N598FE

Part: SKIN — DAMAGED (AFT) · airframe 85,427 hrs · 17,869 cycles

NR 3 PACK DOOR CUT OUT UPPER AFT CORNER SKIN LOOKS TO BE CRACKED. PERFORMED HFEC OF SUSPECTED DAMAGED AREA, REF BOEING NTSPM 06-10-.01 PROCEDURE 11. CONFIRMED CRACK DEFECT INDICATION AND MARKED LENGTH. SHGN 02NOV20 06:31 MEM U. DUCT IN PACK 3 BAY REMOVED TO FOM AND PLACED IN PACK 3 BAY OUT OF THE WAY. SHGN 02NOV20 21:09 MEM U. THIS EVENT REQUIRES AN SDR STRP 02NOV20 21:09. MEM U SHGN 02NOV20 23:39 MEM U. REMOVED DAMAGE IN REFERENCE TO MD10 SRM 53-50-00 STRP 02NOV20 23:39. MEM U SHGN 02NOV20 23:53 MEM U. VERIFIED ALL DAMAGED IS REMOVED WITH HFEC, PER MD11 NDTSPM PT6 STRP 02NOV20 23:53. MEM U FACT 04NOV20 10:32 MEM. REPAIRED NR 3 PACK DOOR CUTOUT SKIN IN THE UPPER AFT CORNER, IAW EA 1-5300-T0357828 P1 AND SRM 53-20-15-2R REPAIR 3.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 83,973 hrs · 17,528 cycles

L1 EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST LIGHT INOP. RELEASED FOR SERVICE PER MEL : 25-61-02 CATEGORY : C EXPIRATION : 18MAY20 MEL 25-61-02: L1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY. RELAMPED L1 SLIDE REMOTE PRESSURE INDICATOR REF AMM 25-61-04-4. INDICATOR OPS CHECKS GOOD. A/C OKAY FOR SERVICE.

Part: CABLE — FAILED (PARKING BRAKE) · airframe 82,587 hrs · 17,105 cycles

UNABLE TO SET PARK BRAKE.PARK BRAKE KEEPS SPRINGING BACK. PARKING BRAKE CABLE AND ROD END REPLACED IAW AMM 32-44-00-5. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SPRING — BROKEN (L1 DOOR) · airframe 81,926 hrs · 16,903 cycles

MDIS 598 52-10 1538 02JUL19 IND OPEN U WHEN AIRCRAFT BLOCKED IN THE L1 MAIN CABIN DOOR EMERGENCY EXIT SIGN MOVABLE CEILING PANEL WOULD NOT GO UP WITH DOOR INTO CEILING. SEEMS THE DRIVE CABLE IS BROKEN MEL 02JUL19 06:52 IND U RELEASED FOR SERVICE PER MEL : 52-10-03-03 CATEGORY : C EXPIRATION : 12JUL19 "MEL 52-10-03-03: (IDENTIFY 1L OR 1R) _1L__ MAIN ENTRY (IDENTIFY DOOR OR SLIDE/RAFT) _DOOR_______ - (IDENTIFY INOP OR REMOVED) __INOP___ - EXTENDED OVERWATER OPS REQUIRES TWO SLIDES AND/OR RAFTS." UPON INVESTIGATION FOUND L-1 CABIN DOOR SLIDING CEILING PANEL TENSION SPRING BROKEN. REPLACED SPRING AND TUBE REF AMM 25-23-23-4. OPS CHECK NORMAL. THIS CLEARS WRI. A/C OK FOR SERVICE.

Part: BRACKET — CORRODED (RT WING) · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # : 1-5750-T0331088A P1 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- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501069 FOR WORK DETAILS.

Part: BRACKET — CORRODED (LT WING) · airframe 81,789 hrs · 16,867 cycles

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

Part: BRACKET — CORRODED (RT WING) · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # : 1-5750-T0331088A P1 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- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501069 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

MAIN DECK AFT FLOOR SUPPORT AT STATION 1887 - 2007 X = - 57 FOUND CORROSION . MAIN DECK AFT FLOOR SUPPORT AT STATION 1887 TO STATION 2007 X = - 57 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 . CORRODED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = - 57 AS PER SRM 51-31-01-0G . FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7551 REV G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING UPPER WING SURFACE TRAILING EDGE FOUND CORROSION AT XORS 1070. REPAIR CARRIED OUT AT RIGHT WING - UPPER WING SURFACE TRAILING EDGE AT XORS 1070 AS PER ENGINEERING AUTHORIZATION : 1-5730-T0347222 P1 TITLE : WING - PLATES AND SKINS - RIGHT WING - ARB7404-4 TAPERED UPPER AFT SKIN CORROSION REPAIR BETWEEN XORS 1070.000 AND XORS 1093.639. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.CORROSION REMOVED ON RIGHT HAND WING UPPER SURFACE SKIN AT XORS 1070 AND FOUND OUT OF LIMITS AS PER SRM 57-00-01-1A FIGURE 101 ALLOWABLE DAMAGE 1.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND LOWER BARREL NUT FACE EXCEED LIMIT BASED THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAX REWORK LIMITS FOR BARREL NUT HOLE. MINIMUM THICKNESS : 0.3685". REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # : 1-5750-T0347199 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- RH WING- OUTBD FLAP INBD HINGE ASSY (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750- T0347199 P1 AND SNRM NO. N00491 FOR WORK DETAILS.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 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 AND UPPER BARREL NUT FACE EXCEED LIMIT BASED THE DIFFERENCE BETWEEN DRAWING LIMIT AND CMM MAX REWORK LIMIT FOR BARREL NUT HOLE. MINIMUM THICKNESS : 0.3685". REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # : 1-5750-135631A P2 STEP 2. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-135631A P2 AND SNRM NO. N00401 FOR WORK DETAILS.

