMENT IPI REQUIRED IAW 1C- 135-2-3-2 PG 12-37 PARA 12.3.16 STEPS 2-3 SEE WCE 001 2 EA C/B COLLARS INSTALLED 1OF 2 LH A/C SHUTOFF VALVE C/B 2O F 2 AIR COND MONITOR C/B NOTE: DO NOT RESET!! SEE WCE 001 AN D 0 LH WATER SEPARATOR REMOVED TO FOM IAW 1C-135-2-3-2 SEE WCE 0 01 AND 002 LH KEEL BEAM BAY LOWERED TO FOM IAW 1C-135-2-3-2 SEE WCE 002 AND 004 LEAK AND OPS CHK DUE ON LH PACK IAW 1C-135-2-3-2 PG 13-13 PA RA 13.3 SEE WCE 001 AND 002 GROUND AIR EJECTOR VALVE REQ'S R2 SEE THIS JCN WCE 006 (CORR ECTIVE ACTION) LEAK AND OPS CHK DUE ON LH PACK LEFT ACM PACK SHOWS "LLLL" WHILE PACK IS TURNED OFF (NOTE: D O NOT OPERATE LH PACK!) LH PACK PRESSURE TRANSDUCER REQS R2 CENTER WING ACCESS PANEL LOWERED TO FOM SEE THIS JCN WCE 001 LH S-DUCT REMOVED TO FOM SEE THIS JCN WCE 001 GROUND COOLING T-DUCT REMOVED TO FOM SEE THIS JCN WCE 001 LH PRESSURE REGULATOR REQ R2 SEE THIS JCN WCE 001 LEAK CHECK DUE ON LH S-DUCT SEE THIS JCN WCE 005 OPS CHECK DUE ON LH PRESSURE REGULATOR SEE THIS JCN WCE 007 AEP WILL NOT LOAD RCS HOOKDET CHANNELS 1+2 NOT RECIEVING FROM IF SWITCH HOOKDET CHANNELS 1+2 NOT RECIEVING FROM IF SWITCH DMCA 4 RXR4/RXR5/RXR7 PPS REFERENCE UNLOCKED DFS3 CH5 RCVR 3 TUNER #1 FAILS TUNER BS SINGLE CHNL PWR SUPPLY CAUSES SCROLLING "NO RESPONSE" ERRORS HLP-C WOULD NOT BOOT. BP2 CONFIGURED AS HLP-C A/C REQUIRES SUPPORT FOR LAUNCH 4 EA WARN TAGS INSTALLED 1OF4 BLEED AIR RECP NOTE:DO NOT APP LY AIR 2OF4 TOW RECP NOTE:DO NOT TOW 3OF4 NOSE JACK RECP NO 2 EA WARNING TAGS INSTALLED 1 OF 2 ON EXT BLEED AIR RECEPTAC LE 2 OF 2 ON #3 ENG THROTTLE NOTE: DO NOT APPLY BLEED AIR OR S SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 RC-135V, T/N 64-14848, 30 April 2015 U-101 LH PACK PRESSURE REGULATOR REQS R2 WC Event Narrative TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 CURE CHECK DUE ON PILOTS NUMBER 3 CHECK AT 1530 PILOTS #3 WINDOW DELAM REQ R2 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP PRIOR TO ENG R UN ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENG RUN 28 DAY FMS UPDATE REQ ABIT RADOME PAINT CHIPPED 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 OPENED FOR LCS INSPECTION ABIT RADOME PAINT CHIPPED SHARKBYTE II ANTENNA INST WEIGHT AND BALANCE REQ'D FOR TCTO RC/TC135-1175 C/W 1800 HR PERFORM OPS CHECKOUT OF GRAVITY FEED CONFIG (SUCTION) PER 2-5 SERIES TO ALL 4 ENG DUE GRAVITY FEED OPS CHECK ALL 4 ENGS DUE I'S AND E'S PRIOR TO NEXT ENG RUN ALL 4 ENGS DUE POST I'S AND E'S AFTER NEXT ENG RUN ROUTINE INSP ON LEFT AND RIGHT MLG ACTUATUORS 7 DAY LCS INSP DUE IAW ETM-RC135-6 FUEL CELL 0 PANEL REMOVED FOR LCS INSP SEE THIS JCN WCE 001 LEFT STATIC BOOM TAPED TO FOM SEE JCN 143500059 TTU 205 CONNECTED TO FOM ON INS 3(LN120), REPLACE LN-120 GPS INTERNAL BATTE RIES IN SIRU INSTALL LABEL WITH NEW DUE DATE A/C REQUIRES SUPPORT FOR LAUNCH AFT CARGO JUMP SEAT C/B CANNOT BE PUSHED IN. ES922 #5 WOULD NOT RESET TO HCP. SI9105 #3 WOULD NOT RESET TO HCP. SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION RC-135V, T/N 64-14848, 30 April 2015 U-102 THIS IS THE INSTALLATION WCE CREATED BY JCN 150070072001 WC Event Narrative ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 OPENED FOR LCS INSPECTION #4 CTW LEAKING REQUIRES FURTHER TROUBLESHOOTING CTW ACCESS DOOR W-45 REMOVE TO FOM CTW ACCESS DOOR W-52 REMOVE TO FOM LK CK DUE ON W45 AND W52 ACCESS DOORS AFTER REFUEL LK CK DUE ON #4 CENTER WING ACCESS DOOR AFTER REFUEL CTW #4 FUEL CELL CAVITY(RT SIDE FLOOR BOARDS)PARTIALLY REMOV ED TO FOM CTW #4 CELL REMOVED TO FOM 8 HR LEAK CHECK DUE ON #4 AND #5 CTW CELL AFTER REFUEL PERFORM WASTE SYS SANITIZING FOR THE ACFT WASTE TA & LAV SVC CART IAW ETM-RC135V/W-2. 5 EA WARNING TAGS INSTALLED ON 1OF5 SPR 2OF5 EXT PWR 3OF5 FM P 4OF5 A/C BATT 5OF5 JFS BATT NOTE: OPEN FUEL TANKS, DO NOTA P LN 120 C/B PULLED AND COLLARD NOTE: OPEN FUEL TANKS DO NOT R ESET 8 EA C/B PULLED AND COLLARD ON PANEL P-14 NOTE: OPEN FUEL TA NKS DO NOT RESET IPI DUE UNDER #4 CTW CELL ACCESS DOOR PRIOR TO CLOSE IAW 1C- 135-2-5-3 -6 INSPECTION DUE UNDER #4 CTW ACCESS DOOR PRIOR TO CLOSE IA W 1C-135-2-5-3 IPI DUE UNDER CTW ACCESS DOOR W-45 PRIOR TO TANK CLOSURE IAW 1C-135-2-5-3 -6 INSPECTION DUE UNDER CTW ACCESS DOOR W-45 PRIOR TO TANK C LOSURE IAW 1C-135-6 IPI DUE UNDER CTW ACCESS W-52 PRIOR TO TANK CLOSURE IAW 1C-1 35-2-5-3 -6 INSPECTION DUE UNDER CTW ACCESS DOOR W-52 PRIOR TO TANK C LOSURE IAW 1C-135-6 IPI DUE PRIOR TO INSTALLATION OF #4 CTW CELL (CAVITY PREP) I AW 1C-135-2-5-3 PARA 1.3.45 STEPS A-C WEATHER DOOR REQ REMOVAL TO FOM MAIN ACFT BATT DISCONNECTED FOR FUEL CELL MAINT ACCOMPLISH NAVIGATOR ALTIMETER REPLACEMENT LEFT STATIC BOOM TAPED TO FOM RC-135V, T/N 64-14848, 30 April 2015 U-103 CTW CELL #4 ACCESS DOOR REMOVED TO FOM WC Event Narrative TTU 205 CONNECTED TO FOM 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 OPENED FOR LCS INSPECTION REMOVAL OF ITEM FOR CANNIBALIZATION INSTALL AFTER CANNIBALIZATION MAIN AND JFS ACFT BATT DISCONNECTED FOR WASH/LUBE SEE PG BLK JFS ACFT BATT DISCONNECTED FOR WASH/LUBE SEE PG BLK POWER RUDDER S/O VLV IN LT W/W CLOSED. 1EA WARNIN G TAG INSTALLED DO NOT OPEN 10 EA COVE LIP DOORS OPEN FOR ACFT WASH CLOSE IAW 1C-135-2-8 PG 5-220 PAR 5-159 STP 11 #2 ENG FAN COWL OPN FOR ACFT WASH CLOSE IAW 1C-135-2-2 PG 5-16A PAR PAR 5-28B #3 ENG FAN COWL OPN FOR ACFT WASH CLOSE IAW 1C-135-2-2 PG 5-16A PAR PAR 5-28B #4 ENG FAN COWL OPN FOR ACFT WASH CLOSE IAW 1C-135-2-2 PG 5-16A PAR PAR 5-28B #1 ENGINE FAN DUCTS OPEN FOR ACFT LUBE CLOSE IAW 1C-135-2-2 PG 5-16H PAR 5-28G #2 ENGINE FAN DUCTS OPEN FOR ACFT LUBE CLOSE IAW 1C-135-2-2 PG 5-16H PAR 5-28G #3 ENGINE FAN DUCTS OPEN FOR ACFT LUBE CLOSE IAW 1C-135-2-2 PG 5-16H PAR 5-28G #4 ENGINE FAN DUCTS OPEN FOR ACFT LUBE CLOSE IAW 1C-135-2-2 PG 5-16H PAR 5-28G RT KEEL BEAM BAY DOOR LOWERED FOR POST WASH LUBE CLOSE IAW 1C-135-2-2 PG 6-110 PAR 6-115 LT KEEL BEAM BAY DOOR LOWERED FOR POST WASH LUBE CLOSE IAW 1C-135-2-2 PG 6-110 PAR 6-115 STAB TRIM ACCESS PANEL REMOVED FOR POST WASH INSTALL IAW 1C-135-2-8, PG 6-7, PAR 6-21, STEP 5 OVERWING HATCH KICKPLATES REMOVED FOR CCI OVERWING HATCH KICKPLATES REMOVED FOR CCI HORSESHOE PANEL REMOVED FOR CCI LOX SIDE/FLOOR PANELS REMOVED FOR CCI CARGO DOOR FLOOR BOARDS REMOVED/CARPET PULLED UP FOR CCI WEATHER DOOR REMOVED FOR CCI LAV SHROUD REMOVED FOR CCI 4EA WNG TAGS INST 1/4BAT PWRSWTCH2/4MAIN BAT QD3/4JFS BAT QD 4/4EXT PWR RCPT NOTE DO NOT APPLY PWR 8 EA SPOILER LOCKS INSTALLED 3 EA WARNINGTAGS INSTALLED. 1/3 SPOILER HANDLE 2/3 INBD CUT OUT SWITCH 3/3 OTBD CUT OUT SWI T RUDDER LOCK INSTALLED 1 EA WARNING TAG INSTALLED ON RUDDER P WR SWITCH NOTE DO NOT OPERATE 8 EA LEADING EDGE FLAP LOCKS INSTALLED 1 EAWARNING TAG INSTA LLED ON FLAP HANDLE NOTE DO NOT OPERATE STAB TRIM LOCK INSTALLED 1 EA WARNING TAG INSTALLED ON STAB TRIM CUT OUT SWITCH NOTE DO NOT OPERATE RC-135V, T/N 64-14848, 30 April 2015 U-104 #1 ENG FAN COWL OPN FOR ACFT WASH CLOSE IAW 1C-135-2-2 PG 5-16A PAR PAR 5-28B WC Event Narrative ACFT PROTECTIVE COVERS AND TAPE INSTALLED FOR WASH ACFT REQS POST WASH LUBE IAW 1C-135-6WC-3 CARDS 5- 001 THRU 5-049 ALL STEPS JFS INLET AND EXHAUST COVERED WITH FOIL FOR WASH IPI REQ FOR APPLYING SCH100 GREASE ON MLG BRAKE COLLAR FITTI NGS MAIN/JFS BATTS DISCONNECTED FOR CCI 4EA WARNING TAGS INSTALL ED 1/4 BATT PWR SWITCH 2/4 MAIN BATT QD 3/4 JFS BATT QD 4/4 EX 2EA JACK PAD ACCESS PANELS REMOVED FOR A&D JACKED 1 EA STUCK SCREW ON LOWER NOSE ACCESS PNL WASH ACFT IAW 1C-135-6WC-3 CARDS 1-001 THRU 4-008 LUBE ACFT IAW 1C-135-6WC-3 CARDS 5-001 THRU 5-049 ACFT A&D JACKED FOR NLG SWING 1EA JACK PAD INSTALLED FOR A&D JACK PRIOR TO DOWNJACKING ENSURE LANDING GEAR HANDLES IS IN DOWN AND LOCKED DETENT 28DAY FMS UPDATE REQUIRED RT OVER WING HATCH SEAL WORN OUT OF LIMITS REQ REPLACEMENT 8HR CUR CHECK DO ON RT OVER WING HATCH SEAL STARTING AT 1500 FINISHED AT 2300 ACFT OUTBD WING JACKS SEATED FOR FUEL CELL MAINT 2 EA OUTBD WING JACK PADS INSTALLED ON ACFT ACCOMPLISH ANTENNA LEADING EDGE TAPE REPLACEMENT LK AND OPS CK DUE NLG LOCK RETENTION ACT IAW 1C-135-2-7-1 PG 7-87 PARA 7.15.4 #2 ENG COWL OPENED TO FOM HYD MULE HT08 CONNECTED TO #2 ENG TO FOM IPI DU TO ENSURE LANDING GEAR LEVER IS RETURNED TO DOWN AND LOCKED POSITION IAW TO 1C-135-2-7-1 PG 7-5 PARA 7.4.4 C/W MODE IV/MODE C CHECK IAW ACCI 21-101 SEC 22F COMPLY WITH ACFT RECORDS CHECK IAW ACCI 21-101, OA FBS1 LN-120 BATT DISCONNECTED TO FOM. SEE JCN 143380016 WCE 001. SEE THIS JCN WCE 2 FOR WARNING TAGS. 4EA WARN TAGS INSTALLED 1/4INS3 400HZ 3PHASE 2/4INS3 BATT HE AT400HZ 3/4INS3 BATT CHARGING 28 VDC C/BS PULLED 4/4LN-120 B AT RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-2 SEE THIS J CN WCE 001 RH ACM LIMIT VALVE REMOVED TO FOM IAW 1C-135-2-3-2 SEE THIS JCN WCE 001 RH ACM LIMIT VALVE SENSING LINES REMOVED TO FOM IAW 1C-135-2 -3-2 SEE THIS JCN WCE 001 RH PRIMARY HEAT EXCHANGER CONDITIONED AIR AND BLEED AIR DUCT S REMOVED TO FOM IAW 1C-135-2-3-2 SEE THIS JCN WCE 001 LEAK AND OPS CHK DUE ON RH PACK IAW 1C-135-2-3-2 RC-135V, T/N 64-14848, 30 April 2015 U-105 ACCOMPLISH MINOR CCI IAW 1C-135-6WC-3 CARDS 6-001 THRU 6-003 WC Event Narrative PUZZLE BRACKET DUCTS REQ REALIGNMENT DUE TO LEAKING SEE THIS JCN WCE 042 LK AND OPS CK DUE ON RH PAC IAW 1C-135-2-3-2 SEE THIS JCN WE C 043 048 050 051 RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-2 SEE THIS J CN WCE 001 RH ACM LIMIT VALVE REMOVED TO FOM IAW 1C-135-2-3-2 SEE THIS JCN WCE 001 RH ACM LIMIT VALVE SENSING LINES REMOVED TO FOM IAW 1C-135-2 -3-2 SEE THIS JCN WCE 001 RH PRIMARY HEAT EXCHANGER CONDITIONED AIR AND BLEED AIR DUC TS REMOVED TO FOM IAW 1C-135-2-3-2 SEE THIS JCN WCE 001 LCS DRAIN LINE DUST COVER FWD OF FUEL CELL 1 BROKEN REMOVED MAIN BATTERY DISCONNECTED FOR FUEL CELL SEE THIS JCN WCE 001 JFS BATTERY DISCONNECTED FOR FUEL CELL SEE THIS JCN WCE 001 MAIN ACFT BATT DISCONNECTED FOR FUEL CELL MAINT JFS BATT DISCONNECTED FOR FUEL CELL MAINT NLG LOCK RETENTION ACT CANN'D TO A4127 (JCN 143389615) REMOVAL OF ITEM FOR CANNIBALIZATION INSTALL AFTER CANNIBALIZATION CENTER WING FUEL TANK REQUIRES FUEL LEAK EVALUATION CTW CAVITY DRAIN LINES 4,5,6,COMMON REMOVED FOR FUEL LEAK EV AL 8HR LEAK CK DUE ON CTW CAVITY DRAIN LINES 4,5,6,COMMON AFTER REFUEL #6 CTW CELL LEAKING REQUIRES FURTHER TROUBLESHOOTING CENTER WING ACCESS DOOR W-45 REMOVE TO F.O.M CENTER WING ACCESS DOOR W-52 REMOVE TO F.O.M CTW CELL #4 ACCESS DOOR REMOVED TO FOM 8EA INTERCONNECTS IN #4 CTW CELL HAVE BOLTS REMOVED TO FOM 8EA INTERCONNECTS IN #5 CTW CELL HAVE BOLTS REMOVED TO FOM ALL PLUMBING AND ASSOCIATED HARDWARE REMOVED FROM #6 CTW CEL L TO FOM #6 CTW CELL REMOVED TO FOM #4 CTW CELL HAS 8EA PRESSURE PLATES AND ASSOCIATED HARDWARE INSTALLED FOR HORSHOW PRESSURIZATION #5 CTW CELL HAS 8EA PRESSURE PLATES AND ASSOCIATED HARDWARE INSTALLED FOR HORSHOE PRESSURIZATION #6 CTW CELL HAS 10EA PRESSURE PLATES AND ASSOCIATED HARDWARE INSTALLED FOR HORSHOE PRESSURIZATION ALL REQUIRED PRESSURE EQUIPMENT INSTALLED IN LEFT AND RIGHT CTW FOR HORSESHOE PRESSURIZATION LK CK DUE ON CTW CELLS 4,5,6 8 HOURS AFTER REFUELN IAW 1C-13 5-2-5-3 LEAK CHECK DUE ON LEFT, RIGHT AND #4 CELL CENTER WING ACCESS DOOR AFTER REFUEL RC-135V, T/N 64-14848, 30 April 2015 U-106 RIGHT WING JACK PAD PANEL REMOVED TO FOM WC Event Narrative CTW #5 CELL ROLLED BACK FOR METALS TECH. CAVITY PREP REQUIRED ON #6 CENTER WING CAVITY PRIOR TO CELL INSTALLATION #6 CENTER WING CAVITY FLOOR PULLED BACK TO F.O.M CTW #4 CELL REQUIRES SAFTEY WIRE ON 8 EA INTERCONNECTS HELI-COIL REQUIRES R2 IN CTW #5 CELL ON LT UPPER VENT FLOW T HRU CTW #6 CELL CAVITY FLOOR BOARD REQUIRE REMOVAL TO FOM NUT PLATE REQUIRES R2 IN CTW CELL #6 BOTTOM RT FLOW THRU RT KEEL BEAM BAY DOOR OPENED TO FOM 2 EA WARNING TAGS INSTALLED 1 OF 2- BLEED AIR RECEP NOTE: DO NOT APPLY BLEED AIR 2 OF 2- THROTTLES NOTE: DO NOT ADVANCET H 4EA WARNING TAGS INSTALLED FOR FUEL CELL 1OF4 EXTERNAL PWR R ECP 2OF4 BATTPWR SWTCH 3OF4 MAIN BATT Q/D 4OF4 JFS BATT Q/D 4 EA WARNING TAGS INSTALLED 1/4 BATT PWR SWITCH 2/4 MAIN BAT T QD 3/4 JFS BATT QD 4/4 EXT PWR RECEP 1EA WARNING TAG INSTALLED TO FOM (SEE JCN 143386500) TAG1OF1 INSTALLED ON LT HYD SYS DP SW NOTE: DO NOT OPERATE IPI DUE UNDER CENTER WING ACCESS DOOR W-45 PRIOR TO TANK CLO SURE -6 INSPECTION DUE UNDER CENTER WING ACCESS DOOR W-45 PRIOR T IPI DUE UNDER CENTER WING TANK ACCESS DOOR W-52 PRIOR TO TAN K CLOSURE -6 INSPECTION DUE UNDER CENTER WING TNAK ACCESS DOOR W-52 PR IOR TO TANK CLOSURE IPI DUE UNDER #4 CTW CELL ACCESS DOOR PRIOR TO CLOSE IAW 1C- 135-2-5-3 -6 INSP DUE UNDER #4 CTW ACCESS DOOR PRIOR TO CLOSE IAW 1C-1 35-6 POSITION 23 FOOT SWITCH REQUIRES SCREW LEFT PAC OVER PRESSURE, ON FLOW CONTROLLER ABOVE LIMITS. CENTER WING ACCESS PANEL OPENED TO FOM IAW 1C-135-2-3-2 T-DUCT REMOVED TO FOM IAW 1C-135-2-3-2 FLEX BOOT CLAMP BROKE N REQ R2 SEE THIS JCN WCE 011 LH S-DUCT REMOVED TO FOM IAW 1C-135-2-3-2 AIRFLOW CONTROLLER REQUIRES R2 LEAK AND OPS CHECK DUE ON LH PACK IAW 1C-135-2-3-2 PG13-3 PA RA 13.2.4 SEE 5HIS JCN WCE 007 & 006 S-DUCT/FLOW CONTROLLER DUCTING NOT ALIGNED PROPERLY. DUCTING REQ REALIGNMENT LK AND OPS CK DUE ON LH PAC IAW 1C-135-2-3-2 SEE THIS JCN WC E 009 T-DUCT FLEX BOOT CLAMP BROKEN, REQ R2 SEE THIS JCN WCE 005 CO PILOT MAP LIGHT INOP FWD A/R PUMP PANEL REMOVED TO FOM SEE THIS JCN WCE 006 FWD BODY FUEL TANK PANEL REMOVED TO FOM SEE THIS JCN WCE 007 RC-135V, T/N 64-14848, 30 April 2015 U-107 FUEL NOT CONFIGURED FOR FLIGHT WC Event Narrative **REDBALL** COPILOT APC INOP 2 EA HYDRAULIC LINES, UNION, CHECK VALVE REMOVED FROM FWD BO DY FWD PUMP TO FOM HYDRO STATIC LEAK CHECK DUE ON THE FWD BODY FWD A/R PUMP IAW 1C-135-2-6-1 LK CK DUE ON FWD BODY FWD AR PUMP HYDRO LINES # 1 ENG COWLING OPEN TO FOM FRONT P UMP IN FORWARD BODY TANK SOUNDED ABNORMAL AND THERE WERE SLIGHT ABNORMAL VIBRATIONS IN THE FLIGHT DECK FLOOR FWD BDY FWD A/R PUMP REQUIRES R2 FWD BODY #3 ACCESS DOOR REMOVED TO FOM LK AND OPS CHECK DUE ON FWD BODY FWD A/R PUMP IAW 1C-135-2-6 -1 TEAPARTY QRC INSTALLED REQ'S REMOVAL AFTER FLIGHT STAMPEDING SEROW QRC INSTALLED REQ'S REMOVAL AFTER FLIGHT DRP SCREWS ARE STRIPPED THEY NEED TO BE REPLACED SUPPORT REQD FOR A/C LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY 1 EA WARNING TAG INSTALLED TO FOM 1 OF 1 LT HYD DP SWITCH NO HYDR MULE CONNECTED TO #1 ENG TO FOM ALL 4 ENGS DUE PRE ENG RUN I'S AND E'S INSP ALL 4 ENGS DUE POST ENG RUN I'S AND E'S INSP ALL 4 ENGS DUE PRE ENG RUN I'S AND E'S INSP ALL 4 ENGS DUE POST ENG RUN I'S AND E'S INSP 5EA WARNING TAGS INSTALLED (1 OF 5) EXT PWR (2 OF 5) FMP (3O F 5) SPR (4 OF 5) A/C BATT (5 OF 5) JFS LN 120 CB PULLED AND COLLARED 9 EA CIRCUIT BREAKERS PULLED AND COLLARED ON PNL P-14 IPI DUE ON #3 FWD BODY PRIOR TO TANK CLOSURE IAW 1C-135-2-5- 3 PARA 1.3.45 STEPS A-C -6 INSP DUE UNDER #3 FWD BODY ACCESS DOOR PRIOR TO CLOSURE I AW 1C-135-6 RC-135V, T/N 64-14848, 30 April 2015 U-108 1 EACH STRIPPED RIV NUT ON FORWARD BODY FORWARD AR PUMP RETU RN LINE NEAR T-FITTING. REP AS REQ WC Event Narrative LK CHK DUE ON #3 FWD BODY ACCESS DOOR AFTER REFUEL IAW 1C-13 5-2-5-3 LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 FUEL LEAKING FROM CENTER WING CAVITY DRAIN. REQUIRES EVALUAT ION 8HR LEAK CK DUE ON CTW AFTER REFUEL IAW 1C-135-2-5-3 CTR WING CAVITY DRAIN LINES 4, 5, 6, AND COMMON DISCONNECTED AND BAGGED 10 EA COVELIP DOORS LOWERED FOR HPO INSPECTION 10 EA COVELIP DOORS LOWERED FOR HPO INSPECTION STAB ACCESS PANEL REMOVED FOR HPO INSP DRAIN AND SERVICE LT ACM HPO INSP IN PROGRESS DRAIN AND SERVICE RT ACM HPO INSP IN PROGRESS RT KEEL BEAM BAY DOOR OPEN FOR HPO INSP JFS STARTER DRAINED AND RESERVICED FOR HPO INSPECTION AUDIBLE IGNITION OPS CHECK REQUIRED IC-135-6WC-1 & 1C-135-2-4-1 #1 ENG FAN COWL OPEN FOR HPO INSP #1 ENG FAN DUCT OPEN FOR HPO INSP #2 ENG FAN COWL OPEN FOR HPO INSP #2 ENG FAN DUCT OPEN FOR HPO INSP #3 ENG FAN COWL OPEN FOR HPO INSP #3 ENG FAN DUCT OPEN FOR HPO INSP #4 ENG FAN COWL OPEN FOR HPO INSP #4 ENG FAN DUCT OPEN FOR HPO INSP LT MLG STRUT DEFLATED FOR HPO INSPECTION RT MLG STRUT DEFLATED FOR HPO INSPECTION NLG STRUT DEFLATED FOR HPO INSPECTION COMPLY WITH 60 DAY HPO CARDS IAW 1C-135-6WC-1 COMPLY WITH 60 DAY HPO CARD IAW ETM-RC135-6WC-1 CARD 7-001 1OF1 WARN TAG INSTALLED ON FLAP HANDLE HPO INSP INPROGESS NOTE DO NOT OPERATE FLAPS 3EA WARNTAGS 1OF3 I/B CUTOUT SW,2OF3 O/B CUTOUT SW 3OF3 SPOILER HANDLE NOTE DO NOT OPERATE 8EA LEADING EDGE FLAP LOCKS INSTALLED FOR HPO INSPECTION 8EA SPOILER LOCKS INSTALLED FOR HPO INSPECTION ARR DOOR LOCK INSTALLED FOR HPO INSPECTION RC-135V, T/N 64-14848, 30 April 2015 U-109 LT KEEL BEAM BAY DOOR OPEN FOR HPO INSP WC Event Narrative STAB TRIM LOCK INSTALLED 3EA CIRCUIT BREAKER SAFETY LOCKS INSTALLED 2EA WARNTAGS 1OF2 STABTRIM CUTOUT SWITCH, 2OF2 FCS PWR SWITCH. NOTE DO NOT MOVE STAB TRIM LOCK INSTALLED FOR HPO INSPECTION 1EA C/B SAFETY LOCK INSTALLED ON JFS STARTER C/B HPO INSPECTION INPROGRESS 4EA C/B SAFETY LOCKS INSTALLED ON ENGINES 1-4 FIRE SUPPRESSION C/B ON P-100 PANEL 4EAWARN TAGS #1THANDLE,#2THANDLE,#3THANDLE,#4THAN DLE,ALL T-HANDLES PULLED. NOTE: DONT PUSH IN 4EA C/B SAFETY LOCKS INSTALLED 1-4 ENG FIRE SHUT- OFF C/B'S P-13 PANEL COMPLY WITH 60 DAY HPO CARD IAW ETM-RC135-6WC-1 CARD 6-001 55ISS COMPLY WITH 60 DAY HPO IAW ETM-RC135-6WC-1 CARD 4-001, 5-001 PILOT'S YOKE TRANSMIT BUTTON NEEDS PRESSED TWICE IN ORDER TO TRANSMIT OUT ON FD'S. **REDBALL** LN100 #1 INOP **REDBALL** LN-120 W/N TIE INTO FMS #1 ENG HAS SINGLE IGNITION.(LT SIDE NOT WORKING) #1 ENG DUE AUDIBLE IGNITION CK AFTER MAINTENANCE IAW 1C-135- 2-4-1-1 #1 ENG. LEFT SIDE IGNITION LEAD MISSING WHITE PLASTIC BUSHIN G AT 4:00 DENT ON LFT ELEVATOR BALANCE BAY PANEL REQ. SHEETMETAL EVAL A/C REQ'S SUPPORT FOR LAUNCH SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY FIRE SUPPRESSION 1-4 C/B SAFETY LOCKS INSTALLED FOR AUDIBLEI GNITION CHECK OUT. FUEL SHUT OFF VALVES 1-4 C/B SAFETY LOCKS INSTALLED FOR AUDI BLE IGNITION CHECK OUT. LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 S29105-3 WILL NOT RESET TO HCP 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 FUEL CELL 0 ACCESS PANEL REMOVED TO FOM IAW ETM-RC135-2-3 SE E WCE 001 RH PUZZLE BRACKET REMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 14 3280206 RC-135V, T/N 64-14848, 30 April 2015 U-110 55 ISS COMPLY WITH 60 DAY HPO IAW ETM RC135-6WC-1 CARD 4-001 AND 5-001 WC Event Narrative RH PRIMARY HEAT EXCHANGER COND AIR AND ENG BLEED AIR DUCTS R EMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 143280206 RH ACM LIMIT VALVE REMOVED TO FOM IAW 1C-135-2-3-1 SEE JCN 1 43280206 RH ACM LIMIT VALVE SENSING LINES REMOVED TO FOM IAW 1C-135-2 -3-1 SEE JCN 143280206 LEAK CHK AND OPS CHK DUE ON RH PACK IAW 1C-135-2-3-2 SEE TH IS JCN WCE'S002-004 RH KEEL BEAM BAY LOWERED TO FOM IAW 1C-135-2-3-2 SEE WCE 006 DRT RCVR TOP LEFT AND BOTTOM RIGHT SCREWS REQUIRE INSTALL 2EA WARNING TAGS INSTALLED 1OF2-BLEED AIR RECEP-NOTE:DO NOTA PPLY AIR 2OF2-TOW BAR CONNECTION-NOTE:DO NOT TOW SEE THIS TR#2 SHOWED FLUCTUATING VOLTAGE IN FLIGHT LOAD DROPPED TO ZE RO. LOAD DISTRIBUTION CB 50PLB POPPED DURING FLIGHT #2 MAIN TANK FWD BOOST PUMP,#3 MAIN TANK AFT BOOST PUMP, AND CENTER WING RIGHT OVERRIDE PUMP CBS POPPED DURING FLIGHT DC POWER AMMETER/ VOLTMETER KNOB FELL OFF DURING FLIGHT. PLA CED IN NAV DESK DRAWER 2 EA AFT A/R PUMP PANELS REMOVED FOR FUEL CELL #1 AFT BODY PANEL REMOVED FOR FUEL CELL RT KEEL BEAM DOOR OPENED FOR FUEL CELL MAIN AND JFS BATTERIES DISCONNECTED FOR FUEL CELL MAINT. 4 E A. WARNING TAGS INSTALLED SERIES YAW DAMPER WILL NOT ENGAGE #2 ENG COWLING OPENED TO FOM #1 ENG FAN COWL OPEN TO FOM #2 ENG FAN COWL OPEN TO FOM #3 ENG FAN COWL OPEN TO FOM #4 ENG FAN COWL OPEN TO FOM #1 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #2 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #3 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #4 ENG CHIP DETECTORS(4 EACH) REMOVED FOR INSP #1 ENG FUEL STRAINER REMOVED FOR INSP #2 ENG FUEL STRAINER REMOVED FOR INSP #3 ENG FUEL STRAINER REMOVED FOR INSP #4 ENG FUEL STRAINER REMOVED FOR INSP FUEL LEAK AFT OF MLG DOORS REQ EVAL 8 HR LEAK CHECK REQUIRE AT 1930 ON CWG TANK #3 COMMON, #4,5,AND 6 CAVITY DRAIN LINES DISCONNECTED TO FOM RC-135V, T/N 64-14848, 30 April 2015 U-111 Q- INLET HEAT INOP WC Event Narrative CTR WING #6 CELL LEAKING SEE JCN 143280108 CTR WING #4 CELL DOOR REMOVED TO FOM LT CTR WNG ACCESS DOOR W-45 REMOVED TO FOM RT CTR WNG ACCESS DOOR W-52 REMOVED TO FOM CTR WNG CELL #6 REMOVED LEAK CHECK DUE ON CTR WNG CELL #6 8 HOURS AFTER REFUEL IAW T O 1C-135-2-5-3 CAVITY PREP REQUIRED ON CTR WNG CELL #6 CAVITY PRIOR TO INST ALL CTR WNG CELL #6 PLUMBING AND ASS HARDWARE REMOVED TO FOM LK CK DUE ON CTR WNG CELL #4 ACCESS DOOR, W-45, AND W-52 IAW TO 1C-135-2-5-3 ES822 #5 WILL NOT RESET TO HCP SECONDARY STRUCTURE/PANEL INSPECTION DUE AFTER FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP AFTER ENGINE FUNCTION ACFT LAV REQ REQ DRAIN IMMEDIATELY UPON LANDING PER ETM-RC135-6WC-1 CARD 1-001 SECONDARY STRUCTURE/PANEL INSPECTION DUE PRIOR TO FLIGHT IAW OAFBI 21-100 PARA 7.2.1 ALL 4 ENGINES INLETS AND EXHAUST REQUIRE INSP FOD PRIOR TO NEXT ENGINE FUNCTION ACFT LAV REQ SERVICE AT CREW SHOW PER ETM-RC135-6WC-1 CARD 1-001 FUEL NOT CONFIGURED FOR FLIGHT 4 EA. WARNING TAGS INSTALLED FOR FUEL CELL MAINT. 1OF4 EXT P WR RECPT. 