N587FE

Part: BATTERY PACK — WARNING MESSAGE (EMERGENCY LIGHTS) · airframe 92,146 hrs · 21,925 cycles

DURING EMERGENCY LIGHTS TEST, RECEIVED LEVEL 1 EMER LT BAT 1 LO. REFERENCED QRH. REMOVED AND REPLACED EMERGENCY LIGHTING POWER SUPPLY IAW FIM 33-51-00-2 AND AMM 33-51-01-5. TESTED NORMAL ACFT OKAY FOR SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 91,715 hrs · 21,778 cycles

AFTER PERFORMING EMERGENCY LIGHT TEST WE RECEIVED A LEVEL 1 ALERT EMER LT BATB6 LO. REMOVED AND REPLACED EMER LIGHTS BATT REF AMM 33-51-01-4; OPS CHECK SATISFACTORY.

Part: VALVE — LEAKING (N/A) · airframe 91,641 hrs · 21,759 cycles

ON APPROACH TO FINAL RKSI RECEIVED LEVEL 1 HYD QTY LO. CARRIED OUT MISSED APPROACH TO RUN QRH. ON VECTORS FOR SECOND APPROACH RECEIVED HYD 2 OFF. ALSO RECEIVED ENG 2 FADEC FAULT (SEPARATE WRI WRITE UP). RAN QRH. DECLARED EMERGENCY WITH RKSI TOWER AND EMERGENCY EQUIPMENT LOOKED US OVER AFTER LANDING. THEN TAXIED TO PARKING. ***EMERGENCY DECLARED*** REMOVED & REPLACED INBD FLAPS LOCK VALVE (MPN : AYG7323-5509 S/N : DAC1732), BLED THE FLAP LOCK V/V AND PERFORMED FLAP OPERATION/RANGE OF MOVEMENT TEST, THEN ALL TEST PASSED AND NO LEAKAGE NOTED PER AMM 27-52-11-4. A/C OK FOR SERVICE.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-T0331129 C PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57500519 FOR DETAILS)

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND LOWER FACE EXCEED LIMIT BASE THE DIFFERENCE BETWEEN DRAWING AND CMM MAXIMUM REWORK LIMITS FOR BARREL NUT HOLE. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # 1- 5750-T0365254 PART 1 STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00578 ATTACHED E.A. # 1-5750-T0365254 PART 1 FOR DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-07 AND E.A.# 1-5750-T0331130 C PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57500514 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-T0331130 C PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57500514 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-T0331129 C PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57500519 FOR DETAILS)

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 90,262 hrs · 21,364 cycles

DURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION FOUND CRACK INDICATION APPROXIMATELY 0.2" IN LENGTH AT LEFT HAND WING CORNER NUMBER 5 SLAT ACTUATOR ACCESS DOOR AT FORWARD INBOARD CORNER AT STATION XOS 490.85. LEFT HAND WING CORNER NUMBER 5 SLAT ACTUATOR ACCESS DOOR AT FORWARD INBOARD CORNER AT STATION XOS 490.85 REPAIR CARRIED OUT AS PER EA # 1-5710-132361 A PART 2 TITLE : WINGS - LH WING LEADING EDGE - EXISTING SKIN REPAIRS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 90,262 hrs · 21,364 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON FLOOR BEAM AT MAIN DECK CARGO COMPARTMENT STATION 859 BETWEEN X= -19 AND X= -35. EXISTING REPAIR ON FLOOR BEAM AT MAIN DECK CARGO COMPARTMENT STATION 859 BETWEEN X= -19 AND X= -35 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH EA #1- 5310-78024, TITLE: FUSELAGE - FLOOR BEAMS - ELONGATED HOLES AT STATION RBL 27.5 FS 859 - REPAIR BUT REPAIR CLASSIFIED AS MINOR. EA#1-5310-78024 REVISION A ISSUED TO REVISE CLASSIFICATION FROM MINOR TO MAJOR. EO 1-5100-7-5001 B6 PART1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: FLOORBEAM — NONE (N/A) · airframe 90,262 hrs · 21,364 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON FLOOR BEAM AT MAIN DECK CARGO COMPARTMENT STATION 839 BETWEEN X= -19 AND X= -35. EXISTING REPAIR ON FLOOR BEAM AT MAIN DECK CARGO COMPARTMENT STATION 839 BETWEEN X= -19 AND X= -35 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH EA #1- 5310-78025, TITLE: FUSELAGE - FLOOR BEAMS - ELONGATED HOLES AT STATION RBL 27.5 FS 839 - REPAIR BUT REPAIR CLASSIFIED AS MINOR. EA#1-5310-78025 REVISION A ISSUED TO REVISE CLASSIFICATION FROM MINOR TO MAJOR. EO 1-5100-7-5001 B6 PART1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SKIN — NONE (ZONE 814) · airframe 90,262 hrs · 21,364 cycles

CENTER CARGO - DOOR , FORWARD BOTTOM CORNER STATION 1717.500 TO STATION 1708.437 FOUND CHAFFING. CENTER CARGO - DOOR FORWARD BOTTOM CORNER STATION 1717.500 TO STATION 1708.437 CHAFFING MARKED FOUND EXCEED LIMIT AS PER SRM 52-00-00-2R FIGURE 202 REPAIR GENERAL. REPAIR CARRIED OUT AS PER E.A 1-5230-T0365222 P1 TITLE : DOORS - CARGO DOOR / HYD SYS - CENTER CARGO DOOR - REPAIR FOR OUTER SKIN AT FWD LOWER CORNER. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — UNKNOWN (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

AT THE TIME OF AIRCRAFT INSPECTION ON FEDEX EO 1-5100-7-5001 PART1, FOUND 01 EACH EXISTING REPAIR ON PRIMARY STRUCTURE AT LEFT HAND WING FIXED LEADING EDGE INNER COMPARTMENT AT XOS 584.892 WAS NOT DOCUMENTED FOR EVALUATION. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE INNER COMPARTMENT AT XOS 584.892 EVALUATED AND FOUND FABRICATED PART WITH PART MARKED "FX ARB2931-13" INSTALLED IN ACCORDANCE WITH SRM 51-31-01-0G AND DOUGLAS DRAWING ARB2931 REVISION H. EO #1-5100-7-5001 B6 PART1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING OUTBOARD FLAP VANE NUMBER 1 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE NUMBER 1 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA #1- 5750-T0365265 PART 1 STEP 1A, TITLE: WINGS - FLIGHT SURFACES - LH WING - OUTBD FLAP VANE ASSY - TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING OUTBOARD FLAP VANE NUMBER 4 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE NUMBER 4 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA #1- 5750-T0365265 PART 1 STEP 1A, TITLE: WINGS - FLIGHT SURFACES - LH WING - OUTBD FLAP VANE ASSY - TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00739 ATTACHED EA #1-5750-T0365265 PART 1 FOR DETAILS.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING OUTBOARD FLAP VANE NUMBER 5 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE NUMBER 5 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA #1- 5750-T0365265 PART 1 STEP 1A, TITLE: WINGS - FLIGHT SURFACES - LH WING - OUTBD FLAP VANE ASSY - TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00739 ATTACHED EA #1-5750-T0365265 PART 1 FOR DETAILS.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND WING OUTBOARD FLAP VANE NUMBER 1 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP VANE NUMBER 1 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA #1- 5750-T0365264 PART 1 STEP 1A, TITLE: WINGS - FLIGHT SURFACES - RH WING - OUTBD FLAP VANE ASSY - TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND WING OUTBOARD FLAP VANE NUMBER 2 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP VANE NUMBER 2 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA #1- 5750-T0365264 PART 1 STEP 1A, TITLE: WINGS - FLIGHT SURFACES - RH WING - OUTBD FLAP VANE ASSY - TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00773 ATTACHED EA #1-5750-T0365264 PART 1 FOR DETAILS.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND WING OUTBOARD FLAP VANE NUMBER 4 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP VANE NUMBER 4 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA #1- 5750-T0365264 PART 1 STEP 1A, TITLE: WINGS - FLIGHT SURFACES - RH WING - OUTBD FLAP VANE ASSY - TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00773 ATTACHED EA #1-5750-T0365264 PART 1 FOR DETAILS.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING OUTBOARD FLAP VANE NUMBER 3 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE NUMBER 3 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA #1- 5750-T0365265 PART 1 STEP 1A, TITLE: WINGS - FLIGHT SURFACES - LH WING - OUTBD FLAP VANE ASSY - TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00739 ATTACHED EA #1-5750-T0365265 PART 1 FOR DETAILS.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP OUTBOARD AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-04 AND E.A. # 1-5750-78012 A PART 2 STEP 2 AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1- 5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE (FLAP SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND WING OUTBOARD FLAP VANE NUMBER 3 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP VANE NUMBER 3 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA #1- 5750-T0365264 PART 1 STEP 1A, TITLE: WINGS - FLIGHT SURFACES - RH WING - OUTBD FLAP VANE ASSY - TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00773 ATTACHED EA #1-5750-T0365264 PART 1 FOR DETAILS.

Part: DOUBLER — UNKNOWN (ZONE 520) · airframe 90,262 hrs · 21,364 cycles

AGING AIRCRAFT - EXISTING BEADED DOUBLER REPAIR FOUND AT LEFT HAND WING FIXED LEADING EDGE INNER COMPARTMENT XOS 649. EXISTING BEADED DOUBLER REPAIR AT LEFT HAND WING FIXED LEADING EDGE INNER COMPARTMENT XOS 649 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57- 40-02-2R REPAIR 15 FIGURE 203. EO 1-5100-7-5001 B6 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING OUTBOARD FLAP VANE NUMBER 2 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE FOUND CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE NUMBER 2 (FROM INBOARD) TEE FITTING FORWARD ATTACH BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA #1- 5750-T0365265 PART 1 STEP 1A, TITLE: WINGS - FLIGHT SURFACES - LH WING - OUTBD FLAP VANE ASSY - TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00739 ATTACHED EA #1-5750-T0365265 PART 1 FOR DETAILS.

Part: SKIN — NONE (N/A) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND WING LEADING EDGE # 3 SLAT LOWER SKIN SURFACE FOUND WITH DEEP CHAFFED MARK AT STATION XOS 479.957. RIGHT HAND WING LEADING EDGE # 3 SLAT LOWER SKIN SURFACE AT STATION XOS 479.957 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 3 FIGURE 201 AND EA # 1-5750- T0365332 PART 1 TITLE : WINGS - FLIGHT SURFACES - REPAIR ON RH WING NO 3 SLAT INNER SKIN - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-T0331130 C PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57500514 FOR DETAILS)

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-08 AND E.A. # 1-5750-T0365299 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00761 ATTACHED E.A. # 1-5750-T0365299 PART 1 FOR DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.# 1-5750-T0331129 C PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI : 57500519 FOR DETAILS)

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # 1-5750-T0365299 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00761 ATTACHED E.A. # 1-5750-T0365299 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # 1-5750-T0365299 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00761 ATTACHED E.A. # 1-5750-T0365299 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # 1-5750-T0365299 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-08 AND E.A. # 1-5750-T0365299 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00761 ATTACHED E.A. # 1-5750-T0365299 PART 1 FOR DETAILS.

Part: SKIN — CRACKED (N/A) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND WING DROOPED LEADING EDGE UPPER SKIN SURFACE FOUND CRACK AT AROUND FASTENER HOLE AREA STATION XDLE 325.114. RIGHT HAND WING DROOPED LEADING EDGE UPPER SKIN SURFACE AT STATION XDLE 325.114 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 5 FIGURE 201. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-156846 F PART 2 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500472 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT INBOARD LUG BORE FOUND CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT INBOARD LUG BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-156845 F PART 2 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500467 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT INBOARD LUG BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT INBOARD LUG BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 03 AND E.A. # 1-5750-156846 F PART 2 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500472 FOR DETAILS)

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 03 AND E.A. # 1-5750-156845 F PART 2 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57500467 FOR DETAILS)

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # 1-5750-T0365254 PART 1 STEP 1B AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00578 ATTACHED E.A. # 1-5750-T0365254 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. # 1-5750-T0365211 PART 1 STEP 1C AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00688 ATTACHED E.A. # 1-5750-T0365211 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-09 AND E.A. # 1-5750-T0365211 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00688 ATTACHED E.A. # 1-5750-T0365211 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. # 1-5750- T0365211 PART 1 STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00688 ATTACHED E.A. # 1-5750-T0365211 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. # 1-5750-T0365211 PART 1 STEP 1D AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00688 ATTACHED E.A. # 1-5750-T0365211 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-09 AND E.A. # 1-5750-T0365211 PART 1 STEP 1C AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00688 ATTACHED E.A. # 1-5750-T0365211 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. # 1-5750-T0365211 PART 1 STEP 1D AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # 1-5750-T0365254 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00578 ATTACHED E.A. # 1- 5750-T0365254 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED BY MACHINING AS PER MD-11 CMM 57-44-09 AND FOUND EXCEED LIMIT. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-09 AND E.A. # 1-5750-T0365211 PART 1 STEP 1B AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00688 ATTACHED E.A. # 1-5750-T0365211 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,262 hrs · 21,364 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. # 1-5750-T0365211 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00688 ATTACHED E.A. # 1-5750-T0365211 PART 1 FOR DETAILS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 90,262 hrs · 21,364 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK ALONG X = 8.5 CORROSION FOUND ON FLANGE BETWEEN STATION 5-05 AND STATION 5-113. MAIN DECK CARGO COMPARTMENT FLOOR AT SEAT TRACK FLANGE BETWEEN STATION 5-05 AND STATION 5-113 , X = 8.5 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1531/5-0 TO STATION 1531/5-123 , X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1527) · airframe 90,262 hrs · 21,364 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK ALONG X = 8.5 FLANGE AT STATION 1527 FOUND CORRODED. MAIN DECK CARGO COMPARTMENT FLOOR AT SEAT TRACK FLANGE STATION 1527 X = 8.5 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1.CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1451 TO STATION 1531/5-0 , X= 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. # 1-5750-78011 A PART 2 STEP 1, TITLE: WINGS- TRAILING EDGE FLAPS- TRAILING EDGE & TRAILING EDGE DEVICES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00494 ATTACHED E.A. # 1-5750-78011 A PART 2 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. # 1-5750-78011 A PART 2 STEP 1, TITLE: WINGS- TRAILING EDGE FLAPS- TRAILING EDGE & TRAILING EDGE DEVICES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 09 AND E.A. # 1-5750-78011 A PART 2 STEP 1, TITLE: WINGS- TRAILING EDGE FLAPS- TRAILING EDGE & TRAILING EDGE DEVICES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00494 ATTACHED E.A. # 1-5750-78011 A PART 2 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-09 AND E.A. # 1-5750-78011 A PART 2 STEP 1, TITLE: WINGS- TRAILING EDGE FLAPS- TRAILING EDGE & TRAILING EDGE DEVICES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00494 ATTACHED E.A. # 1-5750-78011 A PART 2 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-09 AND E.A. # 1-5750-78011 A PART 2 STEP 1, TITLE: WINGS- TRAILING EDGE FLAPS- TRAILING EDGE & TRAILING EDGE DEVICES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00494 ATTACHED E.A. # 1-5750-78011 A PART 2 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 09 AND E.A. # 1-5750-78011 A PART 2 STEP 1, TITLE: WINGS- TRAILING EDGE FLAPS- TRAILING EDGE & TRAILING EDGE DEVICES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00494 ATTACHED E.A. # 1-5750-78011 A PART 2 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 500) · airframe 90,262 hrs · 21,364 cycles

LEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 09 AND E.A. # 1-5750-78011 A PART 2 STEP 1, TITLE: WINGS- TRAILING EDGE FLAPS- TRAILING EDGE & TRAILING EDGE DEVICES- EO 1-5750-7-5002- LH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00494 ATTACHED E.A. # 1-5750-78011 A PART 2 FOR DETAILS.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND AFT LOWER FUSELAGE - APU EXHAUST DOOR CUTOUT UPPER FORWARD CORNER SKIN STATION 2140 AT LONGERON - 36 RIGHT CRACKED. RIGHT HAND AFT LOWER FUSELAGE - APU EXHAUST DOOR CUTOUT UPPER FORWARD CORNER AT STATION 2140 LONGERON - 36 RIGHT CRACKED SKIN AREA REPAIRED AS PER EA # 1-5330- T0365377 PART 1 TITLE : FUSELAGE - PLATES & SKINS - TAIL AFT BODY - CRACK FOUND ON RH SKIN AT STA 2140 , L - 36R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 731. LEFT HAND WING FIXED LEADING EDGE INTERNAL DOUBLER AT STATION XOS 731 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 90,262 hrs · 21,364 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 645. RIGHT HAND WING FIXED LEADING EDGE INTERNAL DOUBLER AT STATION XOS 645 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 90,262 hrs · 21,364 cycles

LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 610. LEFT HAND WING FIXED LEADING EDGE INTERNAL DOUBLER AT STATION XOS 610 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CRACKED (N/A) · airframe 90,262 hrs · 21,364 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK ALONG X = 8.5 FOUND WITH CROWN CRACKED AT STATION 1541. MAIN DECK CARGO COMPARTMENT FLOOR , CRACKED SEAT TRACK AT STATION 1541 X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1571 TO STATION 1531/5-123 X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 89,350 hrs · 21,114 cycles

EMERGENCY LIGHTING BAT LO ALERT ON PREFLIGHT REPLACED FWD EMERGENCY LIGHTING POWER SUPPLY. OPS CHECKS SATISFACTORY

Part: ENGINE — FLAMED OUT (NR 2) · airframe 89,297 hrs · 21,094 cycles

NUMBER TWO ENGINE FLAMED OUT WITH THROTTLE ADVANCE FOR TAKE OFF. RAN QRH CONTACTED MOCC, RESTARTED ENGINE, NORMAL START AND CLIMB OUT. SHGN 18MAY21 08:25 MEM U STARTED AND RAN ENGINE #2 FOR 5 MINUTES IN REFERENCE PER MD11 JRH, ENGINE #2 STARTED GOOD AND ALL THE PARAMETERS ARE WITHIN LIMITS. A/C HAD SAT ON GROUND FOR EXTEND TIME BEFORE DEPARTURE THIS RESULTED IN #2 ENGINE FUEL STRAVATION CAUSEING FLAME OUT NO FUTHER MX ACTION REQUIRED OK FOR SERVICE.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 89,297 hrs · 21,094 cycles

ENGINE 2 FLAMEOUT AFTER ADDING POWER FOR TAKEOFF. RAN QRH CONTACTED MOCC , NORMAL RELIGHT AND TAKEOFF. SHGN 18MAY21 08:18 MEM U STARTED AND RAN ENGINE #2 FOR 5 MINUTES IN REFERENCE PER MD11 JRH, ENGINE #2 STARTED GOOD AND ALL THE PARAMETERS ARE WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,447 hrs · 20,047 cycles

CABIN - SEAT TRACK AT STATION 455 TO STATION 475 X = 0 FOUND CORROSION . CABIN AT SEAT TRACK STATION 455 TO STATION 475 X = 0 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-31-01-0G AT STATION 421 TO STATION 495 X = 0 . SEAT TRACK REWORKED BY MACHINING AS PER DOUGLAS DRAWING SP11530031 REVISION D . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (LT WING) · airframe 85,447 hrs · 20,047 cycles

LEFT WING LEADING EDGE COMPARTMENT APPROXIMATELY AT STATION XOS 761 , BEADED DOUBLER FOUND WITH CRACKS. LEFT WING LEADING EDGE COMPARTMENT STATION XOS 761 BEADED DOUBLER CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,447 hrs · 20,047 cycles

REWORK: MAIN DECK FLOOR SEAT TRACK FOUND CORROSION AT STATION 1620 - 1661 , X = 75.25 . MAIN DECK FLOOR AT SEAT TRACK STATION 1620 TO STATION 1661 X = 75.25 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1611 TO STATION 1671 X = 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,447 hrs · 20,047 cycles

REWORK : MAIN DECK FLOOR SEAT TRACK FOUND CORROSION AT STATION 1821 X = - 75.25 . MAIN DECK FLOOR AT SEAT TRACK STATION 1821 X = - 75.25 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED AS PER E.A. # : 1-5321-T0350490 P1 . TITLE : FUSELAGE - CARGO COMP FLOORS - SEAT TRACK CORROSION STATION 1761 - 1887 , X = - 75.25 - PTF VARIATION DRAWING - SRM SPLICE REPAIR . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: INTERCOSTAL — CRACKED (EMPENNAGE) · airframe 85,447 hrs · 20,047 cycles

EMPENNAGE LEFT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL FOUND CRACK. EMPENNAGE LEFT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL CARRIED OUT REPAIR AS PER EA #1-5330-T0350369P1. TITLE: STABILIZERS- VERTICAL STABILIZER- REAR CENTER SPAR TO REAR SPAR LOWER PANEL- CRACK FOUND ON LH INTERCOSTAL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,447 hrs · 20,047 cycles

CABIN , SEAT TRACK AT STATION 1408 , X = 47.5 CROWN DAMAGED . CABIN , SEAT TRACK AT STATION 1408 , X = 47.5 DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1391 TO EXISTING SPLICE STATION 1491 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,447 hrs · 20,047 cycles

CABIN , FOUND SEAT TRACK AT STATION AT STATION 1151 , X = 47.5 CROWN DAMAGED . CABIN AT SEAT TRACK STATION 1151 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO EXISTING SPLICE STATION 1129 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,447 hrs · 20,047 cycles

CABIN , FOUND SEAT TRACK AT STATION 1289 X = 47.5 CROWN DAMAGED . CABIN AT SEAT TRACK STATION 1289 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO STATION 1311 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,447 hrs · 20,047 cycles

CABIN , FOUND SEAT TRACK AT STATION 1545 , X = 47.5 CROWN DAMAGED . CABIN , SEAT TRACK AT STATION 1545 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1571 TO EXISTING SPLICE STATION 5-123/1531 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,447 hrs · 20,047 cycles

CABIN , FOUND SEAT TRACK AT STATION 5-6 , X = 47.5 CROWN DAMAGED . CABIN AT SEAT TRACK STATION 5-6 , X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-63 TO EXISTING SPLICE STATION 5-0/1531 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,447 hrs · 20,047 cycles

CABIN , FOUND COMPARTMENT SEAT TRACK AT STATION 1425 , X = 47.5 CROWN DAMAGED . CABIN AT SEAT TRACK STATION 1425 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1391 TO EXISTING SPLICE STATION 1491 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REFER TO SNRM N01012 FOR WORK DETAILS . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (RT WING) · airframe 85,447 hrs · 20,047 cycles

RIGHT WING FIXED LEADING COMPARTMENT STATION XOS 764 BEAD DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 85,447 hrs · 20,047 cycles

HFEC INSPECTION CARRIED OUT AT PSE SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT LEFT HAND FORWARD FLANGE OF THE REAR UPPER SPAR LEFT HAND REAR SPAR CAP FORWARD FLANGE LOCATED AT UPPER SECTION OF THE #4 BANJO FITTING OF LOWER VERTICAL STABILIZER STATION Y= 2164 CRACKED APPROXIMATELY 1.3" TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAIR 5. REPAIR CARRIED OUT ON LEFT HAND #4 BANJO FITTING AS PER SRM 55-30-02-2R FIGURE 202 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT 5400 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2700 FLIGHT CYCLES AS PER SRM 55-30-02-2R TABLE 203 FIGURE 202 REPAIR 5.

Part: DOUBLER — CRACKED (RT WING) · airframe 85,447 hrs · 20,047 cycles

RIGHT WING FIXED LEADING COMPARTMENT, STATION XOS 790 BEAD DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 85,447 hrs · 20,047 cycles

HFEC INSPECTION CARRIED OUT AT PSE, LOWER VERTICAL STABILIZER SPAR. FOUND A CRACK INDICATION AT THE RIGHT FORWARD FLANGE OF THE REAR UPPER SPAR. THE RIGHT REAR SPAR CAP FORWARD FLANGE LOCATED AT UPPER SECTION OF THE NR 4 BANJO FITTING OF LOWER VERTICAL STABILIZER STATION Y= 2164 WAS CRACKED APPROXIMATELY 2.1 INCHES, TRIMMED IAW SRM 55-30-02-2R, FIGURE 201, REPAIR 5. REPAIRED IAW SRM 55-30-02-2R, FIGURE 202, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (OBSERVER'S SEAT) · airframe 85,447 hrs · 20,047 cycles

COCKPIT, RIGHT OBSERVER SEAT BASE WEB AT BS 360 FOUND TO HAVE A CRACKED LIGHTENING HOLE. THE WEB WAS REPAIRED IAW SRM 53-10-51-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 85,447 hrs · 20,047 cycles

RIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 906 STRINGER FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING COMPARTMENT STATION XOS 906 STRINGER AS PER SRM 57-40-03-2R FIGURE 202 REPAIR 2 .REPAIR CLASSIFIED AD MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 85,447 hrs · 20,047 cycles

RIGHT WING, FIXED LEADING COMPARTMENT STATION XOS 820 BEAD DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 85,447 hrs · 20,047 cycles

RIGHT WING, FIXED LEADING COMPARTMENT STATION XOS 648 BEAD DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1721) · airframe 85,447 hrs · 20,047 cycles

CABIN - LEFT HAND FRAME AT STATION 1721 LONGERON 12 FOUND DENTED. CABIN - DENTED LEFT HAND FRAME AT STATION 1721 LONGERON 12 LEFT REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2 . REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-00- 07-2R TABLE 201 REPAIR 2 , METHOD HFEC . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: INDICATOR — FAILED (SLIDE PRESSURE) · airframe 85,118 hrs · 19,932 cycles

R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM, INOPERATIVE. R & R THE REMOTE PRESSURE INDICATOR ASSEMBLY FOR R1 DOOR, OPS CHECK GOOD IAW AMM 25-61-04-4.

Part: NOT REPORTED — CRACKED (VERTICAL STAB) · airframe 84,359 hrs · 19,670 cycles

2IN CRACK ON LT LOWER CENTER VERTICAL ON NR 2 ENG. COMPLIED WITH FINAL EA# 1-5530-T0346813 A.

Part: BEARING — SEIZED (MLG) · airframe 84,153 hrs · 19,601 cycles

WHEN CHANGING THE NR 7 BRAKE FOUND THE BEARINGS SEIZED UP ON NR 7 MAIN TIRE. REMOVED AND REPLACED NR 7 MAIN LANDING GEAR TIRE ASSEMBLY.

Part: BRAKE — DRAGGING (MLG) · airframe 84,153 hrs · 19,601 cycles

DURING TAXI AFTER LANDING THE NR 7 MAIN WHEEL BRAKE WAS HANGING UP AND OVERHEATING. TEMP GOT AS HIGH AS 475 WHILE ALL OTHER BRAKES WERE AT 220. CALLED FOR FIRE SUPPORT AS A PRECAUTION. MAINTENANCE TOWED US IN WITH THE BRAKE STILL HANGING UP. TEMP HAD DROPPED TO 385, BUT CLIMBED BACK UP TO 515 DEGREES AFTER BEING TOWED TO PARKING. FACT 21MAR19 08:52 MEM U UPDATED DISCREPANCY DUE TO SDR. REOP 21MAR19 08:52 U DSCRP IS REOPEN FOR WORK. FOUND NR 7 MAIN LANDING GEAR BRAKE ASSY DRAGGING. REMOVED AND REPLACED NR 7 BRAKE ASSY. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: ECU — FAULTY (NR 1 ENGINE) · airframe 84,138 hrs · 19,596 cycles

PDIS 587 73-22 7630 15MAR19 MEM OPEN U LOGPAGES:3028560 ON TAKEOFF JUST AFTER DEPARTING THE RUNWAY THE RED ENGINE FAIL LIGHT ILLUMINATED. A FEW SECONDS LATER AN ODD BOOMING NOISE WAS HEARD FOR ABOUT THREE SECONDS. THERE WERE NO ABNORMALITIES SHOWN ON ANY OF THE ENGINE GAUGES. FACT 15MAR19 19:44 MEM UNABLE TO ACCESS ECU1A THROUGH MCDU. FADEC GROUND TEST ALSO FAILS ECU1. ECU1B SHOWS FAULT CODE: LABEL 160-28. REMOVED AND REPLACED NR 1 ENG ECU IAW MM 73-21-02-4-1. ALL RTS TEST PASS. PERFORMED HIGH POWER ENGINE RUNS PER JRH. ALL PARAMETERS NORMAL/ NO FAULTS.

Part: TIRE — SEPARATED (MLG) · airframe 82,847 hrs · 19,193 cycles

POSTFLIGHT FOUND NR 9 TIRE WITH THROWN TREAD AND TREAD SEPARATION. PER AMM 32-40-00-6 INSPECTION CHECK OF TIRE THAT HAS THROWN TREADS, R&R TIRE. INSPECTED CENTER GEAR TIRE AND WHEEEL PER AMM 32-41-01, NO OTHER DEFECTS FOUND. REMOVED AND REPLACED NR 9 CENTER TIRE PER AMM 32-41-01. OP'S CHECKS GOOD. A/C OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,415 hrs · 18,760 cycles

EMERGENCY LIGHT BATTERY 6 LOW LEVEL 1. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-01-4. OPS TESTED GOOD.