Part: SEAT TRACK — CORRODED (BS 421-107.25) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

MAIN DECK RIGHT HAND OUTBOARD FLOOR CURVE SEAT TRACK AT STATION 421 X = -107.25 FOUND CORROSION . MAIN DECK RIGHT HAND OUTBOARD FLOOR AT CURVE SEAT TRACK STATION 421 X = - 107.25 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED CURVE SEAT TRACK REPAIRED AS PER E. A. #: 1-5321- T0347197 P 1. TITLE : FUSELAGE - CARGO COMP FLOORS - MAIN DECK CARGO COMPARTMENT - CORROSION FOUND ON RH OUTBOARD SEAT TRACK AT X = - 107.25 , BETWEEN STA 416 AND STA 421.578 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SKIN — DENTED (CARGO DOOR) · airframe 81,789 hrs · 16,867 cycles

AFT CARGO DOOR FORWARD EDGE APPROXIMATELY10 INCHES BELOW FORWARD UPPER CORNER FOUND DENT 5.5" LENGTH X 1.5" WIDTH X 0.086"DEPTH AT STATION Y = 1942 DENT AT AFT CARGO DOOR FORWARD EDGE APPROXIMATELY 10 INCHES BELOW FORWARD UPPER CORNER CARRIED OUT REPAIRED AS PER ENGINEERING AUTHORIZATION # 1-5232- T0347226 P1 TITLE : DOOR - AFT CARGO DOOR - ACCOMPLISH SRM REPAIR ON AFT CARGO DOOR , STATION Y1942 ASSEMBLY - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 81,789 hrs · 16,867 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 605 LOWER STRINGER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB2933 REVISION AJ. INSTALLED DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 605 LOWER AREA AS PER SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 81,789 hrs · 16,867 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 EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # : 1-5750-T0331088A P1 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- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501069 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (LT WING) · airframe 81,789 hrs · 16,867 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT LOWER STATION XOS 546 STRINGER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB2933 REVISION AJ. INSTALLED FABRICATED DOUBLER AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT LOWER STATION XOS 546 AS PER SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 81,789 hrs · 16,867 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 939 FORMER FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB1292 REVISION G. INSTALLED FORMER AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 939 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING TE FLAP) · airframe 81,789 hrs · 16,867 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. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # : 1-5750- T0331087A P1 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- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501102 FOR WORK DETAILS.

Part: SKIN — CRACKED (LT WING) · airframe 81,789 hrs · 16,867 cycles

HFEC INSPECTION CARRY OUT AND FOUND CRACK APPROXIMATELY 1/4" IN LENGTH AT LEFT HAND SIDE CORNER NUMBER 11 FUEL ACCESS DOOR FORWARD INBOARD CORNER. REPAIR CARRIED OUT AT LEFT HAND SIDE CORNER NO.11 FUEL ACCESS DOOR FORWARD INBOARD CORNER AT XOS 586 AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 18. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT NEXT ' C ' CHECK NOT EXCEEDING 24 MONTHS AND REPETITIVE INSPECTION EVERY ' C ' CHECK NOT EXCEEDING 24 MONTHS BY VISUAL METHOD AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 18 TABLE 204.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR 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-T0347199 P1 STEP 1B. TITLE : WINGS- FLIGHT SURFACES- EO 1- 5750-7- 5002- RH WING- OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347199 P1 AND SNRM NO. N00491 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 08.SHOULDER BUSHING FABRICATED BY MACHINING AND REPAIR SHIM FABRICATED AS PER MD- 11 CMM 57-44-08 AND E.A. # : 1-5750-T0347199 P1 STEP 1A AND STEP 1 AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # : 1-5750-T0347199 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- RH WING- OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347199 P1 AND SNRM NO. N00491 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND E.A. # : 1-5750-135627E PART 5 STEP 2A AND STEP 2.B. TITLE : WINGS- FLIGHT SURFACES- LT WING - INBD FLAP - OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND E.A. # : 1-5750-76657F PART 6 STEP 2.A AND STEP 2.B. TITLE : WINGS- FLIGHT SURFACES- RT WING - INBD FLAP - OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CHAFED (BS 535) · airframe 81,789 hrs · 16,867 cycles

MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT FOUND EXISTING REPAIR OUTER ANGLE CHAFFED . MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT , CHAFFED MARK AT EXISTING OUTER REPAIR ANGLE REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00- 2R FIGURE 205 . CHAFFED OUTER EXISTING REPAIR ANGLE REMOVED AS PER SRM 51-31-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND E.A. # : 1-5750-76657F PART 6 STEP 2.A AND STEP 2.B. TITLE : WINGS- FLIGHT SURFACES- RT WING - INBD FLAP - OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750- 76657F PART 6 AND SNRM N00553 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR 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-T0347199 P1 STEP 1B. TITLE : WINGS- FLIGHT SURFACES- EO 1- 5750-7- 5002- RH WING- OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLES) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND E.A. # : 1-5750-135627E PART 5 STEP 2A AND STEP 2.B. TITLE : WINGS- FLIGHT SURFACES- LT WING - INBD FLAP - OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750- 135627E PART 5 AND SNRM N00533 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 08. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # : 1-5750- T0347199 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- RH WING- OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347199 P1 AND SNRM NO. N00491 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 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-T0347199 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750- 7- 5002- RH WING- OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347199 P1 AND SNRM NO. N00491 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 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-T0347329 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- RH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347329 P1 AND SNRM NO. N00418 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT INBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT INBOARD HOLE BORE (#2 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-T0347329 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- RH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE (#2 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-T0347329 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750- 7- 5002- RH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347329 P1 AND SNRM NO. N00418 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 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-T0347329 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750- 7- 5002- RH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347329 P1 AND SNRM NO. N00418 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR 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-T0347329 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1- 5750- 7- 5002- RH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347329 P1 AND SNRM NO. N00418 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. REPAIR EVALUATED AND FOUND FORWARD MOUNT OUTBOARD LUG SURFACE REMAINING THICKNESS : 0.376" ACCEPTED AS PER E.A. # : 1-5750-T0347329 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750- 7- 5002- RH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347329 P1 AND SNRM NO. N00418 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (RT WING) · airframe 81,789 hrs · 16,867 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 664 BEADED DOUBLER FOUND CRACKED REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 664 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 81,789 hrs · 16,867 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 669 BEADED DOUBLER FOUND CRACKED REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 669 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1386) · airframe 81,789 hrs · 16,867 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1386 X = 8.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR AT SEAT TRACK STATION 1386 X = 8.5 CROWN DAMAGED EDGE BLEND OUT 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 1311 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (BS 1541) · airframe 81,789 hrs · 16,867 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1541 X = 27.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1541 X = 27.5 , DAMAGED CROWN EDGE BLEND OUT 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 1551 TO EXISTING SPLICE STATION 1531 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (RT WING) · airframe 81,789 hrs · 16,867 cycles

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

Part: SEAT TRACK — DAMAGED (BS 1541) · airframe 81,789 hrs · 16,867 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1541 X = 8.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1541 X = 8.5 , DAMAGED CROWN EDGE BLEND OUT 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 1551 TO EXISTING SPLICE STATION 1531 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (LT WING) · airframe 81,789 hrs · 16,867 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 701 BEADED DOUBLER FOUND CRACKED REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 701 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 81,789 hrs · 16,867 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 613 BEADED DOUBLER FOUND CRACKED REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 613 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR 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-T0347329 P1 STEP 1. TITLE : WINGS- FLIGHT SURFACES- EO 1- 5750- 7- 5002- RH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-T0347329 P1 AND SNRM NO. N00418 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (BULKHEAD WEB) · airframe 81,789 hrs · 16,867 cycles

FUSELAGE - CENTER LANDING GEAR COMPARTMENT FORWARD BULKHEAD LEFT HAND WEB DOUBLER FOUND 1" CRACKED AT STATION Y = 1381. FUSELAGE - CENTER LANDING GEAR COMPARTMENT FORWARD BULKHEAD LEFT HAND WEB DOUBLER 1" CRACKED AT STATION Y = 1381 REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 81,789 hrs · 16,867 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 760 BEADED DOUBLER FOUND CRACKED REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 760 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1139) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1139 X = 75.25 FOUND CORROSION . MAIN DECK FLOOR SEAT TRACK AT STATION 1139 X = 75.25 , CORROSION REMOVED AND FOUND TO EXCEED LIMIIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO EXISTING SPLICE STATION 1129 X = 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR 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. # : 1-5750-135629A P2 STEP 2B. TITLE : WINGS- FLIGHT SURFACES- EO 1- 5750-7-5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-135629A P2 AND SNRM NO. N00378 FOR WORK DETAILS.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT INBOARD HOLE BORE (#2 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. # : 1-5750-135631A P2 STEP 2A AND STEP 2. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-135631A P2 AND SNRM NO. N00401 FOR WORK DETAILS.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR 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. # : 1-5750-135631A P2 STEP 2B AND STEP 2. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750- 135631A P2 AND SNRM NO. N00401 FOR WORK DETAILS.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR 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. # : 1-5750-135629A P2 STEP 2B. TITLE : WINGS- FLIGHT SURFACES- EO 1- 5750-7-5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-135629A P2 AND SNRM NO. N00378 FOR WORK DETAILS.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT LEFT 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. # : 1-5750-135629A P2 STEP 2A AND STEP 2. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-135629A P2 AND SNRM NO. N00378 FOR WORK DETAILS.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE (#2 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. # : 1-5750-135631A P2 STEP 2A AND STEP 2. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 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. # : 1-5750-135629A P2 STEP 2A AND STEP 2. TITLE : WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,789 hrs · 16,867 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR 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. # : 1-5750-135631A P2 STEP 2B AND STEP 2. TITLE : WINGS- FLIGHT SURFACES- EO 1- 5750-7-5002- LH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. # : 1-5750-135631A P2 AND SNRM NO. N00401 FOR WORK DETAILS.