2OF4 BATT PWR SWTCH 3OF4 MAIN BATT QD 4OF4 JFS BAT T TEMS OR FDR REQUIRES DOWNLOADS F108 ENGINES ONLY HYD MULE HT03 CONNECTED TO #2 ENG FOR DEFUEL 120 HOUR INSPECTION DUE FOR F108 ENGINES IAW 1C-135-6 ENG'S 1,2,3,4 T-HANDLES PULLED ENG STARTER C/B'S P ULLED FIRE SPRSN C/B'S PULLED FIRE SHUTOFF PULLED 4 EACH WARNING TAGS INSTALLED ON #1 ENG STARTER C/ B,FIRE SPRN C/B,T-HANDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #2 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #3 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 4 EACH WARNING TAGS INSTALLED ON: #4 ENG STARTER C /B,FIRE SPRN C/B,T-HNDLE,FIRE SHUTOFF C/B 2 EACH WARNING TAGS INSTALLED ON: ACFT BATT SWITCH AND EXTERNAL POWER RECEPTACLE INSP ALL 4 ENG TRANS GEARBOXES FOR LEAKS,LOOSE OR ALL FOUR ENG STARTERS DUE OIL CHECK IAW 1C-135(K)R -2-4JG-6 TASK 6-29-1 PG 6-136 INSPECT ALL FOUR ENG CHIP DETECTORS 1AW IAW 1C-135-6 PG S-A-031 STEP 22 ITEM C INSP DIFFERENTIAL OIL PRESSURE INDICATOR(DPI) FOR POPPED INDICATION. ON#1,2,4 IDG'S IAW 1C-135-6 RC-135V, T/N 64-14848, 30 April 2015 U-112 AWG 7122C HARD DRIVE CHASSIS IS INSTALLED UPSIDE DOWN WC Event Narrative INSP ALL 4 MAIN FUEL STRAINER FOR TOP-COAT C ONTAMINATION IAW 1C-135-6 PG 2-A-032 UTEN 30STEP A ALL 4 ENG DUE IDLE RUN LEAK CHECK ON OIL AND FUEL SYSTEMS IAW 1C-135(K)R-2-4JG-5 TASK 5-12-1 PG.5-28 INLETS AND EXHAUSTS INSP DUE PRIOR TO ENG RUN INLETS AND EXHAUSTS INSP DUE POST TO ENG RUN C/W 60 HR INSP IDG DIFFERENTIAL OIL PRESSURE INDICATOR FOR POPPED INDICATION C/W 60 HR CHECK IDG DIFFERENTIAL OIL LEVEL PER 2-2 SERIES TO 5 EA WARNING TAGS INSTALLED 1OF5 SPR, 2OF5 EXT POWER, 3OF5 F MP, 4OF5 A/C BATT, 5OF5 JFS BATT NOTE DO NOT REFUEL/DEFUEL,A PP 8 EA CIRCUIT BREAKERS PULLED ON PANEL P140 NOTE DO NOT RESET CIRCUIT BREAKERS 1 EA CIRCUIT BREAKER PULLED ON LN120 BATT NOTE DO NOT RESET CIRCUIT BREAKER IPI DUE ON CTR WNG CELLS #4, #5, AND #6 PRIOR TO CLOSE IPI DUE UNDER LT CTR WNG ACCESS DOOR W-45 PRIOR TO CLOSE -6 INSP DUE UNDER LT CTR WNG ACCESS DOOR PRIOR TO CLOSE IPI DUE UNDER RT CTR WNG ACCESS DOOR W-52 PRIOR TO CLOSE -6 INSP DUE UNDER RT CTR WNG ACCESS DOOR W-52 PRIOR TO CLOSE -6 INSP DUE UNDER LT CTR WNG ACCESS DOOR W-45 PRIOR TO CLOSE LGNJ PERFORM POST FLIGHT INSPECTION PER ETM-RC135- 6WC-1 CARD 1-001 28 DAY FMS UPDATE C/W MICROWAVE INOP REQ REPLACEMENT AFTER FLIGHT SUPPORT REQUIRED FOR A/C LAUNCH NABRE CONFIGURED FOR FIRE BAT SECONDARY SUPERVISORY MODULE W/N BOOT HSDC A SHOWS NO VIDEO # 2 ENG COWLING OPEN TO FOM # 2 ENG LOW OIL PRESSURE SWITCH CANNED TO A4132 # 2 ENG REMOVAL OF ITEM FOR CANNIBALIZATION INSTALL AFTER CANNIBALIZATION CLASS A F/L ON RT JACK PAD RE-EVALUATE RT JACKPAD FUEL LEAK CLASS "A" F/L AFT OF JACKPAD. FLYABLE CONDITION RT JACKPAD PANEL REMOVED TO FOM LEAK CHECK DUE ON RIGHT AFT JACK PAD TWO HOURS AFTER REFUELI AW 1C-135-2-5-3 RC-135V, T/N 64-14848, 30 April 2015 U-113 -6 INSP DUE ON CTR WNG CELL #4, #5, AND #6 PRIOR TO CLOSE WC Event Narrative REMOVAL OF ITEM FOR CANNIBALIZATION INSTALL AFTER CANNIBALIZATION PERFORM WASTE SYS SANITIZING FOR THE ACFT WASTE TA & LAV SVC CART IAW ETM-RC135V/W-2. # 2 ENG LOW OIL PRESS SWITCH REQUIRES LEAK AN OPS CHECK I'S AND E'S INSP REQUIRED PRIOR TO ENG RUN I'S AND E'S INSP REQUIRED AFTER ENGINE RUN 1 EA WARNING TAG INSTALLED ON OIL PRESS WARN. C/B TAG 1 0F 1 ENG OIL PRESS WARN C/B NOTE: DO NOT RESET IRIDIUM REQUIRES OP CHECK DUE TO R2/REGISTRATION OF TRANSCEI VER 7 DAY LCS INSPECTION DUE IAW ETM-RC135-6 REMOVAL OF ITEM FOR CANNIBALIZATION PANEL ASSEMBLY REQ INSTALL AFTER CANNIBALIZATION #5 C/L/D LATCH REM TO SHEET METAL FOR PRIMER THIS IS THE INSTALLATION WCE CREATED BY JCN 143180090001 # 5 MOST INBOARD COVE LIP DOOR REQS. R2 #4 C/L/D LOWERED TO FOM SEE THIS JCN WCE 001 #5 C/L/D REM FOR SHEET METAL WORK THIS IS THE INSTALLATION WCE CREATED BY JCN 143170183009 #5 COVE LIP DOOR REQ REMOVAL FOR SHEET METAL #5 COVE LIP DOOR REQ INSTALL MOHAIR REQ BETWEEN #4 AND #5 COVE LIP DOORS 2 EA SPOILER LOCKS INSTALLED ON #3 & #4 SPOILER ACTUATORS TO FOM SEE THIS JCN WCE 001 2 EA WARNING TAGS INST 1 OF 2 SPIL ER RC-135V, T/N 64-14848, 30 April 2015 U-114 FUEL CELL ZERO PANEL OPENED FOR INSPECTION MDS PWC WUC AT HMAL POSTFLIGHT C/W HLGNJ 04199 28 DAY FMS UPDATE C/W A83CN 727AB L 944 URINAL UNCLOGGED. OPS CK GOOD A83FL 12GA0 V 301 CND IAW 00-20-1 PG 5-10 PARA 5.7.3.19.6 OPS CHECK GOOD IAW 1 A83HY 14AL0 X 799 COMBINE SPOILER SPEED BRAKE CHECKOUT C/W NO DEFECT NOTED A83JE 14AL0 X 799 DUPLICATE WRITE UP IAW TO 00-20-1 PARA 5.7.3.19.4.1 HLGNJ 82SCA X 799 RESEATED CHANNEL 5 SLICE O/C/G HLGNJ 82AFQ L 956 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-175 STEPS 1-5 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PARA 4.1.1 STEPS X THROUGH AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) C/W NDN A83EE 41799 X 799 R2 TRUCK LEVEL SWITCH IAW 1C-135-2-7-1 PARA 6.35.3 OPS CHECK DUE A83EE 13EAE R 255 JOB CORRECTED IN RELATION TO JCN 151180307 WCE 001 A83EE 13EBB X 799 R2 RH TRUCK LEVEL SW IAW 1C-135-2-7-1 PARA 6.35.2 OPS CHK DU E SEE THIS JCN WCE 006 A83EE 13EAE R 255 OPS CHK GOOD NDN. FOR IPI SEE THIS JCN WCE 005 A83EE 13EAE X 799 JOB RELATED TO JCN 151180307 WCE 001 A83EE 13EAE X 799 GEAR SWING OPS CHK GOOD IAW 1C-135-2-7-1 PARA 6.4.1.5 FOR IP I SEE THIS JCN WCE 005 A83HY 13A00 X 799 CLOSED COWLING IAW 1C-135-2-2-2 PARA 20.3.2 A83HY 118D0 S 800 REINSTALLED 4EA PANELS IAW 1C-135-2-2CL-3-1 PG5-6 PARA 5.4 A83JE 11310 S 800 DUPLICATE WRITE UP IAW T.O. 00-20-1 PARA 5.7.3.19.4.1 HLGNJ 823AC X 799 COLD STARTED HCP O/C/G HLGNJ 823AC X 799 A83EE 04199 (Null) INSP C/W IAW OAFBI 21-100 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) IPI C/W BY IAW 1C-135-2-7-1 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-115 C/A MDS PWC WUC AT HMAL INSP C/W IAW 1C-135-2-4CL-1-1 PG 4-2 + 4-3 PARA 4.1.1 STEPS X THROUGH AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) HYD MULE DISCONNECTED IAW 1C-135-2-2-2 PG 14-163 PARA 14.38.2 STEP D A83HY 01000 (Null) 1EA ACFT DOWBJACKED IAW 1C-135-2-2CL-3-1 PG 5-6 PARA 5.4 A83JE 01000 (Null) 5EA JACK PADS AND 1EA BOB REMOVED IAW 1C-135-2-2CL-3-1 PG 5-6 PARA 5.4 A83JE 01000 (Null) LANDING GEAR HANLDE IN D/L POSITION IAW 1C-135-2-2-2 PG1-60 PARA 1-10 STEP I A83JE 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) FOUND AND REPAIRED BROKEN WIRE ON MANIFOLD REFUEL VALVE LIMI T SW IAW 1-1A-14 SECT 014 PG 12 PARA 16 A83EE 46717 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 4-2 THROUGH 4-3 PARA 4.1.1 STEPS X THROUGH AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOADED C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) PERFORMED # 4 ENG PLA GAIN CHECK PMC ON/OFF CHECK AND HYDROM ECHANICAL CHECKS OPS CHECK GOOD NDN A83JE 27H99 X 799 # 4 ENG COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-5 PARA 20.3.2 A83JE 118D0 S 800 PLA TESTER REMOVED IAW 2J-F108-2-1 SEC 73-21-30 PG 501 STEP 9 A83JE 04199 (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PARA 4.1.1 STEPS X-AF A83JE 0413C (Null) I'S AND E'S INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83JE 0413C (Null) R2 AIRFLOW CONTROLLER LEAK AND OPS CHECK GOOD SEE THIS JCN W CE 004 FOR MX A83EE 41216 R 255 CLOSED CENTER WING ACCESS DOOR IAW 1C-135-2-3-2 PG 13-76 PAR A 13.14.68 STEP 14 A83EE 11PAD S 800 CLOSED DOOR IAW 1C-135-2-3-2 PARA 13.2.7 STEP C A83EE 11430 S 800 R2 AIRFLOW CONTROLLER IAW 1C-135-2-3-2 PARA 13.14.4 LEAK AND OPS CHECK GOOD A83EE 41216 R 255 REINSTALLED S-DUCT IAW 1C-135-2-3-2 PARA 13.14.54 LEAK CHECK GOOD A83EE 411DA S 800 T-DUCT INSTALLED A83EE 4125M S 800 REMOVED 2EA WARNING TAGS IAW LPS-55MXG-00-20-1 OFC3 PG 2 PARA 5.7.3.16.5.1.3.10 A83EE 01490 APPLIED WAX STRING TO RELIEVE TENSION OFF J1C RIU MOUNT BUND LE SEE THIS JCN WCE 002 FOR IFOC A83CN 72200 L 692 IFOC GOOD PER AIRCREW A83CN 722C0 X 799 R2 LANDING LIGHT OPS CHK GOOD IAW 1C-135-2-10-1 PARA 19.11.4 A83EE 44263 R 80 G 70 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-116 C/A MDS PWC WUC AT HMAL REINSTALLED PANEL IAW 1C-135-2-10-1 PARA 19.11.4 A83EE 44263 S 800 DISCREPANCY ENTERED ERROR IAW TO 00-20-1 PARA 4.6.5 HLGNJ 823AC X 799 RESEATED CABLE O/C/G HLGNJ 82CAA L 956 RESEATED RX ANT CABLE O/C/G HLGNJ 82LD0 L 255 INSP CW IAW OAFBI 21-100 PARA 7.2.1. A83FL 04199 (Null) INSP CW IAW 1C-135-2-4CL-1 PG42-43 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) ANTENNA MOUNT NOT CRACKED; PROPERLY SECURED A83FL 11000 X 799 REINSTALLED MOUNT IAW ETM-RC-135-2-11 PARA 1.6.32 A83FL 11BAW S 800 #1 ENG COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 P ARA 20.3 A83JE 118D0 S 800 #2 ENG COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 P ARA 20.3 A83JE 118D0 S 800 #3 ENG COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 P A83JE 118D0 S 800 #4 ENG COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 P ARA 20.3 A83JE 118D0 S 800 #1 ENG CHIP DETECTOR (4EA) INSTALLED IAW 1C-135-2-4-1-1 PG 7 -11 PARA 7.6 A83JE 27A4D S 800 #2 ENG CHIP DETECTOR (4EA) INSTALLED IAW 1C-135-2-4-1-1 PG 7 -11 PARA 7.6 A83JE 27A4D S 800 #3 ENG CHIP DETECTOR (4EA) INSTALLED IAW 1C-135-2-4-1-1 PG 7 -11 PARA 7.6 A83JE 27A4D S 800 #4 ENG CHIP DETECTOR (4EA) INSTALLED IAW 1C-135-2-4-1-1 PG 7 -11 PARA 7.6 A83JE 27A4D S 800 #1 ENG FUEL STRAINER INSTALLED IAW 1C-135-2-4-1-1 PG 6-18 PA RA 6.9.2 A83JE 27H99 S 800 #2 ENG FUEL STRAINER INSTALLED IAW 1C-135-2-4-1-1 PG 6-18 PA RA 6.9.2 A83JE 27H99 S 800 #3 ENG FUEL STRAINER INSTALLED IAW 1C-135-2-4-1-1 PG 6-18 PA RA 6.9.2 A83JE 27H99 S 800 #4 ENG FUEL STRAINER INSTALLED IAW 1C-135-2-4-1-1 PG 6-18 PA RA 6.9.2 A83JE 27H99 S 800 INSTALLED ANTENNA IAW ETM-RC135V/W-2 VOL II PG 1-136 PARA 1. 6.3.8 HLGNJ 81CBM S 800 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-117 C/A MDS PWC WUC AT HMAL INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) SEALANT CURED A83FL 01000 (Null) FDR DOWNLOADED C/W A83GC 04199 (Null) INSP C/W NDN A83JE 04199 (Null) ENG 1,2,3,4 THNDLE, STRTR C/B, FIRE SPRSN C/B ANDFIRESHUTOFF C/B RESET IAW 1C-135-2-4-1-1 PG 6-18 PARA A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED IAW IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED IAW IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 A83JE 06000 (Null) 2 EA WARNING TAGS REMOVED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 A83JE 06000 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C.W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PARA 4.1.1 STEPS Y-AF A83JE 0413C (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83JE 0413C (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) USED 205 TEST SET TO PURGE PRESSURE LINES. NO WATER FOUND IN DRAIN LINES. SYS OPS CHK GOOD. A83CN 72MAA X 799 IFOC GOOD PER AIRCREW A83CN 72BAB X 799 R2 FCD O/C/G HLGNJ 81NCP R 308 O/C/G W MAINT LOAD HLGNJ 81NWA X 799 INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-118 C/A MDS PWC WUC AT HMAL INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C.W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) R2 TCAS PROCESSOR IAW ETM-RC135-2-11 PG 2-206 PARA 2.42.2 SY STEM OPS CHK BAD. SEE THIS JCN WCE 002 FOR NE A83CN 73AA0 R 644 R2 TCAS PROCESSOR IAW ETM-RC135-2-11 PG 2-206 PARA 2.42.2 SY STEM OPS CHK BAD. SEE THIS JCN WCE 003 FOR NE A83CN 73AA0 R 644 R2 INU IAW ETM-RC135-2-11 PAG 5-154 PARA 5.13.4 SYS OP CK GO OD A83CN 727BA R 943 R2 RADAR RT IAW ETM-RC135-2-11 PG 2-55 PARA 2.6.15 SYSTEM OP S CHK GOOD. SEE JCN 151110030 WCE 001 FOR IFOCA83CN 72BAB R 644 7 LVL INSPECTION C/W IAW ETM-RC135-2-11 PG 2-45 PARA 2.4.4A S/O/C/G A83CN 72B00 X 799 7 DAY LCS INSP C/W NDN A83EE 41000 X 799 FUEL TUBE DRAINED IAW 1C-135-2-2-2 PG 15-314 PARA 15.25 A83FL 46738 X 799 REMOVED AND REPLACED 28VDC TR/POWER SUPPLY. SYSTEM OP CHECK S GOOD.. IAW ETM 420-21800-01 PG 5-39 PARA ARCEC 81ZAJ R 255 REMOVED AND REPLACED 28VDC POWER SUPPLY/TR. SYSTEM OPS CHEC K GOOD IAW ETM 420-21800-01 PG 5-39 PARA 5 ARCEC 81ZAJ R 255 R2 SPARE FCD HLGNJ 82CBB R 901 COLD START HCP O/C/G HLGNJ 82AB0 L 254 RESCRIPTED DSS LAN SWITCH O/C/G HLGNJ 82QAB L 254 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP CW IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 4-1 PARA 4.1 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) REMOVED AND REINSTALLED DEHYDRATOR FOR SILICA REPLACEMENT IA W ETM-RC135-2-11 PG 2-258 PARA 2.54.13 NDNA83CN 72MAD G 307 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) ISNP C/W IAW 1C-135-2-4CL-1-1 PG 4-2/4-3 STEP X-AF A83FL 04199 (Null) R2 RADAR ANTENNA IAW ETM-RC135-2-11 PG 2-48 PARA 2.6.2 SYS O P CK REQUIRED SEE THIS JCN WCE 008 A83CN 72BAD R 692 7 LVL INSP C/W A83CN 72BA0 X 799 RADOME ACCESS PANEL REINSTALLED IAW ETM-RC135-2-11 PG 2-59 P ARA 2.6.27 STEP I A83CN 11AAD S 800 RC-135V, T/N 64-14848, 30 April 2015 U-119 C/A MDS PWC R2 RIU IAW ETM-RC135-2-11 PG 5-62B PARA 2.6.37 SYS OPS CHK G OOD ON GROUND SEE THIS JCN WCE 001 FOR ORIGINA83CN WUC AT HMAL 72BAN R 644 REINSTALLED NOSE RADOME IAW ETM-RC135-2-11 PG 2-59 PARA 2.6. 27 A83CN 1111J S 800 NOSE RADOME ACCESS PANEL REINSTALLED IAW ETM-RC135-2-11 PG 2 -59 PARA 2.6.27 STEP I A83CN 11666 S 800 RADAR SYS OP CHK GOOD A83CN 72BL0 X 799 IFOC BAD PER AIRCREW -1 SEE JCN 151100193 FOR NEW DISCREPANC Y A83CN 72BA0 X 553 RESET TCAS PROCESSOR SYS OPS CHECK GOOD IAW ETM-RC135-2-11 P G 2-193 PARA 2.40.2 A83CN 73BA0 L 254 R2 RADAR PRESSURE SWITCH IAW ETM-RC135-2-11 PG 2-255 PARA 2. 54.4 OPS CHK BAD SEE THIS JCN WCE 002 A83CN 72MAB R 901 R2 RADAR PRESSURE PUMP IAW ETM-RC135-2-11 PG 2-254 PARA 2.54 .2 SYS OP CHK GOOD ON GROUND. SEE JCN 151060A83CN 72MAA R 692 CLOSED IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83FL 118D0 S 800 RELOCATED J1 CANNON PLUG IAW TAR #8-82700C/15A-0020 AND IAW 1-1A-14 WP 023 PG 7 PARA 40 SYSTEM OPS CHECKA83GC 52AAL L 6 RELOCATED J2 CANNON PLUG IAW TAR #8-82700C/15A-0020 AND IAW 1-1A-14 WP 023 PG 7 PARA 40 SYSTEM OPS CHECKA83GC 52AAL L 6 REINSTALLED AP PROCESSOR IAW 1C-135-2-11-3 PG 2-126 PARA 2-1 63 OPS CHECK DUE SEE THIS JCN WCE 004 A83GC 52AA0 S 800 A/P SYSTEM OPS CHECK GOOD A83GC 52AA0 X 799 FWD GAP ANTENNA INSTALLED IAW ETM-RC135V/W-2 PARA 4.1.6.12 HLGNJ 81CCE Q 799 5 EA WARNING TAGS REMOVED IAW LPS-55MXG-00-20-1 OFC3 STEP 5.7.3.16.5.1.3.10 A83CN 01490 (Null) INSP C/W OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) INSP C/W IAW OAFBI PARA 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) R2 RADAR R/T IAW ETM-RC135-2-11 PG 2-55 PARA 2.6.15. SYS OPS CHECK GOOD. SEE JCN 151066407 FOR RELATED DISCA83CN 72BAB R 692 NUTPLATE DOES NOT REQUIRE REPLACEMENT, ADJUSTED NUTPLATE. SC REW REINSTALLED. A83CN 72BAF G 105 LH PACK RAN GOOD ON GROUND RECALIBRATED PANEL IFOC DUE SEE T HIS JCN WCE 002 A83EE 413AA L 127 IFOC GOOD PER AIRCREW A83EE 41210 X 799 RESEAT CRYPTO CONNECTION ON MIDS TERMINAL O/C/G HLGNJ 82LGA L 6 RC-135V, T/N 64-14848, 30 April 2015 U-120 C/A MDS PWC WUC AT HMAL INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) INSP C/W A83FL 04199 (Null) R2 NAV'S RADAR MONITOR DISPLAY IAW ETM-RC135-2-11 PG 2-52 PA RA 2.6.5B SYS OPS CHK GOOD. A83CN 72BAF R 957 REINSTALLED ORIGINAL NAV MONITOR AFTER ETR IAW ETM-RC135-2-1 1 PG 2-52 PARA 2.6.5B SEE JCN 151036411 A83CN 72BAP S 800 RADAR OPS CHK STILL BAD AFTER ETR SEE JCN 151030133 FOR ORIG INAL DISCREPANCY A83CN 72BAP X 553 7 DAY LCS INSPECTION C/W NDN A83EE 41799 X 799 REPLACED 2 EA BROKEN FITTINGS A83FL 12G00 R 70 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 4-2/4-2 STEP X-AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) TQS MOUNT TCTO COMPLIED W/ IAW 1RC/TC135-1180 HLGNJ 04199 (Null) REMOVED AND REPLACED RADAR RT IAW ETM-RC135-2-11 PG 2-55 PAR A 2.6.15 SYSTEM OPS CHK GOOD A83CN 72BAB R 691 DUST COVER REINSTALLED IAW 1C-135-2-7-1 PARA. 9.14 PG 9-91 I PI C/W IAW STEP 27 BY A83FL 13AMD S 800 TRANSDUCER REINSTALLED IAW 1C-135-2-7-1 PARA. 9.12 IPI C/W I AW 1C-135-2-7-1 PARA. 9.12 STEPS 2-4 AND LPS-55MXA83FL 13EBE S 800 OPS CK GOOD A83FL 13EB0 X 799 #1 TIRE R2 IAW 1C-135-2-7-1 PG. 57-6-63 PARA. 6.13.2 IPI C/W IAW 1C-135-2-7-1 PARA. 16.3.2 STEPS 2&3 PARA. 16.3.3 SA83FL 13AM0 R 20 RESEATED CANNON PLUGS OPS CHECK GOOD A83GC 51P00 L 255 R2 FILLER CAP SEAL OPS CHK GOOD A83HY 45124 G 381 R2 OWS HLGNJ 82GAA R 255 RC-135V, T/N 64-14848, 30 April 2015 U-121 C/A MDS PWC WUC AT HMAL A/C LAUNCH SUPPORTED A83CN 01000 (Null) INSP C/W OAFBI 21-100 PARA. 7.2.1 A83FL 04199 (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED BY MAN #86425 A83FL 01000 (Null) FDR DL C/W A83GC 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83JE 0413C (Null) AXLE DOWNJACKED IAW 1C-135-2-2-2 PG 21-59 PARA. 21.16.3 A83JE 01000 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) IFOC GOOD C/W BY MATT DOWNING 232-1246 A83FL 51QAA MODE 4 CK C/W SYS OP CK GOOD A83CN 04MD4 (Null) OPS CHECK GOOD A83EE 04MD4 (Null) INSP C/W A83FL 01000 (Null) UPLOAD C/W A83FL 01000 (Null) WRITEUP ENTERED IN ERROR NO DISCREP EXISTS IAW 00-20-1 4-4 PA 4.6.6.2 A83JE 01000 (Null) WRITEUP ENTERED IN ERROR NO DISCREP EXISTS IAW 00-20-1 4-3 PA 4.6.6.1 A83JE 01000 (Null) AFE UPLOAD C/W ARCEC 01000 (Null) FL 15 C/W HLGNJ 01000 (Null) R2 R/T. IAW ETM-RC135-2-11 PG 2-172 PARA 2.36.2 OPS CHK BAD SEE THIS JCE WCE 002 FOR NEW DISCREPANCY A83CN 72VA0 R 37 R2 RADIO ALT #2 IAW ETM-RC135-2-11 PG 2-172 PARA 2.36.2 OPS CHK BAD SEE THIS JCE WCE 004 FOR NEW DISCREPANA83CN 72VA0 R 673 CLOSED FUEL CELL #1 ACCESS PANEL IAW ETM-RC135-2-11 PG 2-172 PARA 2.36.2 STEP H A83CN 1151E S 800 R2 RADIO ALT #2 R/T IAW ETM-RC135-2-11 PG 2-172 PARA 2.36.2 OPS CHK GOOD SEE JCN 150980029 WCE 001 FOR IFOCA83CN 72VA0 R 673 MODE IV/MODE C CHECK C/W, SYS OPS CHK GOOD A83CN 04MD4 (Null) DR C/W A83FL 07000 (Null) REPAIRED COMM CORD, OPS CHK GOOD A83CN 647Q0 G 105 R2 LIGHT BULB OPS CHECK GOOD A83FL 44213 S 800 NDN HANDLE WORKS AS REQ. A83FL 11340 X 799 RESET APCS RAN WS PTT MBIT OPS CHECK GOOD A83GC 51SAA X 799 REPLACED SPARE KEYBOARD HLGNJ 82GAJ R 718 O/C/G W/ MX LOAD HLGNJ 823AC X 799 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 X 799 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-122 C/A MDS PWC WUC AT HMAL INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) IFOC CHECKED GOOD PER AIRCREW A83CN 72BA0 X 799 INSPECTION C/W NDN A83EE 41000 X 799 28 DAY TAWS UPDATE C/W A83GC 51Q00 L 944 PERFORMED RADAR OPS CHECK IAW ETM-RC135-2-11 PG 2-45 PARA 2. 4.41 FOR ONE HOUR. NDN, SYS OP CHK GOOD A83CN 72BA0 X 799 SYSTEM WORKS AS ADVERTISED, RA NOT TO BE USED ABOVE 2,500FT PER ETM-RC135-2-11 PG 2-157 PARA 2.31. A83CN 72V00 X 948 7 LEVEL INSPECTION FOR RECUR C/W A83CN 51Q00 X 799 C/S HCP O/C/G W/ MX LOAD HLGNJ 823AC X 799 C/S HCP O/C/G W/ MX LOAD HLGNJ 823AC X 799 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STPS 31 THRU 38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) R2 FLOW CONTROLLER IAW 1C-135-2-3-2 PARA 13.14.4 LEAK AND OP S CHK GOOD SEE THIS JCN WCE 004 A83EE 41216 R 255 CLOSED CENTER WING ACCESS DOOR IAW 1C-135-2-3-2 PARA 13.14.5 4 PG 13-70 A83EE 11PAD S 800 CLOSED LH K/B/B IAW 1C-135-2-3-2 PARA 13.2.7 STEP C A83EE 11430 S 800 R2 AIRFLOW CONTROLLER IAW 1C-135-2-3-2 PARA 13.14.4 LEAK AND OPS CHK GOOD A83EE 41216 R 255 REINSTALLED S-DUCT IAW 1C-135-2-3-2 PARA 13.14.54 LEAK CHK G OOD A83EE 411DA S 800 T-DUCT REINSTALLED IAW 1C-135-2-3-2 PG 13-73 PARA 13.14.60 A83EE 4125M S 800 CLEANED WINDOW A83FL 1114E V 230 URINAL SNAKED OPS CHECK GOOD A83FL 12GA0 V 230 RC-135V, T/N 64-14848, 30 April 2015 U-123 C/A MDS PWC WUC AT HMAL COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-5 PARA 20. 3.2 A83JE 118D0 S 800 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-5 PARA 20. 3.2 A83JE 118D0 S 800 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-5 PARA 20. 3.2 A83JE 118D0 S 800 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-5 PARA 20. 3.2 A83JE 118D0 S 800 4 EA CHIP DET INST IAW 2J-F108-2-1 S 79-00-00 PG 201 A83JE 27A4D S 800 4 EA CHIP DET INST IAW 2J-F108-2-1 S 79-00-00 PG 201 A83JE 27A4D S 800 4 EA CHIP DET INST IAW 2J-F108-2-1 S 79-00-00 PG 201 A83JE 27A4D S 800 4 EA CHIP DET INST IAW 2J-F108-2-1 S 79-00-00 PG 201 A83JE 27A4D S 800 C/S HCP O/C/G W/ MX LOAD HLGNJ 823AC X 799 SUPPORTED A/C LAUNCH A83CN 01000 (Null) REMOVED 2EA WARNING TAGS IAW LPS-55MXG-00-20-1 OFC3 PG 2 PARA 5.7.3.16.5.1.3.10 A83EE 01490 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) C/W IAW 1C-135-2-4CL-1-1 PGS 4-2 THRU 4-3 STEPS X/AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) INSP C/W A83JE 04199 (Null) 4EA WARNING TAGS REMOVED C/B RESET IAW 1C-135-2-4-1-1 PG 8-67 PARA 8.25.2 A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) I'S AND E'S C/W IAW 1C-135-2-4CL-1-1 PG 4-2 THRU 3 STEPS X-AF A83JE 0413C (Null) I'S AND E'S C/W IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83JE 0413C (Null) INSP C/W A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) SWAPPED RAD ALT #1 AND #2 IAW ETM-RC135-2-11 PG 2-172 PARA 2 .36.2 A83CN 72VA0 S 800 RC-135V, T/N 64-14848, 30 April 2015 U-124 C/A MDS PWC WUC AT HMAL C/W IAW 1C-135-2-4CL-1-1 PG4-2 THRU 4-3 STEPS X-AF A83FL 0413C (Null) C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) R2 ADL IAW ETM-RC135-2-11 PG 5-105 PARA 5.7.1.1, SYS OPS CHK GOOD. A83CN 72XJ0 R 939 RESEATED RADIO ALT. SEE JCN 150910025 A83GC 51Q00 L 956 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) 28D FMS UPDATE C/W A83CN 727AB L 944 INSP C/W NO DEFECT NOTED A83EE 41799 X 799 CLOSED FUEL CELL 0 ACCESS PANEL IAW 1-1A-8 PARA 10.2 A83EE 41799 S 800 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 PG 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-CL-1-1 PG 4-2 THRU 4-3 STEPS X-AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-125 C/A MDS PWC WUC AT HMAL INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) 1 EA FIRST AID KIT IN FLIGHT DECK REPLACED A83FL 91211 R 70 HDP CALL TEST C/W HLGNJ 82EA3 X 799 C/S HCP O/C/G W/ MX LOAD HLGNJ 823AC X 799 C/S HCP O/C/G W/ MX LOAD HLGNJ 823AC X 799 C/S HCP O/C/G W/ MX LOAD HLGNJ 823AC X 799 C/S HCP O/C/G W/ MX LOAD HLGNJ 823AC X 799 C/S HCP O/C/G W/ MX LOAD HLGNJ 823AC X 799 O/C/G WITH MX LOAD HLGNJ 82SC0 X 799 O/C/G WITH MX LOAD HLGNJ 823AC X 799 R2 HDP O/C/G HLGNJ 82EA3 R 949 DUPLICATE DISCREPANCY IAW 00-20-1 PARA 5.7.3.19.4.1 HLGNJ 82CAB X 799 R2 HSDC O/C/G HLGNJ 82QAC R 956 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1 PG 4-2 AND 4-3 STEPS X THRU AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-126 C/A MDS PWC WUC AT HMAL INSPECTION C/W NDN A83EE 41000 X 799 REINSTALLED PNL IAW ETM-RC135-2-3 P.7-141 PARA 7.1.6.12 STEP M A83EE 11PAD S 800 TORQUE TUBE BRACKET R2 A83FL 14ECG R 70 3 EA PATCHES INSTALLED A83FL 14EJ0 G 105 #4 OUTBOARD FLAP MOHAIR REPLACED A83FL 14EG0 G 105 HPO CARDS C/W A83FL 03300 (Null) CARD C/W A83FL 03300 (Null) CARDS COMPLIED WITH. NO DEFECTS NOTED ARCEC 03300 (Null) HPO C/W HLGNJ 03300 (Null) 10EA COVE LIP DOORS RAISED IAW 1C-135-2-8-1 PG 14-388 PARA 1 4.86.3 STP12 A83FL 14EL0 X 799 PANEL REINSTALLED IAW 1C-135-2-8-1 PG15-33 PARA 15.8.2 STP9 A83FL 11EAE S 800 KEEL BEAM BAY DOOR CLOSED IAW 1C-135-2-2-2 PG15-600 PARA 15. 