Part: WIRE — CUT (GROUND TERMINAL) · airframe 81,023 hrs · 18,652 cycles

LEVEL 1 ALERT FOR EMERGENCY LIGHT BATTERY AFTER EMERGENCY LIGHT SWITCHED TO TEST. FOUND A WIRE CUT AT 905R GROUND TERMINAL IAW WDM 33-52-01. CRIMPED & SECURED THE TERMINAL IAW SWPM 20-20-01. ALL EMERGENCY LIGHTS ILLUMINATED AND OPS CHECKED NORMAL IAW AMM 33-51-01-5, & 33-52-04-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,655 hrs · 18,551 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 5-83, X= 8.5 FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEEDED ALLOWABLE DAMAGE LIMIT OF SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT REPAIR PER SRM 53-00-52-2R REPAIR 1 FIG 201 FROM STA 5-0 TO STA 5-123, X=8.5. REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100, REFER SNRM N00480 FOR REPAIR DETAILS.

Part: HINGE — WORN (FUSELAGE) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK CARGO DOOR MOST HINGE SECTION ON FUSELAGE SIDE FOUND FWD 12EA HINGE LOBE HOLES WORN EXCEEDED LIMITS AT STA 635 -STA 652. HOLES REWORKED AND FOUND NR 1 - NR 7 HOLES EXCEED LIMIT AS PER SRM 52-30-16-1A FIGURE 101, NR 1 EXISTING HOLES DIA 0.452''-0.455''. NR 2 - NR 7 EXISTING HOLES DIA 0.451'' - 0.455'', NR 8 - NR 12 EXISTING HOLE: DIA 0.4035'', NR 1 - NR 7 FINAL HOLE DIA 0.491'', NR 8 - NR 12 FINAL HOLE: DIA 0.459'', MAXIMUM ALLOWABLE HOLE: 0.462'' REPAIR BUSHINGS (12EA) FABRICATED AND INSTALLED AS PER EA 1-5310-T0336250 PART 1 STEP 2 AND STEP 5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,655 hrs · 18,551 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1780, X= -8.5 FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEEDED ALLOWABLE DAMAGE LIMIT OF SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT REPAIR PER SRM 53-00-52-2R REPAIR 1 FIG 201 FROM EXISTING SPLICE AT STA 1651 TO STA 1791, X=-8.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,655 hrs · 18,551 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1760, X= 27.5 FOUND CORROSION MAIN DECK FLOOR AT SEAT TRACK STA 1760, X= 27.5. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES AT STA 1711 TO STA 1771 X= 27.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1169) · airframe 80,655 hrs · 18,551 cycles

CABIN MAIN DECK CARGO TRACK CORROSION AT BS 1169 RBL 47.5. REPLACED THE CARGO TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,655 hrs · 18,551 cycles

EMPENNAGE AFT ACCESSORY COMPT RT STA 2164 SKIN FOUND CORROSION AS MARKED. CORROSION REMOVED FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THICKNESS : 0.100", MATERIAL REMOVED : 0.090" AND REMAINING THICKNESS : 0.010". AFT ACCESSORY COMPT RT STA 2164 SKIN CORROSION CARRIED OUT REPAIR AS PER SRM 53-70-01-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 80,655 hrs · 18,551 cycles

LEFT WING FIXED LEADING EDGE AT STA XOS 820 FOUND CRACKED. SUPPORT CLIP AT LT WING FIXED LEADING EDGE XOS 820 AREA REMOVED AS PER SRM 51-31-01-0G. NEW SUPPORT CLIP FABRICATED AS PER DWG ARB 2929 REV F AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 80,655 hrs · 18,551 cycles

DURING HFEC INSPECTION AT LTW FIXED LEADING EDGE SKIN AT CORNER 11, FUEL ACCESS DOOR FWD INBD CORNER, FOUND CRACK APPROX 0.25 INCH IN LENGTH, AT STA XOS 611. LT WING FIXED LEADING EDGE SKIN CORNER NR 11 FUEL ACCESS DOOR FWD I/B CORNER APPROX STA XOS 611 CRACKED AREA CARRIED OUT REPAIR PER SRM 57-40-01-2R FIG 201 REPAIR 18. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (RT WING) · airframe 80,655 hrs · 18,551 cycles

RIGHT WING - EXISTING REPAIR ON FIXED LEADING EDGE SKIN AT STA XOS 993. LOWER SKIN FOUND CHAFED RT WING XOS 993 FIXED LEADING EDGE SKIN EXISTING REPAIR DOUBLER CHAFFED MARK. REMOVED AND FOUND EXCEEDED LIMIT PER SRM 57-00-00-2R FIG 202. DAMAGED REPAIR DOUBLER AT RT WING XOS 993 FIXED LEADING EDGE SKIN REMOVED PER SRM 51-31-01-0G. NEW REPAIR DOUBLER FABRICATED AND INSTALLED PER SRM57-40-01-2R FIG 201 REPAIR 9. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,655 hrs · 18,551 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 646 FOUND CRACKED. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 646 CRACKED AREA CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,655 hrs · 18,551 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 653 FOUND CRACKED. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 653 CRACKED AREA CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GYM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1701) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK BS 1701, RBL 8.5 FOUND WITH CROWN DAMAGE. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, REPAIR 1, FIG 201. THE REPAIR WAS LASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 80,655 hrs · 18,551 cycles

DURING HFEC INSPECTION AT RT WING FIXED LEADING EDGE SKIN AT CORNER 5 OF SLAT ACTUATOR ACCESS DOOR INBD CORNER, FOUND APPROX CRACK 1.00 INCH IN LENGTH, STA XOS 491. RT WING FIXED LEADING EDGE SKIN AT CORNER 5, SLAT ACTUATOR ACCESS DOOR FWD INBD CORNER STA XOS 491 CRACKED AREA CARRIED OUT REPAIR PER SRM 57-40-01-2R FIG 201 REPAIR 17. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,655 hrs · 18,551 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 634 FOUND CRACKED. RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 634 CRACKED AREA CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (MAIN DECK) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK, BS 5-6, LBL 27.5 FOUND WITH CROWN DAMAGE. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,655 hrs · 18,551 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 575 FOUND CRACKED. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 575 CRACKED AREA CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 80,655 hrs · 18,551 cycles

DURING HFEC INSPECTION AT LTW FIXED LEADING EDGE SKIN AT CORNER NR 13 SLAT TRACK 10 CUTOUT AFT INBOARD CORNER, FOUND CRACK APPROX 0.25 INCH IN LENGTH, STA XOS 657. LT WING STA XOS 657 FIXED LEADING EDGE SKIN CORNER 13 SLAT TRACK 10 CUTOUT AFT INBOARD CORNER CRACKED AREA CARRIED OUT REPAIR PER SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: DOUBLER — CHAFED (LT WING) · airframe 80,655 hrs · 18,551 cycles

LEFT WING FIXED LEADING EDGE TELESCOPIC DUCT CUT OUT REPAIR DOUBLER LOWER SURFACE FOUND CHAFED AT STA XOS 462 AND XOS 471. EXISTING REPAIR DOUBLER CHAFED MARK REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 57-00-00-2R FIG 202. LT WING XOS 462 AND XOS 471 FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT DAMAGED DOUBLER REMOVED PER SRM 51-31-01-0G. NEW REPAIR DOUBLER FABRICATED PER SRM 57-40-01-2R FIG 201 REPAIR 10. NEW FABRICATED REPAIR DOUBLER INSTALLED PER SRM 57-40-01-2R FIG 201 REPAIR 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1701) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK BS 1701, LBL 8.5 FOUND WITH CROWN DAMAGE. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, REPAIR 1, FIG 201. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,655 hrs · 18,551 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 654 FOUND CRACKED. RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 654 CRACKED AREA CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 80,655 hrs · 18,551 cycles

RIGHT WING FIXED LEADING EDGE FORMER AT STA XOS 585 FOUND CRACKED . FORMER AT RIGHT WING FIXED LEADING XOS 585 AREA REMOVED AS PER SRM 51-31-01-0G. NEW FORMER FABRICATED AS PER DWG ARB 2931 REV H AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1701) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK BS 1701, LBL 27.5 FOUND WITH CROWN DAMAGE. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,655 hrs · 18,551 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 706 FOUND CRACKED. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 706 CRACKED AREA CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,655 hrs · 18,551 cycles

MAIN DECK FLOOR SEAT TRACK STA 1155, X= 8.5 FOUND CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1129 TO STA 1169 X = 8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. CORROSION ON MAIN DECK STA 1155 X = 8.5 FLOOR SEAT TRACK REMOVED AND FOUND EXCEEDED LIMITS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1.

Part: SEAT TRACK — CORRODED (BS 1801) · corrosion level 2 · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK BS 1801, LBL 8.5 FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, REPAIR 1, FIG 201. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (MAIN DECK) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK BS 5-6, LBL 8.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, REPAIR 1, FIG 201. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,655 hrs · 18,551 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 695 FOUND CRACKED. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 695 CRACKED AREA CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,655 hrs · 18,551 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 568 FOUND CRACKED. LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 568 CRACKED AREA CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK FLOOR SEAT TRACK STA 1701, X= -27.5 FOUND CROWN DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA1671 TO STA 1711 X = -27.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK, BS 635, LBL 8.5 FOUND CRACKED. THE SEAT TRACK WAS REPLACED FROM BS 625 TO 645 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (BS 1370-1381) · airframe 80,655 hrs · 18,551 cycles

CENTER LANDING GEAR WHEEL WELLBS 1370 - 1381, RT SIDE FWD BULKHEAD CUT-OUT DOUBLER CRACKED. REMOVED AND REPLACED THE DOUBLER.

Part: SEAT TRACK — CRACKED (BS 715) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK BS 715, LBL 8.5 FOUND CRACKED. THE SEAT TRACK WAS REPLACED FROM BS 705 TO 745, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BEAM — CRACKED (R3 DOOR) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK R3 DOOR NR 3 BEAM FOUND CRACKED AT BS 838.330. REMOVED AND REPLACED THE BEAM IAW SRM 51-31-01-0G, THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK FLOOR SEAT TRACK STA 755, LBL 47.5 FOUND CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK BS 635, RBL 27.5 FOUND CRACKED. REPLACEMENT FROM BS 625 TO 645 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 775) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK BS 775, LBL 75.25 FOUND THE CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 765 TO 809 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK BS 635, LBL 27.5 FOUND CRACKED. REPLACED THE SEAT TRACK FROM BS 625 TO 645, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK FLOOR SEAT TRACK BS 635, X=- 8.5 FOUND CRACKED. THE SEAT TRACK WAS REPLACED FROM BS 625 TO 645 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK SEAT TRACK, BS 635, LBL 47.5 FOUND CRACKED. REPLACED THE SEAT TRACK FROM BS 625 TO 645 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BEAM — CRACKED (L3 DOOR) · airframe 80,655 hrs · 18,551 cycles

MAIN DECK L3 DOOR NR K BEAM, FOUND CRACKED AT BS 793.670. REMOVED THE BEAM IAW SRM 51-31-01-0G. A NEW BEAM WAS INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100.

Part: DOUBLER — CRACKED (BS 1370-1381) · airframe 80,655 hrs · 18,551 cycles

CENTER LANDING GEAR WHEEL WELL BS 1370 - 1381, LT SIDE FWD BULKHEAD CUT-OUT DOUBLER CRACKED. THE DAMAGED DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: COVER — CRACKED (ESCAPE SLIDE) · airframe 79,808 hrs · 18,300 cycles

EMERGENCY ESCAPE SLIDE COVER HAS A 4 INCH CRACK ON THE RIGHT SIDE. TRANSFERRED FROM WRI 25-60/5109 MEL 23JUN17 04:51 MEM U RELEASED FOR SERVICE PER MEL : 52-10-01 CATEGORY : C EXPIRATION : 24JUN17 "MEL 52-10-01: R1 ELECTRIC DOOR ACTUATOR - INOP. FOR EMERGENCY EGRESS, USE PNEUMATIC SYSTEM TO OPEN DOOR." C/7100174 FACT 25JUN17 10:32 MEM INSTALLED EMER. EXCAPE SLIDE COVER IAW AMM 25-23-07-4-1.OPS CHECK GOOD.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 77,900 hrs · 17,698 cycles

AT CRUISE, RECEIVED LEVEL 1 HYD OFF ALERT WITH 3.0 GALLONS REMAINING. AFTER NORMAL GEAR EXTENSION RECEIVED LEVEL 2 HYD FAIL ALERT AS ANTICIPATED. 1.4 GALLONS REMAINING IN NR 3 HYD RESERVOIR. CRASH, FIRE, RESCUE REPORTED HYDRAULIC LEAK FROM NR 3 ENGINE AREA INSTALLED NEW HOSE ASSY. MOTORED ENGINE, LEAK CHECK GOOD, REF MM 29-11-22. CLOSED THRUST REVERSER AND FAN COWL REF MM 71-10-00-2-1. RAN ENGINE IAW LEAK AND OPS CHECK GOOD, PN OF HOSE CHANGED WAS AEB794-167.

Part: SEAL — CUT (SLIDING WINDOW) · airframe 77,560 hrs · 17,590 cycles

35 MINS INTO FLIGHT FO'S WINDOW HAD LOUD SQUEAL SOUND. UNABLE TO COMMUNICATE IN COCKPIT, IT IS TOO LOUD. T/S AS PER FIM 56-12-05, FOUND FO`S SLIDING WINDOW INNER SEAL CUT AT THE UPPER AFT CORNER. F/O SLIDING WINDOW RUBBER SEAL COMPLETELY CURED. PERFORMED FUSELAGE PRESSURE DECAY TEST AS PER MM 21-00-00-5. TEST PASSED. NO LEAK NOTICED. A/C OK FOR SERVICE.

Part: ROLLER TRAY — CRACKED (CARGO BAY) · airframe 76,460 hrs · 17,202 cycles

CENTER CARGO, CTR ROLLER TRAY FOUND CRACK AS MARKED, AT APPROX STATION 1642. CARRIED OUT REPAIR IAW EA 1-5321-T0322812 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53213278 FOR WORK DETAILS. X=0 CTR POSITION.