Part: WIRE — SHORT (LT WING) · airframe 80,203 hrs · 16,378 cycles

RECEIVED LEVEL 2, SLAT DIAG, ALERT ON APPROACH AFTER SELECTING FLAPS 15 DEG. ISOLATED SHORT IN N011-10-20RD NEAR CLAMP UNDER PANEL 517CT AT TRANSITION POINT BETWEEN NR 1 ENGINE PYLON AND OUTBOARD LEADING EDGE. REMOVED AND REPLACED 3 FOOT SECTION OF TWISTED PAIR WIRES IAW WDM 27-84-01 SH 2 AND SWPM 20-10-03.

Part: SENSOR — FAULTY (LE SLAT) · airframe 80,139 hrs · 16,356 cycles

SLAT DISAG LEVEL 2 ALERT AFTER SLAT EXTENSION ON APPROACH. INTERMITTENT ALERT FROM FLAPS 28 THROUGH TOUCHDOWN. CALL TO MOCC ON SATCOM INDICATED THAT IT WAS A SENSOR PROBLEM AS REPORTED BY ACFT TELEMETRY. REMOVED AND REPLACED LT NR 4 SLAT POSITION SENSOR A P/N 8-621-02 IAW AMM 27-84-03-4. OPERATIONAL CHECK GOOD. NO SLAT DISAGREE MESSAGES NOTED.

Part: CYLINDER — SHEARED (MLG) · airframe 79,603 hrs · 16,162 cycles

DURING GEAR EXTENSION FOR APPROACH, UNSAFE CENTER GEAR INDICATION ON BOTH PRIMARY & SECONDARY POSITION INDICATORS. AFTER GO-AROUND WITH GEAR EXTENDED, CREW REFERENCED QRH. ALTERNATE GEAR EXTENSION, NO HELP. ALTERNATE CENTER GEAR EXTENSION RESULTED IN A SAFE PRIMARY AND SECONDARY CENTER GEAR INDICATION. DURING GVI OF CENTER GEAR, FOUND THE UNLOCK CYLINDER SHEARED COMPLETELY OFF OF THE UPPER LOCK LINK. THE SURROUND STRUCTURE SHOWS WEAR, EITHER FROM IT RUBBING OR WHEN IT SHEARED OFF. COMPLETED AN OPS CHECK, OPS CHECKED GOOD, NORMAL EXTENSION. AND RETRACTION, ALTERNATE CENTER GEAR EXTENSION WITH AND WITHOUT HYDRAULICS ALL GOOD IAW AMM 32-32-00-5, AND 32-32-00-5.

Part: CABLE — FAILED (RT MLG) · airframe 78,155 hrs · 15,719 cycles

PDIS 598 32-60 9240 06DEC17 MCO OPEN U LOGPAGES:2606906 AFTER T/O RIGHT MAIN GEAR UNSAFE. CHECK CONFIG PAGE. SHOWED UNSAFE AS WELL. CYCLED GEAR DOWN AND BACK UP. GEAR UP AND LOCKED. REPLACED RH GEAR DOOR FOLLOW UP CABLE IAW M/M 32-31-10-4. JACKED AIRCRAFT PER M/M 07-11-00-2. PERFORMED LANDING GEAR AND DOOR OPERATIONAL CHECK PER M/M 32-31-00-05, CHECKS NORMAL.

Part: SWITCH — BROKEN (ESCAPE SLIDE) · airframe 77,861 hrs · 15,639 cycles

FOUND THE EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST BUTTON BROKEN. REMOVED AND REPLACED THE PRESS-TO TEST SWITCH IAW AMM 25-61-04-4, OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 77,356 hrs · 15,508 cycles

MAIN DECK SEAT TRACK AT BS 5-63, LBL 8.5 FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 77,356 hrs · 15,508 cycles

AGING A/C-EXISTING REPAIR ON FRAME AT MAIN CARGO COMPARTMENT STA 1721, L11L. EXISTING REPAIR ON FRAME AT MAIN CARGO COMPARTMENT STA 1721 L11L EVALUATED AND FOUND EXISTING FRAME REPAIR DAMAGED. DAMAGED EXISTING REPAIR ON FRAME AT MAIN CARGO COMPARTMENT STA 1721 L11L REMOVED AND INSTALLED WITH NEW REPAIR ANGLE PER SRM 53-00-07-2R REPAIR 2 FIG 201. EO 1-5100-7-5001 B6 PT1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 77,356 hrs · 15,508 cycles

AGING A/C-EXISTING REPAIR ON FRAME UPPER YOKE AREA AT MAIN CARGO COMPARTMENT STA 535 L19L. EXISTING REPAIR ON FRAME UPPER YOKE AREA AT MAIN CARGO COMPARTMENT STA 535 L19L EVALUATED AND FOUND DAMAGED. DAMAGED EXISTING REPAIR ON FRAME UPPER YOKE AREA AT MAIN CARGO COMPARTMENT STA 535 L19L REMOVED AND CARRIED OUT NEW REPAIR AS PER SRM 53-20-07-2R REPAIR 1 FIG 202. EO 1-5100-7-5001 B6 PT1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FIUSELAGE) · airframe 77,356 hrs · 15,508 cycles

AGING A/C-EXISTING REPAIR ON SEAT TRACK AT MAIN CARGO COMPARTMENT BETWEEN STA 745 TO STA 765, X=-8.5 EXISTING REPAIR ON SEAT TRACK AT MAIN CARGO COMPARTMENT BETWEEN STA 745 TO STA 785, X=-8.5 EVALUATED AND FOUND DAMAGED. DAMAGED SEAT TRACK AT MAIN CARGO COMPARTMENT BETWEEN STA 745 TO STA 785, X=8.5 REMOVED AND REPLACED WITH NEW SEAT TRACK SEGMENT, REPAIR AS PER SRM 53-00-52-2R REPAIR 1 FIG 201. EO 1-5100-7-5001 B6 PT 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 77,356 hrs · 15,508 cycles