95.2 SECTION C STP 4 A83FL 11430 X 799 LT KEEL BEAM BAY CLOSED IAW 1C-135-2-2-2 PG15-600 PARA 15.95 .2 SECTION C STP4 A83FL 11430 X 799 ENG FAN COWL CLOSED IAW 1C-135-2-2-2 PG. 20-5 PARA 20.3.2 A83GC 118D0 S 800 ENG FAN COWL CLOSED IAW 1C-135-2-2-2 PG. 20-5 PARA 20.3.2 A83GC 118D0 S 800 ENG FAN COWL CLOSED IAW 1C-135-2-2-2 PG. 20-5 PARA 20.3.2 A83GC 118D0 S 800 ENG FAN COWL CLOSED IAW 1C-135-2-2-2 PG. 20-5 PARA 20.3.2 A83GC 118D0 S 800 ENG DUCT COWL CLOSED IAW 1C-135-2-2-2 PG 20-21 PARA 20.8 A83GC 118D0 S 800 ENG DUCT COWL CLOSED IAW 1C-135-2-2-2 PG 20-21 PARA 20.8 A83GC 118D0 S 800 ENG DUCT COWL CLOSED IAW 1C-135-2-2-2 PG 20-21 PARA 20.8 A83GC 118D0 S 800 ENG DUCT COWL CLOSED IAW 1C-135-2-2-2 PG 20-21 PARA 20.8 A83GC 118D0 S 800 1EA WARNING TAG REMOVED AND C/B RESET JFS DRAINED AND SERVICED IAW 1C-135-2-4-1-1 P 8-72 P 8.27 A83JE 27CBF X 799 8EASPOILRLCKS REMIAW1C-135-2-2-2PG14-14PARA14.4.4 3EAWARNGTAGS REMIAWLPS-55MXG-00-20-1-OFC3 PG5-7 PARAA83FL 06000 (Null) 1EA WARNG TAG REM IAW LPS-55MXG-00-20-1-OFC3 PG 5-7 PARA 5 .7.3.16.5.1.3.10 8EA LEADING EDGE FLAP LOCKS REM A83FL 06000 (Null) 2EA WARNING TAGS REM IAW LPS-55MXG-00-20-1-OFC3 PG 5-7 PARA 5.7.3.16.5.1.3.10 A83FL 01490 (Null) CARDS C/W A83FL 03999 (Null) INSP C/W IAW LPS MXG-1C-135-6WC-1-OFC1 CARD 4-022 ITEM 1 SCH 100 AVIATION GREASE USED IPI C/W INSP IAW LPS A83FL 04199 (Null) CARDS C/W A83FL 03999 (Null) RT ACM DRAINED & RESERVICED IAW 1C-135-2-2-2 PG 15-600 PARA 15.95.2 SECTION C A83FL 01000 (Null) LT ACM DRAINED & RESERVICED IAW 1C-135-2-2-2 PG 15-600 PARA 15.95.2 SECTION C A83FL 01000 (Null) HPO C/W NDN A83GC 03999 (Null) 1 EACH WARNING TAG REMOVED IAW LPS-55MXG-00-20-1-OFC3 PG 4 P ARA 5.7.3.16.5.1.3.10. A/R DOOR LOCKED REMOV A83HY 06000 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-127 C/A MDS PWC WUC AT HMAL HPO C/W A83HY 03999 (Null) 4EA WARNING TAGS REMOVED AND C/BS RESET IAW 1C-135-2-4-1-1 9-1 P 9.3 A83JE 06000 (Null) 4EA WARNING TAGS REMOVED AND T-HANDLES RESET IAW 1C-135-2-4-1-1 P 9-1 P 9.3 A83JE 06000 (Null) 4EA WARNING TAGS REMOVED AND C/BS RESET IAW 1C-135-2-4-1-1 9-1 P 9.3 A83JE 06000 (Null) INSP C/W NDN A83JE 03999 (Null) INSP C/W NDN A83JE 04136 (Null) R2 TACAN #1 CONTROL PANEL IAW ETM-RC135-2-11 PG 2-153 PARA 2 .30.2 SYS OP CHECK GOOD A83CN 71ZD0 R 255 DISCREPANCY ENTERED IN ERROR IAW TO 00-20-1 PARA 4.6.6.4 A83CN 1151E X 799 DISCREPANCY ENTERED IN ERROR. IAW TO 00-20-1 PARA 4.6.6.4 A83CN 1151E X 799 R2 TUNER O/C/G HLGNJ 82CAB R 956 REPLACED SPARE KEYBOARD HLGNJ 82GAJ R 255 R2 C/B O/C/G HLGNJ 82GA9 G 6 SUPPORTED A/C FOR LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) R2 RIU IAW ETM-RC135-2-11 PG 2-62B PARA 2.6.37 SYS OPS CHK G OOD A83CN 72BA0 R 957 ASS. EQUIP MAL. SEE JCN 150789615001 FOR ORIGINAL MALFUNCTIO N A83CN 72BA0 L 602 O/C/G WITH MX LOAD HLGNJ 82SC0 L 940 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP CW IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP CW IAW 1C-135-2-4CL-1-1 PG42/43 STEPS X-AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-128 C/A MDS PWC WUC AT HMAL POSTFLIGHT C/W HLGNJ 04199 R2 HATCH IAW 1C-135-2-2-2 PG. 18-188 PARA. 18.72 A83FL 11360 R 70 HATCH REMOVED FOR SHEET METAL PAINT A83FL 11360 P 757 OVERWING HATCH INSTALLED A83FL 11360 Q 799 R2 WHEEL AND TIRE IAW 1C-135-2-7-1 PG 6-53 PARA 6.13.3 IPI C /W IAW 1C-2-7-1 PARA 16.3.2 STEP 2,3 AND PARA 16.3. A83FL 13AP0 R 20 0A83FL 13AMD S 800 TRANSDUCER REINSTALLED IAW AC-135-2-7-1 PARA 6.13.3 PG 6-62 IPI C/W IAW 1C-135-2-7-1 STEPS 9,11 AND PARA9.12. A83FL 13EBE S 800 #2 ENG COWLING CLOSED TO IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83HY 118D0 S 800 INSPECTED AREA, NO DEFECT NOTED. OPS CHECK PUMP WITH THE RIG HT AMOUNT OF FUEL, PUMP CHECK GOOD MULTI A83JE 46711 X 799 SUPPORTED A/C LAUNCH A83CN 01000 (Null) AXLE DOWNJACKED IAW 1C-135-2-2-2 PG 21-59 PARA 21.16.3 A83FL 01000 (Null) OPS CHECK GOOD A83FL 04199 (Null) INSP C/W IAW OAFBI 21-100 PARA. 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG. 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR D/L C/W A83GC 04199 (Null) HYD MULE DISCONNECTED FROM #2 ENG IAW 1C-135-2-2-2 PG 14-161 PARA 14.38 A83HY 01000 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) C/W A83FL 04199 (Null) RELOADED WAYPOINT DATA SYS OPS CHK GOOD A83CN 72XJ0 L 939 INSPECTION C/W NDN A83EE 41799 X 799 REINSTALLED PANEL IAW ETMRC-135-2-3 PARA 7.2.5.6 STEP M A83EE 118AM S 800 NO DEFECT OPERATING RADIO ALTIMETERS PASS OUT OF LIMITS OPS CHK GOOD IAW ETM-RC135-2-11 PG 2-157 PARA 2 A83GC 51Q00 X 799 COULD NOT DUPLICATE MALFUNCTION, RAN SYSTEM WITH MAINT SOFTW ARE, INITED/ICOLD/TCOLD SEVERAL TIMES WHARCEC 82SA0 H 799 REBUILT SOFTWARE O/C/G HLGNJ 82EAM L 254 REBUILT SOFTWARE O/C/G NDU RECONFIGURED TO A SIDE HLGNJ 82EAM L 940 COLD START HCP O/C/G HLGNJ 823AC L 940 COLD START HCP O/C/G HLGNJ 823AC L 940 RECONFIGURED AIRCRAFT TO NDU A HLGNJ 82EAM L 956 DUST COVER REINSTALLED IAW 1C-135-2-7-1 PARA 9.14 IPI C/W IA W 1C-135-2-7-1 PARA 9.14 STEP 27 BY (Null) RC-135V, T/N 64-14848, 30 April 2015 U-129 C/A MDS PWC WUC AT HMAL INSP C/W OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) LAV SERVICED A83FL 01000 (Null) FDR D/L C/W A83GC 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1 PG 3-104 STEPS 31-36 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) COPILOTS MFD R2 IAW ETM-RC135-2-11 PG 4-341 PARA 4.18.5 AND 4.18.6 OPS CHK GOOD IAW ETM-RC135-2-11 PG 4-271A83GC 51PAA R 255 COPILOTS MFD R2 IAW ETM-RC135-2-11 PG 4-341 PARA 4.18.5 AND 4.18.6 A83GC 51PAA R 255 INSTALLED HARNESS IAW 1C-135-2-7-1 PG 6-31 PARA 6.7.4 STEP 1 3 SEE THIS JCN WCE 016, 021, 022 FOR OPS CHECKS A83EE 13EA0 S 800 OPS CHECK GOOD IAW 1C-135-2-7-1 PG 9-61 PARA 9.8.2 A83EE 13EB0 X 799 INSTALLED DUST COVER IAW 1C-135-2-7-1 PG 9-91 PARA 9.14.2 ST EP 27 IPI C/W BY SSGT IAW 1C-135- A83EE 13AMD S 800 INSTALLED DUST COVER IAW 1C-135-2-7-1 PG 9-91 PARA 9.14.2 ST EP 27 IPI C/W BY SSGT IAW 1C-135- A83EE 13AMD S 800 INSTALLED DUST COVER IAW 1C-135-2-7-1 PG 9-91 PARA 9.14.2 ST EP 27 IPI C/W BY SSGT IAW 1C-135- A83EE 13AMD S 800 INSTALLED DUST COVER IAW 1C-135-2-7-1 PG 9-91 PARA 9.14.2 ST EP 27 IPI C/W BY SSGT IAW 1C-135- A83EE 13AMD S 800 OPS CHECK BAD SEE THIS JCN WCE 027 FOR MX ACTION A83EE 13EAE X 553 OPS CHECK GOOD IAW 1C-135-2-7-1 PG 6-31 PARA 6.7.4 A83EE 13EAD X 799 R2 RH TRUCK LEVEL SWITCH IAW 1C-135-2-7-1 PG 6-136 PARA 6.35 .2 OPS CHECK GOOD A83EE 13EAE R 255 RT MLG RESEALED IAW 1C-135-2-7-1 PG 6-321 PARA 6.97. NITROGE N REQ SERVICE. LEAK AND OPS CHECK DUE. IPI ENSUA83HY 13AB0 G 381 RT MLG RT MLG TRUNNION TO DRAG BRACE BRAKE LINES INSTALLED I AW 1C-135-2-7-1 PG 6-332 PARA 6.97.6. A83HY 13EA0 S 800 RT MLG STRUT LEAK CHECK GOOD A83HY 13AB0 X 799 BLEED C/W IAW T.O. 1C-135-2-7-1 PG 9-106 PARA 9.20 A83HY 13C00 L 651 LEAK CHECK GOOD A83HY 13CBA X 799 CLOSED #2 ENG COWL IAW TO 1C-135-2-2-2 PG 20-4 PARA 20.3 A83HY 118D0 S 800 CLOSED #1 ENGINE COWL IAW TO 1C-135-2-2-2 PG 20-4 PARA 20.3 A83HY 118D0 X 799 CLOSED #1 ENGINE COWL IAW TO 1C-135-2-2-2 PG 20-4 PARA 20.3 A83HY 118D0 X 799 INFLATED RT MLG STRUT IAW TO 1C-135-2-2-2 PG 15-528 PARA 15. 76 A83HY 13C00 X 799 RC-135V, T/N 64-14848, 30 April 2015 U-130 C/A MDS PWC WUC AT HMAL DISCREPANCY ENTERED IN ERROR IAW TO 00-20-1 PG 4-3 PARA 4.6. 6.1 A83HY 13C00 X 799 RT MLG INSTALLED IAW 1C-135-2-7-1 PG 6-391 PARA 6.107 A83JE 13AA0 S 800 SAFTEY & RTV MLG IAW 1C-135-2-7-1 PG. 6-391 PARA. 6.107 A83JE 13000 L 127 STRUT CONFIGURED A83FL 01000 (Null) FUEL CONFIGURED IAW 2-2-CL-2-1 PG 4-26 A83FL 01000 (Null) 2 EACH WARNING TAGS REMOVED IAW LPS-55MXG-00-20-1-OFC3 PG 4 PARA 5.7.3.16.5.1.3.10. A83HY 01490 (Null) SERVICED RT MLG STRUT IAW T.O. 1C-135-2-2-2 PG 15-535 PARA 15.77 A83HY 01000 (Null) RT MLG SERVICED IAW 1C-135-2-7-1 PG 6-329 PARA 6.97.5. A83HY 01000 (Null) MLG OPS CHECK GOOD A83HY 04122 (Null) IPI C/W TO ENSURE BACKUP RINGS ARE PROPERLY INSTALLED WITH ROUNDED EDGES FACING THE RING SEALS. ALSO TOA83HY 04199 (Null) IPI C/W TO ENSURE INNER CYLINDER IS FREE OF FOD PRIORTOASSEMBLY IAW 1C-135-2-7-1 PARA 6.98.7 PRIOR TO STEPA83HY 04199 (Null) HYD MULE DISCONNECTED FROM #2 ENG IAW TO 1C-135-2-2-2 PG14-158 PARA 14.38 A83HY 01000 (Null) REMOVED MULE FROM #1 ENGINE IAW TO 1C-135-2-2-2PG14-158PARA14.38 A83HY 01000 (Null) REMOVED MULE FROM #1 ENGINE IAW TO 1C-135-2-2-2PG14-158PARA14.38 A83HY 01000 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) 4 EA JACK PANELS INSTALLED IAW 1C-135-2-2CL-3-1 PG 5-6 PARA 5.4 A83JE 01000 (Null) 5EA JACK PADS REMOVED IAW 1C-135-2-2CL-3 PG 5-6 PARA 5.4 A83JE 01000 (Null) 1 EA PLUMB BOB REMOVED IAW 1C-135-2-2CL-3 PG 5-6 PARA 5.4 A83JE 01000 (Null) ACFT DOWN JACKED IAW 1C-135-2-2CL-3-1 PF 5-6 PARA 5.4 A83JE 01000 (Null) AUX SEAT WALK AROUND BOTTLE BRACKET R2 A83FL 4714A R 70 R2 RELIEF VALVE IAW 1C-135-2-13-1 PG 3-250 PARA 3.52. LK AND OPS CHECK GOOD. A83HY 45110 R 875 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 PARA 20. 3 A83JE 118D0 S 800 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 PARA 20. 3 A83JE 118D0 S 800 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 PARA 20. 3 A83JE 118D0 S 800 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 PARA 20. 3 A83JE 118D0 S 800 4 EA CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 PG 201 SEC 7 9-00-00 A83JE 27A4D S 800 4 EA CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 PG 201 SEC 7 9-00-00 A83JE 27A4D S 800 4 EA CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 PG 201 SEC 7 9-00-00 A83JE 27A4D S 800 4 EA CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 PG 201 SEC 7 9-00-00 A83JE 27A4D S 800 FUEL STRAINER REINSTALLED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6. 9.2 A83JE 27H99 S 800 FUEL STRAINER REINSTALLED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6. 9.2 A83JE 27H99 S 800 RC-135V, T/N 64-14848, 30 April 2015 U-131 C/A MDS PWC WUC AT HMAL FUEL STRAINER REINSTALLED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6. A83JE 27H99 S 800 FUEL STRAINER REINSTALLED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6. 9.2 A83JE 27H99 S 800 INSP CW IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP CW IAW 1C-135-2-4CL-1-1 PG42/43 STEPS X-AF A83FL 0413C (Null) C/W A83FL 01000 (Null) INSP CW IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) C/W IAW 1C-135-2-4CL-1-1 PGS 4-2 THRU 4-3 STEPS X-AF A83FL 0413C (Null) C/W A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) 1 EA WARNING TAG REMOVED IAW LPS-55MXG-00-20-1-OFC3 PARA 5.7.3.16.5.1.3.10 PG 4 A83HY 01490 (Null) INSP C/W NDN A83JE 04199 (Null) ALL T-HANDLES AND C/BS RESET IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG 8-67 PARA 8.25.2 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG 8-67 PARA 8.25.2 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG 8-67 PARA 8.25.2 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG 8-67 PARA 8.25.2 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG 8-67 PARA 8.25.2 A83JE 06000 (Null) 2 EA WARNING TAGS REMOVED IAW LPS-55MXG-00-20-1-OFC3 PARA5.7.3.16.5.1.3.10 A83JE 06000 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PARA 4.1.1 STEPS X-AF A83JE 0413C (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83JE 0413C (Null) POST FLIGHT C/W HLGNJ 04199 (Null) OPERATOR ERROR. HLGNJ 82EAK X 799 COLD STARTED TNT. O/C/G HLGNJ 82LH0 L 956 COLD STARTED TNT. O/C/G HLGNJ 82LH0 L 956 QRC REMOVED HLGNJ 82ZA0 P 799 OPS CK GOOD PER AIRCREW A83EE 41210 X 799 R2 WHEEL AND TIRE IAW IAW 1C-135-2-7-1 PARA 6.13.3 IPI C/W I AW 1C-135-2-7-1 PARA 6.13.2STEP 3, STEP 3, 6.13.3 STA83FL 13AP0 R 20 RC-135V, T/N 64-14848, 30 April 2015 U-132 C/A MDS PWC WUC AT HMAL #2 DUST COVER REINSTALLED IAW \ 1C-135-2-7-1 PARA 9-13.4 STE P 27 IPI C/W IAW IAW 1C-135-2-7-1 PARA 9-13.4 STE A83FL 13AMD S 800 #2 XDUCER REINSTALLED IAW 1C-135-2-1 PARA 6. 13.3 STEP S 9, 11 & PARA 9.12.2. IPI C/W IAW1C-135-2-1 PARA 6.13.3 A83FL 13EBE S 800 DOWNJACKED IAW 1C-135-2-2-2 PARA 21.16.3 A83FL 01000 (Null) OPS CHECK GOOD A83FL 04199 (Null) MANUFACTURED NEW BOOM END A83JE 01000 (Null) REINSTALLED COVERS IAW TO 1C-135-2-10-1 PG 19-31 PARA 19.24. 4 STEP 2 A83EE 4422A S 800 SYMBOL ENTERRED IN ERROR SIGNED OFF IAW 00-20-1 PG 4-4 PARA 4.6.6.2 NO CORRECTED BY REQUIRED, SIGNED OFF A83EE 4422A X 799 R2 BULBS OPS CHK GOOD A83EE 4422A R 255 REMOVED TAG IAW TO LPS55MXG-00-20-1-OFC3 PG 2 PARA5.7.3.16.5.1.3.10 A83EE 01490 (Null) REMOVED LOCK IAW TO 1C-135-2-10-1 PG 19-31 PARA 19.24.4 STEP 3 A83EE 06000 (Null) 28 DAY FMS UPDATE C/W A83CN 727AB L 944 OPS CK GOOD PER AIRCREW A83EE 41210 X 799 REMOVED RT SLIPWAY DOOR FOR STMA REPAIR IAW 1C-135-2-6-1 PAG 23-169 PAR 23.47. A83HY 46973 P 800 RE-INSTALLED SLIPWAY DOOR AFTER SHEET METAL REPAIR IAW T.O. 1C-135-2-6-1 PG. 2-172 PARA. 23.48 A83HY 46973 Q 799 REINSTALLED UPPER A/R MANIFOLD IAW 1C-135-2-6-1 PG 23-125 PA RA 23.28 A83JE 46981 S 800 LK CHK C/W NO DEFECTS NOTED A83JE 46981 X 799 SLIPWAY TORN REQS REPAIR ASTMA 46973 G 190 SUPPORTED A/C LAUNCH A83CN 01000 (Null) RESEET CB AND REMOVED 2 WARNING TAGS IAW TOLPS-55MXG-00-20-1-OFC3 PARA 5.7.3.16.1.3.10 PG 2 A83EE 01490 (Null) INSP. C/W IAW:21-100 PARA.7.2.1 A83FL 04199 (Null) INSP. C/W IAW:1C-135-2-4-1-1 PG.3-104 STEPS.31-38 A83FL 0413C (Null) DRAIN C/W A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) REMOVED 2 EA WARNING TAGS IAW TO 1C-135-2-6-1 PG 23-125 PARA 23.28 A83JE 01490 (Null) IPI C/W NO DEFECTS NOTED IAW 1C-135-2-6-1 PARA 1.16 STEP A A83JE 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-133 C/A MDS PWC WUC AT HMAL INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) A83JE 9111B R 70 SPARE KEYBOARD R2 HLGNJ 82GAJ R 308 REBUILT CRYPTO FILL CABLE HLGNJ 82L00 G 70 O/C/G HLGNJ 84WD0 X 799 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 P3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) VALIDATION OF CURRENT PN/SN FOR THE SIRU INSTALLATION C/W. C K GOOD. A83CN 72XN0 X 799 RECYCLED SYS POWER. PERFORMED GC ALIGNMENT IAW ETM-RC135-2-1 1 PG 5-95 PARA 5.5.8.1. SYS OPS CHK GOOD A83CN 72XN0 L 644 SUPPORTED A/C LAUNCH A83CN 01000 (Null) F-108/TF-33 - INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PGS 4-2 THRU 4-3 STEPS X-AF A83FL 0413C (Null) C/W A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) SEARCH CONDUCTED, ITEM NOT FOUND IAW AFI 21-101 PARA 10.8.1. 8.1. SEARCH CLEARED BY . RC-135V, T/N 64-14848, 30 April 2015 U-134 C/A MDS POST FLIGHT C/W DUST COVER INSTALLED IAW 1C-135-2-7-1 PARA 9.14.2 STEP 27 IP I C/W BY EJ1 PWC WUC AT HMAL HLGNJ 04199 (Null) IAW 1C-135-2-7-1 PARA 9.14 A83EE 13AMD S 800 R2 35 DEGREE CONTROL VALVE LEAK AND OPS CK GOOD IAW 1C-135-2 -3-2 PG 12-39 PARA 12.3.20 A83EE 41225 R 255 CLOSED DOOR IAW 1C-135-2-3-2 PG 13-15 PARA 13.3.2.2 STEP R A83EE 11430 S 800 CLOSED DOOR IAW 1C-135-2-3-2 PG 13-15 PARA 13.3.2.2 STEP Q A83EE 41225 S 800 R2 WHEEL AND TIRE IAW 1C-135-2-7-1 PARA 6.13.2 STEP 3, PG 6- 62 - 6-63, PARA 6.13.3 STEPS 1,5,6 IPI C/W BY A83FL 13AP0 P 20 WHEEL SPEED TRANSDUCER REINSTALLED IAW 1C-135-2-7-1 PARA 6.1 3.3 STEPS 9,11 AND PARA 9.12.2 IPI C/W A83FL 13EBE S 800 R2 WHEEL AND TIRE IAW 1C-135-2-7-1 PARA 6.13.2 STEP 3, PG 6- 62 - 6-63, PARA 6.13.3 STEPS 1,5,6 IPI C/W BY A83FL 13AP0 Q 799 OPS CHECK GOOD A83EE 04199 (Null) MLG AXLW DOWN JACKED IAW 1C-135-2-2-2 PG 21-59 PARA 21.16.3 STEP 4 A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP CW IAW OAFB1 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP CW IAW 1C-135-2-4CL-1-1 PG 42/43 STEPS X-AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) SYMBOL ENTERED IN ERROR IAW 00-20-1 PG 4-3 PARA 4.6.6.1 SEE THIS JCN WCE 003 A83EE 41799 X 799 CLOSED FUEL CELL 0 IAW 1-1A-8 PG 10-1 CH 10.2 A83EE 11PAD S 800 C/W A83EE 41799 X 799 CALIBRATED LH PACK CONTROL PANEL IAW TO ETM-RC-135-2-3 PG4-4 6 PARA 4.1.6.12 OPS CHK GOOD A83EE 413AA K 255 CLOSED KBB DOOR IAW TO 1C-135-2-3-2 PARA13.3.2.2 PG13-16 STE P R A83EE 11430 S 800 CLOSED KBB DOOR IAW TO 1C-135-2-3-2 PARA13.3.2.2 PG13-16 STE P R A83EE 11430 S 800 CLOSED PANEL IAW TO 1C-135-2-3-2 PARA13.3.2.2 PG13-16 STEP Q A83EE 118AM S 800 REINSTALLED WATER SEPARATOR IAW TO 1C-135-2-3-2 PARA 13.14.3 6 PG13-82 LEAK AND OPS CHK GOOD A83EE 41214 S 800 R2 TORQUE MOTOR IAW TO 1C-135-2-3-2 PARA 13.14.22 PG 13-48 L EAK AND OPS CHK GOOD A83EE 4123J R 255 R2 TORQUE MOTOR TEMP SENSOR IAW TO 1C-135-2-3-2 PARA 13.14.2 4 PG 13-49 LEAK AND OPS CHK GOOD A83EE 4121C R 255 REINSTALLED VALVE IAW TO 1C-135-2-3-2 PG 12-39 PARA 12.3.20 LEAK AND OPS CHK GOOD A83EE 41225 S 800 REINSTALLED VALVE IAW TO 1C-135-2-3-2 PG12-39 PARA13.3.20 LE AK AND OPS CHK GOOD A83EE 41225 S 800 R2 PROCESSOR O/C/G HLGNJ 82EAB R 956 5 EA WARNING TAGS REMOVED IAW TO LPS-55MXG-00-20-1-OFC3 PG2 PARA 5.7.3.16.5.1.3.10 A83EE 01490 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-135 C/A MDS PWC WUC AT HMAL ADJUSTED HATCH OPS CHK GOOD ON GROUND A83FL 11360 L 127 O/C/G WITH MX LOAD HLGNJ 82EAG X 799 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) ISNP C/W IAW 1C-135-2-4-1-1 PG 3-104 PARA 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) R2 KDU IAW ETM-RC-135-2-11 PG 4-341 PARA 4.18.6 OPS CHK GOOD A83GC 51PAA INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) R2 GCU. OPS CHECKED GOOD IAW 1C-135-2-10-1, PG 13-37, PARA 1 3.26 A83EE 42930 R 255 CLOSED COWLING. IAW 1C-135-2-2-2, PG. 20-4, PARA. 20.3 A83EE 118D0 S 800 RESEATED CABLES O/C/G HLGNJ 82EAF L 956 O/C/G WITH MAINT LOAD HLGNJ 82EA2 X 799 SUPPORTED A/C LAUNCH A83CN 01000 (Null) SANITIZATION C/W A83FL 04199 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW IC-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) ALLOWED PACK ENOUGH TIME TO STABILIZE OPS CHECK GOOD A83EE 413AA X 799 LUBRICATED PILOTS SEAT RAILS A83FL 12AA0 X 799 RECYCLE SYSTEM POWER. OPS CHK GOOD. NO LAG A83GC 5131G L 181 R 957 RC-135V, T/N 64-14848, 30 April 2015 U-136 C/A MDS PWC WUC AT HMAL FAN COWL CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20.3 PARA 20 -4 A83JE 118D0 X 799 FAN COWL CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20.3 PARA 20 -4 A83JE 118D0 X 799 FAN COWL CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20.3 PARA 20 -4 A83JE 118D0 X 799 FAN COWL CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20.3 PARA 20 -4 A83JE 118D0 X 799 #1 ENGINE CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 PG 202 PARA 79-00-00 A83JE 27A4D S 800 #2 ENG CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 PG 202 PAR 79-00-00 A83JE 27A4D S 800 #3 ENG CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 PG 202 PAR 79-00-00 A83JE 27A4D S 800 #4 ENG CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 PG 202 PAR 79-00-00 A83JE 27A4D S 800 ALL RUB BUTTONS ARE IN PLACE AND DOING THEIR JOB. NORMAL WEA R ON PAINT WHERE RUB BUTTON MAKES CONTACASTMA 14EHA F 20 THE PLASTIC RUB BUTTONS ARE IN PLACE AND DOING THERE JOB. NO RMAL WEAR ON PAINT WHERE RUB BUTTON MAKEASTMA 14EHA F 20 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP /CW IAW IC-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW IC-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) INSP C/W NDN A83JE 04199 (Null) WARNING TAGS REMOVED AND C/B'S RESET IAW 2J-F108-2-1 PG 202 PAR 79-00-00 A83JE 04199 (Null) ALL 4 ENGINE TGB INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) ALL 4 ENGINE CHIP DETECTORS INSP C/W A83JE 04199 (Null) OIL LEVELS ON 1,2, AND 4 IDG'S INSP NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) PRE RUN I'S AND E'S INSP C/W IAW 1C-135-2-4CL-1-1 PG 4.11 PAR X-AF A83JE 0413C (Null) POST RUN I'S AND E'S INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 7.1 7-1 A83JE 0413C (Null) INSP C/W NDN A83JE 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) MODE IV/MODE C CHK C/W NDN A83CN 04MD4 (Null) HOT GAS PURGE C/W NDN A83EE 01000 (Null) SERVICED LOX C/W IAW 1C-135-2-2-2 PARA 10.56 A83FL 01000 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-137 C/A MDS PWC WUC AT HMAL PITOT-STATIC SYS OPS CHK GOOD AND LEAK CHK GOOD. A83GC 0418A (Null) ADC OPS CHK GOOD A83GC 04199 (Null) TAPE REMOVED FROM PILOT'S PITOT TUBE IAW ETM-RC135-2-11 PG 5-321 PARA5.42.2.1 A83GC 0418A (Null) TAPE REMOVED FRO COPILOT'S PITOT TUBE IAW ETM-RC135-2-11 PG 5-321 PARA5.42.2.1 A83GC 0418A (Null) TAPE REMOVED FROM PILOT'S STATIC BOOM IAW ETM-RC135-2-11 PG 5-321 PARA5.42.2.1 A83GC 0418A (Null) TAPE REMOVED FROM COPILOT'S STATIC BOOM IAW ETM-RC135-2-11PG 5-321 PARA5.42.2.1 A83GC 0418A (Null) TTU-205 DISCONNECTED FROM A/C IAW ETM-RC135-2-11 PG 5-321 PARA5.42.2.1 A83GC 0418A (Null) 900 HOUR INSP - C/W IAW 1C-135-6WC-7 ALL APPLICABLE CARDS A83JE 0341F (Null) SERVICED ALL 3 LOX CONVERTERS AFTER HOT GAS PURGE IAW 1C-135 -2-2-2 PG 15-451 PARA 15.56 A83EE 47110 X 799 ADJUSTED LONG-WIRE ONTO CHUCK ASSEMBLY A83JE 61DK0 L 127 WITHIN LIMITS IAW TAR 645AESS/15A-0009 A83JE 61DK0 X 799 REEVALUATED, GOOD A83JE 61DK0 X 799 TEST STAND DISCONNECTED IAW 1C-135-2-2-2 PG 14-159 PARA 14.3 8.2 A83JE 45110 S 800 REPLACED AND GLUED NEW SLEEVE A83JE 61DK0 G 105 C/W A83EE 41799 X 799 CLOSED PANEL IAW ETM-RC135-2-3 PG 7-141 PARA 7.1.6.12 STEP M . NDN A83EE 11PAD S 800 R2 SEALS A83FL 13AJ0 R 20 R2 SEALS A83FL 13AJ0 R 20 WRITE UP ENTERED IN ERROR IAW 00-20-1 PARA 4.6.6.1 A83FL 41415 X 799 LEFT KEEL BEAM BAY DOOR CLOSED IAW 1C-135-2-2-2 PAGE 15-611 STEP 4 A83FL 41415 X 799 RIGHT KEEL BEAM BAY DOOR CLOSED IAW 1C-135-2-2-2 PAGE 15-611 STEP 4 A83FL 41415 X 799 LEFT AND RIGHT ACM DRAINED AND SERVICED IAW 1C-135-2-2-2 PG 15-610 PARA 15.96.2 A83FL 41415 X 799 SHEET MEAL INSPECTED AREA. WILL FIX NEXT DOWNTIME A83FL 14EHL G 20 SHEET METAL EVALED. WILL REPAIR NEXT DOWNTIME A83FL 14EHL Z 212 PREVIOUSLY C/W BOLT RETAINER ALREADY INSTALLED A83JE 27A99 X 799 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG. 20-4 20.3 A83JE 118D0 S 800 REMOVED AND REPLACED CTW CAVITY DRAIN LINE IAW 1C-135-2-5-3 PG.20-8 PARA.20.8 A83JE 465AG R 780 LT OB AIL TAB MIDDLE HINGE RESEATED A83JE 14AHE L 127 LONG-WIRE TENSION WITHIN TOLERANCE IAW TAR 645AESS/15A-0009 A83JE 61DK0 X 799 MAINT. C/W AROUND L/E FLAPS IAW 1C135 6WC-2 I CARDS A83JE 14E00 X 799 L/E FLAP NOT REMOVED FOR FAN DUCT OPENING IAW 1C-135-2-2-2 P ARA 20.7.2 STEP 2 PG 20-19 A83JE 14EM0 X 799 L/E FLAP NOT REMOVED FOR FAN DUCT OPENING IAW 1C-135-2-2-2 P ARA 20.7.2 STEP 2 PG 20-19 A83JE 14EM0 X 799 RC-135V, T/N 64-14848, 30 April 2015 U-138 C/A MDS PWC WUC AT HMAL REMOVED, INSPECTED, CLEANED AND REINSTALLED BLEED ORIFICE IA W 1C-135-2-13-1 PG 3-94 PAR 3.11.6 STEP 9 A83JE 45199 S 804 LEAK CHECK GOOD IAW 1C-135-2-13-1 PG 3-125 PARA 3.16.3 A83JE 45199 X 799 REMOVED, CLEANED, INSP, REINSTALLED ORIFICE IAW 1C-135-2-13- 1 PARA 3-11-6 PG 3-94 A83JE 45199 S 804 LEAK CHECK GOOD IAW 1C-135-2-13-1 PG 3-125 PARA 3.16.3 A83JE 45199 X 799 REMOVED AND REPLACED HYDRAULIC RETURN FILTER IAW 1C-135-2-13 -1 PG 3-210 PAR 3.3.39.3 AND PG 3-214 PAR 3.40 A83JE 45154 R 878 LEAK CHECK GOOD IAW 1C-135-2-13-1 PG 3-218 PARA 3.40.5 A83JE 45199 X 799 REMOVED AND REPLACED FILTER IAW 1C-135-2-13-1 PARA 3.39.3 PG 3-210 AND PARA 3.40.3 PG 3-214 A83JE 45154 R 878 LEAK CHECK GOOD IAW 1C-135-2-13-1 PG 3-218 PARA 3.40.5 A83JE 45154 X 799 2 EA WARNING TAGS REMOVED AFTER TCTO 566 IAW LPS 55MXG 00-20 -1 PFC3 PG 2 PARA 5.7.3.16.5.1.3.10. WUC SHOUL A83JE 27000 X 799 L/E FLAP NOT REMOVED FOR FAN DUCT OPENING IAW 1C-135-2-2-2 P ARA 20.7.2 STEP 2 PG 20-19 A83JE 14EM0 X 799 L/E FLAP NOT REMOVED FOR FAN DUCT OPENING IAW 1C-135-2-2-2 P ARA 20.7.2 STEP 2 PG 20-19 A83JE 14EM0 X 799 RESET T-HANDLES IAW IC-135-2-4-1-1 PG 6-32 PARA 6.13 A83JE 27HA0 X 799 REMOVED AND REPLACED #1 FUEL PUMP IAW 2J-F108-2-1 WP 73-21-1 0 PG 201 IPI C/W IAW 2J-F108-2-1 WP 73-11-10 PGA83JE 27HAA R 799 VSV RIG CHECK COMPLIED WITH. A83JE 27HA0 X 799 VBV RIG CHECK COMPLIED WITH. A83JE 27A20 X 799 PLA GAIN NOT REQ IAW IC-135-2-4-1-1 PG 6-80 PARA 6.31 A83JE 27HA0 X 799 WET MOTOR C/W A83JE 27HA0 X 799 LEAK CHECK GOOD. A83JE 27A99 X 799 REMOVED AND REPLACED #1 FUEL PUMP IAW 2J-F108-2-1 WP 73-21-1 0 PG 201 IPI C/W IAW 2J-F108-2-1 WP 73-11-10 PGA83JE 27HAA R 799 #2 VSV RIG CK GOOD NO DEFECT NOTED A83JE 27HA0 X 799 VBV RIG CK GOOD NO DEFECT NOTED A83JE 27A20 X 799 PLA GAIN NOT REQ IAW IC-135-2-4-1-1 PG 6-80 PARA 6.31 A83JE 27HA0 X 799 WET MOTOR C/W A83JE 27HA0 X 799 #2 ENGINE LEAK CHECK C/W. A83JE 27A99 X 799 REMOVED AND REPLACED #3 FUEL PUMP IAW 2J-F108-2-1 WP 73-21-1 A83JE 27HAA R 799 #3 ENGINE VSV STATIC RIG CHECK C/W A83JE 27HA0 X 799 #3 ENGINE VBV STATIC RIG CHECK C/W A83JE 27A20 X 799 PLA GAIN NOT REQ IAW IC-135-2-4-1-1 PG 6-80 PARA 6.31 A83JE 27HA0 X 799 WET MOTOR C/W. A83JE 27HA0 X 799 #3 ENGINE LEAK CHECK C/W. A83JE 27A99 X 799 REMOVED AND REPLACED #4 FUEL PUMP IAW 2J-F108-2-1 SECTION 73 -21-10 PG 201. IPI C/W IAW 2JF108-2-1 WP 73-21- A83JE 27HAA R 799 #4 ENGINE VSV STATIC RIG CHECK C/W 27HA0 X 799 A83JE RC-135V, T/N 64-14848, 30 April 2015 U-139 C/A MDS PWC WUC AT HMAL #4 VBV STATIC RIG CHECK C/W A83JE 27A20 X 799 PLA GAIN NOT REQ IAW IC-135-2-4-1-1 PG 6-80 PARA 6.31 A83JE 27HA0 X 799 WET MOTOR C/W. A83JE 27HA0 X 