Part: SKIN — CRACKED (LE SLAT) · airframe 76,460 hrs · 17,202 cycles

LEFT WING NR 6 LE SLAT, LE SKIN FOUND DENT AT STATION XOS 822. CARRIED OUT DOUBLER REPAIR IAW SRM 57-40-02-2R FIG 201 REPAIR 2 & EA 1-5750-T0322778 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO SNRM N00977 & WRI 57503266 FOR WORK DETAILS.

Part: SKIN — CRACKED (LE SLAT) · airframe 76,460 hrs · 17,202 cycles

LEFT WING NR 6 LE SLAT, LE SKIN FOUND DENT AT STATION XOS 823.5. CARRIED OUT DOUBLER REPAIR IAW SRM 57-40-02-2R FIG 201 REPAIR 2 & EA 1-5750-T0322778 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57503266 FOR WORK DETAILS.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 76,460 hrs · 17,202 cycles

CENTER CARGO STATION 1781, X=--56, FLOOR SUPPORT BRACKET CRACKED. CARRIED OUT REPAIR IAW EA 1-5321-T0322723 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53213274 FOR WORK DETAILS.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 76,460 hrs · 17,202 cycles

AFT CARGO COMPARTMENT, STATION 1967, X= 23, STANCHION FOUND WITH CORROSION. DAMAGED STANCHION R & R WITH NEW FABRICATED STANCHION IAW SRM 51-31-01-0G. NEW STANCHION FABRICATED IAW DWG AGA 7978 REV NEW. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 76,460 hrs · 17,202 cycles

AFT CARGO COMPARTMENT STATION 1967, X= -43, STANCHION FOUND WITH CORROSION. DAMAGED STANCHION R & R WITH NEW FABRICATED STANCHION IAW SRM 51-31-01-0G. NEW STANCHION FABRICATED IAW DWG AGA7978 REV NEW. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 76,460 hrs · 17,202 cycles

AFT CARGO COMPARTMENT, STATION 1967, X=1, STANCHION FOUND WITH CORROSION. DAMAGED STANCHION R & R WITH NEW FABRICATED STANCHION IAW SRM 51-31-01-0G. NEW STANCHION FABRICATED IAW DWG AGA 7978 REV NEW. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STANCHION — CORRODED (FUSELAGE) · airframe 76,460 hrs · 17,202 cycles

AFT CARGO COMPARTMENT STATION 1967, X= -23, STANCHION FOUND WITH CORROSION. DAMAGED STANCHION R & R WITH NEW FABRICATED STANCHION IAW SRM 51-31-01-0G. NEW STANCHION FABRICATED IAW DWG AGA7978 REV NEW. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 76,460 hrs · 17,202 cycles

RIGHT WING, OTBD AILERON TE WEDGE, INBD SIDE UPPER SKIN FOUND DELAMINATION, ABOUT 4 INCHES BY 9 INCHES. CARRIED OUT REPAIR IAW EA 1-5750-T0322903 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57503280 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,460 hrs · 17,202 cycles

LEFT WING FIXED LE, DOUBLER FOUND CRACKED AT STATION XOS 667. R & R WITH NEW FABRICATED DOUBLER IAW SRM 51-31-01-0G. NEW DOUBLER FABRICATED IAW DWG ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,460 hrs · 17,202 cycles

RIGHT WING FIXED LE, BEADED DOUBLER AT STATION XOS 665, FOUND CRACKED DURING OTBD SLAT DRIVE CABLE INSPECTION. CARRIED OUT INNER DOUBLER REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 76,460 hrs · 17,202 cycles

LEFT WING FIXED LE, UPPER STRINGER FOUND CRACKED AT STATION XOS 666. CARRIED OUT REPAIR IAW SRM 57-40-03-2R FIG 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 76,460 hrs · 17,202 cycles

RIGHT WING, NR 15 SLAT TRACK CUT OUT SKIN, AT STATION XOS 944, FOUND CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,460 hrs · 17,202 cycles

LEFT WING FIXED LE, BEADED DOUBLER FOUND CRACKED AT WS XOS 664. CARRIED OUT INNER DOUBLER REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 76,460 hrs · 17,202 cycles

AGEING ACFT, EXISTING REPAIR AT NLG RT TRUNNION FITTING, STATION 595. EVALUATED & FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 53-10-14-2R FIG 202 REPAIR 2. HOWEVER, AFTER HFEC INSPECTION CARRIED OUT, FOUND CRACK PROPAGATED APPROX 0.2" LENGTH. EXISTING REPAIR FILLER REMOVED IAW SRM 51-33-01-0G. NEW REPAIR ACCOMPLISHED IAW EA 1-5310-107815A PT 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53103256 FOR WORK DETAILS.

Part: WEB — CRACKED (BS 1305-1315) · airframe 76,460 hrs · 17,202 cycles

MAIN DECK, WHILE REMOVED L3 DOOR PLUG FOR PSE INSPECTION, FOUND L3 DOOR AFT JAMB, LOWER WEB BOX AT BS 1305.25 - 1315.42, LONGERON 26 - 27L, CRACKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 76,460 hrs · 17,202 cycles

AGEING ACFT, EXISTING FILLER REPAIR ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT AT STATION 1355, X= 75.25. EXISTING FILLER, SLOT, REPAIR EVALUATED & FOUND SEAT TRACK CROWN DAMAGED. CARRIED OUT REPAIR BY SECTIONAL REPLACEMENT FROM STATION 1259 - 1391, X = 75.25 IAW SRM 53-00-52-2R FIG 201 REPAIR 1, EO 1-5100-7-5001 B6 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1411) · airframe 76,460 hrs · 17,202 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1411, X= 8.5, FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1401-1501) · airframe 76,460 hrs · 17,202 cycles

MAIN DECK SEAT TRACK, BETWEEN BS 1401 & 1501, X= -8.5, FOUND CROWN DAMAGED, TWO LOCATIONS. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 76,460 hrs · 17,202 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 5 - 6, X= -8.5, FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1641) · airframe 76,460 hrs · 17,202 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1641, X= -8.5, FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10.

Part: SEAT TRACK — CORRODED (BS 1611-1641) · airframe 76,460 hrs · 17,202 cycles

MAIN DECK FLOOR SEAT TRACK, BETWEEN STATION 1611 & 1641, X=8.5, FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 76,460 hrs · 17,202 cycles

MAIN DECK FLOOR SEAT TRACK, BS 5 - 83, X=27.5, FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1275-1380) · airframe 76,460 hrs · 17,202 cycles

MAIN DECK SEAT TRACK, BETWEEN BS 1275 & 1401, X= -8.5, FOUND CROWN DAMAGED, IN TWO LOCATIONS. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BRAKE — DELAMINATED (NR 5) · airframe 756 hrs · 16,940 cycles

NUMBER 5 BRAKE NEEDS TO BE REPLACED. REPLACED NR 5 BRAKE IAW AMM 32-43-20-4. REF MTSI WRI 32-46 2674, MPN OFF 2609472-4B, SN OFF B-0239, MPN ON 2609472-4B & SN ON B-0293.

Part: FIRE WARNING — ACTIVATED (CARGO BAY) · airframe 73,565 hrs · 16,306 cycles

LOWER CARGO FIRE WARNING 4 TIMES. COMPLIED WITH QRH & LANDED.

Part: SENSOR — FAULTED (ANTI ICE) · airframe 71,949 hrs · 15,792 cycles

DURING CLIMB OUT PASSING FL 340, RECEIVED AN ANTI -ICE SENSOR FAIL ALERT. WING, TAIL, & ENGINE ANTI-ICE WAS OFF. TROUBLESHOT IAW FIM 36-11-01 FIGURE 103. ANTI-ICE SENSOR FAIL ALERT DISAPPEARED WHILE FOLLOWING FIM PROCEDURE. ONLY SENSOR SHOWING A FAULT IS PE2 X'D OUT IN PSC-1. ALL OTHER SENSORS APPEAR TO BE WORKING NORMALLY IN PSC-1 & PSC-2. TROUBLESHOT PE2 SENSOR IAW FIM 30-12-03-00 AND WAS HARD FAULTED WITH A HISTORY ALREADY ON MEL. WHILE TROUBLESHOOTING, HAD PE1 SENSOR WITH INTERMITTENT FAULTS, WHEN PE1 FAULTED ANTI-ICE SENSOR FAIL MESSAGE WOULD APPEAR. REPLACED PE1 SENSOR REF 36-11-05-4 NO MESSAGES, PE2 STILL ON MEL. REPLACED PE2 PRIMARY & PE2 BACKUP SENSORS.

Part: COALESCER BAG — DIRTY (ZONE 100) · airframe 71,936 hrs · 15,786 cycles

AFTER TAKEOFF TO CRUISE HAD A FAIRLY STRONG ACRID & OILY ODOR. ALSO OCCURRED FROM TOP OF DESCENT TO LANDING. FOUND COALESCE BAGS DIRTY. REPLACED ALL COALESCE BAGS. OPS NORMAL & NO ODOR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,706 hrs · 15,692 cycles

MAIN DECK CARGO COMPARTMENT LONGITUDINAL SEAT TRACK AT STATION 1801, X 27.25 FOUND WITH MULTIPLE SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1771 TO STATION 1811 X= 27.25 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,706 hrs · 15,692 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1821 TO STATION 1841, X -27.25 FOUND WITH MULTIPLE SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1811 TO STATION 1861 X=-27.25 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,706 hrs · 15,692 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5 - 10 TO STATION 5 - 113, X -75 FOUND WITH MULTIPLE SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-0 TO STATION 5-123, X=-75 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119.

Part: SKIN — CRACKED (LT WING) · airframe 71,706 hrs · 15,692 cycles

DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION, HFEC, AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS 683.4 & STATION XORS 713.6 FOUND FOUR EACH FASTENER HOLES 11, 15, 27 & 36 WITH CRACK INDICATIONS. REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,706 hrs · 15,692 cycles

CABIN MAIN DECK CARGO COMPARTMENT STATION 5 113, X 8.5 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-83 TO STATION 5-123, X=-8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,706 hrs · 15,692 cycles

CABIN MAIN DECK CARGO COMPARTMENT STATION 1239, X -75.25 SEAT TRACK FLANGE FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO STATION 1266 X=-75.25 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,706 hrs · 15,692 cycles

CABIN MAIN DECK CARGO COMPARTMENT LT STATION 1256, LONGERON 26 LT FWD L3 DOOR JAMB LOWER WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119.

Part: SKIN — CRACKED (RT WING) · airframe 71,706 hrs · 15,692 cycles

DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION, HFEC, AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS 683.4 & STATION XORS 713.6 FOUND FOUR EACH FASTENER HOLES 6, 7, 10 & 38 WITH CRACK INDICATIONS. REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 53 . REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 71,706 hrs · 15,692 cycles

CABIN MAIN DECK CARGO COMPARTMENT RT STATION 1256, LONGERON 26RT FWD R3 DOOR JAMB LOWER WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,706 hrs · 15,692 cycles

CABIN MAIN CARGO COMPARTMENT LT STATION 1321, X 8.5 SEAT TRACK FLANGE FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1311 TO STATION 1351 X=8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119

Part: SKIN — CRACKED (RT WING) · airframe 71,706 hrs · 15,692 cycles

RIGHT WING LE LOWER ACCESS PANEL 619CB CUTOUT INBD CORNER, FOUND CRACKED AT XOS 612. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 53. REPAIRED CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.

Part: SKIN — CRACKED (LT WING) · airframe 71,706 hrs · 15,692 cycles

LEFT WING NR 12 LE SLAT TRACK CUTOUT OTBD CORNER FOUND CRACKED AT XOS 776. REPAIRED IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 71,706 hrs · 15,692 cycles

MAIN DECK CARGO BS 1551, X 8.5 CARGO TRACK FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1531 - 1571 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.

Part: CARGO TRACK — CORRODED (BS 1581) · corrosion level 2 · airframe 71,706 hrs · 15,692 cycles

MAIN DECK CARGO BAY BS 1581, X -8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1531 - 1591 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 119.

Part: BOTTLE — LEAKING (R4 DOOR ASSIST) · airframe 71,215 hrs · 15,536 cycles

AFTER SERVICING OF R4 AFT PASSENGER DOOR STORAGE RESERVOIR, FOUND AN AIR LEAK COMING FROM THE INDICATOR. R & R R4 AFT PASSENGER DOOR STORAGE RESERVOIR IAW MM:52-11-04-4 AND MM:52-11-07-2. SERVICED THE STORAGE RESERVOIR IAW MM:12-25-04-3. LEAK TEST OK. ACFT OK TO CONTINUE.

Part: LANDING GEAR — MALFUNCTIONED · airframe 68,813 hrs · 14,785 cycles

DURING A CAT 3 AUTOLAND CHECK, ACFT LANDED SLIGHTLY RIGHT OF CENTERLINE. ON NOSE WHEEL TOUCHDOWN, ACFT MADE AN AGGRESSIVE BID LEFT TO CENTERLINE. ACFT BEGAN TO SHAKE FOLLOWED BY CENTER GEAR MALFUNCTION AND FEW SECONDS LATER HYD 3 FAIL LEVEL 2 ALERT. CLG DRAG BRACE FAILURE, RETRACT ACTUATOR FAILURE, CLG ASSY TRANSLATED AFT OF GEAR WELL CAUSING SKIN DAMAGE. CLG STRUT DOORS DAMAGED, NR 3 HYD SYS DEPLETED TO 0. ENGINE NR 3 HYD PUMPS PROBABLE CAVITATION, AND HYD SYS NR 3 FILTERS PROBABLE CHANGE. REPAIR ACCOMPLISHED PER E.A. T1-5430- 163925. CLG R&R ACCOMPLISHED PER W.I.C. 32T1904. FUN CTIONAL TEST ACCOMPLISHED PER E.A. 1-3215-161680.

Part: SEAT TRACK — CORRODED (BS 446) · corrosion level 2 · airframe 67,208 hrs · 14,324 cycles

BS 446, X= -32 SEAT TRACK FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 48 FROM BS 440 TO 495. SEAT TRACK FABRICATED IAW DRAWING SP11530031 REVISION N. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 67,208 hrs · 14,324 cycles

LEFT WING OTBD FLAP VANE NR 3 TEE FITTING TRACK ATTACH HOLE FOUND CORRODED. HOLE REWORKED AND FOUND EXCEED LIMIT IAW SRM 57-50-02 REPAIR 5 FIGURE 201 REVISION 48. EXISTING HOLE SIZE: 0.873" X 0.597". FINAL SIZE: 0.964"X0.696". MAXIMUM ALLOWABLE SIZE: 0.940"X0.670". BUSHING FABRICATED IAW EA 1-5750-156848 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 67,208 hrs · 14,324 cycles

RIGHT WING OTBD FLAP VANE NR 2 TEE FITTING TRACK ATTACH HOLE FOUND CORRODED. HOLE REWORKED AND FOUND EXCEED LIMITS IAW SRM 57-50-02 REPAIR 5 FIGURE 201 REVISION 48. EXISTING HOLE SIZE: 0.894" X 0.670". FINAL HOLE SIZE: 0.995" X 0.726". MAXIMUM ALLOWABLE SIZE: 0.940" X 0.670". BUSHING FABRICATED IAW EA 1-5750-156849 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.