AGING A/C-EXISTING REPAIR FOUND IN COCKPIT FLOOR AT RT OBSERVER SEAT BASE WEB PANEL STA 360, X=0. EXISTING REPAIR FOUND IN COCKPIT FLOOR AT RT OBSERVER SEAT BASE WEB PANEL EVALUATED AND FOUND DAMAGED. DAMAGED EXISTING REPAIR REMOVED AND REPLACED WITH NEW COCKPIT FLOOR STRUCTURE MEMBRANE WEB REPAIR AS PER SRM 53-10-51-2R REPAIR 1 FIG 201. EO 1-5100-7-5001 B6 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 77,356 hrs · 15,508 cycles

AGING A/C-EXISTING REPAIR ON FRAME LOWER YOKE AREA AT MAIN CARGO COMPARTMENT STA 535 L24L. EXISTING REPAIR ON FRAME LOWER YOKE AT MAIN CARGO COMPARTMENT STA 535 L24L EVALUATED AND FOUND DAMAGED. DAMAGED EXISTING REPAIR ON FRAME LOWER YOKE AT MAIN CARGO COMPARTMENT STA 535 L24L REMOVED AND CARRIED OUT NEW REPAIR AS PER SRM 53-20-07-2R REPAIR 1 FIG 201, EO 1-5100-7-5001 B6 PT1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,356 hrs · 15,508 cycles

RIGHT WING FIXED LEADING EDGE DOUBLER AT XOS 667 FOUND CRACKED. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REVISION K. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 77,356 hrs · 15,508 cycles

LEFT WING FIXED LEADING EDGE RIB DOUBLER FORMER AT XOS 584 FOUND CRACKED. THE FORMER WAS FABRICATED IAW DRAWING ARB2931, REVISION J. REMOVED AND REPLACED THE FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK SEAT TRACK AT STATION 5-6, RBL 47.5, FOUND THE CROWN DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK SEAT TRACK AT STATION 5-6, LBL 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 — GOUGED (BS 1288) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK SEAT TRACK AT BS 1288, RBL 8.5, FOUND CROWN DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,356 hrs · 15,508 cycles

RIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 584 FOUND CRACKED. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB2931, REVISION J. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,356 hrs · 15,508 cycles

RIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACKED. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REVISION K. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 695) · airframe 77,356 hrs · 15,508 cycles

FORWARD CARGO BAY ABOVE CEILING LOCATION AT BS 695, LBL 27.5 MAIN DECK SEAT TRACK CRACKED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,356 hrs · 15,508 cycles

LEFT WING-FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, REPAIR 15, FIG 203, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,356 hrs · 15,508 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, REPAIR 15, FIG 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK SEAT TRACK AT STATION 5-6, RBL 8.5, FOUND CROWN DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,356 hrs · 15,508 cycles

LEFT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 905 FOUND CRACKED. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REVISION K. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — GOUGED (BS 1288) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK SEAT TRACK AT BS 1288, LBL 47.5, FOUND CROWN DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — GOUGED (BS 1288) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK SEAT TRACK AT BS 1288, LBL 8.5, FOUND CROWN DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAWGMM 6-2-100.

Part: SEAT TRACK — GOUGED (BS 1288) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK SEAT TRACK AT BS 1288, RBL 47.5, FOUND CROWN DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101 ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 77,356 hrs · 15,508 cycles

RIGHT WING FIXED LEADING EDGE FORMER ASSY AT XOS 667 FOUND CRACKED. A NEW FORMER WAS FABRICATED IAW DRAWING ARB2924, REVISION B. REMOVED AND REPLACED THE FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,356 hrs · 15,508 cycles

RIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 906 FOUND CRACKED. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954 REVISION K. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 77,356 hrs · 15,508 cycles

DURING HFEC INSPECTION ON RT WING CORNER 5 OF FIXED L/E SKIN AT FWD I/B CORNER OF SLAT ACTUATOR ACCESS DOOR, CRACK FOUND APPROX 1/2 INCH LENGTH AS MARKED. CARRIED OUT REPAIR AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 17. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: BEAM — CRACKED (R3 DOOR) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK R3 DOOR INTERIOR NR 5 BEAM (FROM TOP) FOUND CRACKED. REMOVED AND REPLACED WITH NEW BEAM AS PER SRM 51-35-01-0G. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (BS 1250-1256) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX AT STA 1250.75-STA 1256.75, L-26L-L-27L. FOUND CRACKED. REPAIRED AS PER SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (BS 1250-1256) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK R3 DOOR FWD JAMB LOWER BOX AT STA 1250.75-STA 1256.75, L-26R-L-27R FOUND CRACKED. MAIN DECK R3 DOOR FWD JAMB LOWER BOX AT STA 1250.75-STA 1256.75, L-26R-L-27R REPAIRED AS PER SRM 53-40-15-2R FIG 201. REPAIR 3. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: BEAM — CRACKED (R3 DOOR) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK R3 DOOR INTERIOR NR 1 BEAM FROM TOP FOUND CRACKED. REMOVED AND REPLACED WITH NEW BEAM IAW SRM 51-35-01-0G. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (BS 1305-1315) · airframe 77,356 hrs · 15,508 cycles

MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25-1315.42, L26R-L27R FOUND CRACKED. REPAIRED AS PER SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LE SLAT) · airframe 77,356 hrs · 15,508 cycles

LEFT WING DROOPED LEADING EDGE UPPER SKIN AT XDLE 328 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-40-01-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — WORN (CARGO DOOR) · airframe 76,707 hrs · 15,310 cycles

MCD AFT HINGE SECTION HAS CORROSION. REMOVED AND REPLACED THE HINGE IAW AMM 52-34-04

Part: HINGE — WORN (CARGO DOOR) · airframe 76,707 hrs · 15,310 cycles

UPPER CARGO DOOR FUSELAGE HINGE WORN IAW AMM 52-34-00-6. REMOVED AND REPLACED THE DOOR HINGE IAW DWG ACA7223, AND MM 20-50-02.

Part: PROBE — FAULTY (FUEL SYSTEM) · airframe 735 hrs · 14,173 cycles

IN CRUISE, THE TNK 1 QTY LO & FWD PUMP LO, ALERTS APPEARED. PERFORMED PRECAUTIONARY CROSS FEEDING TO ENG NR 1 TO PREVENT FLAME OUT ON APPROACH. R & R FQUIS PROBE 19 IAW AMM 28-41-01-4. PERFORMED OPERATIONS CHECKED GOOD.

Part: FRAME — DENTED (BS 1701) · airframe 730 hrs · 14,030 cycles

CABIN MAIN DECK CARGO BAY, BS 1701, LONGERON 12R, FRAME EXISTING REPAIR FOUND DENTED. REPAIRED IAW SRM 53-00-07-2R FIGURE 201 REPAIR 2. CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 730 hrs · 14,030 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 770 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 730 hrs · 14,030 cycles

NOSE LANDING GEAR RT TRUNNION WEB CRACKED. REPAIRED IAW SRM 53-10-14-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: PANEL — CORRODED (LT WING) · airframe 730 hrs · 14,030 cycles

LEFT WING TE PANEL 541JB CUT OUT HAS SURFACE CORROSION. CAP REMOVED IAW SRM 51-31-01-0G & REPLACED WITH NEW CAP IAW SRM 51-33-01-0G, SRM 51-35-01-0G & DWG ARC0291 REVISION AY. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: PANEL — CORRODED (RT WING) · airframe 730 hrs · 14,030 cycles

RIGHT WING TE PANEL 641JB CUT OUT, HAS SURFACE CORROSION. CAP REMOVED IAW SRM 51-31-01-0G & REPLACED THE CAP IAW SRM 51-33-01-0G, SRM 51-35- 01-0G & DWG ARC0291 REVISION AY. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (BS 535) · airframe 730 hrs · 14,030 cycles

CABIN MAIN DECK CARGO BAY, BS 535, LONGERON 24R FRAME FOUND CHAFED. REPAIRED IAW SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 730 hrs · 14,030 cycles

LEFT WING LE EDGE CAVITY FORMER AT XOS 1025 FOUND CRACKED. FORMER REMOVED IAW SRM 51-31-01-0G & FABRICATED IAW DWG ARB 2920 REVISION BB. INSTALLED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 730 hrs · 14,030 cycles

NOSE LANDING GEAR LT TRUNNION WEB FOUND CRACKED. REPAIRED IAW SRM 53-10-14-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1681) · airframe 730 hrs · 14,030 cycles

CABIN MAIN DECK CARGO BAY BS 1681, LONGERON 12L, FRAME REPAIR FOUND DENTED. REPAIRED IAW SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (BS 535) · airframe 730 hrs · 14,030 cycles

MAIN DECK CARGO BAY, BS 535, LONGERON 19L. FRAME REPAIR FOUND CHAFED. CHAFE REMOVED IAW SRM 51-21-0-0G & FOUND WITHIN LIMITS IAW SRM 53-00-00-2R, REPAIR GENERAL FIGURE 202. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 730 hrs · 14,030 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 700 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (BS 535) · airframe 730 hrs · 14,030 cycles

CABIN MAIN DECK CARGO BAY, BS 535, LONGERON 24L. FRAME REPAIR FOUND CHAFED. CHAFE REMOVED IAW SRM 51-21-0-0G & FOUND WITHIN LIMIT IAW SRM 53-00-00-2R, REPAIR GENERAL FIGURE 202. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 730 hrs · 14,030 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 640 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,376 hrs · 12,520 cycles

FRAME FOUND CRACKED AT BS 5-53, LONGERON 12 RT. REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 68,376 hrs · 12,520 cycles

MAIN DECK, DURING OPEN HOLE INSPECTION ON SUPPORT FITTING NR 7, HOLE "B" FOUND CRACKED, APPROXIMATELY 0.030". SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,376 hrs · 12,520 cycles

MAIN DECK CARGO TRACK AT BS 1351, LBL 107.5 FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1331 TO 1371 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.

Part: CARGO TRACK — DAMAGED (ZONE 200) · airframe 68,376 hrs · 12,520 cycles

MAIN DECK CARGO TRACK AT BS 755, LBL 47.5 FOUND FLANGE CHIPPED OFF. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 725 TO 765 IAW SRM 53- 00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 67,825 hrs · 12,363 cycles

ON PREFLIGHT, RECEIVED A LEVEL ONE EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED EMERGENCY LIGHT TEST AND ALL TEST PASSED. NEXT MORNING RECEIVED THE MESSAGE AGAIN. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY. CHECKED GOOD IAW AMM CH 33-51-01-4.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,825 hrs · 12,363 cycles

PERFORMED EMERGENCY LIGHTS TEST AND ALL TEST PASSED. TESTED AGAIN AND REPRODUCED PROBLEM. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY.