799 #4 ENGINE LEAK CHECK C/W. A83JE 27A99 X 799 , VA83JE 27HAC R 70 REINSTALLED MEC THROTTLE CONTROL ASSY IAW IC-135-2-4-1-1 PG 6-43 PARA 6.14 A83JE 27NAC S 800 FDR DOWNLOAD C/W A83GC 04199 (Null) SYMBOL ENTERED IN ERROR, DISCREPANCY AND CORRECT SYM BOLENTERED ON PAGE 31 ITEM 1. IAW 00-20-1 PG 4-4 STA83JE 03999 (Null) PANEL SHEET C/W IAW 00-20-1 PG 5-7 PARA 5.7.3.16.3.3.1 A83JE 01000 (Null) REMOVED 3EA WARNING TAGS IAW LPS-55MXG-00-20-1-OFC3 PG2 PA5.7.3.16.5.1.3.10 A83JE 01490 (Null) REMOVED 8 EA SPOILER LOCKS IAW 1C135 2-2-2 PG 14-14 PA 14.4.4 A83JE 06000 (Null) REMOVED 1EA WARNING TAG IAW LPS-55MXG-00-20-1-OFC3 PG2 PA 5.7.3.16.5.1.3.10 A83JE 01490 (Null) REMOVED LEADING EDGE F;AP LOCKS IAW 1C-135-2-2-2 PARA 14.4.6 PG 14-17 A83JE 06000 (Null) 2 WARNING TAGS REMOVED IAW 1C-135-2-2-2 PG 14-18 PARA 14.4.8 A83JE 01490 (Null) STAB LOCK AND 3 C/B SAFETY LOCKS REMOVED IAW 1C-135-2-2-2 PG 14-18 PARA 14.4.8 A83JE 06000 (Null) ANTENNA COVERS REMOVED IAW 1C-135-2-2-2 PG 2-41 PARA 2-4 A83JE 06000 (Null) 3 WARNING TAGS REMOVED IAW LPS-55MXG- 00-20-1- OFC3 PG2 PARA 5.7.3.16.5.1.3.10 A83JE 01490 (Null) 2 WARNING TAGS REMOVED IAW 1C-135-2-2-2 PG 14-18 PARA14.4.8 A83JE 01490 (Null) SERVICED HYD RESERVOIR 1C-135-2-2-2 PG 15-415 PARA15.45.2 A83JE 01000 (Null) SERVICED RT HYD RESERVOIR IAW 1C-135-2-2-2 PG 15-415PARA14.45.2 A83JE 01000 (Null) REMOVED C/B LOCKS IAW IC-135-2-4-1-1 PG 6-32 PARA 6.13 A83JE 06000 (Null) REMOVED C/B LOCKS IAW IC-135-2-4-1-1 PG 6-32 PARA 6.13 A83JE 06000 (Null) REMOVED 4 TAGS IAW IC-135-2-4-1-1 PG 6-32 PARA 6.13 A83JE 01490 (Null) THROTTLE RIG CW IAW IC-135-2-4-1-1 PG 6-78 PARA 6.31 A83JE 06000 (Null) #1 ENG TRIM TOOL REMOVED IAW 1C-135-2-4-1 PARA 3.17.8 PG 3-290 A83JE 01000 (Null) #1 ENGINE TRIM RUN C/W. A83JE 04139 (Null) THROTTLE RIG CW IAW IC-135-2-4-1-1 PG 6-78 PARA 6.31 A83JE 06000 (Null) #2 ENG TRIM TOOL REMOVED IAW 1C-135-2-4-1 PARA 3.17.8 PG 3-290 A83JE 01000 (Null) #2 ENGINE TRIM RUN C/W. A83JE 04139 (Null) THROTTLE RIG CW IAW IC-135-2-4-1-1 PG 6-78 PARA 6.31 A83JE 06000 (Null) #3 ENG TRIM TOOL REMOVED IAW 1C-135-2-4-1 PARA 3.17.8 PG 3-290 A83JE 01000 (Null) #3 ENGINE TRIM RUN C/W. A83JE 04139 (Null) REM'D & REPLACED MEC IAW 2J-F108-2-1 WP 73-11-10-401 IPI REQ 'D PARA B STP 3 C/W BY WG-10 RC-135V, T/N 64-14848, 30 April 2015 U-140 C/A MDS PWC WUC AT HMAL THROTTLE RIG CW IAW IC-135-2-4-1-1 PG 6-78 PARA 6.31 A83JE 06000 (Null) #4 ENG TRIM TOOL REMOVED IAW 1C-135-2-4-1 PARA 3.17.8 PG 3-290 A83JE 01000 (Null) #4 ENGINE TRIM RUN C/W. A83JE 04139 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 3-4 PARA 3.1.1 STEPS AB-AI A83JE 0413C (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 STEPS A-F A83JE 0413C (Null) REPLACED COMM CORD OPS CHECK GOOD A83CN 6416W INSP C/W A83FL 07000 28 DAY FMS UPDATE C/W A83CN 727AB L 944 RADIO ALT OPERATING RANGE IS -20 TO 2500FT AND BEING USED OU TSIDE OF SYSTEM PARAMETERS IAW ETM-RC135-2A83GC 51QAA X 799 TAWS UPDATE C/W A83GC 51Q00 L 944 R2 OIL PRESS WARNING SWITCH LEAK AND OPS CHECK GOOD IAW 1C-1 35-2-4-1-1 PG 13-132 PARA 13.43 A83JE 27A4J S 800 COWLING CLOSED AND SECURE NDN IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83JE 118D0 S 800 LEAK AND OPS CHECK GOOD A83JE 27000 X 799 R2 R/T O/C/G HLGNJ 81JD0 R 956 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP /CW IAW IC-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD CW A83GC 04199 (Null) POST FLIGHT COMPLIED WITH HLGNJ 04199 (Null) R2 POWER DIVIDER IAW ETM-RC135-2-11 PAGE 5-158 PARA 5.13.11 SYS OP CHK GOOD A83CN 727BE R 254 R2 SIRU IAW ET-RC135-2-11 PG 5-106 PARA 5.7.1.4 SYS OPS CHK BAD FOR BUS A. SEE THIS JCN WCE 002 FOR NEW WRITA83CN 72XN0 R 255 2 EA MED KITS R2 A83FL 91211 R 20 LEFT WING LANDING LIGHT PANEL INSTALLED IAW 1C-135-2-10-1 PG .19-8 PARA 19.11.4 STEP 9 A83FL 44263 S 800 WOUND CLOCK. A83GC 51214 X 948 RADIO ALTIMETER ON OUTSIDE OF OPERATING LIMITS A83GC 51Q00 X 799 O/C/G WITH MX LOAD HLGNJ 823AC X 799 RESEAT CONNECTIONS ON ESW117 O/C/G HLGNJ 82AFD L 6 R2 KEYBOARD O/C/G HLGNJ 82GA0 R 901 O/C/G WITH MX LOAD HLGNJ 82ACE X 799 G 693 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-141 C/A MDS PWC WUC AT HMAL R2 CONQPMC-2 CABLE ASSEMBLY. SEE JCN 150340142004 FOR OPS CH ECK. HLGNJ 72XN0 G 6 O/C/G PER AIRCREW IAW ETM-RC135V/W-2 VOL 2 PARA 40.1.4 HLGNJ 82EAM H 799 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PAGE 3-108 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) C/W NDN A83EE 41799 X 799 CLOSED PANEL IAW ETM-RC135-2-3 PG 7-141 PARA 7.1.6.12 STEP M A83EE 11PAD S 800 MAIN ACFT BATTERY REMOVED IAW 1C-135-2-10-1 PG 15-34 PARA 15 .27.2 A83FL 42143 P 255 MAIN ACFT BATTERY REINSTALLED IAW 1C-135-2-10-1 PG 15-34 PAR A 15.27.2 NDN OPS CHECK GOOD A83FL 42143 Q 799 CURE CK C/W. CURE CK BAD. REQUIRES MORE TIME. SEE THIS JCN W CE 002. A83CN 727AE H 799 CURE CK C/W. CURE CK GOOD. A83CN 727AE H 799 REMOVED SECRW ASTMA 727BC G 70 RE-SEATED TX LINE ON R/T O/C/G HLGNJ 82LD0 L 254 O/C/G WITH MX LOAD HLGNJ 82SC0 X 799 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 P.3-175 PARA 3.9.12 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 4-2/4-3 STEP X-AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) NO LK NOTED RESIDUAL FLUID DUE TO COMPONENT CHANGE SEE JCN 1 50584848 A83HY 46711 X 799 INSTALLED FWD FWD AND FWD AFT A/R PUMP ACCESS PANELS IAW 1C- 135-2-6-1 PG 22-39 PARA 22.13.4 A83HY 11BBD S 800 O/C/G WITH MX LOAD HLGNJ 82QE0 X 799 O/C/G PER AIRCREW HLGNJ 82AFB X 799 RC-135V, T/N 64-14848, 30 April 2015 U-142 C/A MDS PWC WUC AT HMAL SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PGS 4-2 THRU 4-3 STEPS X-AF A83FL 0413C (Null) C/W A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) I'S AND E'S INSP C/W NDN IAW 1C-135-2-4CL-1-1 PARA 4.1.1 STEPS X-AF A83JE 0413C (Null) I'S AND E'S INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83JE 0413C (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) R2 GPS 1 ANTENNA IAW ETM-RC135-2-11 PG 6-100A PARA 6.6.15 SE E THIS JCN WCE 002 FOR OPS CHK. SEE JCN 1503064A83CN 727AE R 255 FMS 1 OPS CK GOOD. A83CN 727AE X 799 FWD BDY FWD A/R PUMP PRESS LINE FITTING R2 IAW 1C-135-2-6-1 PG 22-26 PARA 22.11.4 LEAK AND OPS CHECK DUE A83HY 4511T R 305 FWD BDY FUEL CELL ACCESS PANEL INSTALLED IAW 1C-135-2-6-1 PG 22-26 PARA 22.11.9. A83HY 11BBC S 800 LEAK AND OPS CHECK GOOD. A83HY 4511T X 799 FORWARD BODY FORWARD ACCESS PANEL INSTALLED IAW 1C-135-2-6-1 PG 22-26 PARA 22.11.9 A83HY 4511T S 800 #2 ENGINE FAN COWL CLOSED IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83HY 118D0 S 800 HYDRAULIC TEST STAND HT08 DISCONNECTED IAW 1C-135-2-2-2 PG 1 4-58P ARA 14.38. A83HY 4511J S 800 1 OF 1 WARNING TAGS REMOVED IAW LPS-55MXG-00-20-1-OFC3 PARA 5.7.3.16.5.1.3.10 PG 4 A83HY 4516A S 800 O/C/G WITH MX LOAD HLGNJ 82SC0 X 799 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1 PARA 4.1.1 STEPS X-AF A83JE 0413C (Null) INSP C/W IAW 1C-135-2-4CL-1 PARA 7.1 PG 7-1 A83JE 0413C (Null) POST FLIGHT C/W HLGNJ 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-143 C/A MDS PWC WUC AT HMAL REINSTALLED S-DYCT IAW 1C-135-2-3-2 PG 13-70 PARA 13.14.54 L EAK CHECK GOOD A83EE 411DA S 800 REINSTALLED T-DUCT OPS AND LEAK CHECK GOOD A83EE 4111H S 800 CLOSED ACCESS PANEL IAW 1C-135-2-3-2 PARA 13.3.2.2 STEP Q A83EE 11PAD S 800 BATTERY CAP CHK C/W. BATTERY REQUIRES REPLACEMENT SEE JCN 150265410 WCE 001 A83CN 04117 (Null) W/C 7-001 C/W NDN A83EE 03300 (Null) REMOVED 5 EACH WARNING TAGS IAW LPS-55MXG-00-20-1-OFC3 PG 2 PARA 5.7.3.16.5.1.3.10 A83EE 01490 (Null) INSP C/W A83FL 03300 (Null) CARDS C/W. ARCEC 03300 (Null) HPO C/W HLGNJ 03300 (Null) R2 BATTERY IAW ETM-RC135-2-11 PG. 5-108A PARA 5.7.1.8. SYS O PS CK GOOD. A83CN 72XD0 R 25 INSPECTION C/W NDN A83EE 41799 X 799 CLOSED PANEL IAW ETM-RC135-2-3 PG 7-141 PARA 7.1.6.12 STEP M NDN A83EE 11PAD S 800 RH KEEL BEAM BAY CLOSED IAW 1C-135-2-2-2 PARA 15.96.2 STEP C -4 A83EE 11430 S 800 LH KEEL BEAM BAY CLOSED IAW 1C-135-2-2-2 PARA 15.96.2 STEP C -4 A83EE 11430 S 800 FRONT URINAL UNCLOGGED A83FL 12GB0 V 70 10 EA COVE LIP DOORS RAISED IAW 1C-135-2-8-1 PG 14-118 PARA 14.30.2 STEP 12 A83FL 14EL0 X 799 STAB TRIM ACCESS PANEL REINSTALLED IAW 1C-135-2-8-1 PG 15-7 PARA 15.4.14 STEP 2 A83FL 11EAE X 799 #4 ENG FAN COWL CLOSED IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83GC 118D0 S 800 #3 ENG FAN COWL CLOSED IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83GC 118D0 S 800 #2 ENG FAN COWL CLOSED IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83GC 118D0 S 800 #1 ENG FAN COWL CLOSED IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83GC 118D0 S 800 #1 ENG DUCT COWL CLOSED IAW 1C-135-2-2-2 PG 20-21 PARA 20.8 A83GC 118D0 S 800 #2 ENG DUCT COWL CLOSED IAW 1C-135-2-2-2 PG 20-21 PARA 20.8 A83GC 118D0 S 800 #3 ENG DUCT COWL CLOSED IAW 1C-135-2-2-2 PG 20-21 PARA 20.8 A83GC 118D0 S 800 #4 ENG DUCT COWL CLOSED IAW 1C-135-2-2-2 PG 20-21 PARA 20.8 A83GC 118D0 S 800 REMOVED 1 EA WARNING TAG AND RESET ALL C/B'S IAW LPS-55MXG-0 0-20-1-OFC3 PARA 5.7.3.16.5.1.3.10 A83JE 27A99 X 799 O/C/G WITH MX LOAD HLGNJ 823AC L 940 O/C/G WITH MX LOAD HLGNJ 823AC L 940 RESEATED CABLES ON R/T O/C/G HLGNJ 82LDA L 956 SUPPORTED A/C LAUNCH A83CN 01000 (Null) WORKCARD C/W. NDN. SEE JCN 150260124 WCE 28 AND 29 A83EE 03999 (Null) RH ACM SERVICED IAW 1C-135-2-2-2 PARA 15.96.2 STEP C A83EE 01000 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-144 C/A MDS PWC WUC AT HMAL LH ACM SERVICED IAW 1C-135-2-2-2 PARA 15.96.2 STEP C A83EE 01000 (Null) WORKCARD C/W NDN A83EE 03999 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) ACFT LAV DRAINED A83FL 01000 (Null) PANEL INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) ENG INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) 8 EA SPOILER LOCKS REMOVED IAW 1C-135-2-2-2 PG 14-14 PARA 14.4.4 A83FL 06000 (Null) 8 EA L/E FLAP LOCKS REMOVED IAW 1C-135-2-2-2 PG 14-17 PARA 14.4.6 A83FL 06000 (Null) 5 EA WARNING TAGS REMOVED IAW LPS 55MXG 00-20-1-5.7.3.16.5.1.10 A83FL 01490 (Null) CARDS C/W A83FL 03999 (Null) IPI C/W IAW LPS MXG-1C-135-6WC-OFCI CARD 4022 ITEM 1 A83FL 04199 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) INSPECTION C/W A83GC 03999 (Null) REMOVED AR DOOR LOCK IAW T.O. 1C-135-2-6-1 PARA 23.34.2 STEP 12 A83HY 06000 (Null) C/W 1C-135-6WC-1 CARD 4-019 ITEMS 2 THRU 4 A83HY 03999 (Null) 4 EA WARNING TAGS REMOVED ALL C/B'S RESET IAW 1C-135-2-4-1-1 PG 9-7 PARA 9.3 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED ALL T-HANDLES RESET IAW 1C-135-2-4-1-1 PG 9-7 PARA 9.3 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED ALL C/B'S RESET IAW 1C-135-2-4-1-1 PG 9-7 PARA 9.3 A83JE 06000 (Null) INSP C/W NDN A83JE 03999 (Null) AUDIBLE IGNITION CHK C/W NDN A83JE 04136 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) R2 CONTACTOR IAW ETM-RC135-2-12 DIA 12281-28004K SHT 2 OPS C K GOOD A83EE 42128 R 255 COLD STARTED FMS #1 GPS, SYS OPS CHECK GOOD A83CN 727AB L 255 R2 KEYBOARD O/C/G HLGNJ 82GAJ R 956 FIRST DMCA 1 UP WE HAD RECEIVERS 1 AND 6 COMPLETELY DEAD. RE CEIVER 7 HAD 1 PPS ERROR SPORATICALLY. DOW HLGNJ 81NV0 Y 956 DMCA 1 WOULD NOT RESET AT ALL. SCROLLED ERRORS FOR G3, STAT ING THAT IT WAS FAILING CBIT. ALL MORPH AND HLGNJ 82EA0 Y 956 R2 QUAD PC BOARD O/C/G HLGNJ 823AC R 254 O/C/G W/ MX LOAD HLGNJ 82ADG L 956 30 DAY WASTE SYS C/W A83FL 04199 (Null) INSP C/W A83FL 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-145 C/A MDS PWC WUC AT HMAL INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 4-2 THRU 4-3 STEPS X THRU AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) INSP C/W A83JE 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG. 20-5 PARA 20 .3.2 A83JE 118D0 S 800 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG. 20-5 PARA 20 .3.2 A83JE 118D0 S 800 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG. 20-5 PARA 20 .3.2 A83JE 118D0 S 800 COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG. 20-5 PARA 20 .3.2 A83JE 118D0 S 800 RC-135V, T/N 64-14848, 30 April 2015 U-146 C/A MDS PWC WUC AT HMAL CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 SECT 79-00-00 PG 201 A83JE 27A4D S 800 CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 SECT 79-00-00 PG 201 A83JE 27A4D S 800 CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 SECT 79-00-00 PG 201 A83JE 27A4D S 800 CHIP DETECTORS REINSTALLED IAW 2J-F108-2-1 SECT 79-00-00 PG 201 A83JE 27A4D S 800 FUEL STRAINER REINSTALLED IAW 2J-F108-2-1 SECT 73-11-10 PG 2 01 A83JE 27H99 S 800 FUEL STRAINER REINSTALLED IAW 2J-F108-2-1 SECT 73-11-10 PG 2 01 A83JE 27H99 S 800 FUEL STRAINER REINSTALLED IAW 2J-F108-2-1 SECT 73-11-10 PG 2 01 A83JE 27H99 S 800 FUEL STRAINER REINSTALLED IAW 2J-F108-2-1 SECT 73-11-10 PG 2 01 A83JE 27H99 S 800 INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-175 STEPS 1-5 A83FL 0413C (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) INSP C/W NDN A83JE 04199 (Null) ALL C/BS RESET IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG8-87 PARA 8.25 A83JE 06000 (Null) ALL C/BS RESET IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG 8-87 PARA 8.25 A83JE 06000 (Null) ALL C/BS RESET IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG 8-87 PARA 8.25 A83JE 06000 (Null) ALL C/BS RESET IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG 8-87 PARA 8.25 A83JE 06000 (Null) ALL C/BS RESET IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 AND PG 8-87 PARA 8.25 A83JE 06000 (Null) 2 EA WARNING TAGS REMOVED IAW 1C-135-2-4-1-1 PG 6-18 PARA 6.9.2 A83JE 06000 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) LEAK CHECK C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-147 C/A MDS PWC WUC AT HMAL INSP C/W NDN A83JE 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) R2 BULB OPS CHECK GOOD IAW 1C-135-2-10-1 PG 19-31 PARA 19.24 .4 A83FL 4422A G 80 R2 LIGHT IAW 1C-135-2-10-1-WA-1 PARA 19.21.4 AND 19.21.5 A83FL 44200 R 80 R2 WIDEBAND PROCESSOR CARD O/C/G HLGNJ 82SCD R 956 O/C/G WITH MX LOAD HLGNJ 82SC0 X 799 REBUILT SOFTWARE O/C/G HLGNJ 82EAV L 956 REBUILT SOFTWARE O/C/G HLGNJ 82EAV L 956 REMOVED A/R DOOR LOCK IAW 1C-135-2-10-1 PG 19-31 PARA 19.24.4 STEP 3 A83EE 06000 DUPLICATE DISCREPANCY SEE JCN 150140129 WCE 001 A83CN 727BA X 799 R2 OVERHEAD ANNUNCIATOR CONTROL UNIT IAW ETM-RC135V/W-2 VOL I PG 1-29 PARA 1.2.2.2 OPS CHK DUE SEE THIS A83EE 44127 R 255 RECALIBRATED AUX HEAT PANEL IAW ETM-RC135-2-3 PG 4-44 PARA 4 .1.6.11 OPS CHK GOOD A83EE 51899 L 127 OPS CHECK NOT REQUIRED A83FL 44100 X 799 COULD NOT DUPLICATE, SYSTEM INTERFERENCE DUE TO HIGH ACTIVIT Y IN AREA. ARCEC 81AX1 H 799 POOL UPPED CHANNEL B O/C/G HLGNJ 81RNB X 799 O/C/G W/ MX LOAD HLGNJ 81AP6 X 799 O/C/G W/ MX LOAD HLGNJ 81NZC X 799 STAMPEDING SEROW QRC REMOVED HLGNJ 82ZA0 P 799 TEAPARTY QRC REMOVED HLGNJ 82ZA0 P 799 SUPPORTED A/C LAUNCH. A83CN 01000 (Null) C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PGS 4-2 THRU 4-3 STEPS X-AF A83FL 0413C (Null) ACFT LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) INSPECTION C/W NDN A83EE 41000 X 799 REINSTALLED PNL IAW ETM-RC135-6 P.7-141 PARA 7.1.6.12 A83EE 11PAD S 800 INSP C/W IAW 1C-135-2-4-1-1 PG3-104 STEPS 31-38 A83FL 0413C (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-175 PARA 3.7.12 A83FL 0413C (Null) (Null) RC-135V, T/N 64-14848, 30 April 2015 U-148 C/A MDS PWC WUC AT HMAL INSTALLED WAVEGUIDE IAW ETM-RC135-2-11 PAGE 2-59 PARA 2.6.27 STEP H A83EW 83C99 S 800 WX RADAR R2 IAW ETM-RC135-2-11 PAGE 2-48 PARA 2.6.2 SEE THIS JCN WCE 003 FOR OPS CHECK A83CN 72BA0 R 649 NOSE RADOME REINSTALLED IAW ETM-RC135-2-11 PAGE 2-59 PARA 2. 6.27 A83CN 1111L S 800 RADAR OP CHECK C/W. SYS OP CHECK GOOD. A83CN 72BA0 X 799 INSPECTED CONNECTOR NO DEFECT NOTED A83CN 727BA X 799 RECYCLED SYSTEM POWER, OPS CHK GOOD A83CN 727BA L 255 R2 BULB OPS CHECK GOOD A83EE 4412A G 80 R2 #4 GCU IAW 1C-135-2-10-1 PARA 13.25.2 OPS CHK GOOD NDN A83EE 42930 R 255 R2 OVERHEAD ANN CONTROL UNIN IAW ETM-RC135V/W-2 VOL 1 PARA 1 .2.2.1 OPS CHECK DUE SEE THIS JCN WCE 003 A83EE 42A3F R 255 OPS CHK GOOD ON OVERHEAD ANN CONT UNIT BUT ORIGINAL DEC STIL L EXIST A83EE 42900 X 799 #1 ENGINE COWLING CLOSED IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83EE 118CG S 800 #2 ENGINE COWLING CLOSED IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83EE 118DA S 800 #4 ENGINE COWLING CLOSED IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83EE 118DA S 800 RESET IDG IAW 1C-135-2-10-1 PG 13-3 PARA 13.5.2 STEP 34 OPS CHECK GOOD NDN A83EE 42910 L 127 RESET IDG IAW 1C-135-2-10-1 PG 13-3 PARA 13.5.2 STEP 34 OPS CHECK GOOD NDN A83EE 42910 L 127 SERVICED #4 IDG NDN A83EE 42910 X 799 R2 BULB. OPS CHK GOOD A83EE 42910 G 80 RESET IDG IAW 1C-135-2-10-1 PG 13-3 PARA 13.5.2. STEP 34 OPS CHK GOOD NDN A83EE 42910 L 127 RESET C/B'S RAN SYSTEMS WITH EXT PWR AND GENERATORS DURING E NGINE RUN. ALL SYSTEMS OPERATED NORMALLYA83EE 42199 L 127 CB'S POPPED AND SYSTEM FAILURE ASSOCIATED WITH #2 GEN DISTRI BUTION CB POPPING. RESET CB'S OPS CHK GOOD A83EE 42199 L 127 RAN SYSTEM THROUGH MULTIPLE TIMES LIGHTS NEVER FLICKERED OP S CHECK GOOD A83EE 44210 X 799 CABIN PRESSURE TEST GAUGE REMOVED IAW 1C-135-2-3-2 PG 11-17 PARA 11.1.2 STEP 57 REINSTALLED CAP ON SENSINGA83EE 41120 P 799 REMOUNTED CABIN PRESSURE ALTIMETER IAW 1C-135-2-3-2 PG 11-18 PARA 11.1.2 STEP 61 A83EE 41120 S 800 NO EXCESSIVE WHISTLING 6 SOUND FOUND DURING MULTIPLE ENGINE RUNS AT VARIOUS SETTINGS AND PRESSURIZATIA83FL 41123 X 799 DISCREPANCY ENTERED IN ERROR IAW 00-20-1 PG 4-4 PARA 4.6.6.2 A83GC 51WAA X 799 R2 SCU#2 IAW ETM-RC135-2-11 PG 6-306 PARA 6.24.2 OPS CHECK G OOD A83GC 51WAA R 956 RESEALED #10 AND #11 SPOILER SWIVEL IAW 1C-135-2-8-1 PG 13-1 56 PARA 13.43 LK AND OP CK GOOD A83HY 14APG G 381 CLOSED #6 AND #7 COVE LIP DOORS IAW 1C-135-2-8-1 PG 13-151 P ARA 13.42.3 STEP 6(B) A83HY 14ELS S 800 COWLING CLOSED AND SECURE NDN IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83JE 118D0 S 800 COWLING CLOSED AND SECURE NDN IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83JE 118D0 S 800 COWLING CLOSED AND SECURE NDN IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83JE 118D0 S 800 RECONFIGURED CONTROLLER CARD O/C/G HLGNJ 82CAA L 721 RC-135V, T/N 64-14848, 30 April 2015 U-149 C/A MDS PWC WUC AT HMAL RESEATED RAM O/C/G HLGNJ 82EAG L 956 O/C/G W/ MX LOAD HLGNJ 82SC0 X 799 SUPPORTED A/C LAUNCH A83CN 01000 (Null) 1EA PLUG REM IAW1C-135-2-3-2 PG11-18 PRA11.1.2 ST60 1EA WRNTAG REM IAW LPS-55MXG-00-20-1-OFC3 PRA 5.7.3.16.5A83EE 01490 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PGS 4-2 THRU 4-3 STEPS X-AF A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) 2 EA WARNING TAGS REMOVED IAW 1C-135-2-8-1 PG 13-157 PARA. 13.43.2 STEP(2)(A) A83HY 01490 (Null) SPOILER LOCK REMOVED IAW 1C-135-2-8-1 PG 13-157 PARA 13.43.2 STEP A(1) A83HY 06000 (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 4.1.1 STEPS X-AF A83JE 0413C (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83JE 0413C (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 4.1.1 STEPS X-AF A83JE 0413C (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83JE 0413C (Null) INSP C/W NDN IAW 1C-135-2-4-1-1 PG 3-102 PARA 3.9.2 A83JE 0413C (Null) INSP C/W NDN IAW 1C-135-2-4-1-1 PG 3-175 PARA 3.9.12 A83JE 0413C (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) REMOVED STUCK SCREW ASTMA 11AA0 G 135 REMOVED STUCK SCREW ASTMA 11AA0 G 135 INSP. C/W IAW MB 1RC/TC135-1148 HLGNJ 04199 RECYCLED SYS POWER. SYS OPS CHK GOOD A83CN 727AB L 255 C/W NDN A83EE 41799 X 799 CLOSED PANEL IAW ETM-RC135-2-3 PG 7-141 PARA 7.1.6.12 STEP M A83EE 11PAD S 800 R2 LH FLOW CONTROLLER IAW 1C-135-2-3-2 PG 13-39 PARA 13.14.4 LEAK ABND OPS CHECK GOOD A83EE 41216 R 255 CLOSED CENTER WING ACCESS PANEL IAW 1C-135-2-3-2 PG 13-16 PA RA 13.3 STEP Q A83EE 11PAD S 800 R2 AIRFLOW CONTROLLER IAW 1C-135-2-3-2 PG 13-39 PARA 13.14.4 SEE JCN 150120129008 FOR LEAK AND OPS CHECK A83EE 41216 R 255 REINSTALLED S-DUCT IAW 1C-135-2-3-2 PG 13-70 PARA 13.14.54 S EE JCN 150120129008 FOR LEAK CHECK A83EE 411DA S 800 "T" DUCT RE-INSTALLED IAW 1C-135-2-3-2 A83EE 411B0 S 800 R2 WATER SEPERATOR COALESCER LEAK AND OPS CHECK GOOD SEE THIS JCN WCE 002 FOR MX A83EE 41210 R 230 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-150 C/A R2 LH WATER SEPARATOR SOCK IAW 1C-135-2-3-2 PG 12-37 PARA 12 .3.16 IPI C/W BY MDS PWC WUC AT HMAL IAW 1C-135-2-3-A83EE 41214 R 230 A83EE 41214 L 127 REINSTALLED LH WATER SEPARATOR IAW 1C-135-2-3-2 PG 13-62 PAR A 13.14.36 LEAK AND OPS CHK DUE SEE WCE 006 A83EE 41214 S 800 LH KEEL BEAM BAY CLOSED IAW 1C-135-2-3-2 PG 13-16 PARA 13.3 STEP R A83EE 11400 S 800 LEAK CHK GOOD/OPS CHK BAD. GROUND AIR EJECTOR VALVE REQ'S R2 SEE THIS JCN WCE 007 A83EE 41000 X 799 R2 GROUND EJECTOR VALVE IAW 1C-135-2-3-2 PG 13-63 PARA 13.14 .40 LEAK AND OPS CHECK GOOD A83EE 41221 R 255 LEAK AND OPS CHECK C/W A83EE 41000 X 799 R2 LH PRESSURE REGULATION FOR MX ACTION SEE THIS JCN WCE 007 A83EE 411CE R 255 R2 PRESSURE TRANSDUCER IAW 1C-135-2-3-2 PG 13-41 PARA 13.14. 