Part: FLOOR SUPPORT — CORRODED (BS 1942) · corrosion level 2 · airframe 67,208 hrs · 14,324 cycles

BS 1942, X= -55 FLOOR SUPPORT FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 48. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 114.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 67,208 hrs · 14,324 cycles

CORROSION FOUND DURING FPI ON LT WING (FLAP SIDE) INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03 REVISION 72. EXISTING DIAMETER 1.329",FINAL DIAMETER 1.335", MAXIMUM ALLOWABLE DIAMETER 1.220". BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-156845 PART 1 STEP 4 AND STEP 5. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV .114.

Part: HINGE FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 67,208 hrs · 14,324 cycles

CORROSION FOUND DURING FPI ON LT WING SIDE OTBD FLAP, OTND HINGE PIVOT BORE HOLE. REPAIRED IAW EA 1-5750-156843 PART 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV.114.

Part: HINGE FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 67,208 hrs · 14,324 cycles

CORROSION FOUND DURING FPI ON LT WING (FLAP SIDE) INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 REVISION 72. EXISTING DIAMETER 1.256",FINAL DIAMETER 1.261", MAXIMUM ALLOWABLE DIAMETER 1.220". BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-156845 PART 1 STEP 4 AND STEP 5. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV .114.

Part: BUSHING — WORN (ZONE 600) · airframe 67,208 hrs · 14,324 cycles

RIGHT WING OTBD FLAP INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156842 PART 1 STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 114.

Part: BUSHING — WORN (RT WING) · airframe 67,208 hrs · 14,324 cycles

RT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156842 PART 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 114.

Part: HINGE FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 67,208 hrs · 14,324 cycles

RT WING OTBD FLAP INBD FORWARD HINGE BRACKET LOWER OTBD STUD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-156842 PART 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 114.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 67,208 hrs · 14,324 cycles

LT WING OTBD FLAP INBD HINGE BRACKET LOWER OTBD STUD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-156841, PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156841, PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — DAMAGED (ZONE 600) · airframe 67,208 hrs · 14,324 cycles

RIGHT WING INBD FLAP OTBD HINGE BRACKET PIVOT OTBD BORE FOUND SCRATCHED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING DIAMETER 1.256", FINAL DIAMETER 1.2825", MAXIMUM DIAMETER 1.220". FABRICATED BUSHING INSTALLED IAW EA.1-5750-156846, STEP 4 AND STEP 5 PART 1, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (ZONE 600) · airframe 67,208 hrs · 14,324 cycles

FOUND CRACK INDICATIONS AT RT WING LOWER SKIN ACCESS PANEL CUT-OUT BETWEEN RWS 683.4 AND 713.6. REPAIR CARRIED OUT IAW DRAWING SG11570004 REVISION C AND EA 1-5710-156850 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.

Part: SKIN — CRACKED (LT WING) · airframe 67,208 hrs · 14,324 cycles

CRACK INDICATIONS AT LEFT WING LOWER SKIN ACCESS PANEL CUT-OUT BETWEEN LWS 683.4 AND 713.6. REPAIR CARRIED IAW DRAWING SG11570004 REVISION C AND EA 1-5710-156850 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.

Part: BUSHING — WORN (ZONE 500) · airframe 67,208 hrs · 14,324 cycles

LT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156843, PART 1, NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156843 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — DAMAGED (ZONE 600) · airframe 67,208 hrs · 14,324 cycles

RT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT BORE FOUND SCRATCHES. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING DIAMETER 1.3275", FINAL DIAMETER 1.3355", MAXIMUM DIAMETER 1.220". FABRICATED BUSHING INSTALLED IAW EA 1-5750-156846, STEP 4 AND STEP 5 PART 1, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 67,208 hrs · 14,324 cycles

RT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REPAIRED IAW EA 1-5750-156844, PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156844 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 600) · airframe 67,208 hrs · 14,324 cycles

RT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. BUSHING REPAIRED IAW EA 1-5750-156844 PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156844 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 500) · airframe 67,208 hrs · 14,324 cycles

LT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH OTBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156841 PART 1, REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1- 5750-156841, PART 1 STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 67,208 hrs · 14,324 cycles

LEFT WING OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING CONTACT SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5750-156841 PART 1, REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-156841, PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 500) · airframe 67,208 hrs · 14,324 cycles

LT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BUSHING FOUND WORN. REMOVED IAW CMM 20-20-07, REV 72 BORE MEASURED DIAMETER 1.256" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220". REWORKED CARRIED OUT AND FABRICATED BUSHING IAW EA 1-5750-156845, PART 1, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 500) · airframe 67,208 hrs · 14,324 cycles

LT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BUSHING FOUND WORN. REWORKED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.329 AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220". REWORK CARRIED OUT AND FABRICATED BUSHING INSTALLED IAW EA 1-5750-156845 PART 1, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 500) · airframe 67,208 hrs · 14,324 cycles

LT WING OTBD FLAP, INBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156841 PART 1, NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156841 PART 1, STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR GMM 6-2-100, REV 114.

Part: BUSHING — WORN (ZONE 500) · airframe 67,208 hrs · 14,324 cycles

LT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BUSHING FOUND WORN. REPAIRED IAW EA 1-5750-156843 PART 1, NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-156843 PART 1 STEP 4 AND STEP 5. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 67,208 hrs · 14,324 cycles

VERTICAL STABILIZER RT REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. CARRIED OUT REPAIR IAW SRM 55-30-02 FIGURE 201 REVISION 48 AND SRM 51-33-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.

Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 67,208 hrs · 14,324 cycles

LEFT WING INBD T/E ACCESS PANEL 541JB ATTACHMENT SUPPORT TEE FOUND SURFACE CORROSION ON SEVERAL LOCATION. R & R IAW EA 1-5710-157949, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: TEE FITTING — CRACKED (WW BULKHEAD) · airframe 67,208 hrs · 14,324 cycles

CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT CHORD CRACKED NEAR DETRIM ACTUATOR AREA. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 67,208 hrs · 14,324 cycles

BS 5-123 LONGERON 24LT SPLICE FITTING FOUND CRACKED. SPLICE FABRICATED IAW DWG A5A7112 REV D. SPLICE R & R IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 67,208 hrs · 14,324 cycles

DUTING X-RAY INSPECTION ON TRANSVERSE SKIN, FOUND CRACKED AT STA 5-0, LONGERON 7L FWD SIDE OF CENTER SPLICE 3RD TO 4TH FASTENER. R & R IAW SRM 51-33-01, REV 48. NEW LONGERON SPLICE FABRICATED IAW DWG AEA7633 REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: FASTENER — LOOSE (NR 2 NOSE COWL) · airframe 66,930 hrs · 14,260 cycles

NR 2 ENGINE NOSE COWL HAS NUMEROUS RIVETS LOOSE IN NOSE LIP SKIN. NOSE COWL REPLACED.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 66,930 hrs · 14,260 cycles

RIGHT INBD UPPER SKIN CRACKED. REPAIRED IAW EA 1-5750-157590, PART 1.

Part: HANDLE — UNSECURE (L1 DOOR) · airframe 66,135 hrs · 14,073 cycles

L1 DOOR MANUAL LIFTING HANDLE IS NOT SECURELY ATTACHED ON THE FORWARD SIDE ADJUSTED SPRING AT L1 DOOR FWD LIFTING HANDLE FWD SIDE IAW IN REF OF 52-11-00-0-0. SYS CK NML. FINAL CLOSED.

Part: BATTERY — INOPERATIVE (LT DOOR SLIDE) · airframe 65,840 hrs · 14,004 cycles

TRANSIT CHK FOUND LT ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYS INOPERATIVE. REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD IAW AMM 25-23-07-4-1 AND 25-61-15-4-0. OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 65,119 hrs · 13,827 cycles

TAKING OFF ON 30R AT APPROXIMATELY 1000FT EXPERIENCED A NR 2 ENGINE EGT OVERHEAT 966 DEGREES AND LARGE BANGING SOUND (COMPRESSOR STALL). PULLED NR 2 THROTTLE TO IDLE IMMEDIATELY. EGT CAMEBACK TO NORMAL (740-760 ) AND COMPRESSOR STALL STOPPED. AFTER THROTTLE AT IDLE N1 REMAINED AT 26 EGT AT 740-760 , N2 53-58. DUMPED FUEL AND RETURNED TO LAND. RT ENG INLET AND EXHAUST CHECKED PER MM 72-00-04 NO FAULTS NOTED EGR PERFORMED PER JRH N1 HUNG AT 14.8% EGT 754 N2 53% FF 1330. RT ENGINE FAILED BORESCOPE INSPECTION WITH CATASTROPHIC DAMAGE IN AFT HPC STAGES. R&R NR 2 ENGINE WORK CARD 71T0902.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,902 hrs · 13,511 cycles

LEVEL 1 'EMER LT BAT 6 LO' ALERT DISPLAYED DURING EMERGENCY LIGHT TEST. R & R AFT EMERGENCY LIGHT BATTERY PACK (U1-2070) REF AMM 33-51-01-4-0. OPS CHECKS NORMAL.

Part: FAN BLADE — BENT (NR 3 ENGINE) · airframe 63,842 hrs · 13,498 cycles

DURING TAKEOFF GOT "ICE DETECTED" FOLLOWED BY EVM COMP NR 3 ENG 5.6 WITH AMBER BOX. CREW FELT THE EXCESSIVE VIBRATION. ON ARRIVAL INSPECT FAN AREA AND FOUND 2 FAN BLADE BENT. FOUND ALSO SLIGHT REMAIN OF BLOOD AROUND THE ICE DECTECTOR AND NEAR THE OUTER FAN AREA. FOUND NO EVIDENCE OF CORE INGESTION. THE INGESTED BIRD WENT THRU THE FAN AREA. REPLACED/INSTALLED NR 30 AND NR 31 FAN BLADES IAW MM 72-31-02-4. NR 3 ENG SPINNER IAW MM 72-31-01-4. PERFORMED NR3 ENG VIBRATION SURVEY.

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,544 hrs · 12,984 cycles

MAIN DECK CARGO - L3 DOOR CUTOUT AFT JAMB MID SECTION FOUND CORROSION. MAIN DECK CARGO - L3 DOOR CUTOUT AFT JAMB MID SECTION REPAIRED AS PER SRM 53-40- 15 FIGURE 201 REPAIR 4, REVISION 42. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100 REVISION 109.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 61,544 hrs · 12,984 cycles

CENTER TANK AFT UPPER SURFACE APPROX STA 1229, X = 17 FOUND WITH SURFACE CORROSION. MAIN DECK CARGO -CTR TANK AFT UPPER SURFACE APPROX STA 1229, X =17, SURFACE CORROSION REPAIRED IAW EA 1-5710-132348. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 109.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 61,544 hrs · 12,984 cycles

CENTER TANK AFT UPPER SURFACE APPROX STA 1229, X = -45. FOUND SEVERAL LOCATIONS WITH SURFACE CORROSION. MAIN DECK CARGO - CTR TANK AFT UPPER SURFACE APPROX STA 1229, X = -45, SURFACE CORROSION REPAIRED IAW EA 1-5710-132348. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 109.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 61,544 hrs · 12,984 cycles

CENTER TANK UPPER SURFACE APPROX STA 1341, X =107, FOUND SURFACE CORROSION. MAIN DECK CARGO - CTR TANK UPPER SURFACE APPROX STA 1341, X =107, SURFACE CORROSION REPAIRED IAW EA NR 1-5710-132364. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — DAMAGED (RUDDER) · airframe 61,544 hrs · 12,984 cycles

VERTICAL STABILIZER AFT RUDDER LOWER EDGE FWD SKIN FOUND PEELED. REPAIRED IAW EA NR 1-5540-132347. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SKIN — CORRODED (RWS 258) · airframe 61,544 hrs · 12,984 cycles

RT WING, UPPER WING SURFACE AT XORS258 FOUND CORROSION. RT WING, UPPER WING SURFACE AT XORS258 REPAIRED IAW EA NR 1-5710-132362. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — CRACKED (LT WING) · airframe 61,544 hrs · 12,984 cycles

CRACK INDICATION DURING HFEC OPEN HOLE INSP AT ONE HOLE (XORS696.730, STR36) ON LT WING LOWER SKIN PANEL, OUTER WING ACCESS DOOR CUT OUT. REPAIRED IAW EA NR 1-5710-132354. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT FUSELAGE SKIN, STA 630 TO STA 635, LONGERON 25 LT TO LONGERON 26 LT. EXISTING REPAIR AT LT FUSELAGE SKIN, STA 630 TO STA 635, LONGERON 25 LT TO LONGERON 26 LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REPAIRED IAW SRM 53-00-15 FIGURE 202 REPAIR 8, REVISION 42. REPETITIVE HFEC INSP TO BE CARRIED OUT ON REPAIRED AREA IAW SPECIFICATION 53.10.07.1 REVISION 14 AT 12600 FLIGHT CYCLE AND SUBSEQUENT INSPECTION AT 7000 FLIGHT CYCLE. EO NR 1-5100-7- 5001A4 PART 1, REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 109.

Part: DOUBLER — NONE (100) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT RT FUSELAGE SKIN, APPROX STA 2010, LONGERON 45 RT. EXISTING REPAIR AT RT FUSELAGE SKIN, APPROX STA 2010, LONGERON 45 RT. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW EA NR 1-5310-78002, TITLE: FUSELAGE - AFTER FUSELAGE COMPARTMENT ENTRY DOOR FRAME - REPAIR EO 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — NONE (ZONE 500) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT UPPER SKIN APPROX STA XIFH 243. EXISTING REPAIR AT LT WING INBD FLAP, INBD SEGMENT, UPPER SKIN APPROX STA XIFH 243, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-01 FIGURE 201, REPAIR 1 REVISION 42. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 109.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT UPPER SKIN APPROX STA XIFH 256. EXISTING REPAIR AT LT WING INBD FLAP, OTBD SEGMENT UPPER SKIN APPROX STA XIFH 256, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT ON EXISTING REPAIR IAW SRM 57-00-01, FIGURE 201, REPAIR 1 REVISION 42. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES -REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 109.