Part: FLOORBEAM — CORRODED (BS 377) · airframe 64,870 hrs · 11,525 cycles

FLOORBEAM UPPER TEE BS 377 LBL 64 - RBL 10 GOUGED . REMOVED GOUGE, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 PG 104 DETAIL III. REPAIRED PER SRM 53-00-51, FIG 201, REPAIR 3 . MAJOR REPAIR.

Part: FIRE SUPPRESSION — FALSE ACTIVATION (NR 2) · airframe 64,703 hrs · 11,484 cycles

PRIOR TO PUSHBACK, FIRE SUPPRESSION SYS ACTIVATED IN POSITION 2L. PEFORMED MX PROCEDURES IAW MM 43.0, 43.1, 43.2, AND 43.3.

Part: INDICATION SYS — FALSE INDICATION (MLG) · airframe 64,243 hrs · 11,353 cycles

ON APPROACH, LOWERING LANDING GEAR, ALL FOUR GEAR INDICATED UNSAFE ON BOTH PRIMARY AND SECONDARY INDICATION SYS. HYD PRESSURE NORMAL. NO YAW DETECTED. NORMAL SOUND/VIBRATIONS ASSOCIATED WITH GEAR EXTENSION. EXECUTED MISSED APPROACH. SUBSEQUENT GEAR EXTENSION NORMAL. SUSPECT GEAR HANDLE NOT FULLY SEATED, CAUSING UNSAFE INDICATIONS. IAW FIM 32-30-05-01, PROXIMITY SWITCH UNIT TESTED OK. GEAR HANDLE SWITCH S1-431 VISUALLY EXAMINED AND APPEARS TO OPERATE NORMALLY. CHECKED RIG OF LANDING GEAR CONTROL VALVE INPUT. OK IAW AMM 32-31-00-5. PERFORMED GEAR SWINGS. CYCLED GEAR THREE TIMES, ALL OPS & INDICATIONS NORMAL. REF MM 32-31-00-5-0.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 63,225 hrs · 11,081 cycles

CENTER CARGO DOOR SKIN FOUND MISREPAIRED. REPAIRED AS PER EA 1-5230-155832. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 113.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 63,225 hrs · 11,081 cycles

CENTER CARGO DOOR MIDDLE EXTERNAL SKIN FOUND MISREPAIRED. REPAIRED AS PER EA 1-5230-155832. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 113.

Part: SKIN — MISREPAIRED (LT WING NR 6 SLA) · airframe 63,225 hrs · 11,081 cycles

LT WING NR6 SLAT OTBD L/E MISREPAIRED. NR 6 SLAT REMOVED AND REPLACED AS PER AMM 27-80-30-4 REV 70.1. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-30-5 REV 70.1. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 113.

Part: SKIN — CRACKED (RT WING) · airframe 63,225 hrs · 11,081 cycles

06 EA FASTENER HOLES FOUND CRACKED INDICATION DURING OPEN-HOLE HFEC INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STA XORS=713.6. REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.

Part: SKIN — CRACKED (LT WING) · airframe 63,225 hrs · 11,081 cycles

13 EA FASTENER HOLES FOUND CRACKED DURING OPEN-HOLE HFEC INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS= 683.4 AND STA XORS= 713.6. REPAIR CARRIED OUT AS PER DOUGLAS DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.

Part: LONGERON — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,225 hrs · 11,081 cycles

FOUND LONGERON 28 WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 113.

Part: LONGERON — CRACKED (ZONE 200) · airframe 63,225 hrs · 11,081 cycles

MAIN DECK COMPARTMENT LT SIDEWALL LONGERON 24, STA 5-93 FOUND CRACKED AT APPROX 2.5" LONG. REPAIR FABRICATED AS PER SRM 53-00-05 FIG.202 REV 47.REPAIR PARTS INSTALLED AS PER SRM 51-31-01 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 113.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 63,225 hrs · 11,081 cycles

MAIN DECK CARGO COMPT FLOOR SEAT TRACK AT BS 635, X= 47 FOUND REPAIR CRACKED. REMOVED AND REPAIRED AS PER SRM 53-00-52 FIG.201 REVISION 47 .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.

Part: FRAME — DENTED (BS 1721) · airframe 63,225 hrs · 11,081 cycles

CABIN - RT STA 1721, L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REPAIR 2 REVISION 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 63,225 hrs · 11,081 cycles

MAIN DECK CARGO COMPARTMENT BALLMAT AREA, FOUND SEAT TRACK AT STA 635 X=27 CRACKED. REPAIRED AS PER SRM 53-00-52 FIG 201 REVISION 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.

Part: CARGO TRACK — CHAFED (BS 1512) · airframe 63,225 hrs · 11,081 cycles

MAIN DECK CARGO TRACK CROWN AT BS 1512, X=27, FOUND CHAFED. REPAIRED AS PER SRM 53-00-52, FIGURE 201 REVISION 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 113.