6 LEAK AND OPS CHK GOOD ORIGINAL DISCREPANCYA83EE 413BH R 255 DISCREPANCY ENTERED IN ERROR IAW 00-20-1 PARA 4.6.6.2 A83EE 411CD X 799 CLOSED CENTER WING PANEL IAW 1C-135-2-3-2 PG 13-13 PARA 13.3 A83EE 118DM S 800 LH S-DUCT REINSTALLED IAW 1C-135-2-3-2 PG 13-70 PARA 13.14.5 4 LEAK CHECK DUE SEE THIS JCN WCE 008 A83EE 411DA S 800 REINSTALLED T-DUCT A83EE 411B0 S 800 R2 LH PRESSURE REGULATOR IAW 1C-135-2-3-2 PG 13-43 PARA 13.1 4.8 OPS CHECK DUE SEE THIS JCN WCE 009 A83EE 411CE R 377 LEAK CHECK GOOD A83EE 41000 X 799 OPS CHK GOOD NDN A83EE 411CE X 799 SYSTEM OPS CHECK GOOD, MISSION SOFTWARE HAD BAD RCS LOAD. ARCEC 81AX1 H 799 WE R2 THE HDP WITH NO CHANGE. FURTHER TROUBLESHOOTING REQUIR ED HLGNJ 82EA0 Y 956 R2 HDP HLGNJ 82EA3 R 721 O/C/G W/MX LOAD HLGNJ 82CA0 X 799 R2 CCA O/C/G HLGNJ 823AC R 721 R2 HLP OCG HLGNJ 82AFL R 254 R2 HLP OCG HLGNJ 82EAP R 254 SUPPORTED A/C LAUNCH. A83CN 01000 (Null) REMOVED 4 EACH WARNING TAGS REMOVED IAW LPS-55MXG-00-20-1-OFC3 PG 2 PARA 5.7.3.16.5.1.3.10 A83EE 01490 (Null) 2 EA WARNING TAGS REMOVED IAW LPS-55 MXG-00-20-1-OFC3 PG 2 PARA 5.7.3.16.5.1.3.10 A83EE 01490 (Null) INSP C/W IAW:21-100 PARA.7.2.1 A83FL 04199 (Null) INSP. C/W IAW: 1C-135-2-4-1-1 PARA.3-104 STEPS.31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) 2 EA C/B COLLARS REMOVED AND BREAKERS RESET IAW 1C-135-2-3-2 PG 13-62 PARA 13.14.36 STEP 20 RC-135V, T/N 64-14848, 30 April 2015 U-151 C/A MDS PWC WUC AT HMAL FDR DOWNLOAD C/W A83GC 04199 (Null) POSTFLIGHT C/W HLGNJ 04199 (Null) POST FLIGHT COMPLIED WITH HLGNJ 04199 (Null) CURE CHECK GOOD A83FL 11140 X 799 PILOTS #3 WINDOW R2 IAW 1C-135-2-2-2 PARA 19.41 PG 19-155 OP S CHECK GOOD A83FL 11140 R 846 INSP C/W IAW 1C-135-2-4CL-1-1 PGS 4-2 THRU 4-3 STEPS X-AF A83FL 0413C (Null) INSP C/W IAW 1C-135-2-4CL-1-1 PG 7-1 PARA 7.1 A83FL 0413C (Null) 28 DAY FMS UPDATE C/W A83CN 727AB L 944 RADOME REMOVED BY DEPOT TEAM AND TAKEN TO FAB SHOP FOR PAINT ING A83FL 1111J P 425 ANTENNA RADOME INSTALLED AND SEALED WITH B&1/2 A83FL 1111J Q 799 C/W NDN A83EE 41799 X 799 CLOSED PANEL IAW ETM-RC135-2-3 PG 7-141 PARA 7.1.6.12 STEP M A83EE 11PAD S 800 JOB ENTERED IN ERROR SEE JCN 150070072 A83FL 04199 (Null) SHARKBYTE II ANTENNA INSTALLATION C/W I.A.W MB 1RC/TC135-11 75 ADD01 04199 (Null) W/B C/W IAW 1-1B-50 PG 4-1 PARA 4-5.1.3 AMXQI 04199 (Null) INSPEC C/W NDN A83JE 04199 (Null) INSPEC C/W NDN IAW 1C-135-2-4-1-1 A83JE 04199 (Null) INSPEC C/W NDN IAW 1C-135-2-4-1-1 PARA 3.2.4 A83JE 0413C (Null) INSPEC C/W NDN IAW 1C-135-2-4-1-1 PARA 3.9.12 PG 3-175 A83JE 0413C (Null) ROUTINE INSP ON LEFT AND RIGHT MLG ACTUATUORS IAW TCTO 1C-1 35-WA-1-1892 NO CRACKS FOUND A83HY 04199 (Null) INSP C/W NDN A83EE 41799 X 799 REINSTALLED PANEL IAW 1-1A-8 PARA 10.2 A83EE 11PAD S 800 TAPE REMOVED IAW ETM-RC135-2-11 PG 5-386 PARA 5.48.4 A83GC 51132 L 753 TTU 205 DISCONNECTED IAW ETM-RC135-2-11 PG 5-386 PARA 5.48.4 A83GC 51132 L 870 120 GPS INTERNAL BATTERY REPLACEMENT C/W A83CN 04199 (Null) NEW GPS LABEL INSTALLATION C/W A83CN 04199 (Null) SUPPORTED A/C LAUNCH A83CN 01000 (Null) R2 C/B OPS CHECK GOOD A83CN 42299 R 255 RESEATED CONNECTOR OCG HLGNJ 82CAA L 730 RESEATED ACFT LAN CABLE O/C/G HLGNJ 82CAB L 721 INSP. C/W IAW:21-100 PARA.7.2.1 A83FL 04199 (Null) INSP. C/W IAW: 1C-135-2-4-1-1 PARA.3-104 STEPS.31-38 A83FL 0413C (Null) RC-135V, T/N 64-14848, 30 April 2015 U-152 C/A MDS PWC WUC AT HMAL C/W A83FL 01000 (Null) INSP. C/W IAW:21-100 PARA.7.2.1 A83FL 04199 (Null) INSP. C/W IAW: 1C-135-2-4-1-1 PARA.3-104 STEPS.31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) C/W NDN A83EE 41799 X 799 CLOSED PANEL IAW 1-1A-8 CH 10 PARA 10.2 A83EE 11PAD S 800 EVIDENCE OF RESIDUAL FUEL UNDER #4 CTW CAVITY FLOOR BOARDS/F UEL REMOVED ZERO SIGNS OF INTEGRAL AND B AFUEL 46440 X 799 REMOVED AND REINSTALLED ACCESS DOOR IAW 1C-135-2-5-3 PARA 14 .11 PG 14-16 AFUEL 46453 S 800 REMOVED AND REINSTALLED ACCESS DOOR IAW 1C-135-2-5-3 PARA 14 .9 PG 14-15 AFUEL 46336 S 800 REMOVED AND REINSTALLED ACCESS DOOR IAW 1C-135-2-5-3 PARA 14 .9 PG 14-15 AFUEL 46347 S 800 INSPECTED AREA LEAK CHECK GOOD AFUEL 46440 X 799 INSPECTED AREA LEAK CHECK GOOD AFUEL 46440 X 799 REMOVED AND REINSTALLED CTW#4 FLOOR BOARD IAW 1C-135-2-5-3 PARA 23.13 PG 23-35 AFUEL 46440 S 800 REMOVED AND INSTALLED CTW #4 IAW 1C-135-2-5-3 PARA 23.13 PG 23-34 AFUEL 46440 R 381 INSPECTED AREA LEAK CHECK GOOD AFUEL 46440 X 799 INSP C/W A83FL 04199 (Null) FUEL CELL MAINT. C/W 5 EA WARNING TAGS REMOVED IAW 1C-135-2-5-3 PARA 14.44 PG 14-47 AFUEL 01490 (Null) FUEL CELL MAINT. C/W LN-120 COLLAR REMOVED IAW 1C-135-2-5-3PARA 14.44 PG 14-47 AFUEL 01000 (Null) FUEL CELL MAINT. C/W 8 EA C/B'S RESET IAW 1C-135-2-5-3 PARA 14.44 PG 14-47 AFUEL 01000 (Null) IPI C/W PRIOR TO TANK CLOSURE IAW 1C-135-2-5-3 PARA 1.3.45 PG 1-47 STEPS A-C AFUEL 04199 (Null) -6 INSPECTION C/W PRIOR TO TANK CLOSURE AFUEL 04199 (Null) IPI C/W PRIOR TO TANK CLOSURE IAW 1C-135-2-5-3 PARA 1.3.45 PG 1-47 STEPS A-C AFUEL 04199 (Null) -6 INSPECTION C/W PRIOR TO TANK CLOSURE AFUEL 04199 (Null) IPI C/W PRIOR TO TANK CLOSURE IAW 1C-135-2-5-3 PARA 1.3.45 PG 1-47 STEPS A-C AFUEL 04199 (Null) -6 INSPECTION C/W PRIOR TO TANK CLOSURE AFUEL 04199 (Null) IPI C/W PRIOR TO CELL BE INSTALLED FOR CAVITY PREP IAW1C-135-2-5-3 PARA 1.3.45 PG 1-47 AND PG 23-35 PARA 23.13AFUEL 04199 (Null) WEATHER DOOR REINSTALLED IAW 1C-135-2-2-2 PG 18-238 PARA 18. A83FL 11370 S 800 WRITE UP ENTERED IN ERROR IAW 00-20-1 PG 4-4 PARA 4.6.5 A83FL 42143 X 799 ACCOMPLISH NAVIGATOR ALTIMETER REPLACEMENT A83GC 04199 (Null) LEFT STATIC BOOM TAPED TO FOM A83GC 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-153 C/A MDS PWC WUC AT HMAL TTU 205 CONNECTED TO FOM A83GC 04199 (Null) C/W NDN A83EE 41799 X 799 CLOSED FUEL CELL 0 IAW 1-1A-8 CHAPTER 10 PARA 10.2 A83EE 11PAD S 800 REMOVED ACTUATOR ROLLER. IAW 1C-135-2-2-2, PARA. 1.12 A83EE 1134W T 875 INSTALLED NEW CARGO DOOR ACTUATOR; OPS CK GOOD IAW 1C-135-2- 2-2 PARA 18.7 A83EE 1134W U 875 MAIN BATT RECONNECTED IAW 1C-135-6WC-3 CARD 5-001 A83FL 42143 X 799 JFS BATT RECONNECTED IAW 1C-135-6WC-3 CARD 5-001 A83FL 42143 X 799 PWR RUDDER S/O VALVE OPENED IAW 1C-135-2-2-2 PG 14-21 PARA 1 4-4-10 A83FL 14BJM S 800 10 EA C/L/D CLOSED IAW 1C-135-2-8-1 PG 14-69 PARA 14.13.4 A83FL 14EL0 X 799 FAN COWL CLOSED IAW 1C-135-2-2-2 PG 20-5 PARA 20.3.2 A83FL 118D0 X 799 FAN COWL CLOSED IAW 1C-135-2-2-2 PG 20-5 PARA 20.3.2 A83FL 118D0 X 799 FAN COWL CLOSED IAW 1C-135-2-2-2 PG 20-5 PARA 20.3.2 A83FL 118D0 X 799 FAN COWL CLOSED IAW 1C-135-2-2-2 PG 20-5 PARA 20.3.2 A83FL 118D0 X 799 FAN DUCT CLOSED IAW 1C-135-2-2-2 PG 20-22 PARA 20.8.2 A83FL 118D0 X 799 FAN DUCT CLOSED IAW 1C-135-2-2-2 PG 20-22 PARA 20.8.2 A83FL 118D0 X 799 FAN DUCT CLOSED IAW 1C-135-2-2-2 PG 20-22 PARA 20.8.2 A83FL 118D0 X 799 FAN DUCT CLOSED IAW 1C-135-2-2-2 PG 20-22 PARA 20.8.2 A83FL 118D0 X 799 RT KEEL BEAM BAY DOOR RAISED IAW 1C-135-2-2-2 PG 18-246 PARA 18.98 STEP 8 A83FL 11430 L 127 LT KEEL BEAM BAY DOOR RAISED IAW 1C-135-2-2-2 PG 18-246 PARA 18.98 STEP 8 A83FL 11430 L 127 STAB TRIM PANEL INSTALLED IAW 1C-135-2-8-1 PG 15-1 PARA 15.4 .2 A83FL 11EAE L 127 REINSTALLED KICK PLATES IAW 1C-135-2-2-2 PG 1-61 PARA 1.12 A83FL 12B99 S 800 KICK PLATES REINSTALLED IAW 1C-135-2-2-2 PG 1-61 PARA 1.12 A83FL 12B99 S 800 HORSESHOE PANEL REINSTALLED IAW 1C-135-2-7-1 PG 7-119 PARA 8 .23.2 A83FL 13FBV S 800 LOX PANELS REINSTALLED IAW 1C-135-2-2-2 PG 1-61 PARA 1.12 A83FL 12B99 S 800 CARGO DOOR FLOOR BOARDS REINSTALLED IAW 1C-135-2-2-2 PG 1-61 PARA 1.12 A83FL 11114 S 800 WEATHERDOOR REINSTALLED IAW 1C-135-2-2-2 PG 18-238 PARA 18.9 4 A83FL 11370 S 800 LAV SHROUD REINSTALLED IAW 1C-135-2-2-2 PG 17-146 PARA 17.67 .2 STEP 14 A83FL 12J99 S 800 4EA WARNING TAGS REMOVED IAW LPS-55-MXG-00-20-1 OFC 3 PARA 5.7.3.16.5.1.3.10 A83FL 01490 (Null) 8EALOCKS REMOVEDIAW 1C-135-2-2-2PG14-14 PARA14.14.4 3EAWARNINGTAGSREMOVED IAWLPS55MXG-00-20-1 OFC3PA A83FL 06000 (Null) RUDDER LOCK REMOVED IAW 1C-135-2-2-2 PG 14-17 PARA 14.4.10 A83FL 06000 (Null) 8EALOCKSREMOVED IAW 1C-135-2-2-2PG14-17 PARA 14.4.6 1EAWARNIGNTAG REMOVEDIAW LPS-55-MXG00-20-1OFC3PARA83FL 06000 (Null) STABTRIM LOCKREMOVEDIAW1C-135-2-2-2PG 16-18 PARA16.5ST18 5EAWARNINGTAGS REMOVEDIAWLPS55MXG-00-20-1 OA83FL 06000 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-154 C/A MDS PWC WUC AT HMAL ACFT PROTECTIVE COVERS REMOVED IAW 1C-135-6WC-3 PG 5-001 STEP 3 A83FL 01000 (Null) ACFT LUBED IAW 1C-135-6WC-3 CARDS 5-001 THRU 5-049 A83FL 02110 (Null) FOIL REMOVED IAW 1C-135-6WC-3 CARD 5-001 A83FL 02100 (Null) IPI C/W SCH100 GREASE APP TO MLG BRAKE COLLAR IAW 1C-135-6WC-3 CRD 5-044 IPI BY A83FL 02100 (Null) MAIN/JFS BATTS RECONNECTED IAW 1C-135-2-10-1 PG 15-32 PARA 15.24 A83FL 02110 (Null) INSTALLED 2EA JACK PAD ACCESS PANELS IAW 1C-135-2-2CL-3 PG 6 -2 PARA 6.2 AINAR 11310 S 800 REMOVED STUCK SCREW. ASTMA 11310 G 135 ACFT WASHED A83FL 02100 (Null) ACFT LUBED A83FL 02110 (Null) C/W MINOR CCI AS REQUIRED ACOCO 04221 (Null) DOWN JACKED ACFT IAW 1C-135-2-2CL-3 PG 6-2 PARA 6.2 AINAR 01000 (Null) REMOVED 1EA JACK PAD IAW 1C-135-2-2CL-3 PG 6-2 PARA 6.2 AINAR 01000 (Null) ENSURED LANDING GEAR HANDLE WAS IN DOWN AND LOCKED DETENTIAW 1C-135-2-2-2 PG 1-60 PRAR 1.10 STEP K AINAR 04199 (Null) C/W 28D FMS UPDATE A83CN 727AB L 944 RT OVER WING HATCH SEAL REPLACED IAW 1C-135-2-2-2 PG 18-203 PARA 18.81 A83FL 11360 R 20 CURE CHECK GOOD A83FL 11360 X 799 UNSEATED JACKS IAW 1C-135-2-2-2 PG 8-2 PARA 8.2 AINAR 01000 (Null) 2EA PADS REMOVED IAW 1C-135-2-2-2 PG 8-2 PARA 8.2 AINAR 01000 (Null) ACCOMPLISHED ANTENNA LEADING EDGE TAPE REPLACEMENT HLGNJ 04199 (Null) LK AND OPS CK ON NLG LOCK RETENTION ACT GOOD IAW TO 1C-135-2 -7-1 PG 7-87 PARA 7.15.4 A83HY 13GAG X 799 CLOSED #2 COWLING IAW TO 1C-135-2-2-2 PG 20-4 PARA 20.3 A83HY 118D0 S 800 HYD MULE HT08 DISCONNECTED IAW TO 1C-135-2-2-2 PG 14-154 PAR A 14.38 A83HY 01000 (Null) IPI TO ENSURE LANDING GEAR LEVER IS RETURNED TO DOWN ANDLOCKED C/W IAW TO 1C-135-2-7-1 PG 7-87 PARA 7.15 A83HY 04199 (Null) MODE IV/ MODE C CHECK C/W A83CN 04MD4 (Null) RECORDS CHECK C/W A83FL 07000 (Null) RECONNECTED LN-120 BATTERY IAW ETM-RC135-2-11 PG 5-108A PARA 5.7.1.8 SYS OP CK GOOD A83CN 72XD0 S 800 REMOVED WARNING TAGS IAW LPS-55MXG-00-20-1-OFC3 PARA 5.7.3.1 6.5.1.3.10 A83CN 72XD0 X 799 REINSTALLED PUZZLE BRACKET IAW 1C-135-2-3-2 PG 13-65 PARA 13 .42 LEAK CHK DUE SEE THIS JCN WCE 042 A83EE 4123G S 800 REINSTALLED RH ACM LIMIT VLV IAW 1C-135-2-3-2 PG 13-49 PARA 13.14.26 LEAK AND OPS CHK DUE SEE THIS JCN WCE 0A83EE 4123G S 800 REINSTALLED SENSING LINES IAW 1C-135-2-3-2 PG 13-49 PARA 13. 14.26 LEAK CHK DUE SEE THIS JCN WEC 042 A83EE 4123G S 800 REINSTALLED DUCTING IAW 1C-135-2-3-2 PG 13-65 PARA 13.14.42 LEAK CHK DUE SEE THIS JCN WCE 042 A83EE 411DA S 800 LEAK AND OPS CHK BAD. DUCTS REQ REALIGNMENT DUE TO LEAKING P ACK. SEE THIS JCN WCE 043 A83EE 41000 X 799 RC-135V, T/N 64-14848, 30 April 2015 U-155 C/A MDS PWC WUC AT HMAL REALIGNED PUZZLE BRACKET DUCTS IAW 1C-135-2-3-2 PG 13-65 PAR A 13.42 LEAK CHK DUE SEE THIS JCN WCE 044 A83EE 41000 L 127 LEAK AND OPS CK GOOD ON RH PACK IAW 1C-135-2-3-2 PARA 13.3.2 .2 A83EE 4123G X 799 REINSTALLED RH PUZZLE BRACKET IAW 1C-135-2-3-2 PARA 13.14.42 LK AND OPS CK DUE SEE THIS JCN WCE 044 A83EE 411DA S 800 REINSTALLED RH ACM LIMIT VALVE IAW 1C-135-2-3-2 PARA 13.14.2 5 LK AND OPS CK DUE SEE THIS JCN WCE 044 A83EE 4123G S 800 REINSTALLED RH ACM LIMIT VALVE SENSING LINES IAW 1C-135-2-3- 2 PARA 13.14.42 STEPS 29-31 LK AND OPS CK DUE S A83EE 4123G S 800 REINSTALLED RH PRIMARY HEAT EXCHANGER IAW 1C-135-2-3-2 PARA 13.14.42 LEAK AND OPS CK DUE SEE THIS JCN WCEA83EE 411DA S 800 INSTALLED CAP NDN A83EE 41499 R 70 MAIN BATT RECONNECTED IAW 1C-135-2-10-1 PG 15-32 PARA 15.24. 1 A83FL 42149 X 799 JFS BATT RECONNECTED IAW 1C-135-2-10-1 PG 15-32 PARA 15.24.1 A83FL 42149 X 799 PANEL REINSTALLED IAW TO 1-1A-8 PG 2-1 PARA 2.1 A83FL 11300 X 799 CONNECTED MAIN BATT IAW 1C-135-2-10-1 PG 15-32 PARA 15.24.1 A83FL 42143 S 800 JFS BATT RECONNECTED IAW 1C-135-2-10-1 PG 15-32 PARA 15.24.1 A83FL 42143 S 800 DISCREPANCY ENTERED IN ERROR IAW LPS 55 MXG 00-20-1 OFC3 P5- 7 PAR 5.7.3.16.5.1.3.9 (SEE JCN 143386500002) A83HY 13GAG X 799 NLG LOCK RET ACT REM IAW 1C-135-2-7-1 P 7-84 PARA 7.14 INSTA LL REQD (SEE P 28 I 1) (SEE THIS JCN WCE 002) FOR A83HY 13GAG T 875 INSTALLED NLG LOCK RETENTION ACT IAW 1C-135-2-7-1 PG 7-87 PA RA 7-15 LK AND OPS CK DUE SEE JCN 133436405 A83HY 13GAG U 875 LEAK CHECK BAD REQUIRES FURTHER TROUBLESHOOTING AFUEL 46440 X 799 REMOVED AND REINSTALLED CAVITY DRAIN LINES IAW 1C-135-2-5-3 PAGE 20-8 PARA 20.8 AFUEL 46440 S 800 LEAK CHECK BAD REQUIRES FURTHER TROUBLE SHOOTING AFUEL 46440 X 799 REPAIRED FAULTY SEALANT IAW TO 1-1-3 PAGE 6-10 PARA 6.7.2.2 AFUEL 46440 G 381 REMOVED AND REINSTALLED ACCESS DOOR IAW 1C-135-2-5-3 PAGE 14 -5 PARA 14.9 AFUEL 46453 S 800 REMOVED AND REINSTALLED ACCESS DOOR IAW 1C-135-2-5-3 PAGE 14 -15 PARA 14.9 AFUEL 46453 S 800 REMOVED AND REINSTALLED ACCESS DOOR IAW 1C-135-2-5-3 PAGE 14 -16 PARA 14.11 AFUEL 46453 S 800 8 EA INTERCONNECTS IN #4 CTW BOLTS REINSTALLED IAW 1C-135-2- 5-3 PG 13-253 PARA 13.6.40 AFUEL 46400 S 800 8EA INTERCONNECTS REINSTALLED IAW 1C-135-2-5-3 PG 13-253 PAR A 13.6.42 AFUEL 46400 S 800 ALL PLUMBING AND ASSOCIATED HARDWARE REMOVED AND REINSTALLED IAW 1C-135-2-5-3 PAGE 23-53 PARA 23.17 AFUEL 46400 S 800 REMOVED AND REINSTALLED #6 CTW CELL IAW 1C-135-2-5-3 PAGE 23 -53 PARA 23.17 AFUEL 46400 S 800 INSPECTED AREA REMOVED 8 EA PRESSURE PLATES IAW 1C-135-2-5-3 PG 13-255 PARA 13.6.42 AFUEL 46400 X 799 INSPECTED AREA REMOVED 8 EA PRESSURE PLATES IAW 1C-135-2-5- 3 PG 13-255 PARA 13.6.42 AFUEL 46400 X 799 INSPECTED AREA REMOVED 10 EA PRESSURE PLATES IAW 1C-135-2-5 -3 PG 13-255 PARA 13.6.42 AFUEL 46400 X 799 PRESSURE EQUIPMENT REMOVED IAW TO 1C-135-2-5-3 PG 13-255 PAR A 13.6.42 AFUEL 46400 X 799 INSPECTED DRAIN LINES LEAK CHECK BAD ON #4 CTW CELL SEE NEW JCN 143530020. AFUEL 46400 X 799 LK CK C/W NO LEAK NOTED AFUEL 46453 X 799 RC-135V, T/N 64-14848, 30 April 2015 U-156 C/A MDS PWC WUC AT HMAL RE-LACE AND SECURED #5 CENTER WING CELL IAW 1C-135-2-5-3 PAR A 23.15.13 PG 23-44 AFUEL 46440 S 800 CAVITY PREP C/W IAW 1C-135-2-5-3 PAGE 24-3 PARA 24.8 AFUEL 46440 X 799 REMOVED AND REINSTALLED FLOOR BOARDS IAW 1C-135-2-5-3 PARA 2 4.8 PAGE 24-3 AFUEL 46440 S 800 SAFETY WIRE INSTALLED IAW TO 1C-135-2-5-3 PARA 13.6.42 PG 13 .255 AFUEL 46440 G 20 INSTALLED SLIMSERT AS REQ AMETE 46000 G 105 INSERT INSTALLED AS REQUIRED AMETE 46440 F 20 REPLACED NUTPLATE ASTMA 46000 G 105 CLOSED RT KEEL BEAM BAR DOOR IAW 1C-135-2-3-2PARA13.14.42STEP 33 A83EE 01000 (Null) 2EA WARNING TAGS REMOVED IAW LPS-55MXG-00-20-1OFC3 PARA 5.7.3.16.5.1.3.10 A83EE 01490 (Null) FUEL RECONFIGURED FOR FLIGHT IAW 1C-135-5-1 CHART C APPENDIX J-5 A83FL 01000 (Null) 4EA WARNING TAGS REMOVED IAW 1C-135-2-10-1 PG 15-32 PARA 15.24.1 A83FL 01490 (Null) WARNING TAGS REMOVED IAW 1C-135-2-10-1 PF 15-32 PARA 15.24.1 STEPS 3,6,7 A83FL 01490 (Null) 1 EA WARNING TAG REMOVED IAW LPS-55MXG-00-20-1-OFC3 PARA 5.7.3.16.5.1.3.10 PG 4 A83HY 01490 (Null) IPI C/W NO DEFECTS NOTED IAW 1C-135-2-5-3 PAGE 1-54 PARA 1.3.45 STEPS A-C AFUEL 04199 (Null) -6 INSPECTION C/W NO DEFECTS NOTED AFUEL 04199 (Null) IPI C/W NO DEFECTS NOTED IAW 1C-135-2-5-3 PAGE 1-54 PARA 1.3.45 STEPS A-C AFUEL 04199 (Null) -6 INSPECTION C/W NO DEFECTS NOTED AFUEL 04199 (Null) IPI C/W NO DEFECTS NOTED IAW 1C-135-2-5-3 PAGE 1-54 PARA1.3.45 STEPS A-C AFUEL 04199 (Null) -6 INSPECTION C/W NO DEFECTS NOTED AFUEL 04199 (Null) POSITION 23 FOOR SWITCH SCREW REPLACED A83CN 647M0 G 105 R2 LH FLOW CONTROLLER SEE THIS JCN WCE 007 FOR MX ACTION. O PS CK GOOD IAW 1C-135-2-3-2 PARA 13.3.2.1 A83EE 41216 R 255 CLOSED CENTER WING ACCESS PANEL IAW 1C-135-2-3-2 PARA 13.14. 64 STEP 7 A83EE 11AT0 S 800 REINSTALLED T DUCT A83EE 411B0 S 800 REINSTALLED S DUCT IAW 1C-135-2-3-2 PG 13-70 PARA 13.14.54 L EAK AND OPS CHECK DUE SEE THIS JCN WCE 008 A83EE 411DA S 800 R2 AIRFLOW CONTROLLER IAW 1C-135-2-3-2 PG 13-39 PARA 13.14.4 LEAK AND OPS CHECK DUE SEE THIS JCN WCE 008 A83EE 41216 R 255 LEAK AND OPS CHK BAD. DUCTS REQ REALIGNMENT DUE TO LEAKING. SEE THIS JCN WCE 009 A83EE 41000 X 799 REALIGNED DUCTS IAW 1C-135-2-3-2 PG 13-70 PARA 13.14.54 LEAK CHECK DUE SEE THIS JCN WCE 010 A83EE 41216 L 127 LK AND OPS CK GOOD ON LH PACK IAW 1C-135-2-3-2 PARA 13.3.2.1 NDN A83EE 41216 X 799 R2 CLAMP OPS CHECK GOOD A83EE 411DC R 70 R2 BULB A83EE 44131 G 80 PANEL REINSTALLED IAW TO 1-1A-8 PG 2-1 PARA 2.1 A83FL 11310 X 799 PANEL REINSTALLED IAW TO 1-1A-8 PG 2-1 PARA 2.1 A83FL 11310 X 799 RC-135V, T/N 64-14848, 30 April 2015 U-157 C/A MDS PWC WUC AT HMAL R2 #2APC IAW ETM-RC135-2-11 PAGE 6-207 PARA 6.12.6 OPS CHK G OOD A83GC 51S00 R 956 INSTALLED HYDRO LINES IAW 1C-135-2-6-1 PG 22-26 PARA 22.11.4 LK AND OPS CK DUE SEE PG 25 BLK 3 A83HY 4511T S 800 LEAK CHECK GOOD A83HY 46736 X 799 LK CK GOOD A83HY 4511T X 799 CLOSED AND SECUERED COWLING IAW 1C-135-2-2-2 PAG 20-4 PAR 20 .3 A83HY 118D0 S 800 FWD BODY A/R PUMP CHECK BAD REQUIRES R2 AFUEL 46410 F 8 REMOVED AND REPLACED FWD BODY FWD AR PUMP IAW 1C-135-2-6-1 P AGE 22-21 PARA 22.11 AFUEL 46711 R 70 REMOVED AND REINSTALLED FWD BODY #3 ACCESS DOOR IAW 1C-135-2 -6-1 PAGE 22-28 PARA 22.11.5 STEP 4 ACTUAL CAFUEL 46410 S 800 LK AND OPS CK C/W NO DEFECT NOTED AFUEL 46410 X 799 REPLACED RIVNUT ASTMA 46410 G 105 TEA PARTY REMOVED HLGNJ 81GQ0 P 799 STAMPEDING SEROW REMOVED HLGNJ 81GQ0 P 799 R2 SCREWS HLGNJ 81ZJ0 G 105 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-48 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) 1 EA WARNING TAG REMOVED IAW LPS-55MXG-00-20-1-OFC3 PARA5.7.3.16.5.1.3.10 PG 4 A83HY 01490 (Null) MULE DISCONNECTED IAW 1C-135-2-2-2 PAG 14-158 PAR 14.38 A83HY 06000 (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 4-3 STEPS X-AF A83JE 0413C (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 7-1 PA 7.1 A83JE 0413C (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 4-3 STEPS X-AF A83JE 0413C (Null) INSP C/W NDN IAW 1C-135-2-4CL-1-1 PG 7-1 PA 7.1 A83JE 0413C (Null) 5 EA WARNING TAGS REMOVED IAW 1C-135-2-5-3 PAGE 14-47 PARA 14.44 AFUEL 01490 (Null) RESET CB IAW 1C-135-2-5-3 PAGE 14-47 PARA 14.44 AFUEL 01000 (Null) 9 EA CBS RESET IAW 1C-135-2-5-3 PAGE 14-47 PARA 14.44 STEP 8 AFUEL 01000 (Null) IPI C/W NO DEFECTS NOTED IAW 1C-135-2-5-3 PARA 1.3.45 STEPS A-C AFUEL 04199 (Null) -6 INSPECTION C/W NO DEFECTS NOTED AFUEL 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-158 C/A MDS PWC WUC AT HMAL LK CK C/W NO LEAK NOTED AFUEL 04199 (Null) POST FLIGHT NOT REQ'D HLGNJ 04199 (Null) CTW FUEL LEAK EVALUATION C/W NO DEFECTS NOTED AFUEL 46440 X 799 8HR LEAK CHECK ON CTW AFTER REFUEL C/W NO DEFECTS NOTED AFUEL 46440 X 799 CTR WING CAVITY DRAIN LINES 4, 5, 6 AND COMMON RECONNECTED IAW 1C-135-2-5-3 PARA 20.8.1 PAGE 20-8 AFUEL 46440 S 800 RAISED ALL COVE LIP DOORS IAW IC-135-6WC-1 CARD 4-002 AISOD 14EL0 Q 800 RAISED ALL COVE LIP DOORS IAW IC-135-6WC-1 CARD 4-002 AISOD 14EL0 Q 799 ACCESS PANEL INSTALLED IAW 1C-135-2-8 PG 15-7 PARA 15.14.14 AISOD 1151E S 800 LT ACM DRAINED AND SERVICED IAW TO 1C-135-2-2-2 PAGE 15-602 PARA 15.95 AISOD 4123P X 799 CLOSED DOOR IAW 1C-2-2-2 PG 15-611 STEP 4 AISOD 11430 X 799 RT ACM DRAINED AND SERVICED IAW TO 1C-135-2-2-2 PAGE 15-602 PARA 15.95 AISOD 4123P X 799 CLOSED DOOR IAW 1C-2-2-2 PG 15-611 STEP 4 AISOD 11430 X 799 DRAINED AND RESERVICED JFS STARTER IAW 1C-135-2-4-1-1, PG. 8 -72 - 8-73 PARA. 8-27 AISOD 27CBF X 799 AUDIBLE IGNITION C/W SEE JCN 143350197001 AISOD 27CA0 X 553 CLOSED #1 ENG FAN COWL IAW 1C-135-2-2-2, PG 20-4, PARA. 20.3 AISOD 118D0 S 800 CLOSED #1 ENG. FAN DUCT IAW 1C-135-2-2-2, PG. 20-21, PARA. 2 0.8 AISOD 118D0 S 800 CLOSED #2 ENG FAN COWL IAW 1C-135-2-2-2, PG 20-4, PARA. 20.3 AISOD 118D0 S 800 CLOSED #2 ENG. FAN DUCT IAW 1C-135-2-2-2, PG. 20-21, PARA. 20.8 AISOD 118D0 S 800 CLOSED #3 ENG FAN COWL IAW 1C-135-2-2-2, PG 20-4, PARA. 20.3 AISOD 118D0 S 800 CLOSED #3 ENG. FAN DUCT IAW 1C-135-2-2-2, PG. 20-21, PARA. 20.8 AISOD 118D0 S 800 CLOSED #4 ENG FAN COWL IAW 1C-135-2-2-2, PG 20-4, PARA. 20.3 AISOD 118D0 S 800 CLOSED #4 ENG. FAN DUCT IAW 1C-135-2-2-2, PG. 20-21, PARA. 20.8 AISOD 118D0 S 800 LT MLG STRUT INFLATED IAW 1C-135-2-2-2 PG 15-535 PARA 15-77 AISOD 13AB0 X 799 RT MLG STRUT INFLATED IAW 1C-135-2-2-2 PG 15-535 PARA 15-77 AISOD 13AB0 X 799 NLG STRUT SERVICED IAW 1C-135-2-2-2 PG15-567 PAR 15.85 AISOD 13FC0 X 799 60 DAY HPO CW IAW IC-135-6WC-1 AISOD 03300 (Null) 60 DAY HPO CW IAW ETM-RC135-6WC-1 AISOD 03300 (Null) REMOVED LEADING EDGE FLAP LOCKS AND REMOVED 1 EA WARING TAG FROM FLAP HANDLE IAW IC-135-2-2-2 PARA 14.4AISOD 01490 (Null) REMOVED SPOILER LOCKS AND REMOVED 3 EA WARNING TAGS FROM I/B AND O/B CUTOUT AND SPOILER HANDLE IAW ICAISOD 01490 (Null) REMOVED 8 EA LEADING EDGE FLAP LOCKS IAW IC-135-2-2-2 PARA 14.4.6 PAGE 14-17 AISOD 06000 (Null) REMOVED ALL SPOILER LOCKS IAW IC-135-2-2-2 PARA 14.4.4 PAGE 14-14 AISOD 06000 (Null) ARR DOOR LOCK RMVD IAW 1C-135-2-2-2 PG 14-18 PAR 14.4.8 AISOD 06000 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-159 C/A MDS PWC WUC AT HMAL REMOVED 3 CIRCUIT BREAKER COLLARS IAW 1C-135-2-2-2 PG 14-18 PARA 14.4.8 STEP 2 AISOD 06000 (Null) 2 WARNING TAGS REMOVED IAW 1C-135-2-2-2 PG 14-18 PARA 14.4.8 AISOD 01490 (Null) STAB TRIM LOCK REMOVED IAW 2 1C-135-2-2-2 PG 14-18 PARA 14.4.8 AISOD 06000 (Null) REMOVED 1 EA. C/B SAFETY LOCK IAW 1C-135-2-4-1-1, PG. 8-73, PARA. 8-27, STEP Q AISOD 01490 (Null) 4 EA C/B SAFTY LOCKS REMOVED C/B RESET IAW 1C-135-2-4-1-1 PARA 9.3 PG 9-1 AISOD 06000 (Null) WRITE UP ENTER IN ERROR IAW 00-20-1 PAGE 4-4 PARA 4.6.6.2 AISOD 01490 (Null) 4 EA C/B SAFTY LOCKS REMOVED C/B RESET IAW 1C-135-2-4-1-1 PARA 9.3 PG 9-1 AISOD 06000 (Null) 60 DAY HPO INSP C/W IAW ETM=RC135-6WC-1 CARD 6-001 ARCEC 03300 (Null) POST FLIGHT C/W HLGNJ 03300 (Null) HPO C/W HLGNJ 03300 (Null) TIGHTENED LOOSE SCREW ON PILOTS YOKE MIC SWITCH. SYS OP CHK GOOD A83CN 647N0 L 693 R2 LN100 INU IAW ET-RC135-2-11 PG 5-154 PARA 5.13.4 SYS OP C K GOOD A83CN 727BA R 652 RECYCLED SYS POWER OPS CHK GOOD. A83CN 72XA0 L 255 REMOVED AND REPLACED IGNITION LEAD IAW 2J-F108-2-1 WP 74-71- 20 PG 201 PARA 2 C(2) & EXCITER BOX IAW 2J-F10 AISOD 27CAB R 70 AUDIBLE IGNITION SYSTEM CHECKOUT C/W AISOD 27CAB X 799 INSTALLED BUSHINGS AISOD 27CAB G 105 INSPECTED AND NO REPAIR REQ ASTMA 14CE0 G 780 SUPPORTED A/C LAUNCH A83CN 01000 (Null) INSP CW IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 31-38 A83FL 0413C (Null) LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-108 STEPS 35-38 A83FL 0413C (Null) LAV SERVICED A83FL 01000 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) REMOVED 4 EA SAFETY LOCKS IAW 1C-135-2-4-1 PG 9-5 PARA 9.3.3 STP 15 AISOD 06000 (Null) REMOVED 4 EA SAFETY LOCKS IAW 1C-135-2-4-1 PG 9-5 PARA 9.3.3 STP 13 AISOD 06000 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) RESEATED ACFT LAN CABLE O/C/G HLGNJ 82CAB L 721 INSPECTION C/W NDN A83EE 41799 X 799 REINSTALLED PANEL IAW ETM-RC135-2-3 PG 7-141 PARA 7.1.6.12 S TEP M A83EE 11PAD S 800 REINSTALLED PUZZLE BRACKET IAW 1C-135-2-3-2 PG 13-65 PARA 13 .14.42 A83EE 41499 S 800 RC-135V, T/N 64-14848, 30 April 2015 U-160 C/A MDS PWC WUC AT HMAL REINSTALLED DUCTS IAW 1C-135-2-3-2 PG 13-65 PARA 13.14.42 LE AK CHK DUE SEE THIS JCN WCE 006 A83EE 411DA S 800 REINSTALLED ACM LIMIT VALVE IAW 1C-135-2-3-2 PG 13-49 PARA 1 3.14.26 LEAK CHK DUE SEE THIS JCN WCE 006 A83EE 4123G S 800 REINSTALLED ACM LIMIT VALVE SENSING LINES IAW 1C-135-2-3-2 P G 13-49 PARA 13.14.26 STPS 5 AND 6 A83EE 4123G S 800 LEAK AND OPS CHK GOOD NDN A83EE 4123G X 799 CLOSED KEEL BEAM BAY IAW 1C-135-2-3-2 PG 13-16 PARA 13.3.2.2 STEP R A83EE 11430 S 800 R2 SCREWS HLGNJ 81BFC G 105 REMOVED 2EA WARNING TAGS IAW LPS-55MXG-00-20-1-OFC3 PG 2 PARA 5.7.3.16.5.1.3.10 A83EE 01490 RESET DISTRO C/B PULLED BY AIRCREW AND ASSOCIATED C/B'S IAW 1-1A-14 SECTION 028 00 PARA 46 OPS CHK GOOD A83EE 42122 L 127 RESET DISTRO C/B PULLED BY AIRCREW AND ASSOCIATED C/B'S IAW 1-1A-14 SECTION 028 00 PARA 46 OPS CHK GOOD A83EE 46218 L 127 RESET C/B OPS CHK GOOD A83EE 14BKA L 127 REINSTALLED KNOB A83EE 42199 S 800 2 EACH PANELS REINSTALLED IAW 1C-135-2-2-2 PG 1-61 PARA 1.12 A83FL 46972 S 800 2 EACH PANELS REINSTALLED IAW 1C-135-2-2-2 PG 1-61 PARA 1.12 A83FL 46972 S 800 RT KEEL BEAM BAY DOOR IAW 1C-135-2-2-2 PG 15-600 PARA 15.94. 2 STEP 8 A83FL 11430 L 127 BATTERIES RECONNECTED IAW 1C-135-2-10-1 PG 15-32 PARA 15.24. 