Part: SKIN — NONE (ZONE 100) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT RT FUSELAGE SKIN, STA 1781, LONGERON 38 RT TO LONGERON 42 RT. EXISTING REPAIR AT RT FUSELAGE SKIN, STA 1781, LONGERON 38 RT TO LONGERON 42, RT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 53- 00-15, FIGURE 202, REPAIR 8, REVISION 42. REPETITIVE HFEC INSP TO BE CARRIED OUT ON REPAIRED AREA IAW SPECIFICATION 53.10.06.3 REV 14 AT 19900 FLIGHT CYCLE AND SUBSEQUENT INSP AT 6300 FLIGHT CYCLE. EA 1-5310-132346 TITLE: FUSELAGE - EXISTING SKIN REPAIR AT STA =1781 BTWN L-38R AND L41R - FOLLOW UP INSP. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT RT FUSELAGE SKIN, STA 1002 TO STA 1009, LONGERON 37, RT TO LONGERON 39 RT. EXISTING REPAIR AT RT FUSELAGE SKIN, STA 1002 TO STA 1009, LONGERON 37, RT TO LONGERON 39 RT EVALUATED AND FOUND NOT CORRELATE WITH ANY SRM. EXISTING REPAIR DOUBLER REPAIRED IAW SRM 53-00-15 FIG 202 REPAIR 8, REVISION 42. REPETITIVE HFEC INSP TO BE CARRIED OUT ON REPAIRED AREA IAW SPECIFICATION 53.10.06.1 REVISION 14 AT 12600 FLIGHT CYCLE AND SUBSEQUENT INSP AT 6300 FLIGHT CYCLE EO NR1-5100-7-5001A4 PART 1, TITLE: STRUCTURES -REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 109.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR ON FRAME AT LT AIRCON BAY STA 485, LONGERON 36 LT TO LONGERON 38 LT. EXISTING REPAIR AT LT STA 485 FRAME, BETWEEN LONGERON 36 LT AND LONGERON 38 LT, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NR 1-5310-132360. TITLE: FUSELAGE - LT FUSELAGE FRAME EXISTING REPAIR AT STA = 482 - REPAIR. EO NR1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 255. EXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 255, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT ON EXISTING REPAIR IAW SRM 57-00-00, FIGURE 205, REPAIR GENERAL REVISION 42 EO NR1-5100-7-5001A4 PART 1, TITLE: STRUCTURES -REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 109.

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 61,544 hrs · 12,984 cycles

LT WING OTBD FLAP INBOARD T/E WEDGE UPPER SURFACE. FOUND DELAMINATION. LT WING OTBD FLAP INBD T/E WEDGE. R & R IAW CMM 57-52-04 REVISION 66.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT WING FIXED L/E STA XORS 402 (BEHIND NR 3 SLAT). EXISTING REPAIR AT LT WING FIXED L/E STA XORS 402 (BEHIND NR 3 SLAT), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NR 1-5710-132361, TITLE: WINGS - LT WING EXISTING L/E SKIN REPAIR -REPAIR. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT FUSELAGE SKIN, STA 480 TO STA 490, LONGERON 35 LT TO LONGERON 38 LT. EXISTING REPAIR AT LT FUSELAGE SKIN STA 480 TO STA 490, LONGERON 35 LT TO LONGERON 38 LT EVALUATED AND FOUND DOES NOT CORRELATE TO ANY SRM. EXISTING REPAIR, REPAIRED IAW EA NR 1-5310-132359, TITLE: FUSELAGE - LT SIDE FUSELAGE SKIN EXISTING REPAIR AT STA = 480 - REPAIR. EO 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT FUSELAGE SKIN, STA 605 TO STA 615, LONGERON 34 LT TO LONGERON 35 LT. EXISTING REPAIR AT LT FUSELAGE SKIN, STA 605 TO STA 615, LONGERON 34 LT TO LONGERON 35 LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING REPAIR, REPAIRED IAW EA NR 1-5310-132363, TITLE: FUSELAGE - LT SIDE FUSELAGE SKIN EXISTING REPAIR AT STA = 680 -REPAIR. EO 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES -IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 109. REQUIRES REPETITIVE FOLLOW UP INSP AT A 4000 FLIGHT CYCLE INTERVAL.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT FUSELAGE SKIN, STA 705, LONGERON 27 LT (BELOW MAIN CARGO DOOR CUTOUT). EXISTING REPAIR AT LT FUSELAGE SKIN, STA 705, LONGERON 27 LT (BELOW MAIN CARGO DOOR CUTOUT), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NR 1-5310-132351, TITLE: FUSELAGE - MAIN CARGO DOOR LOWER JAMB FUSELAGE SKIN - REPAIR. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SLAT — MISREPAIRED (ZONE 500) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT WING NR 3 SLAT INNER SKIN (04 EACH DOUBLER). EXISTING REPAIR AT LT WING NR 3 SLAT INNER SKIN (04 EACH DOUBLER), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NR 1-5740-132358, TITLE: WINGS - LT WING NR 3 SLAT REPAIR. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES -REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 109.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT WING FIXED L/E STA XORS 433 (BEHIND NR 3 SLAT). EXISTING REPAIR AT L/E WING FIXED L/E STA XORS 433 (BEHIND NR3 SLAT), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NR 1-5710- 132361, TITLE: WINGS - LT WING EXISTING L/E SKIN REPAIR - REPAIR EO NR 1-5100- 7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 109.

Part: SKIN — NONE (ZONE 600) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT RT WING INBD FLAP INBD SEGMENT LOWER SKIN APPROX STA XIFH 217. EXISTING REPAIR AT RT WING INBD FLAP INBD SEGMENT LOWER SKIN APPROX STA XIFH 217, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-00 FIGURE 205, REPAIR GENERAL REVISION 42. EO 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES -REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 109.

Part: SKIN — NONE (ZONE 500) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT WING INBD FLAP, INBD SEGMENT, UPPER SKIN APPROX STA XIFH 193. EXISTING REPAIR AT LT WING INBD FLAP, INBD SEGMENT UPPER SKIN APPROX STA XIFH 193, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-00 FIGURE 201, REPAIR 1, REV 42. EO 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES -REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 109.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 61,544 hrs · 12,984 cycles

EXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 243. EXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 243, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT ON EXISTING REPAIR IAW SRM 57-00-00 FIGURE 205, REPAIR GENERAL REVISION 42. EO NR1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 109.

Part: STRAP — CRACKED (TE FLAP HINGE) · airframe 61,544 hrs · 12,984 cycles

RT WING OTBD FLAP INBD HINGE TENSION STRAP FOUND CRACKED. RT WING OTBD FLAP INBD HINGE CRACKED TENSION STRAP. R & R WITH A NEW TENSION STRAP IAW EO NR 1-5750-7-5004, REV 3, PART 2. REPAIR CLASSIFIED MINOR REPAIR IAW GMM 6-2-100, REVISION 109.

Part: POSITION SWITCH — MALFUNCTIONED (MLG) · airframe 60,489 hrs · 12,722 cycles

GEAR HORN WHEN LANDING GEAR SELECTED ON FINAL. UNSAFE GEAR INDICATIONS IN LANDING GEAR LIGHTS AND ON CONFIG PAGE. DURING GO AROUND THE LIGHTS TURNED GREEN AS GEAR HANDLE WAS PULLED OUT TO RAISE THE GEAR. PUSHED HANDLE BACK IN AND LEFT THE GEAR DOWN AND CAME BACK AROUND AND LANDED. REPLACED LANDING GEAR HANDLE POSITION SWITCH AND ACTUATOR REF AMM 32-61-04-4, OPS CHECKS NORMAL.

Part: COMPUTER — FAILED (ZONE 100) · airframe 60,090 hrs · 12,628 cycles

ON DEPARTURE, ATS FAILED, BOTH AUTOPILOTS FAILES AND BOTH FLIGHT DIRECTORS FAILED AND WINDSHEAR DET FAIL LIGHT ILLUMINATED. UNABLE TO GET ANY OR ALL BACK. RETURNED TO DEPARTURE. MCDU SCRATCHED MESSAGE 'THRUST LIMIT MISMATCH' ALSO ILLUMINATED. PERFORMED BOTH FCC'S DETAILED RTS FCC-1 FAILED: FCC-1, AIL ACT-LIB, AIL ACT-ROB, ELEV ACT-ROB, ELEV ACT-LIB, EL MOD LVDT-ROB, EL MOD LVDT- LIB, LWR RUD MOD LVDT-A, LWR RUD MOD LVDT-B, LWR RUD ACT. FCC-2 R-T- PASSED REMOVED AND REPLACED BOTH FCC'S AND R-T-S PASSED IAW AMM 22-01-03 -4.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 56,723 hrs · 11,901 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. REPAIR CARRIED OUT AT MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 56,723 hrs · 11,901 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING HOLES A, B, C AND D CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,723 hrs · 11,901 cycles

MAIN DECK CARGO AT APPROXIMATELY STATION 5-73 TO 5-93, X = -27.5 FOUND SEAT TRACK CORROSION. CABIN MAIN DECK CARGO SEAT TRACK REPAIRED FROM STA 5-00 TO STA 5-123, X = -27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,723 hrs · 11,901 cycles

CABIN, MAIN DECK CARGO COMPARTMENT AT APPROXIMATELY STATION 1761 TO 1821, X = -8.50 FOUND SEAT TRACK CORROSION. CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK REPAIRED FROM STA 1761 TO STA 1831, X = -8.50 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STANCHION — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,723 hrs · 11,901 cycles

FORWARD CARGO COMPARTMENT FOUND AFT BULKHEAD LOCATION WITH LINERS SUPPORTING STANCHION X = -9 INCHES WITH CORROSION. FORWARD CARGO COMPARTMENT AFT BULKHEAD LOCATION WITH LINERS SUPPORTING STANCHION X = -9 INCHES CARRIED OUT REPAIR AS PER EA NR 1-5310-122419. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,723 hrs · 11,901 cycles

MAIN DECK CARGO COMPARTMENT AT APPROXIMATELY STATION 1541, X = -8.5 FOUND SEAT TRACK FLANGE CORROSION. CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK REPAIRED FROM STA 1531 TO STA 1551, X = -8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 56,723 hrs · 11,901 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B , NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FABRICATED AS PER FEDEX EA NR 1-5300-122409A, TITLE: FUSELAGE, GENERAL: MAIN CARGO DOOR LOWER JAMB SPOOL FITTING, MATERIAL SUBSTITUTION. SUPPORT FITTING NR 6 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED ON MAIN CARGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 56,723 hrs · 11,901 cycles

8 FASTENERS HOLES FOUND CRACK INDICATIONS AS MARKED DURING OPEN-HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.400 AND STATION XORS = 713.600. REPAIR CARRIED OUT AT LEFT WING FUEL TANK LOWER SKIN CUTOUT AS PER EA NR 1-5710-122418, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 56,723 hrs · 11,901 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B AND NR C. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FABRICATED AS PER FEDEX EA NR 1-5300-122409A, TITLE: FUSELAGE, GENERAL: MAIN CARGO DOOR LOWER JAMB SPOOL FITTING, MATERIAL SUBSTITUTION. SUPPORT FITTING NR 5 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED ON MAIN CARGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,723 hrs · 11,901 cycles

MAIN DECK CARGO AT APPROXIMATELY STA 1641, X = 27.5 FOUND SEAT TRACK CORROSION. CABIN MAIN DECK CARGO SEAT TRACK REPAIRED FROM STA 1631 TO STA 1651, X = 27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 56,723 hrs · 11,901 cycles

05 EACH FASTENER HOLES FOUND CRACK INDICATION AS MARKED DURING OPEN-HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.400 AND STATION XORS = 713.600. REPAIR CARRIED OUT AT RT WING FUEL TANK LOWER SKIN CUTOUT AT STA XORS = 683.400 AND STA 713.600 AS PER FEDEX EA NR 1-5710-122417, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 56,723 hrs · 11,901 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B , NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FABRICATED AS PER EA NR 1-5300-122409A, SUPPORT FITTING NR 7 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED ON MAIN CARGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 56,723 hrs · 11,901 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FABRICATED AS PER FEDEX EA NR 1-5300-122409A. SUPPORT FITTING NR 4 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED ON MAIN CARGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 56,723 hrs · 11,901 cycles

DURING OPEN-HOLE INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FABRICATED AS PER FEDEX EA NR 1-5300-122409A, SUPPORT FITTING NR 3 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED ON MAIN CARGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (LT WING) · airframe 56,723 hrs · 11,901 cycles

LEFT WING, FIXED LEADING EDGE TELESCOPE DUCT CUTOUT REPAIR DOUBLER AT XOS 467 FOUND CHAFFED. REMOVED DAMAGED REPAIR DOUBLER AS PER SRM 51-31-01 VOLUME II. FABRICATED NEW DOUBLER AND INSTALLED AT LEFT WING FIXED LEADING EDGE TELESCOPE DUCT CUTOUT AS PER SRM 57-10-00 FIGURE 43 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (MLG WW BULKHEAD) · airframe 56,723 hrs · 11,901 cycles

CENTER LANDING GEAR WHEEL WELL RIGHT BULKHEAD FORWARD LOWER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AND REPLACED WITH NEW PART AT CENTER LANDING GEAR WHEEL WELL RIGHT BULKHEAD FORWARD LOWER AREA AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (MLG WW BULKHEAD) · airframe 56,723 hrs · 11,901 cycles

CENTER LANDING GEAR WHEEL WELL LEFT BULKHEAD FORWARD LOWER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AND REPLACED WITH NEW PART AT CENTER LANDING GEAR WHEEL WELL LEFT BULKHEAD FORWARD LOWER AREA AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: UNKNOWN — MALFUNCTIONED (NR 2 ENGINE) · airframe 54,661 hrs · 11,451 cycles

NR 2 ENG RPM LO ON CLIMB-OUT (FLAMEOUT). CREW REPORTED DURING CLIMB-OUT NR 2 ENG N1 WENT TO 11 PERCENT WITH N2 ALMOST 0 PERCENT, LOW EGT, AND FF APPROX 600 PPM. INSP NR 2 ENG INLET AND EXH FOR METAL PARTICLES AND FOD. NO DEFECTS NOTED. CHKD NR 2 ECU, NO FAULTS FOUND IN BOTH CHNLS A AND B. PERFORMED RTS ON NR 2 ECU CHNLS A AND B. ALL TESTS PASSED. PERFORMED NR 2 ENG RUN, NRML ENG START. PERFORMED HIGH PWR RUN AT 70 PERCENT N1 ON ALL 3 ENG. RECEIVED SAME READINGS ON ALL 3 ENGS WENT DOWN TO IDLE AND RAN NR 2 ENG AT 85 PERCENT N1 BACK TO IDLE AND WENT UP TO 100 PERCENT N1. NR 2 ENG IND NML AND STEADY WHOLE TIME. WENT BACK TO IDLE AND RETURNED TO GATE. ENG RUNS PERFORMED BY FLT CREW. R & R NR 2 ENG ECU, HMU AND MAIN FUEL PUMP PER APPLICABLE MM.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 52,430 hrs · 10,935 cycles

CABIN SEAT TRACK CROWN AREA FOUND CHIPPED OFF AT STA 899 X = -47. CABIN SEAT TRACK AT STA 899 X= -47 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 200) · airframe 52,430 hrs · 10,935 cycles

CABIN, RIGHT LONGERON 17 FOUND CRACKED AT STA 1239. [SUP 4-18-07] REMOVED AND REPLACED AS PER SRM 51-33- 01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 52,430 hrs · 10,935 cycles

LEFT WING DROOPED LEADING EDGE UPPER SURFACE FOUND CRACKED. [SUP 4-19-07] REMOVED AND REPLACED AS PER AMM 27-80-10. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 200) · airframe 52,430 hrs · 10,935 cycles

CABIN LEFT LONGERON 17 FOUND CRACKED AT STA 1239. 4-18-07, REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 100) · airframe 52,430 hrs · 10,935 cycles

FORWARD CARGO DOOR AFT CUTOUT LOWER SKIN FOUND DENT AND CHAFED. CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — CRACKED (ZONE 200) · airframe 52,430 hrs · 10,935 cycles

CABIN, RT WEB ANGLE FOUND CRACKED AT STA 1219 LONGERON 27. REPAIRED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DEFORMED (ZONE 200) · airframe 52,430 hrs · 10,935 cycles

CABIN SEAT TRACK AT STA 1485, X = 47 FOUND DEFORMED. 4-18-07, CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 52,430 hrs · 10,935 cycles

CABIN, SEAT TRACK CROWN AREA AT STA 755, X = -8 FOUND CRACKED. 4-18-07, CARRIED OUT REPAIR AS PER SRM 53-70- 00 VOLUME I. FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (RT WING) · airframe 52,430 hrs · 10,935 cycles

RIGHT WING TIP LOWER SURFACE FOUND CORROSION. [SUP 4-19-07] REPAIRED AS PER FEDEX E.A. 1-5710-107829. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 52,430 hrs · 10,935 cycles

RIGHT WING FIXED LEADING EDGE NR 14 SLAT TRACK CUTOUT FOUND CRACKED. 4-18-07, REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 52,430 hrs · 10,935 cycles

NOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. [SUP 4-18-07] REPAIRED AS PER SRM 53-40-00 FIGURE 22 VOLUME I AND FEDEX EA 1-5310-107815, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 500) · airframe 52,430 hrs · 10,935 cycles

LEFT WING TOPSIDE FIXED LEADING EDGE AT TELESCOPING DUCT CUTOUT FOUND 2 SKIN CRACKS AT AFT CORNERS. [SUP 4-19-07] CRACKS AT LT WING TOPSIDE FIXED LEADING EDGE AT TELESCOPIC DUCT CUTOUT CORNERS REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 600) · airframe 52,430 hrs · 10,935 cycles

RIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 4-19-07] CRACKED AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 52,430 hrs · 10,935 cycles

NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. REPAIRED AS PER SRM 53-40- 00 FIGURE 22 VOLUME I AND FEDEX EA 1-5310-107816, REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: WIRE — BURNED (E/E BAY) · airframe 50,271 hrs · 10,441 cycles

PDIS: LEVEL ONE CAC AIR FLO OFF ALERT DURING ENGINE START. MAINT FOUND SIGNIFICANT AMOUNT OF WIRES BURNED IN LWR FWD CARGO COMPARTMENT AFT RT CORNER IN CAC BLOWER AREA. FOUND SEVERAL BREAKERS POPPED IN THE COCKPIT. R&R 57 WIRES DESIGNATED C901.WRAPPED 19 WIRES WITH TEFLON TAPE DESIGNATED C901. R&R ALL 3 CAC COOLING FANS, FLOW SENSORS, FCC1, HSC, FSC, AFSC, EPCU, PSC1 & 2, GCU1, 2 & 3, ELF ACTUATOR, ENVIRONMENTAL SYS CONT PNL, LWR BEACON ENERGY BOX, HI INTENSITY CONT UNIT & FLASHER TIMER, RCCB B1-1261, RELAYS R2-1. ALL PWR AND EQUIPMENT TEST GOOD PER MM. PERFORM TEST FLIGHT. GOOD. RETURNED TO SERVICE.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 47,275 hrs · 9,751 cycles

RIGHT WING, LOWER FUEL TANK PANEL 638CB CUTOUT FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX EA 1-5710-90029.

Part: FRAME — DENTED (ZONE 200) · airframe 47,275 hrs · 9,751 cycles

UPPER CARGO RIGHT SIDEWALL, FRAME AT STA 1561 INNER CHORD FOUND DENT AT LONGERON 12R TO LONGERON 13R. CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I DUE TO CAT B REPAIR. REFER TO FEDEX EA 1-5330-90040.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 47,275 hrs · 9,751 cycles

AFT CARGO, 02 CORROSION FOUND AT RIGHT CEILING FLOOR STRUCTURE AT STA 1921 TO STA 1941 X= -40.

Part: STRINGER — CRACKED (ZONE 600) · airframe 47,275 hrs · 9,751 cycles

CRACK INDICATION FOUND AT STRINGER END OF STRINGER 12 (UPPER STRINGER), APPROXIMATE LENGTH 7 INCHES, RIGHT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I.

Part: STRINGER — CRACKED (ZONE 600) · airframe 47,275 hrs · 9,751 cycles

CRACK INDICATION FOUND AT STRINGER END OF STRINGER 14 (UPPER STRINGER), APPROXIMATE LENGTH 7 INCHES, RIGHT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I .

Part: STRINGER — CRACKED (ZONE 500) · airframe 47,275 hrs · 9,751 cycles

CRACK INDICATION FOUND AT STRINGER END OF STRINGER 13, UPPER STRINGER, LEFT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 47,275 hrs · 9,751 cycles

LEFT WING, UPPER FUEL TANK ACCESS PANEL 534BT CUTOUT FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX E.A. 1-5710-90037.

Part: STRINGER — CRACKED (ZONE 600) · airframe 47,275 hrs · 9,751 cycles

CRACK INDICATION FOUND AT STRINGER END OF STRINGER 16 (UPPER STRINGER), APPROXIMATE LENGTH 17 INCHES, RIGHT SIDE WING TANK. CRACK PROPAGATES TOWARDS INBOARD TO THE NEAREST WEB. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I AND CLIP REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. CLIP.

Part: STRINGER — CRACKED (ZONE 500) · airframe 47,275 hrs · 9,751 cycles

CRACK INDICATION FOUND AT STRINGER END OF STRINGER 10 (UPPER STRINGER), APPROXIMATE LENGTH 11.5 INCHES, LEFT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I.

Part: LONGERON — CORRODED (ZONE 100) · airframe 47,275 hrs · 9,751 cycles

CENTER CARGO, LONGERON CORROSION FOUND AT STA 1701 L50. REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,275 hrs · 9,751 cycles

UPPER CARGO, SEAT TRACK LBL 8 CORRODED AT STA 1551. SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · airframe 47,275 hrs · 9,751 cycles

CENTER CARGO, LONGERON CORROSION FOUND AT STA 1701 R50. REMOVED AS PER SRM 51-21-01 VOLUME II.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,275 hrs · 9,751 cycles

UPPER CARGO, SEAT TRACK RBL 77 CORRODED AT STATION 1350. SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 42,952 hrs · 8,766 cycles

COMPLY WITH EA 1-5510-76669 HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000. HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000' HAS BEEN COMPLIED.

Part: BRACKET — CORRODED (TE FLAPS) · airframe 42,952 hrs · 8,766 cycles

COMPLY EA 1-5750-78010 OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR HAS BEEN COMPLIED.

Part: WIRE — BURNED (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK CABIN AT STA 775 (RT) WIRE NR`S. C029-1-6AL, C029-2-6AL AND C029-3-6AL FND BURNT. GVI ON THE BURNT WIRES SURROUNDING AREAS,CONDUCTIVITY INSP PER DAC NDT SPM PART 06-10-01-001 REV11 ON M/D STA 775R FRAME/SKIN FND ACCEPTABLE RANGE. BURNT CABLES, REPAIRED USING COPALUM SPLICE PER BOEING SWPM20-30-13, CONDUCTIVITY/INSULATION. RESISTANCE CHECK PER SWPM29-21-01 SATIS. AIRPLANE POWER ASSURANCE CHECK/PHASE IMBALANCE TEST CARRIED OUT ON BOTH AUX HYD PUMP SATIS PER AMM29-21-01, SUBSEQUENT OPS CHK CARRIED OUT ON BOTH AUX HYD PUMPS. ALSO, FOUND SATIS PER AMM29-21-01-700-801. FEDEX EA 1-2920-79801 'HYD POWER-AUXILIARY HYD PUMP WIRING, SPLICE REPAIR COMPLIED WITH.

Part: STOP FITTING — CRACKED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. LEFT HAND WING - OUTBOARD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30 AND ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00, FOUND SATISFACTORY.

Part: STOP FITTING — CRACKED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. RIGHT HAND WING - OUTBOARD FLAP CRACKED STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL I.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 42,952 hrs · 8,766 cycles

EMPENNAGE HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 35R SIDEWALL CORROSION BLENDED OUT FOUND EXCEEDED LIMIT. EMPENNAGE HORIZONTAL STABILIZER RIGHT HAND NR 35R BARREL NUT BORE REPAIRED AS PER FEDEX EA 1-5510-78027. HORIZONTAL STABILIZER BARREL NUT BORE NR 35R. BLEND OUT EXCEEDING MAX, LIMITS AFTER BORING THROUGH THE BOTTOM (MD-11 S/B 55-023 REV 1).

Part: SPAR CAP — CORRODED (ZONE 300) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND HORIZONTAL STABILIZER NR 36L FOUND WITH CORROSION BEARING, SIDEWALL AND BOTTOM. CORROSION CLEAN-UP AND FOUND EXCEEDED LIMIT AS PER SB MD11 55-023. HORIZONTAL STABILIZER NR 36L BARREL NUT BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-78026. HORIZONTAL STABILIZER BARREL NUT BORE NR 36L CORROSION REPAIR PER BOEING SB MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000.

Part: CAP — CORRODED (ZONE 300) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND HORIZONTAL STABILIZER NR 36R FOUND WITH CORROSION BEARING, SIDEWALL AND BOTTOM. CORROSION CLEAN-UP AND FOUND EXCEEDED LIMIT PER SB MD11- 55-023. RIGHT HAND HORIZONTAL STABILIZER NR 36R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-78021 TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 36R - CORROSION REPAIR PER BOEING SB MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000.

Part: FITTING — WORN (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING MID AND AFT HOLES FOUND WORN. RIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING REMOVED & REPLACED AS PER EO 1-5750-7-5005 PT2 TITLE : WINGS - TRAILING EDGE DEVICES - INSPECT/MODIFY I/B FLAP VANE ATTACH FITTINGS STEP 32 AND FLAP VANE OPERATION CHECK CARRIED OUT. FOUND SATISFACTORY AS PER AMM 27-50-00.

Part: TEE FITTING — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING AFT HOLE FOUND WORN. LEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING AFT HOLE REAMED AS PER SRM 51-31-01 VOL 2, ORIGINAL DIAMETER=0.875 INCH, FINAL DIAMETER=0.895 INCH, REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78019, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE OUTBOARD (NR 1) TEE FITTING AFT HORIZONTAL BORE WEAR - REPAIR.

Part: VANE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP VANE NR 3 TEE FITTING FORWARD AND AFT BOLT HOLES CORRODED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK SEAT TRACK FOUND CRACKED AT STA 635 RT 8 INCHES.

Part: VANE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP VANE NR 4 TEE FITTING AFT BOLT HOLE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE BRACKET (FLAP SIDE), AFT ATTACHMENT POINT FORWARD BOLT HOLE FOUND CORRODED.

Part: PANEL — CORRODED (ZONE 300) · airframe 42,952 hrs · 8,766 cycles

EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 10 BORE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 10 BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-78022 TITLE: STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE NR 10R - CORROSION REPAIR PER BOEING SB MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000.

Part: PANEL — CORRODED (ZONE 300) · airframe 42,952 hrs · 8,766 cycles

EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 28 BEARING AND BOTTOM SURFACE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND NR 28 BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-78029, TITLE: STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE NR 28R, THIN FLOOR CONDITION, BORE THROUGH, (MD-11 S/B 55-023 REV 1).

Part: PANEL — CORRODED (ZONE 300) · airframe 42,952 hrs · 8,766 cycles

EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 8 BORE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND NR 8 BARREL NUT BORE. REPAIRED AS PER FEDEX EA 1-5510-78023 - STABLIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE 8R. AUTHORIZATION TO BORE THROUGH THE BOTTOM (MD-11 SB 55-023 REV 1)

Part: FITTING — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP VANE NR 3 TEE FITTING AFT BOLT HOLE CORRODED. RIGHT HAND WING, OUTBOARD FLAP VANE NR 3 TEE FITTING AFT BOLT HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. ORIGINAL HOLE SIZE DIA 0.3125 INCH FINAL HOLE SIZE DIA 0.375 INCH REPAIR CARRIED OUT AS PER EA 1-5750-78016. TITLE: WINGS, TRAILING EDGE FLAPS, RT O/B FLAP VANE NR 3 TEE FITTING CORROSION REPAIR.

Part: VANE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP VANE NR 1 TEE FITTING AFT BOLT HOLE CORRODED.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 42,952 hrs · 8,766 cycles

EMPENNAGE - HORIZONTAL STABILIZER LEFT HAND BARREL NUT 24L SURFACE CORROSION BLENDED OUT FOUND EXCEEDED LIMIT. EMPENNAGE - HORIZONTAL STABILIZER LEFT HAND 24L BARREL NUT BORE REPAIRED AS PER FEDEX EA 1-5510-78030, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE 24L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7- 5000.