1 A83FL 42143 S 800 RESET FCAS COMPUTER. MBIT OPS CHK GOOD A83GC 52200 L 644 CLOSED ENG COWL IAW 1C-135-2-2-2 PG 20-4 PARA 20.3 A83HY 118D0 S 800 #1 ENG COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 P ARA 20.3 A83JE 118D0 S 800 #2 ENG COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 P A83JE 118D0 S 800 #3 ENG COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 P ARA 20.3 A83JE 118D0 S 800 #4 ENG COWLING CLOSED AND SECURED IAW 1C-135-2-2-2 PG 20-4 P ARA 20.3 A83JE 118D0 S 800 #1 ENG CHIP DETECTORS (4EA) INSTALLED IAW 2J-F108-2-1 SEC 79 -00-00 PG 201 A83JE 27A4D S 800 #2 ENG CHIP DETECTORS (4EA) INSTALLED IAW 2J-F108-2-1 SEC 79 -00-00 PG 201 A83JE 27A4D S 800 #3 ENG CHIP DETECTORS (4EA) INSTALLED IAW 2J-F108-2-1 SEC 79 -00-00 PG 201 A83JE 27A4D S 800 #4 ENG CHIP DETECTORS (4EA) INSTALLED IAW 2J-F108-2-1 SEC 79 -00-00 PG 201 A83JE 27A4D S 800 #1 ENG FUEL STRAINER INSTALLED IAW 2J-F107-2-1 SEC 73-11-10 PG 301 A83JE 27H99 S 800 #2 ENG FUEL STRAINER INSTALLED IAW 2J-F107-2-1 SEC 73-11-10 PG 301 A83JE 27H99 S 800 #3 ENG FUEL STRAINER INSTALLED IAW 2J-F107-2-1 SEC 73-11-10 PG 301 A83JE 27H99 S 800 #4 ENG FUEL STRAINER INSTALLED IAW 2J-F107-2-1 SEC 73-11-10 PG 301 A83JE 27H99 S 800 INSPECTED AREA, LK CK BAD SEE JCN 1432802060 AFUEL 46882 X 799 LK CK BAD #6 CTW CELL LEAKING SEE JCN: 143280206001 AFUEL 46400 X 799 RECONNECTED CTW CAVITY DRAIN LINES IAW 1C-135-2-5-3 PG 20-8 PARA 20.8.1 AFUEL 46429 S 800 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-161 C/A MDS PWC WUC AT HMAL REMOVED AND REPLACED #6 CTW CELL IAW IC-135-2-5-3 PG 23-53 P ARA 23.17 AFUEL 46400 R 381 CTR WNG #4 CELL DOOR REINSTALLED IAW TO 1C-135-2-5-3 PG 14-1 6 PARA 14.11 AFUEL 46453 S 800 DOOR REINSTALLED IAW TO IC-135-2-5-3 PG 14-15 PARA 14.9 AFUEL 46336 S 800 DOOR REINSTALLED IAW TO 1C-135-2-5-3 PG 14-15 PARA 14.9 AFUEL 46347 S 800 CELL INSTALLED IAW TO 1C-135-2-5-3 PG 23-53 PARA 23.17 AFUEL 46450 R 381 LK CHECK GOOD, NO LEAK NOTED AFUEL 46456 X 799 INSPECTED AREA, #6 CTW CELL CAVITY PREP C/W IAW 1C-135-2-5-3 PG 23-1 PARA 23.5 AFUEL 46456 X 799 PLUMBING AND ASSOCIATED HARDWARE INSTALLED IAW TO 1C-135-2-5 -3 PG 23-60 PARA 23.17.20 AFUEL 46450 S 800 LK CK C/W NO LEAKS NOTED AFUEL 46440 X 799 INSTALLED AWG HARD DRIVE CHASSIS RIGHT SIDE UP HLGNJ 82SDB L 127 GOOD PER AIRCREW HLGNJ 81FAJ X 799 INSPECTION C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSPECTION C/W IAW 1C-135-2-4-1-1 PG 3-175 PARA 3.9.12 A83FL 0413C (Null) ACFT LAV DRAINED A83FL 01000 (Null) INSP C/W IAW OAFBI 21-100 PARA 7.2.1 A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 STEPS 31-38 A83FL 0413C (Null) ACFT LAV SERVICED A83FL 01000 (Null) FUEL CONFIGURED FOR FLIGHT IAW 1C-135-5-1 APPENDIX K-5 A83FL 01000 (Null) TAGS REMOVED IAW 1C-135-2-10-1 PG 15-32 PARA 15.24.1 STEP 6 A83FL 01490 (Null) FDR DOWNLOAD C/W A83GC 04199 (Null) DISCONNECTED MULE HT03 IAW 1C-135-2-2-2 PG 14-154 PARA 14.38 A83HY 01000 (Null) INSPC/W NDN A83JE 04199 (Null) ENG'S 1,2,3,4 T HANDLES, START C/BS, FIRE SPRSN C/BS, FIRE SHUTOFF C/B RESET IAW 1C-135-2-4-1-1 PG 6-176 PARA 6 A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED FROM #1 STARTER, T HANDLE, FIRE SPRSN, AND FIRE SHUTOFF IAW 1C-135-2-4-1-1 PG 6A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED FROM #2 STARTER, T HANDLE, FIRE SPRSN, AND FIRE SHUTOFF IAW 1C-135-2-4-1-1 PG 6A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED FROM #3 STARTER, T HANDLE, FIRE SPRSN, AND FIRE SHUTOFF IAW 1C-135-2-4-1-1 PG 6A83JE 06000 (Null) 4 EA WARNING TAGS REMOVED FROM #4 STARTER, T HANDLE, FIRE SPRSN, AND FIRE SHUTOFF IAW 1C-135-2-4-1-1 PG 6A83JE 06000 (Null) 2 EA WARNING TAGS REMOVED FROM ACFT BATT SWITCH AND POWER RECEPTACLE IAW LPS55MXG-00-20-1OFC3 PARA 5A83JE 06000 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-162 C/A MDS PWC WUC AT HMAL INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) I'S AND E;S C/W IAW 1C-135-2-4CL-1-1 PARA 4.1.1 STEPS X-AF A83JE 0413C (Null) I'S AND E;S C/W IAW 1C-135-2-4CL-1-1 PARA 7.1 PG 7-1 A83JE 0413C (Null) INSP C/W NDN A83JE 04199 (Null) INSP C/W NDN A83JE 04199 (Null) WARNING TAGS REMOVED IAW TO 1C-135-2-5-3 PG 14-47 PARA 14.44 AFUEL 01490 (Null) 8 EA CIRCUIT BREAKERS RESET ON PANEL P140 IAW TO 1C-135-2-5-3 PG 14-47 PARA 14.44 STEP 8 AFUEL 01000 (Null) 1 EA CIRCUIT BREAKER RESET IAW 1C-135-2-5-3 PG14-47PARA14.44 STEP 8 AFUEL 01000 (Null) INSPECTED AREA NO DEFECT NOTED AFUEL 04199 (Null) INSPECTED AREA NO DEFECTS NOTED IAW TO 1C-135-2-5-3 PG 1-54 PARA 1.3.45 AFUEL 04199 (Null) INSPECTED AREA NO DEFECTS NOTED IAW TO IC-135-2-5-3 PG 1-54PARA 1.3.45 AFUEL 04199 (Null) INSPECTED AREA NO DEFECTS NOTED AFUEL 04199 (Null) INSPECTED AREA NO DEFECTS NOTED IAW TO 1C-135-2-5-3 PG 1-54 PARA 1.3.45 STEPS A-C AFUEL 04199 (Null) INSPECTED AREA NO DEFECTS NOTED AFUEL 04199 (Null) JOB ENTERED IN ERROR IAW 00-20-1 PARA 4.6.6.1 AFUEL 04199 (Null) POST FLIGHT C/W HLGNJ 04199 (Null) 28 DAY FMS UPDATE C/W A83CN 727AB L 944 MICROWAVE R2'D BY AIRCREW OPS CHK GOOD NDN A83EE 12EBG R 255 SUPPORTED A/C LAUNCH A83CN 01000 NABRE CONFIGURED FOR NORMAL OPERATIONS PER AIRCREW HLGNJ 82ZJ0 L 956 RESCRIPTED SECONDARY LAN CONTROLLER. O/C/G. HLGNJ 82QBF L 940 R2 HSDC CHASSIS, O/C/G HLGNJ 82QAC R 956 **** NO DDR NARRATIVE **** A83FL 118D0 J 127 INSTALLED NEW LOW OIL PRESSURE SWITCH IAW 1C-135-2-4-1-1 PG 13-115 PARA 13-41.2 A83JE 27DAL R 255 #2 ENG OIL PRESSURE SWITCH REMOVED IAW 1C-135-2-4-1-1 PG 3.1 14 PAR 3.41 A83JE 27DAL T 875 INSTALLED NEW LOW OIL PRESSURE SWITCH IAW 1C-135-2-4-1-1 PG 13-115 PARA 13-41.2 A83JE 27DAL U 875 REPAIRED FAULTY SEALANT AFUEL 46720 G 377 INSPECTED AREA, EVALUATED POSSIBLE FUEL LEAK. SEE JCN 143220 065003 AFUEL 46720 X 799 REPAIRED FAULTY SEALANT AFUEL 46720 G 377 REINSTALLED RT JACKPAD PANEL IAW TO 1C-135-2-2-2 P. 21-13 PA RA 21.7.3 AFUEL 46720 S 800 LK CK C/W NO LEAK NOTED AFUEL 46720 X 799 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-163 C/A MDS PWC WUC AT HMAL BOLT CANNED TO A4132 IAW 1C-135-2-7-1 PG6-252 PARA 6.80.2 AINAR 13AED T 875 INSTALLED LMLG SAFETY BOLT IAW 1C-135-2-7-1 PG 6-254 PAR 6.8 1 AINAR 13AED U 875 SANITIZING C/W A83FL 04199 (Null) OPS CHECK GOOD NO LEAKS NOTED A83FL 04199 (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-104 PARA 3.9.2 STEPS 31-38 A83FL 0413C (Null) INSP C/W IAW 1C-135-2-4-1-1 PG 3-175 PARA 3.9.12 A83FL 0413C (Null) REMOVED 1 EA WARNING TAG AND RESET C/B IAW 1C-135-2-4-1-1PG 13-115 PARA 13-41.2 A83JE 01490 (Null) SYS OPS CHK GOOD A83CN 626A0 X 799 7 DAY LCS INSP C/W NDN A83EE 41799 X 799 FUEL CELL ZERO PANEL CLOSED IAW ETM-RC135-2-3 PG 7-141 PARA 7.1.6.12 STEP M A83EE 11PAD S 800 REMOVED EMERGENCY LIGHT PANEL IAW 1-1A-14 SEC 020 00 PG10 PA RA 40 A83EE 44136 T 875 INSTALLED EMERGENCY LIGHT PANEL IAW 1-1A-14 SEC 020 00 PG 10 PARA 40 OPS CHK GOOD IAW ETM-RC135V/W-2 VOLA83EE 44115 U 875 #5 C/L/D LATCH IAW 1C-135-2-8-1 PARA 14.66 A83FL 14EL0 P 800 DUPLICATE DISCREPANCY IAW 00-20-1 PARA 5.7.3.19.4.1 A83FL 14EL0 Q 799 COVE LIP DOOR INSTALLED IAW 1C-135-2-8-1 PG 14-284 PARA 14.6 3 A83FL 14ELR R 20 COVE LIP DOOR RAISED IAW 1C-135-2-2-2 PG 14-148 PARA 14.37.2 A83FL 14EL0 S 800 #5 C/L/D REM TO SHEET METAL IAW 1C-135-2-8-1 PARA 14.62.3 A83FL 14ELR P 20 COVE LIP DOOR INSTALLED IAW 1C-135-2-8-1 PAGE 14-284 PARA 14 .63 A83FL 14ELR Q 799 #5 COVE LIP DOOR REMOVED FOR SHEET METAL IAW 1C-135-2-8-1 PA RA 14.62.3 PG 14-280 A83FL 14ELR P 127 COVE LIP DOOR INSTALLED IAW 1C-135-2-8-1 PG 14 284 PARA 14.6 3 A83FL 14ELR Q 799 R2 MOHAIR A83FL 14ELR G 20 SPOILER LOCKS REMOVED AND 2EA WARNING TAGS REMOVED IAW 1C-135-2-2-2 PARA 14.4.4 AND LPS 55 MXG 00-20-01 OA83FL 06000 (Null) RC-135V, T/N 64-14848, 30 April 2015 U-164 C/A SYMBOL AMELT - AMELT - AMELT X AMELT X AMELT X AMELT / AMELT / AMELT / AMELT / AMELT / AMELT / AMELT / AMELT / AMELT / AMELT - AMELT - AMELT X AMELT X AMELT X AMELT X AMELT X AMELT X AMELT X AMELT X AMELT X AMELT / AMELT / AMELT X AMELT / AMELT / AMELT / AMELT / INSP_BY RC-135V, T/N 64-14848, 30 April 2015 U-165 Equip_ID User_ID Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-166 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-167 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-168 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-169 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-170 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-171 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-172 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-173 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-174 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-175 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-176 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-177 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-178 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-179 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-180 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-181 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-182 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-183 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-184 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-185 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-186 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-187 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-188 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-189 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-190 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-191 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-192 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-193 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-194 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-195 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-196 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-197 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-198 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-199 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-200 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-201 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT AMELT A4848 A4848 A4848 A4848 A4848 A4848 A4848 AMELT AMELT AMELT AMELT AMELT RC-135V, T/N 64-14848, 30 April 2015 U-202 AMELT Equip_ID User_ID SYMBOL INSP_BY AMELT AMELT AMELT AMELT AMELT AMELT A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-203 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-204 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 AMELT A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-205 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-206 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-207 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-208 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-209 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 AMELT A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-210 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-211 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-212 A4848 Equip_ID User_ID SYMBOL INSP_BY A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 AMELT A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 A4848 RC-135V, T/N 64-14848, 30 April 2015 U-213 A4848 SYMBOL A4848 X A4848 X A4848 - A4848 - A4848 X A4848 X A4848 X A4848 - A4848 - A4848 X A4848 X A4848 X A4848 X A4848 X A4848 X A4848 X A4848 X A4848 X A4848 X A4848 X A4848 / A4848 X INSP_BY RC-135V, T/N 64-14848, 30 April 2015 U-214 Equip_ID User_ID TAB V WITNESS TESTIMONY AND STATEMENTS V1. SUMMARIZED TESTIMONY OF V2. SUMMARIZED TESTIMONY OF V3. SUMMARIZED TESTIMONY OF [Mishap Cryptological Operator] V4. SUMMARIZED TESTIMONY OF [Mishap Search Signals and Development] ......................... V-4.1 V5. SUMMARIZED TESTIMONY OF [Production Superintendent] ........................ V-5.1 V6. SUMMARIZED TESTIMONY OF [Director of Operations] V7. SUMMARIZED TESTIMONY OF [Mishap Firefighter 1] V8. SUMMARIZED TESTIMONY OF V9. SUMMARIZED TESTIMONY OF V10. SUMMARIZED TESTIMONY OF V11. SUMMARIZED TESTIMONY OF ................................ V-1.1 [Mishap Co-Pilot] ............................ V-2.1 [MASE1] [Mishap Firefighter 2] .............................. V-6.1 .................................. V-7.1 ..................................................... V-8.1 [Crew Chief 3] [Quality Control Manager] [Materials and Processes Engineer] .................. V-9.1 ....................................... V-10.1 ................................................ V-11.1 RC-135V, T/N 64-14848, 30 April 2015 1 ..................................... V-3.1 INTENTIONALLY LEFT BLANK 64-14848, 30 April 2015 2 [Mishap Co-Pilot] [Mishap Co-Pilot] [Mishap Co-Pilot] [Mishap Co-Pilot] RC-135V, T/N 64-14848, 30 April 2015 V-1.1 SUMMARIZED STATEMENT OF SENIOR AIRMAN . . . appeared before the Acc1dent Investigation Board, was sworn, and testi?ed substantially as follows: I, of the 343rd Reconnaissance Squadron at Offutt Air Force Base, Nebraska, after being placed under oath, hereby state that before my interview, the difference between the nature of an accident investigation board (AIB) under AFI 51?503 and a safety investigation board (SIB) under AFI 91-204 was explained to me. I understand the difference between an AIB and SIB. I acknowledge that the purpose of this AIB is to produce a publicly releasable report on the facts and circumstances surrounding this accident and to gather and preserve evidence for use in claims, litigation, disciplinary actions, adverse administrative proceedings, and for all other purposes. .I understand that my AIB testimony may be used for any proper purpose and can be released to the public. I am currently assigned as an Airborne Systems Engineer. My duties generally entail maintaining and correcting faults found in electronic warfare systems, as well as manage and maintain cooling equipment throughout the jet. 1 was assigned as an Airborne Systems Engineer at the time of the mishap. I have reviewed my written statement, dated 30 Apr 15 and the transcript of my oral statement, dated 11 May 15, and I adopt these statements as part of my testimony today. I ?nd nothing incorrect or inaccurate in my previous statements and I do not wish to make any additions, clari?cations, or corrections to these statements. [Statement and are located at Tab 12-697]. MAP Signed and sworn before me this 2 Cl day of June 2015. WILLIAM M. EVANS, Jr, Lt Col, USAF President, Accident Investigation Board RC-135V, 64-14848, 30 April 2015 v2.1 [Mishap Cryptologic Operator] [Mishap Cryptologic Operator] [Mishap Cryptologic Operator] [Mishap Cryptologic Operator] RC-135V, T/N 64-14848, 30 April 2015 V-3.1 [Mishap Signals Search & Development] [Mishap Signals Search & Development] [Mishap Signals Search & Development] [Mishap Signals Search & Development] RC-135V, T/N 64-14848, 30 April 2015 V-4.1 [Production Superintendent] [Production Superintendent] [Production Superintendent] [Production Superintendent] RC-135V, T/N 64-14848, 30 April 2015 V-5.1 [Director of Operations] [Director of Operations] [Director of Operations] [Director of Operations] RC-135V, T/N 64-14848, 30 April 2015 V-6.1 FOR OFFICIAL USE ONLY NON-PRIVILEGED WITNESS STATEMENT 7 Date of the mishap I 0 . Crew position (as applicable) Time you began duty 4! . . [Director of Operationshave been advised by _of the following: - of ssKN' (rm-imam Name - a. This investigation is being conducted under the provisions of AF I 91-204 solely for the purpose of mishap prevention the United States Force and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a mishap investigation and I acknowledge that a promise of con?dentiality has not been extended to me. This witness statement may be released to the public pursuant to a Freedom of Information Actrequest. c. The chain of command will review the ?nal mishap report. Provide an account of first-hand observations of what happened, a description of prevailing conditions, circumstances, and associated events (use reverse for continuation). I .1 64+ in HM Flfsodr Auk? fw cams 5W4: +91; ml awki Tia Jr?- 564': am an boos W65 'i'ixw?) owA Gear/:32 Ai? we, 4L0. Mi as chad-NM. FR ?mQ?mm? US 3" wads na?r wad?- Fur 4m \w?xl-ml MS imp om?. 41/1 Plush Swim mol? in RAM. Dwiwb Gem-nag Si-vr?l- 4?ng not 3}th Wyatt!? MK ?3th fag/sand ivw?W?? row-m and Adamo? at inc-1' ga? mar 1w #4 lier deck. Enjsw. hurl. M, dutie? graham?; (All mnei ?ml (mu-9? cm Dead in Wis. eagim w! Mr Omvbo?lrd_ l?l?'lel, 84ml Sim/11M 01A was ?bark; wad Pilot's 304'? iyrlo appeared 8003. AC marginal-ed Ms vars WA: ?6 were 0A5 Fuf rd +0 40 Wtan Switch 017$ ("Fm opera") (2 333?), +02 Nod 63/ i? gamma. AL [3,71, '14 [1k] ?Mama arrival ?math, 9va? M, an}; a Misse? ?(smock ?ll? ?91 AW Md 5;ch from war. gala (noon/Liza to rm rem/t 82'7an Eml'i?wltci ?rla mo I Weed, Came war m6 r13 aus? rma aback +02 sac-ends 4? 5 ermine/MW; Mia: FH- Deck. gpote up i Mil?[Wed Ac m4 coals 1:94 by; Muir," 7 W17 verban Sale a Gm back?re/e. {e Niki?? ?would beading ?Mm bmisag amt SWi'a ?rang fax a: VP Ws .9 ?4 Tu? Copilolr WW fewer and? 464% we were ewe/99:9 ram Owe/in on I _Date._m ?The above statement is true to the best of my knowledge and belief.? Signed. Tact (Ont/u rg-z-z Tlo ?0 RC i?i??f Osir- o?xbauir Idg'i?w?i?? Ground, (W945 unable: +0 Aek?wine, WM was full (?atbed was A969 in text back? 0i' 7th 0"er RC-135V, 64-14848, 30 April 2015 V-6.2 ?94? aka/24H. Tm Lav bm'?nW We ?m?a?lam (Myer, Aroma, 4&2 chad/e and data Jam. Tm ?31? 48? ga?m 49? Ga" i ?56 gee?4147? 9Y2 mar ?s?wivm. we, (Prom; '49" 064 (eH? s'fic o? ?ve/A1ch nose r'vn?o 2?51 yet? (5mg Ex FIQ aw? Vikchs 4D r?e?yd'wa Qwe? Evy?ch grass 7 "w a (4 Side at?!ch [NH?med awoke/W5 MM Qus 11/72. I km VUHnghaL awi wag Tm Jim, gwlrei +0 amt 3 I #5 Eng Du?? 513245614. +94 0Ker bni? 4M. (l?J?upL?5 bad; Wm? (?Ms Ups \0{va( 494- g?rt was did? RC-135V, 64-14848, 30 April 2015 V-6.3 30.249K1f5 . L. 317:: gr 51.. ?dwfp?j??e Alwgr Emma,? ., 1?76 Em; I ., . . Maw} Mm??Ae?a [2319522 (DE-M5 ., Tag.? win a 124(?sirgm?w ?1711. by im w. WT r? RC-135V, 64-14848, 30 April 2015 V-6.4 1?1 Llb? gameJei? N?rd? I V7 52 f3?? ?9?ij Cam! #4 {310 {623 53%? - Maw/7 395+ Cg?rm can; ?y?=?iuj 1817 ea, I m, 7,425 1/0 (an) a AM 7kg; QMQ I, 5/42 99 ?y wigs @w?g?l [(60 7" F.)th DWI-IL lam?frawa, ?ush/Ly: 2H vari-ki?s?? mas a I Mia} 1 imi?; I Axthz a :24 i5! [35?ng RC-135V, 64-14848, 30 April 2015 V-6.5 5m ?25 '1 ,Mm 31577313523: ma?a; Mb?: .. eaAhmmv. QKL, -, MO, 35a- . . ?aw: ,9 .2 ?i?g?g?wf?famn 195 ?Ag; 3:32 -. RC-135V, 64-14848, 30 April 2015 V-6.6 [Mishap Firefighter 1] [Mishap Firefighter 1] [Mishap Firefighter 1] [Mishap Firefighter 1] RC-135V, T/N 64-14848, 30 April 2015 V-7.1 [Mishap Firefighter 2] [Mishap Firefighter 2] [Mishap Firefighter 2] [Mishap Firefighter 2] RC-135V, T/N 64-14848, 30 April 2015 V-8.1 [Crew Chief 3] [Crew Chief 3] [Crew Chief 3] [Crew Chief 3] RC-135V, T/N 64-14848, 30 April 2015 V-9.1 FOR OFFICIAL USE ONLY NON-PRIVILEGED WITNESS STATEMENT . I . Date of the mishap l5 9 Ll go . Crew position (as applicable) - . Time you began duty 0700 [Crew Chief have been advised by of the following: Name Grade SSAN Organization Nadeank of Investigator . a. This investigation is being conducted under the provisions of AF I 91-204 solely for the purpose of mishap prevention within the United States Air and to determine all factors relating to the mishap in order to prevent recurrence. I understand I am being interviewed as a witness in a mishap investigation and I acknowledge that a promise of con?dentiality has not been extended to me. b. This witness statement may be released to the public pursuant to a Freedom of Information Act request. c. The chain of command will review the ?nal mishap report. Provide an account of ?rst-hand observations of what happened, a description of preVailing conditions, circumstances, and associated events (use reverse for continuation). 1 L900 fmvolvcd 1m sot-l1: Gena?alien Fathom, Tint Act-7f we; ?61!?le 0x914? hat (in-5+ .M by My self 0? 1" 0mg[we] (wasp. ??lSo ?15 awe/5 *t Jew/5 5?145 Wei} {Xingu/j}: I Chat/ck; ?ne we }5 up ?P/avtt 4r $.5ngon My Fof?ibm. ?The above statement is true to the best of my knowledge and belief.? Signec )ate. 53 I RC-135V, 64-14848, 30 April 2015 V-9.2 [Quality Control Manager] [Quality Control Manager] [Quality Control Manager] [Quality Control Manager] [Witness] RC-135V, T/N 64-14848, 30 April 2015 V-10.1 [Materials & Processes Engineer] [Materials & Processes Engineer] [Materials & Processes Engineer] [Materials & Processes Engineer] [Witness] RC-135V, T/N 64-14848, 30 April 2015 V-11.1 INTENTIONALLY LEFT BLANK RC-135V, 64-14848, 30 April 2015 V-12 TAB W WEATHER AND ENVIRONMENTAL RECORDS AND DATA NOT INCLUDED IN TAB F NOT USED RC-135V, T/N 64-14848, 30 April 2015 1 INTENTIONALLY LEFT BLANK 64-14848, 30 April 2015 2 TAB STATEMENTS OF INJURY OR DEATH NOT USED 64-14848, 30 April 2015 1 INTENTIONALLY LEFT BLANK 64-14848, 30 April 2015 2 TAB Y LEGAL BOARD APPOINTMENT DOCUMENTS Y1. HOST INSTALLATION SUPPORT MEMORANDUM ................................................ Y-3 Y2. CONVENING ORDER AMENDMENT .......................................................................... Y-6 RC-135V, T/N 64-14848, 30 April 2015 1 INTENTIONALLY LEFT BLANK 64-14848, 30 April 2015 2 DEPARTMENT OF THE AIR FORCE HEADQUARTERS AIR COMBAT COMMAND JOINT BASE VA 8 Jun 15 MEMORANDUM FOR 55 FROM: [-10 SUBJECT: Host Installation Support for Accident Investigation Board (AIB), Class A, RC-135 Mishap, 30 Apr 15, 64?004848, 55 WG, Of?Jtt AFB, NE 1. The attached memorandum convenes an AIB to investigate the subject mishap. Your installation has been designated as the host installation for the accident investigation. 51? 503. paragraph 4.10.1; details the logistical and administrative support required from the host installation. A list of support requirements can be found in AF 1 51?503, Attachment 3, Figure A3. 1. 2. It is your responsibility to appoint a host installation liaison and squadron POC before the AIB arrives at your installation. 3. The board president, Lt Col William Evans, or legal advisor, I I, has been directed to contact your office to make arrangements for the investigation and to obtain the above support. My POCs for this matter are and . I thank you in advance for your assistance. ., Colonel. USAF Staff Judge Advocate Attachment: Convening Order Memo CC: #129656 64mth pawe'z RC-135V, 64-14848, 30 April 2015 DEPARTMENT OF THE AIR FORCE HEADQUARTERS AIR COMBAT COMMAND JOINT BASE LANGLEY-EUSTIS VA 8 Jun 15 MEMORANDUM FOR LIEUTENANT COLONEL WILLIAM M. EVANS, JR. FROM: SUBJECT: Convening Order of AFI 51-503 Accident Investigation Board Class A, RC-135 Mishap, 30 Apr 15, 64-004848, 55 WG, Offutt AFB, NE 1. An accident investigation board is hereby convened under the provisions of AFI 51-503 to investigate the subject mishap. You must avoid accessing any privileged safety information regarding this mishap until approval of the report. This appointment letter is your authority to interview witnesses, take sworn testimony, and review all documents, ?les, and wreckage relevant to your investigation. Upon receipt of a complete Part 1 of the Safety Investigation Board (SIB) Reporter, you and other detailed AIB members are relieved of all other duties until the report is submitted for approval. You may consider releasing any member when his/her responsibilities are complete. The following personnel are detailed to serve on the accident investigation board: LT COL WILLIAM M. EVANS, JR. President Legal Advisor Recorder 2. Your investigation will follow the guidelines and procedures in AFI 51-503. will advise you on preliminary administrative matters. Your legal advisor is required to be present during all witness interviews, and must review all evidence, documents, transcripts, and statements prior to inclusion in your report. Your report will include an Executive Summary, Summary of Facts, and Statement of Opinion as required by AFI 51- 503. All witnesses, documents, records and other evidence within the control of the Air Force will be made available to you, other than privileged safety information. All witnesses who testify must do so under oath or af?rmation. Your report shall be released to the public and shall not contain any privileged safety or Privacy Act-protected information. 3. If a Statement of Opinion is authorized, your Statement of Opinion must be supported by a preponderance of evidence contained in your report. Your legal advisor will assist you in evaluating evidence. Do not include recommendations for corrective or disciplinary action in your report. You and the other board members are not authorized to disclose board ?ndings or opinions, except to members of my staff, without permission prior to the of?cial public release of the AIB report. 24942 79m RC-135V, 64-14848, 30 April 2015 Y-4 4. Travel and billeting will be funded by ACC. ACC board members must utilize their local fund cite and the ESP code of"EM.? Travel orders should be issued locally and authorize variations in travel for all members ofthe AIB. Board members not assigned to ACC must coordinate with in advance regarding their travel and orders. All travel costs needed for witness interviews outside of the local area should be coordinated with in advance. 5. In accordance with AFI 51-503. the host installation will assist you with logistical and administrative support. A host installation liaison officer will be appointed by the installation commander to assist with billeting. vehicles (if available), facilities, administrative support, and reproduction services. Make contact with the host installation and liaison officer through the of?ce of the installation commander at or DSN Additionally. the mishap wing shall appoint a point of contact to assist the AIB with access to Witnesses and evidence secured by the unit. Please make contact with the mishap wing at 6. Your investigation should be completed within 30 days from receipt of non-privileged safety information ?om your legal advisor. Submit any requests for extensions. additional advisors, or other matters to Submit your final report to and she will forward it to me for approval. 7. My point of contact for any questions is or at FOR THE VICE COMMANDER Colonel, USAF Staff Judge Advocate CC: 55 ivo/CC ACC RC-135V, 64-14848, 30 April 2015 Y-S DEPARTMENT OF THE AIR FORCE HEADQUARTERS AIR COMBAT COMMAND JOINT BASE LANGLEY-EUSTIS VA 9 Jun 15 MEMORANDUM FOR LIEUTENANT COLONEL WILLIAM M. EVANS, JR. FROM: SUBJECT: Amendment 1, Convening Order of AFI 51-503 Accident Investigation Board; Class A, RC-135 Mishap, 30 Apr 15, 64-004848, 55 W6, Offutt AFB, NE The above referenced Convening Order, dated 8 June 2015, is hereby amended to detail the following personnel to serve on the accident investigation board in addition to the members detailed on 8 June 2015: CAPT 338 CTS Pilot Member TSGT 55 MXS Maintenance Member Mv nnint of contact for anv questions is or at FOR THE VICE COMMANDER Co?lonel, USAF Staff Judge Advocate cc: 55 ?ve/CC ACC 249% gawk: Pom RC-135V, 64-14848, 30 April 2015 TAB Z PHOTOGRAPHS, VIDEOS, DIAGRAMS, NOT INCLUDED IN TAB S Z1. ACCIDENT INVESTIGATION BOARD PHOTOS ........................................................Z-3 Z1.1 UNDAMAGED GALLEY OXYGEN PLUMBING ..................................................Z-3 Z1.2 UNDAMAGED GALLEY OXYGEN PLUMBING II ..............................................Z-4 Z1.3 UNDAMAGED GALLEY OXYGEN PLUMBING III .............................................Z-5 Z1.4 POST-MISHAP FIRE DAMAGE ...............................................................................Z-6 Z1.5 EXTERNAL FIRE DAMAGE POST-MISHAP.........................................................Z-7 Z1.6 HOLE IN AIRCRAFT ................................................................................................Z-8 Z1.7 HOLE IN AIRCRAFT FROM LEFT OF FUSELAGE ..............................................Z-9 Z1.8 INTERAL STRUCTURAL DAMAGE ....................................................................Z-10 Z1.9 CLOSE-UP OF HOLE IN AIRCRAFT ....................................................................Z-11 Z1.10 UNDAMAGED RC-135 GALLEY ..........................................................................Z-12 RC-135V, T/N 64-14848, 30 April 2015 1 INTENTIONALLY LEFT BLANK 64-14848, 30 April 2015 2 Z1. ACCIDENT INVESTIGATION BOARD PHOTOS Z1.1 UNDAMAGED GALLEY OXYGEN PLUMBING RC-135V, T/N 64-14848, 30 April 2015 Z-3 21.2 UNDAMAGED GALLEY OXYGEN PLUMBING II RC-135V, 64-14848, 30 April 2015 2?4 21.3 UNDAMAGED GALLEY OXYGEN RC-135V, 64-14848, 30 April 2015 Z-S 21.4 FIRE DAMAGE RC-135V, 64-14848, 30 April 2015 Z-6 21.5 EXTERNAL FIRE DAMAGE RC-135V, 64-14848, 30 April 2015 Z-7 21.6 HOLE IN AIRCRAFT RC-135V, 64-14848, 30 April 2015 Z-8 21 .7 HOLE IN AIRCRAFT FROM LEFT OF FUSELAGE - "171? 1' RC-135V, 64-14848, 30 April 2015 Z-9 21.8 INTERAL STRUCTURAL DAMAGE RC-135V, 64-14848, 30 April 2015 21.9 OF HOLE IN AIRCRAFT a. 4'7 UH, . WU: .33. "IN-um? 'uo .1 Hum we . RC-135V, 64-14848, 30 April 2015 Z-ll Zl . 10 UNDAMAGED RC- 1 35 GALLEY RC-135V, 64-14848, 30 April 2015 Z-12 TAB AA FLIGHT DOCUMENTS AA1. 55 OG FORM 25......................................................................................................... AA-3 AA2. LOCAL GO/NO/GO CHECKLIST ............................................................................ AA-4 RC-135V, T/N 64-14848, 30 April 2015 1 INTENTIONALLY LEFT BLANK 64-14848, 30 April 2015 2 55 0G MISSION PLANNING BRIEFING CERTIFICATE 55 06 Form 25 SS OPERATIONS GROUP Flight Duie Sign Aircraft Tail Number Fliqu Order 5' MISSION - BRIEFING CERTIFICATE I LI 3/ 15 d? (I) FII Ilutv Limitations;r [11: ulntu Mission umu' Llulics during AR Missmn crew commander h?ul'ing n. Roll Ca1+ HMS une?ng Im/ Highl- ?Ird?lrs 'i Travel Pa? manila? Addiliunui mis?lun crew brie?ng FCIF Pan 5 Part Read File Dustinaliun Type desrenl Not Within 24 m? Compressed Gas Diving 571m men-um?. Enmuie *yNn: Within I2 CliumherFEI '2 35k ft Field restrictinn?: IFR SuppiAFlsi 9/ N?l 72 [If D?l'l?tlng HIDULI .I dll?i?h??r?unrul. hy??l?i?b; Na: Within I3 01' Crinsuming Almhul {bps time anau'un nol Self-meditate or nul DNJF VFR paucm Aliuude ?1 5 pecial ntere51lleni?t$ll51 Comm Kn. l?ulnu1 [Jirucliws, Jugs. Lunches Prinnucs ouch and Go proeedurcs [?rm dunes} Unplanned gu-aruundx Lost comm. Procedures Simulated emergenucs .f Restnununs! I?ruccdurus ERR WK It" . 1 . ?mm? Full slup consideration: I-I?ei Hum-m! Brake wwrgum'wi'} thihilmns laplnris, ctci eiiery?u- mum?rap Trainin I'l?rioritia [Er Training FnIcluI Review H?dix'idilai Training Frlumies Scuttle guuls I NOTAMS Ei-ulummn mqujmmums FE hrml' Missiun I?Iun Safety nf?igln Aircral'l ugrudcd I?AKv'L'nrgo Requirements and m-gcar Item sh:ng FP?hrcai nI Ihc day I If' nu: ORM review 'nrrn 4E: Mien-lute gear brim WW Mission 0v wiuw: 13-13:: RE it} Mia? Show mm: I bcgmi Busilmerlocahun 5 Rudin Cmi?guralinn 3 Sum pnmin 5 Engmc Start Time I 30L Normal engine slur: procedums! Calls i . awry] Engine H?h'mdir Ignition fimund abnormal prnucdurcs I tmurgencms Star! "lamina-Ham h'i?e?w . Aircraft L'nmmantlc r'itami Bell Signals lmard fa {Wanner Forcuaai I Amidanuc Supervisor Nnrmal takcol'Fpmcedm-ua 0 f. I hkeq?fmmie Winn-11 ?wring 'l'ukcnl?l?muergencies [Erich-u uf ?ight} swim Rudder, I?mv: aw Ra?: rindng?ighr Iann'mg :mmer?me?- a?ur Crew duties during ulnurgcnulca pnrlurt' pmwdurus 'I'muhlc Emergent} mum considcmlimrs r' Landing dam Radar-?wsual seal-J1 HCC Hum) spur Hfin Hum}: arcm Mid-Air L?nllismn m-mduncc mm," um) i'll'i?h?n'l' vii-Him: H'rgf?a: 4f Crch' C'Icnred ul- (350.00 Oxygen Requn?umcms FMS sump Navigulur mulu ut' High lerram- Symmal leu Airspace .4 Emergency air?elds I FL :2 It! Tunkcr u. may Ri?nLIUZVulbi lyric I mem? Pam! purqu .3 .I'I'ninpiu Junkers] y- imnfenwm Training requirement; EMCON Breakaway dunes and End AR rcqucsl hr MW RC-135V, 64-14848, 30 April 2015 AA-3 [Mishap Co-Pilot] [Mishap Navigator] [MASE2] [MASE1] [MASE3] [MR1] [MR1] [MR2] [MAMS] [MCO] [MSSD] [MTC] [Director of Operations] [Mishap Pilot] RC-135V, T/N 64-14848, 30 April 2015 AA-4 TAB BB REGULATIONS, DIRECTIVES, GOVERNMENT DOCUMENTS BB1. TECHNICAL ORDER 00-25-4 ................................................................................... BB-3 BB2. TECHNICAL ORDER 00-20-1 .................................................................................... BB-6 RC-135V, T/N 64-14 848, 30 April 2015 1 INTENTIONALLY LEFT BLANK RC-135V, 64-14 848, 30 April 2015 2 TO 00-25-4 TECHNICAL MANUAL DEPOT MAINTENANCE OF AEROSPACE VEHICLES AND TRAINING EQUIPMENT (ATOS) FOR QUESTIONS CONCERNING TECHNICAL CONTENT OF THIS TECHNICAL MANUAL, CONTACT HQ AFMC/A4FC. THIS MANUAL SUPERSEDES TO 00-25-4, DATED 15 AUGUST 2011. DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. PA Case Number 04-333. Submit recommended changes or problems with this Technical Order to HQ AFMC/A4F, Wright-Patterson AFB, OH 45433. Published under authority of the Secretary of the Air Force 15 JANUARY 2012 RC-135V, T/N 64-14848, 30 April 2015 BB-3 TO 00-25-4 1.2.14 On Condition Maintenance (OCM). OCM is a program to schedule selected aircraft into a depot level facility to correct known specific defects. Selection is based on combinations of critical and multiple major defects. Critical defects are significant faults on primary structure. Major defects are significant faults to secondary structure. OCM is selected so that contracted corrective action can be tailored to known, specific aircraft needs as a result of the ACE program. 1.2.15 Product Group Manager (PGM). The single manager for a Product Group, who has the same responsibilities as a Program Manager or Materiel Group Manager for the assigned products. 1.2.16 Reliability-Centered Maintenance AFMCI 21-103. A maintenance concept that has the objective of achieving the inherent, or designed-in, reliability of a system. The concept is a derivative of the airline/manufacture maintenance planning document MSG published under the auspices of the Air Transport Association. 1.2.17 Reliability-Centered Maintenance Analysis AFMCI 21-103. A structured approach to the development of an RCM concept for a system or end item. It uses FMECA and integrity program outputs and MPPD logic to identify maintenance tasks which must be performed on a scheduled basis to ensure the attainment of inherent reliability. 1.2.18 Modification. A physical alteration of equipment that changes its capabilities or characteristics, i.e., form, fit or function. 1.2.19 Programmed Depot Maintenance (PDM). Inspection and correction of defects that require skills, equipment or facilities not normally possessed by operating locations. 1.2.20 Sectionalized Work Requirements Package. The depot work package developed to identify the maintenance and/or modification, sectionalized by categories of tasks, to be done on aircraft, missile or equipment being input to a source of repair. 1.2.21 Single Manager (SM). The PM or PGM in charge of a weapon/military system or program group. 1.2.22 Source of Repair (SOR). An industrial complex (organic, commercial contract, or inter-service facility) with required technical capabilities to accomplish depot repair, overhaul modification, or restoration of specific types of military hardware or software. 1.2.23 Speedline. The programming of a specific group of aircraft for the accomplishment of specific maintenance tasks or modifications that do not constitute a complete PDM package. 1.2.24 Program Manager (PM). The individual in an AFMC System Program Office (SPO) who is ultimately responsible and accountable for decisions and resources in overall program execution. The single face to the user who oversees the seamless process. PM is the designated title for the single manager of a program who reports to a Program Executive Officer (PEO) or Designated Acquisition Commander (DAC). 1.2.25 Technology Repair Center (TRC). A functional entity with an AFMC source of repair activity which accomplishes depot level maintenance on a specific group of items. 1.2.26 Training Equipment. Aircraft, missile and other training equipment in FSG 69; trainers that are part of a Mobile Training Set (MTS) or Resident Training Equipment (RTE). Training equipment includes all trainers reportable in accordance with AFI 21-103 (Equipment Inventory, Status, and Utilization Reporting). 1.2.27 Safety of Flight (SOF). A SOF write-up indicates that the weapon system or equipment unit is considered unsafe or unfit for flight or use and that the weapon system will not be flown or the equipment used until the unsatisfactory condition is corrected. 1.2.28 Unprogrammed Requirements. Involve those requirements which are generated unpredictably and have associated dollars based on historical usage. Unprogrammed requirements include unplanned (i.e. unforeseen maintenance actions) performed at either the organic or contract depot by depot personnel or on-site by organic or contract field teams. Includes Repair Group Categories (RGCs) B and D. 1.3 TABLES. Table 1-1, Table 1-2, Table 1-3, and Table 1-4 indicate the basis upon which the various mission design series (MDS) aerospace vehicles will be scheduled for depot modification and maintenance. If technical or operational considerations warrant development of a program that deviates from the published tables or intervals specified in the following sub paragraphs, approval can be granted by the assigned PM. The PM has the technical expertise and authority to determine if a RC-135V, T/N 64-14848, 30 April 2015 BB-4 1-3 TO 00-25-4 Table 1-2. Programmed Depot Maintenance Aircraft scheduled on a calendar time cycle (in months) for depot maintenance. The listing of a basic mission design, includes all series and prefixes, unless otherwise indicated. Designation Interval OC-ALC Aircraft: B-1B 60 B-2 84 B-52 48 RC-135 48 KC-135 assigned to Hickam AFB or NASA 48 KC-135 excluding a/c identified above 60* C-135, C-135E, NKC-135, OC-135, TC60* 135, WC-135 E-3 60 JE-3C 72 OO-ALC Aircraft: WR-ALC Aircraft: C-130E/H (PACAF) 54 MC-130E, AC-130H 54 NC-130A, MC-130H, WC-130H, MC-130P, 60 AC-130U LC-130H, HC-130N/P 69**/*** NC-130H, EC-130H, C-130E, C-130H 69*** C-130J, CC-130J, EC-130J, HC-130J, 72*** MC-130-J, WC-130J C-5A 96 C-5B 96 C-5C 96 C-5M 96 F-15**** 72 UH-1N 96 TH-1H 96 HH-60G 78 * Extension inspection at 44-51 months. ** Thirty (30) month Mid-interval inspection on ACC and AFRC HC-130N/P aircraft (Command Option). *** Initial PDM not to exceed 144 months (12 Yrs) from aircraft acceptance date - (Aircraft Data Plate). **** F-15E models cum E210 and up should begin PDM not later than 8 years from delivery, and thereafter maintain a 6 year cycle. Table 1-3. Excepted Aircraft Designation C-17 F-22 MC-12* * Indicates aircraft exempted from ACI 1-8 RC-135V, T/N 64-14848, 30 April 2015 BB-5 Designation MQ-1* MQ-9* T-38 TO 00-20-1 TECHNICAL MANUAL AEROSPACE EQUIPMENT MAINTENANCE INSPECTION, DOCUMENTATION, POLICIES, AND PROCEDURES (ATOS) THIS MANUAL SUPERSEDES TO 00-20-1, DATED 1 APRIL 2013. FOR QUESTIONS CONCERNING TECHNICAL CONTENT OF THIS TECHNICAL MANUAL, CONTACT THE APPLICABLE TECHNICAL CONTENT MANAGER (TCM) LISTED IN THE ENHANCED TECHNICAL INFORMATION MANAGEMENT SYSTEM. HQ AFMC/A4UE, WPAFB, OH IS THE APPROVAL AND WAIVER AUTHORITY FOR THIS TECHNICAL MANUAL. DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. HQ AFMC/PA Certificate Number AFMC PAX-04-329. Submit recommended changes or problems with this technical order to the applicable TO Manager (TM) listed in ETIMS using the Recommended Change Process outlined IAW TO 00-5-1. Published under authority of the Secretary of the Air Force 15 JUNE 2013 RC-135V, T/N 64-14848, 30 April 2015 BB-6 TO 00-20-1 CHAPTER 3 AEROSPACE EQUIPMENT FORMS DOCUMENTATION 3.1 GENERAL. 3.1.1 This chapter prescribes general requirements and procedures for aerospace equipment forms documentation. It specifies filing, disposition, and general documentation requirements. For the purposes of the 00-20-series TOs, the term “Documentation” may refer to hard copy forms, computer produced hard copy, or Air Force approved electronic databases. 3.1.1.1 AFTO FORM 46, PREPOSITIONED LIFE SUPPORT EQUIPMENT (ALERTS generated authorized). 3.1.1.2 AFTO FORM 95, SIGNIFICANT HISTORICAL DATA. 3.1.1.3 AFTO FORM 244/245, INDUSTRIAL SUPPORT EQUIPMENT RECORD. 3.1.1.4 AFTO FORM 427, AEROSPACE VEHICLE INTEGRAL FUEL TANK REPAIR HISTORICAL DATA. 3.1.1.5 AFTO FORM 428, B-1B AIRCRAFT INTEGRAL FUEL TANK REPAIR HISTORY RECORD. 3.1.1.6 AFTO FORM 781, ARMS AIRCREW MISSION FLIGHT DATA DOCUMENT. 3.1.1.7 AFTO FORM 781A, MAINTENANCE DISCREPANCY AND WORK DOCUMENT. 3.1.1.8 AFTO FORM 781C, AVIONICS CONFIGURATION AND LOAD STATUS DOCUMENT. 3.1.1.9 AFTO FORM 781F, AEROSPACE VEHICLE FLIGHT REPORT AND MAINTENANCE DOCUMENT. 3.1.1.10 AFTO FORM 781H, AEROSPACE VEHICLE STATUS AND MAINTENANCE DOCUMENT. 3.1.1.11 AFTO FORM 781J, AEROSPACE VEHICLE-ENGINE FLIGHT DOCUMENT. 3.1.1.12 AFTO FORM 781K, AEROSPACE VEHICLE INSPECTION, ENGINE DATA, CALENDAR ITEM INSPECTION, AND DELAYED DISCREPANCY DOCUMENT. 3.1.1.13 AFTO FORM 781N, J-79 ENGINE RUNUP RECORD. 3.1.1.14 DD FORM 1896, DOD JET FUEL IDENTAPLATE. 3.1.1.15 DD FORM 2026, OIL ANALYSIS RECORD. 3.2 MAINTENANCE INFORMATION SYSTEMS (MIS). MIS refers to the automated maintenance information systems including Integrated Maintenance Data Systems (IMDS), Reliability and Maintainability Information System (REMIS), G081, Comprehensive Engine Management System (CEMS), PMEL Automated Management System (PAMS), Automated Life-sustaining Equipment & Record Tracking System (ALERTS), Automated Life Support Management System (ALSMS), Defense Repair Information Logistics System (DRILS), and and Reliability, Availability, Maintainability Logistics Support System for Pods (RAMPOD). These systems must be developed and used meeting the intent of documentation requirements contained in this publication. Use of systems other than those listed above require Lead Command and HQ AF A4l approval. EXCEPTION F-22 IMIS and F-35 ALIS will utilize embedded electronic forms capabilities in accordance with applicable T.O.’s. F-22 IMIS is the MIS of entry, IMDS facilitates all scheduling functionality. F-22 IMIS users and managers will ensure IMDS accurately reflects documentation in F-22 IMIS. REMIS is the system of record for all maintenance data documentation. 3.3 AUTOMATED FORMS. Use of automated forms is mandatory. As a minimum, AFTO Forms 781A, 781J, 781K, and 95’s generated by the MIS will constitute fully automated forms. (EXCEPTION: F-22 IMIS and F-35 ALIS utilize embedded forms capabilities.) Manual forms produced by a computer program do not meet the intent of automated forms. Use of ALERTS generated AFTO form 46 is authorized. Other automated products may be used for process controls and/or AFTO Form 244/245 documentation RC-135V, T/N 64-14848, 30 April 2015 BB-7 3-1 INTENTIONALLY LEFT BLANK TAB CC MEMORANDA FOR RECORD CC1. SECURITY CAMERA ................................................................................................ CC-3 CC2. COCKPIT VOICE RECORDER.................................................................................. CC-4 RC-135V, T/N 64-14848, 30 April 2015 1 INTENTIONALLY LEFT BLANK 64-14848, 30 April 2015 2 DEPARTMENT OF THE AIR FORCE AIRCRAFT ACCIDENT INVESTIGATION BOARD OFFUTT AIR FORCE BASE, NEBRASKA 24 June 2015 MEMORANDUM FOR RECORD FROM: CAPTAIN [AIB Pilot Member] SUBJECT: Tab S2.1 – Accident Investigation Board (AIB); Class A Mishap, 30 Apr 15, RC135V – T/N 64-14848, 343 RS/55 WG, Offutt AFB, Nebraska 1. I am the Pilot Member for the RC-135V mishap convened at Offutt Air Force Base which occurred on 30 April 2015. I have reviewed the video footage contained in Tab S2.1: Hangar 2 West Security Camera in its entirety. This memorandum serves to document the factual timeline of the mishap, as observed in the footage. 2. Timeline in mm:ss from the start of the recording. 11:20 13:16 13:42 14:38 17:18 17:24 17:37 MA enters active runway from NW Hammerhead MA begins takeoff roll. MA comes to complete stop following abort. First egressing crewmember clear of aircraft First fire department response vehicle enters active runway Last egressing crewmember clear of aircraft First fire department response vehicle at aircraft 3. Please direct questions to me at DSN: or Commercial: . , Capt Pilot Member, Accident Investigation Board RC-135V, T/N 64-14848, 30 April 2015 CC-3 DEPARTMENT OF THE AIR FORCE AIRCRAFT ACCIDENT INVESTIGATION BOARD OFFUTT AIR FORCE BASE, NEBRASKA 25 June 2015 MEMORANDUM FOR RECORD FROM: CAPTAIN [AIB Pilot Member] SUBJECT: Tab L2.1 – Accident Investigation Board (AIB); Class A Mishap, 30 Apr 15, RC135V – T/N 64-14848, 343 RS/55 WG, Offutt AFB, Nebraska 1. I am the Pilot Member for the RC-135V mishap convened at Offutt Air Force Base which occurred on 30 April 2015. I have reviewed the video footage contained in Tab L2.1: Cockpit Voice Recorder in its entirety. This memorandum serves to document the portion of the voice record that is relevant to the mishap sequence. 2. List of Individuals/Facilities: Mishap Pilot (MP), Mishap Copilot (MCP), Mishap Evaluator Tactical Coordinator (METC), Mishap Navigator (MN), Mishap Raven 1 (MR1), Mishap Tactical Coordinator (MTC), Offutt Tower Local Control (OFF TWR LC), Offutt Command Post (OFF CP), Cessna 4987R (CESSNA), Unknown (UNK) 3. Timeline in hh:mm:ss from the start of the recording. 1:31:30 OFF TWR LC: SNOOP 71 Heavy, runway 12, wind calm, cleared for takeoff. Caution wake turbulence, heavy c-135 departure 1:31:35 MCP: SNOOP 71 Heavy is cleared for takeoff on runway 12 1:31:39 MP: Cleared for takeoff crew 1:31:40 MCP: Alright, lights...alright, ignition. Lights are set, IFF is set, TAT heat is on, Before Takeoff Checklist complete. Cleared for takeoff. 1:32:01 MP: Engine and flight instruments are checked, Pilot 1:32:04 MCP: ok 1:32:07 MP: Brake release, set power 1:32:14 CESSNA: Offutt Tower, Cessna 4987R, is inbound to Offutt with Hotel 1:32:21 OFF TWR LC: Cessna 4987R, Offutt Tower…[covered by interphone] 1:32:23 MULTIPLE: Fire, Fire, Fire… We’ve got a fire RC-135V, T/N 64-14848, 30 April 2015 CC-4 1:32:28 MN: Alright, better get on the EP items 1:32:31 UNK: Fire above the microwave 1:32:33 UNK: Fire above the galley. Fire above the galley. 1:32:34 MN: I’m gonna call for 311 1:32:36 METC: Tell tower, tell tower 1:32:38 MP: Tower Topcat, tower SNOOP 11 Heavy is, uh, egressing on the runway. Aborting the aircraft 1:32:44 OFF TWR LC: SNOOP 71 Heavy, Roger. Say nature of emergency, persons on board, fuel…[covered] 1:32:48 MP: Fire. SNOOP 11, SNOOP 11 Heavy has a fire. Roll the trucks at this time. 1:32:54 UNK: Get the chair. 