Part: VANE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP VANE NR 2 TEE FITTING FWD BOLT HOLE CORRODED. CORROSION REMOVED AS PER SRM 51-21-01.

Part: PANEL — CORRODED (ZONE 300) · airframe 42,952 hrs · 8,766 cycles

EMPENNAGE, RIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT HOLE FOUND WITH CORROSION ON BOTTOM AND FOUND EXCEEDED LIMIT PER S/B MD-11 55-023. EMPENNAGE, RIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT BORE REPAIRED AS PER FEDEX EA 1-5510-78028, TITLE: STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE NR 5R, BLEND OUT EXCEEDING LIMITS IN THE FLOOR OF THE BORE (MD-11 S/B 55-023 REV 1).

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD HOLE SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 .

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED.

Part: BRACKET — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. RIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER =1.327 INCH AND REPAIRED AS PER FEDEX EA 1-5750-78013, TITLE: WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP - OUTBOARD BRACKET PIVOT BORE CORROSION - REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. RIGHT HAND WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.254 INCH AND REPAIRED AS PER FEDEX EA NR 1-5750- 78013, TITLE: WINGS, TRAILING EDGE FLAPS, RIGHT HAND INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 AND REPAIRED AS PER EA 1-5750-78012.

Part: FRAME — CHAFED (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

FRAME FOUND CHAFED MARK AT STA 535 LONGERON R19-24.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK UPPER BOLT HOLE FOUND CORRODED.

Part: BRACKET — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.223 INCH AND REPAIRED AS PER FEDEX EA 1-5750-78010, TITLE: WINGS - OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER =1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FEDEX EA 1-5750-78010, OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED.

Part: BRACKET — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.224 INCH AND REPAIRED AS PER FEDEX EA 1-5750-78010, TITLE: WINGS - OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407 ORIG THK 0.52 MATERIAL REMOVED 0.033 REMAINING THICKNESS 0.487 & FOUND WITHIN LIMITS AS PER DWG TOLERANCE OF ARC0502.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FEDEX EA 1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR.

Part: FRAME — DENTED (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK FRAME FOUND DENT AT STA 535 LONGERON L19-24.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING OUTBOARD BOLT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AND REPAIRED AS PER FEDEX EA #1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.225 AND REPAIRED AS PER FEDEX EA 1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR.

Part: BRACKET — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407 ORIGINAL THICKNESS 0.517 INCH, MATERIAL REMOVED 0.004 INCH REMAINING THICKNESS 0.513 INCH & FOUND WITHIN LIMITS AS PER DWG TOLERANCE OF ARC0503.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK SEAT TRACK FOUND WORN AT STA 699 LBL 47 INCHES.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD BOLT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AND REPAIRED AS PER FEDEX EA #1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,952 hrs · 8,766 cycles

RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FEDEX EA 1-5750-78010, OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK SEAT TRACK FOUND CRACKED AT STA 905 RT 28. REMOVED AND REPAIRED IAW SRM 53-70-00 FIG 1 VOL I.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING LOWER WINGLET WING SIDE - AFT INTERNAL MOUNT BOLT HOLE AREAS HAVE MINOR SURFACE CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187", FINAL DIAMETER=1.255 AND REPAIRED AS PER FEDEX EA 1-5750- 76775, TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP - PIVOT BORE - REPAIR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK SEAT TRACK FOUND WORN AT STA 492 RIGHT 63.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD SPOTFACE FOUND CORRODED.

Part: FITTING — CRACKED (ZONE 100) · airframe 42,952 hrs · 8,766 cycles

CENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 44 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED.

Part: FITTING — CRACKED (ZONE 100) · airframe 42,952 hrs · 8,766 cycles

CENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 45 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED.

Part: FITTING — CRACKED (ZONE 100) · airframe 42,952 hrs · 8,766 cycles

CENTER CARGO COMPARTMENT BILGE AREA, LEFT HAND LONGERON 51 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACKED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK - SEAT TRACK FOUND WORN AT STA 492 RT 63.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.328 AND REPAIRED AS PER FEDEX EA 1-5750- 76775, TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP - PIVOT BORE - REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK SEAT TRACK FOUND WORN AT STA 792 RIGHT 48 INCHES.

Part: FITTING — CRACKED (ZONE 100) · airframe 42,952 hrs · 8,766 cycles

CENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 49 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK SEAT TRACK AT R1 DOOR WAY FOUND CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,952 hrs · 8,766 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

FOUND MAIN DECK SEAT TRACK CORROSION AT STA 460 LEFT HAND MOST OUTBOARD. MAIN DECK SEAT TRACK FOUND CORROSION AT STA 460 LEFT HAND MOST OUTBOARD REMOVED AS PER SRM 51-31-01 VOL 2 AND SRM 51-33-01 VOL 2. THE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 PG 7 VOL 1. THE ORIGINAL THK 0.1 INCH REMAIN THK 0.051 INCH TO 0.099 INCH. THE NEW SEAT TRACK INSTALLED AS PER SRM 51-31-01 VOL 2 AND SRM 51-33-01 VOL 2.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

MAIN DECK SEAT TRACK FOUND CORROSION AT STA 5-113 LEFT HAND 8 INCHES.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,952 hrs · 8,766 cycles

SEAT TRACK FOUND CRACKED AT STA 792 RIGHT 28 INCHES. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL 1 AND CRACK FREE ON CUT OUT AREA BY NDT INAPECTION.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 42,461 hrs · 8,640 cycles

AT 200 FT AGL ON LANDING GOT CABIN SMOKE LEVEL 3 ALERT, WENT OUT SHORTLY. ALERT ON DURING LANDING ROLL THEN WENT OUT. EMERGENCY DECLARED. ON TAXI, CABIN SMOKE LEVEL 3 ALERT, STEADY. APU RUNNING, ENGINE SHUTDOWN. F/O WENT BACK TO OPEN DOOR, SMELLED SMOKE. EMERGENCY EVACUATION DECLARED. APU FIRE HANDLE PULLED. AGENT WAS DISCHARGED. EXITED BY L-1 ENTRY DOOR SLIDE. R&R CARGO COMPT AFT CARGO DET 5 PER MM 26-14-01-4, DUE FAIL ON TEST & SENT MESSAGE ALERT. R&R NR 2 FIREX ENG/APU CONTAINER PER MM 26-21-01-4. R&R MSC PER MD-11 MM 31-42-01-4 & OPS TEST PER MD-11 MM 31-42-01-5 FOR PRECAUTIONARY PURPOSE. R&R NR 1, 2 & 3 WATER SEPARATOR COALESCER PER MD-11 AMM 21-54-05-2.

Part: SMOKE — DETECTED · airframe 42,460 hrs · 8,639 cycles

AT 200 FT AGL ON LANDING IN SFS, GOT A CABIN SMOKE LVL 3 ALERT, IT WENT OUT SHORTLY. ALERT ON AGAIN DURING LANDING ROLL, THEN OUT. EMERGENCY DECLARED. ON TAXI IN, CABIN SMOKE LEVEL 3 ALERT ON STEADY. APU RUNNING. ENGINE SHUTDOWN. F/O SMELLED SMOKE. EMERGENCY EVACUATION DECLARED. REMOVED AND REPLACED SMOKE CARGO COMPT DETECTOR AFT CARGO DETECTOR 5 PER MM 26-14-01-4, OPS CHECK PER MM 26-14-01-5 PASSED. REMOVED AND REPLACED NR 2 FIREX ENG/APU CONTAINER. REMOVED AND REPLACED MSC, OPS TEST. REMOVED AND REPLACED NR 1, 2 AND 3 WATER SEPARATOR AMM 21-54-05-2. C/W MTSI ITEM NR 3 WRI 26-1/9032 AIR CONDITIONING PACK AND DISTRIBUTION DUCT ODOR CHECK PER MM 21-53-00-7 SATISFACTORY, A/C OK FOR SERVICE.

Part: TRIM MOTOR — CONTAMINATED (HORIZ STAB) · airframe 39,608 hrs · 8,013 cycles

UPON APPLICATION OF POWER UP FOR TAKEOFF THE STABILIZER MOVED FROM 7.3 TO 5.4. AFTER REJECTED TAKEOFF WHILE ON TAXIWAY STABILIZER, RESET TO 7.3. UPON SUBSEQUENCY TAXI THE STAB MOVED BY ITSELF TO 9.2 AND THEN BACK TO ABOUT 5. T/S AND FOUND NR 2 TRIM MOTOR C/P RECEPTICAL FULL OF WATER AND C/P P1-1924, ALSO FULL OF WATER, DUE PREVIOULSLY BADLY ASSEMBLED. REMOVED AND REPLACED HORIZONTAL STAB TRIM MOTOR, POSITION NR 2, IN REFERENCE TO REMOVED AND REPLACED CANNON PLUG P1-1924 ON NR 2 TRIM MOTOR PER MD11 WDM 22-22-01.

Part: SUPPORT — CRACKED (SLAT TRACK) · airframe 37,747 hrs · 7,606 cycles

RT WING LE SUPPORT LOCATED ON NR 16 SLAT TRACK AT XOS 1005.124. FOUND WITH CRACK APPROX. 1 INCH IN LENGTH. CRACKED SUPPORT RIB ON RT WING LE LOCATED ON NR 16 SLAT TRACK AT XOS 1005.124 REMOVED AND REPLACED AS PER SRM 51-31-01, VOL. II.

Part: SUPPORT — CRACKED (LT WING) · airframe 37,747 hrs · 7,606 cycles

LT WING L/E WING SUPPORT FOUND CRACKED AT NR 16 SLAT TRACK.

Part: TAILPIPE — FIRE (NR 2 ENGINE) · airframe 6,940 hrs · 34,884 cycles

AFTER BLOCK IN & ENGINE SHUTDOWN, NR 2 ENGINE TAILPIPE ON FIRE. R&R APU NR 1 FIRE BOTTLE PER MM 26-21-01-4.

Part: SUPPORT — CORRODED (FLOORBOARD) · airframe 33,937 hrs · 6,723 cycles

CORROSION ON FLOORBOARD HAT SECTION SUPPORT AT BS 457 X=+76 IN AT FWD CABIN. REMOVED AND REPLACED FLOORBOARD PER SRM 51-31-01 VOL II.

Part: ACTUATOR — OUT OF ADJ (AILERON)

A/C MADE AIR TURNBACK DUE DEFLECT AILERON DISAGREE ALERT. LT O/B ACTUATOR ADJUSTED AND SAFETIED PER MXP 27-2 METHOD "D".

Part: SEAT TRACK — CRACKED (CABIN) · airframe 29,903 hrs · 5,835 cycles

MAIN DECK (BALL MAT AREA) RIGHT BS 635, RBL 8.5 SEAT TRACK FOUND CRACKED. *S/D* REMOVED PER 53-70-00 FIG 1, VOL I & 51-33-01 VOL II. FLOOR PNL 232FF & 233EF REMOVED FOR ACCESS AND REINSTALL PER MM 53-21-04-4.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 29,903 hrs · 5,835 cycles

MAIN DECK (BALL MAT AREA) - LEFT BS 635, LBL 8.K, SEAT TRACK FOUND CRACKED. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1, VOL I & 51-33-01 VOL II. FLOOR PANEL 233EF & 233FF REMOVED FOR ACCESS AND REINSTALLED PER 53-21-04-4.

Part: FLAP — MALFUNCTIONED (WING)

DURING T/O, FLAP RETRACT AIL DEFLECT DISAG LEVEL 2 ALERT SHOW BOTH DEFLECTED.

Part: SEAT TRACK — CRACKED (BS 635)

MAIN DECK AREA - CRACK FOUND ON SEAT TRACK AT STA 635 X = 47.5 LT. CRACK LENGTH APPROX 3.85 IN. *S/D* CRACK AREA TRIMMED OUT AT STA 625 & 645. NEW TRACK REWORKED PER DWG NR NCA 6792. SPLICE HATS REWORK AND SPLICE PLATES FAB AND WEB INSTALLED PER SRM 53-70-00.

Part: LINE — LEAKING (NR 1 HYD SYST)

98-0169 - STA-HKG - APPROX 1.5 HR INTO FLT HYD 1 OFF LEVEL 2 ALERT ILLUMINATED WITH HYD 1 RESERVOIR INDICATING 2.8 GAL RESERVOIR QTY CONT TO DROP UNTIL HYD 1 FAIL LEVEL 2 ALERT ILLUM WITH QUAN INDICATING 1 GAL RESERVOIR CONT DECREASE UNTIL REACH ZERO. ON ARRIVAL FND HYD LEAK AT NR 1 ENG RT HYD PUMP CASE DRAIN LINE FAB LINE PER M/M SUP 20-10-01. REPLACED SAME LEAKS CKD OK SERV NR 1 HYD SYS QTY. NR 1 ENG HYD PUMPS OPS AND INDS CKD OK CKD NR 1 HYD MANIFOLD FILTERS, NO CONTAMINATION CKD POP OUT INDICATORS AND ALL STAYED IN.

Part: VALVE CONTROLLER — MALFUNCTION (NR 2 ENGINE)

AT FLIGHT LEVEL OF 24,000 FEET AND DESCENDING A LEVEL 2 ALERT TANK 2 PUMPS OFF ILLUMINATED. THE FUEL SYSTEM CONTROLLER WAS IN AUTO AT THE TIME. SWITCHED THE SYSTEM TO MANUAL TO TRY TO TURN THE PUMPS ON AND AT THIS TIME THE NR 2 ENGINE FLAMED OUT. ACCOMPLISHED CHECKLISTS AND GOT A RESTART. REMOVED AND REPLACED THE NR 2 TANK FILL VALVE CONTROLLER. REMOVED AND REPLACED THE FUEL SYSTEM CONTROLLER. SYSTEM OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — FAILED (FUEL QTY SYST)

LEVEL 2 FUEL QUANTITY USED CHECK ALERT ILLUMINATED APPROXIMATELY 25 MINUTES INTO FLIGHT. ACCOMPLISHED THE CHECK LIST, THEN RAN FUEL SYSTEM IN MANUAL WITH NO APPARENT LOSS OF FUEL FOR APPROXIMATELY 30 MINUTES. RETURNED SYSTEM TO AUTO AND OBSERVED ABNORMAL DEPLETION OF FUEL. PRIOR TO RUNNING CHECK LIST WE WERE SHORT APPROXIMATELY 3600 TO 4200 LBS OF FUEL. REPLACED THE FUEL QUANTITY DATA CONTROL UNIT.