1:32:54 OFF TWR LC: Roger 1:32:57 MP: Go ahead and… 1:32:57 MN: Alright 1:32:58 MP: Crew, Pilot. Ground Evacuation Checklist 1:33:00 MTC: Are you guys putting that out? 1:33:04 MN: Alright, are you gonna shut down the engines? 1:33:05 MP: Yup…flaps 30, speed brakes are down 1:33:13 MCP: Throttles idle…throttles 1:33:15 MP: Throttles idle 1:33:16 MCP: Starter switches as required, lights, TAT heat, depressurize, flaps 30 1:33:25 MP: Flaps are 30 1:33:28 MCP: Speed brakes zero 1:33:29 MP: Speed brakes are zero 1:33:30 MCP: Parking brake set RC-135V, T/N 64-14848, 30 April 2015 CC-5 1:33:31 MP: Parking brake set 1:33:32 MCP: Battery power switch emer 1:33:32 MP: Emer 1:33:33 MCP: Throttles cut-off 1:33:34 MP: Throttles. Shutting down throttles crew 1:33:37 MCP: Starter switches off 1:33:38 MP: Starter switch…[covered] 1:33:39 MCP: Fire switches pull if required 1:33:41 MP: Not required 1:33:42 MCP: Evacuation initiate. We already did that. External power switch trip. 1:33:45 MP: Crew, Pilot. Evacuation initiate 1:33:47 MCP: Battery power switch off 1:33:48 MP: Battery power switch is off 1:33:50 MCP: ESIS…[end of recording] 4. I certify this to be a true and exact transcript of the original recording. Please direct questions to me at DSN: or Commercial: , Capt Pilot Member, Accident Investigation Board RC-135V, T/N 64-14848, 30 April 2015 CC-6 DEPARTMENT OF THE AIR FORCE AIRCRAFT ACCIDENT INVESTIGATION BOARD OFFUTT AIR FORCE BASE, NEBRASKA 25 June 2015 MEMORANDUM FOR RECORD FROM: Board President SUBJECT: Medical Records – Accident Investigation Board (AIB); Class A Mishap, 30 Apr 15, RC-135V – T/N 64-14848, 343 RS/55 WG, Offutt AFB, Nebraska 1. I am the Board President for the AIB convened at Offutt Air Force Base for the mishap which occurred on 30 Apr 15. This memorandum documents the AIB’s review of the medical records of the Mishap Crewmembers (MC). 2. After a thorough review by members of the AIB, nothing relevant to the cause of the mishap was discovered in the MC’s medical records. All MC were in good health and had no performance-limiting illnesses prior to the mishap. All MC were current with their physical health assessments. No evidence of any unusual habits, behavior, or stress on the part of the MC were noted. 3. Subsequent to the mishap, four crewmembers were taken to the Bellevue Medical Center (BMC) complaining of headache and difficulty breathing due to smoke inhalation during the electrical fire. All four crewmembers were released from BMC the same day. There is no indication that any of the crewmembers suffered any injuries beyond minor smoke inhalation. 4. Please direct questions to me at DSN: or Commercial: , USAF President, Accident Investigation Board RC-135V, T/N 64-14848, 30 April 2015 INTENTIONALLY LEFT BLANK TAB DD FACTSHEETS DD1. 55TH WING FACT SHEET ....................................................................................... DD-3 DD2. 55TH OPERATIONS GROUP FACT SHEET .......................................................... DD-6 DD3. 343RD RECONNAISSANCE SQUADRON FACT SHEET .................................... DD-9 DD4. RC-135V/W RIVET JOINT FACT SHEET ............................................................. DD-11 DD5. L3 COMMUNICATIONS FACT SHEET................................................................ DD-15 RC-135V, T/N 64-14 848, 30 April 2015 1 INTENTIONALLY LEFT BLANK RC-135V, 64-14 848, 30 April 2015 2 U.S. Air Force Fact Sheet 55th WING The 55th Wing, located at Offutt Air Force Base, Neb., is Air Combat Command’s largest wing with a budget of more than $477 million annually, 49 aircraft, 32 squadrons and more than 7,000 employees. The wing conducts a global flying mission with worldwide reconnaissance and treaty verification tasked by our nation’s highest levels as well as the National Airborne Operations Center. Additionally, it provides base support to more than 50 associate units, including U.S. Strategic Command, the Air Force Weather Agency and a military community of more than 57,000. The wing is comprised of six groups, five located at Offutt AFB and one at Davis- Monthan AFB, Ariz. 55th Communications Group The 55th CG provides superior command, control, communications, and computers and knowledge management services for the 55th Wing, U.S. Strategic Command, the Air Force Weather Agency and more than 50 associate units at Offutt as well as cyber operations support for numerous Air Force and Department of Defense installations and missions. The group is comprised of more than 450 military, DOD civilian and contractor personnel that operate and maintain the Air Force’s most diverse array of cyber systems to include military satellite communications platforms, secure and non-secure voice, data and radio frequency networks, one-of-a-kind air traffic control and landing systems, hundreds of miles of fiber optic and copper cabling, as well as providing base-wide client systems, information assurance and knowledge operations services. The communications group also provides unprecedented Nuclear Command and Control and Alternate Missile Warning Center capabilities 24/7 for the Secretary of Defense and the President of the United States. 55th Electronics Combat Group The 55th ECG, located at Davis-Monthan, provides combat-ready EC-130H Compass Call aircraft, crews, maintenance and operational support to combatant commanders. The group also plans and executes information operations, including information warfare and electronic attack, in support of theater campaign plans. RC-135V, T/N 64-14848, 30 April 2015 DD-3 55th Maintenance Group The 55th MXG’s approximately 1,100 personnel are proud combat enablers, maintaining 29 combat ready C-135s and four Airborne Command and Control E-4B aircraft. The group executes an annual budget of $20 million and a 20,000-hour flying program to respond to Joint Chiefs of Staff-directed taskings providing critical reconnaissance worldwide; develop maintenance plans to support Airborne Command Post and National Airborne Operations Center missions; and support five geographically separated units. 55th Medical Group The 55th MDG is a four-squadron medical group that operates a full-service outpatient clinic with more than 700 staff providing comprehensive primary and specialty medical/dental care to the almost 28,000 members of Team Offutt. It also services almost 45,000 TRICARE eligible beneficiaries in the greater Omaha area. The medical group is collectively responsible for providing comprehensive health services to maintain the highest degree of readiness in support of contingency war mobilization and homeland defense plans for Offutt and its partner units including U.S. Strategic Command and the Air Force Weather Agency. 55th Mission Support Group The 55th MSG provides vital support to Offutt through engineering, security, mission support, services, supply, transportation, contracting and deployment readiness programs to more than 57,000 active duty, dependent and retiree personnel. This also includes more than 50 associated units, including U.S. Strategic Command, Air Force Weather Agency, the National Airborne Operations Center and presidential-tasked global reconnaissance missions. 55th Operations Group With more than 3,000 Airmen, 12 squadrons and one detachment, the 55th OG is the largest and most diverse operations group in the Air Force, flying all variants of the RC-135, OC-135, WC-135 and E-4B aircraft. The group operates these aircraft around the clock in every geographic command in support of the 55th’s global reconnaissance, contingency operations, treaty verification, National Command Authority support and command and control responsibilities. The group also supports the Federal Emergency Management Agency during times of natural disaster. Permanent overseas operating locations include RAF Mildenhall, England; Souda Bay Naval Support Activity, Crete and Kadena AB, Japan. The 55th OG also operates regularly from five temporary locations. 55th Wing Public Affairs 109 Washington Square, Suite 221 Offutt Air Force Base, NE 68113 ----Com'l: (402) 294-3663 DSN: 272-3663 E-mail: 55wg.paA@offutt.af.mil RC-135V, T/N 64-14848, 30 April 2015 DD-4 Offutt Air Force Base - Fact Sheet (Printable) : 55TH OPERATIONS GROUP Page 1 of 2 U.S. Air Force Fact Sheet 55TH OPERATIONS GROUP The 55th Operations Group, ACC's largest group, located at Offutt air Force Base, Nebraska, has operational control over 12 squadrons and two detachments worldwide. The group consists of approximately 3,200 personnel. It employs 46 aircraft, including 13 models of seven different types. Mission responsibility includes the Air Force's most diverse flying operations supporting worldwide reconnaissance, command and control, Presidential support, and nuclear treaty verification. The 55th Operations Group traces it's lineage to the 55th Pursuit (Interceptor) Group constituted on 20 November 1940 and activated 15 January 1941 at Hamilton Field, California. During World War II, the 55th Pursuit Group garnered two Distinguished Unit Citations. The group fostered 16 aces who were credited with 90 air-to-air victories. Its last mission flew on 21 April 1945 and inactivation occurred on 20 August 1946. On 24 February 1947, Strategic Air Command activated and redesignated the 55th Fighter Group as the 55th Reconnaissance group at MacDill Field, Florida, operating the RB-17. The newly activated group's mission consisted of aerial photography, mapping, charting, and photo reconnaissance missions, some of which flew around the globe. The group then converted to RB-29s and transferred to Topeka (later Forbes) AFB, Kansas, in 1948, but was again inactivated in October 1949. On 1 November 1950, the 55th Strategic reconnaissance group was activated as a "paper organization" with the tactical squadrons attached directly to the 55th Strategic Reconnaissance wing. The wing was bestowed with the awards and honors of the 55th Reconnaissance Group and moved to Ramey AFB, Puerto Rico. In 1952 the group was again inactivated on 16 June 1952 as the Air Force reorganized its wings into the tri-deputate system. As the end of the Cold War dawned in the early 1990s, the Air Force again underwent dramatic changes and reorganizations. the decision was made to return to the group organizational structure. In line with this decision, the 55th Strategic Reconnaissance Group was redesignated as the 55th Operations Group on 29 august 1991 and activated on 1 September 1991. It was assigned to the 55th Wing, Offutt AFB, Nebraska, along with four other groups. The 55th Operations Group activated with one of the largest and most diverse missions in the USAF. Since the end of the Cold War, the 55th Operations Group has maintained an unmatched operational tempo, supporting every US contingency worldwide. These missions have included but were not limited to reconnaissance, command and control, and airlift missions supporting Operations SOUTHERN WATCH, PROVIDE COMFORT, VIGILANT WARRIOR (Southwest Asia), PROVIDE PROMISE, DENY FLIGHT (Bosnia-Herzegovina), SUPPORT DEMOCRACY, UPHOLD DEMOCRACY (Haiti), and TIGER RESCUE (Yemen). Additionally, its squadrons have been called upon to support Distinguished Visitor airlift for the National Command Authorities, the Federal Emergency Management Agency, and numerous exercises. Twenty-four hours a day, three hundred sixty-five days a year, there is a 55th Operations group aircraft airborne or airman deployed somewhere around the globe, thus earning its unofficial motto: "The Sun Never Sets on the Fightin' Fifty-Fifth." http://www.offutt.af.mil/library/factsheets/factsheet_print.asp?fsID=4308&page=1 RC-135V, T/N 64-14848, 30 April 2015 DD-6 6/25/2015 Offutt Air Force Base - Fact Sheet (Printable) : 55TH OPERATIONS GROUP Page 2 of 2 For more informantion, contact: 55th Wing Public Affairs 109 Washington Street, Suite 221 Offutt AFB, NE 68113 DSN 271-3663 (402) 294-3663 http://www.offutt.af.mil/library/factsheets/factsheet_print.asp?fsID=4308&page=1 RC-135V, T/N 64-14848, 30 April 2015 DD-7 6/25/2015 From: To: Subject: Date: Attachments: FW: 343rd fact sheet Thursday, June 25, 2015 5:54:48 PM 343 Fact Sheet.docx -----Original Message----From: Sent: Thursday, June 25, 2015 4:36 PM To: Subject: FW: 343rd fact sheet AIB Pilot Member DSN: -----Original Message----From: Sent: Thursday, June 25, 2015 4:27 PM To: Cc: Subject: RE: 343rd fact sheet , Here is the fact sheet I compiled.  Let me know if you need anything else. , Major, USAF Director of Operations, 343d RS RC-135V, T/N 64-14848, 30 April 2015 DD-9 The 343d Reconnaissance Squadron is rooted in Air Force heritage dating back to World War II. The 343d continues its proud service by supporting Combatant Commands (COCOMs) on a global scale. The mission of the 343d Reconnaissance Squadron is to provide worldwide reconnaissance for national command authorities, COCOMs, the intelligence community, and war fighters. Today, the 343d RS flies the RC-135V/W Rivet Joint reconnaissance aircraft supporting theater and national level consumers with near real-time on-scene intelligence collection, analysis and dissemination capabilities. The aircraft is an extensively modified C-135 and it’s modifications allows the mission crew to detect, identify and geolocate signals throughout the electromagnetic spectrum. Missions are normally tasked by the Joint Chiefs of Staff during peacetime operations and by the COCOM during wartime. The squadron supports the worldwide missions of the Department of Defense to keep the United States aware of potential adversaries. The 343d Reconnaissance Squadron's history began on February 1, 1943 as the 343d Fighter Squadron at McChord Field, Washington. During the Second World War, the squadron flew the P-51 Mustang and P-38 Lightning fighter aircraft, providing escort to heavy bombers of Eighth Air Force in the strategic air campaign against Nazi Germany. It became the 343d Strategic Reconnaissance Squadron in 1947, part of Strategic Air Command (SAC). During the early years of the Cold War, the 343d flew the RB-29, RB-50 and RB-47 reconnaissance, or "ferret", aircraft. These were variants of bombers outfitted with sophisticated electronic surveillance gear, some of which are on display at the SAC Museum. Their mission was to probe Soviet air defenses and stimulate their integrated air defense systems (IADS). The new RC-135, which the squadron still flies, arrived in 1967. For 15 years, the squadron continued to fly its peacetime reconnaissance mission. However, in the early 1980's that peace time mission began to change. The rise of terrorist nations, the fall of the Soviet Union and the realization of the tremendous capabilities of the RC-135 brought new missions and new changes to the 343d. Since then, the 343d has played a role in countless operations including the liberation of Grenada and Panama, the 1986 Libyan raids, the Persian Gulf War, combat air patrols in the no-fly zones over the northern and southern Iraq, the Bosnian conflicts, Operations Iraqi and Enduring Freedom, RC-135V, T/N 64-14848, 30 April 2015 DD-10 Page 1 of 4 RC-135V/W Rivet Joint Published May 23, 2012 PRINT E-MAIL Mission The RC-135V/W Rivet Joint reconnaissance aircraft supports theater and national level consumers with near real time on-scene intelligence collection, analysis and dissemination capabilities. Features The aircraft is an extensively modified C-135. The Rivet Joint's modifications are primarily related to its on-board sensor suite, which allows the mission crew to detect, identify and geolocate signals throughout the electromagnetic spectrum. The mission crew can then forward gathered information in a variety of formats to a wide range of consumers via Rivet Joint's extensive communications suite. The interior seats more than 30 people, including the cockpit crew, electronic warfare officers, intelligence operators and in-flight maintenance technicians. The Rivet Joint fleet was re-engined with CFM-56 engines with an upgraded flight deck instrumentation and navigational systems to FAA/ICAO standards. These standards include conversion from analog readouts to a digital "glass cockpit" configuration. All Rivet Joint airframe and mission systems modifications are overseen by L-3 Communications (previously Raytheon), under the oversight of Air Force Materiel Command. Background The current RC-135 fleet is the latest iteration of modifications to this pool of -135 aircraft going back to 1962. Initially employed by Strategic Air Command to satisfy nationally tasked intelligence collection requirements, the RC-135 fleet has also participated in every sizable armed conflict involving U.S. assets during its tenure. RC-135s were present supporting operations in Vietnam, the Mediterranean for Operation El Dorado Canyon, Grenada for Operation Urgent Fury, Panama for Operation Just Cause, and Southwest Asia for operations Desert Shield, Desert Storm, Enduring Freedom and Iraqi Freedom. RC-135s have maintained a constant presence in Southwest Asia since the early 1990s. All RC-135s are assigned to Air Combat Command. The RC-135 is permanently based at Offutt Air Force Base, Neb., and operated by the 55th Wing, using various forward deployment locations worldwide. More recently, RC-135s have also supported Operation Allied Force in Kosovo, and Operation Odyssey Dawn/Unified Protector in Libya http://www.af.mil/DesktopModules/ArticleCS/Print.aspx?PortalId=1&ModuleId=854&Art... 6/25/2015 RC-135V, T/N 64-14848, 30 April 2015 DD-11 Page 2 of 4 General Characteristics Primary Function: Reconnaissance Contractor: L-3 Communications Power Plant: Four CFM International F108-CF-201 high bypass turbofan engines Thrust: 21,600 pounds each engine Wingspan: 131 feet (39.9 meters) Length: 135 feet (41.1 meters) Height: 42 feet (12.8 meters) Weight: 173,000 pounds (78,743 kilograms) Maximum Takeoff Weight: 297,000 pounds (133,633 kilograms) Fuel Capacity: 130,000 pounds (58,967 kilograms) Speed: 500+ miles per hour (Mach.66) Range: 3,900 miles (6,500 kilometers) Ceiling: 50,000 feet (15,240 meters) Crew: (flight crew) five (augmented) - three pilots, two navigators; (mission flight crew) 21-27, depending on mission requirements, minimum consisting of three electronic warfare officers, 14 intelligence operators and four inflight/airborne maintenance technicians Unit Cost: unavailable Initial operating capability: January 1964 Inventory: Active force, 17; Reserve, 0; Guard, 0 http://www.af.mil/DesktopModules/ArticleCS/Print.aspx?PortalId=1&ModuleId=854&Art... 6/25/2015 RC-135V, T/N 64-14848, 30 April 2015 DD-12 Page 3 of 4 PHOTO DETAILS / DOWNLOAD HI-RES The RC-135V/W Rivet Joint reconnaissance aircraft supports theater and national level consumers with near real time on-scene intelligence collection, analysis and dissemination capabilities. PHOTO DETAILS / DOWNLOAD HI-RES http://www.af.mil/DesktopModules/ArticleCS/Print.aspx?PortalId=1&ModuleId=854&Art... 6/25/2015 RC-135V, T/N 64-14848, 30 April 2015 DD-13 Page 4 of 4 The RC-135V/W Rivet Joint reconnaissance aircraft supports theater and national level consumers with near real time on-scene intelligence collection, analysis and dissemination capabilities. http://www.af.mil/DesktopModules/ArticleCS/Print.aspx?PortalId=1&ModuleId=854&Art... 6/25/2015 RC-135V, T/N 64-14848, 30 April 2015 DD-14 Company Profile - About L-3 - L-3 Page 1 of 1 Company Profile L-3 is a prime contractor in aerospace systems and national security solutions. L-3 is also a leading provider of a broad range of communication and electronic systems and products used on military and commercial platforms. Headquarters L-3 Communications 600 Third Avenue New York, NY 10016 Phone: (212) 697-1111 Fax: (212) 490-0731 www.L-3com.com Executive Management Michael T. Strianese Chairman, President and Chief Executive Officer Curtis Brunson Executive Vice President of Corporate Strategy and Development Ralph G. D'Ambrosio Senior Vice President and Chief Financial Officer Steven M. Post Senior Vice President, General Counsel and Corporate Secretary Richard A. Cody Senior Vice President of Washington Operations Key Information Stock Symbol NYSE:LLL Year Founded 1997 2014 Annual Sales $12.1 billion Employees Approximately 45,000 Corporate Structure L-3 is composed of four business segments: Aerospace Systems Aerospace Systems delivers integrated solutions for the global ISR market and provides modernization, upgrade, sustainment, and maintenance and logistics support for a wide variety of aircraft and ground systems. Electronic Systems Electronic Systems provides a broad range of components, products, subsystems, systems and related services for military and commercial customers. Communication Systems Communication Systems delivers products and services for the global communications market, specializing in strategic and tactical airborne, space, ground and sea-based communication systems. National Security Solutions National Security Solutions provides cybersecurity solutions, high-performance computing, enterprise IT services, analytics and intelligence analysis. http://www.l-3com.com/about-l-3/company-profile.html RC-135V, T/N 64-14848, 30 April 2015 DD-15 6/27/2015 ISR - L-3 Mission Integration Page 1 of 1 Home Contact Us Suppliers Employee Information Webmaster SPYDR® Small Manned ISR SPYDR® is a next-generation small manned Intelligence, Surveillance and Reconnaissance (ISR) platform. For more information, click here. Latest News Company Core Competency Trade Shows Sept 15-19 African Aerospace and Defense Sept 17-19 AFA Air & Space Conference View more trade shows L-3 MID is a world-class systems integration organization specializing in the complex ISR capabilities and equipment, aircraft modification and maintenance, command, control and communications, network-enabling technologies, SIGINT systems and full life-cycle systems support and sustainment. For more products and services, click here. Press Releases L-3 Mission Integration Co-Sponsors 2014 Wings Over the Heartland Event L-3 Unveils SPYDR II – A New, Affordable Tactical ISR Solution L-3 Mission Integration’s Multi-Mission Aircraft Program Achieves New Milestone View more releases The Power Of Engineering Excellence © Copyright 2014 L-3 Communications Holdings, Inc. All rights reserved. L-3 uses this website as a channel of distribution of material company information. Financial and other material regarding L-3 is routinely posted on this website for immediate access. DoD endorsement is neither implied nor intended. http://www2.l-3com.com/mid/index.htm RC-135V, T/N 64-14848, 30 April 2015 DD-16 6/27/2015