Part: CARGO TRACK — DAMAGED (BS 1341) · airframe 63,225 hrs · 11,081 cycles

MAIN DECK CARGO TRACK CROWN AT BS 1341, X= 27, FOUND HOLE ELONGATED. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REVISION 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 113.

Part: CARGO TRACK — DAMAGED (MAIN DECK) · airframe 63,225 hrs · 11,081 cycles

MAIN DECK CARGO TRACK AT STA 6-0, X= -47, FOUND CROWN ELONGATED. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REVISION 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 113.

Part: SHUTOFF VALVE — MALFUNCTIONED (THRUST REVERSER) · airframe 63,057 hrs · 11,035 cycles

ON INITIAL T/O ROLL, LEVEL 1 ALERT " REV PRESS FAULT", ABORTED TO BLOCKS. FAULT EXTINGUISHED AFTER CLEAR OF RUNWAY. PERFORMED FIM 78-30-01, FIG 103, CONTINUITY CHECK BETWEEN J4 PIN 19 (ECU) TO PIN B PRESS, SW DPV AND PIN C (PRESS SW) TO GROUND - OK. HOWEVER R & R PRSOV IAW MM 78-31-07-4-1 AND DPV SOLENOID AND PRESS SW ASSY IAW MM 78-31-08-4-1. PERFORMED OPS CHECK ON NR 1 T/R IAW CHAPTER 7, OK. PERFORMED POWER ASSURANCE CHECK IAW JRH CHAP 7-10, TWICE, SATIS, NO FAULT MESSAGE. ACFT OK FOR SERVICE. OPEN/CLOSE DOOR IAW MM 71-10-00. PREMATURE REMOVAL/INSTALLATION.

Part: FRAME — CORRODED (BS 495) · corrosion level 3 · airframe 62,802 hrs · 10,968 cycles

PACK BAY NR 1, THE LONG FRAME JUST OUTBOARD OF PACK OUTLET DOOR, APPROX 16" FWD OF FRAME 495, THERE APPEARS TO BE CORROSION. REPAIRED DAMAGED AREA AREF. SRM 51-31-01 AND 53-00-05.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 2 NACELLE) · airframe 60,685 hrs · 10,453 cycles

FIRE DET 2 FAULT CYCLES ON/OFF ENROUTE ON STATUS PAGE. RECEIVED ALSO FIRE DET 2, FAIL ENROUTE NUMEROUS TIMES ON STATUS PAGE FOLLOWED BY FIRE WARNINGS FOR NR 2 ENGINE WHICH LASTED A FEW SECONDS ONLY. NO OTHER WARNINGS OCCURED BUT THE FIRE DET 2 FAULT REMAINS. REMOVED AND REPLACED NR 2 ENGINE GEAR BOX FIRE DETECTOR RAIL ASSY REF AMM 26-11-03-4-0. NR 2 ENG FIRE LOOP 'A' OPS CHECKS NORMAL.

Part: FRAME — DAMAGED (BS 1461) · airframe 58,486 hrs · 9,933 cycles

DURING ACCOMPLISHMENT OF EO1-2620-7-5005 B PT1 STEP B2 DWG VA-FSS-26-2101 ARGON TANK INSTALLATION AT STA1461 L-1L TO L-2L AND L-3L TO L-4L FRAME DOUBLER PN VA-FSS-6158 AND VA-FSS-6159 WILL HAVE SHORT EDGE MARGIN WITH EXISTING PILOT HOLES ON NEW HANGAR PN VA-FSS-6088-1 & VA-FSS-6087-1. COMPLIED WITH EA 1-2620-137937. COMPLIED WITH EA 1-2620-137937.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 57,368 hrs · 9,674 cycles

REF SNRM N000669 REWORK REQUIRED FINAL HOLE DIMENSION IS NOT ACCEPTABLE IAW EA 1-5750-76656 DATED 15 APR 2004 RT WING OTBD FLAP OTBD HINGE (WING MOUNTED ) ACTUATOR ATTACHMENT OTBD LUG REWORKED CARRIED OUT IAW EA 1-5750-76656. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 57,368 hrs · 9,674 cycles

REF. SNRM N00668 REWORK REQUIRED FINAL HOLE DIMENSION IS NOT ACCEPTABLE IAW EA 1-5750-76656 DATED 15 APR 2004 RT WING OTBD FLAP HINGE (WING MOUNTED ) ACTUATOR ATTACHMENT INBD LUG REWORKED CARRIED OUT IAW EA 1-5750-76656. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: BEAM — CHAFED (LT MLG DOOR) · airframe 57,368 hrs · 9,674 cycles

LT MLG STRUT DOOR AFT JAMB FOUND CHAFED. LT MLG STRUT DOOR AFT JAMB CHAFED REPAIR CARRIED OUT IAW EA 1-5710-135652, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: TEE FITTING — CORRODED (FLAP VANE) · corrosion level 2 · airframe 57,368 hrs · 9,674 cycles

RT WING OTBD FLAP, FLAP VANE FITTING NR3 FOUND CORROSION. TEE FITTING REWORKED AS PER EA 1-5750-135650. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 108.

Part: TEE FITTING — CORRODED (FLAP VANE) · corrosion level 2 · airframe 57,368 hrs · 9,674 cycles

RT WING OTBD FLAP, FLAP VANE TEE FITTING NR1 FOUND CORROSION. REWORKED AS PER EA 1-5750-135648. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 108.

Part: TEE FITTING — CORRODED (FLAP VANE) · corrosion level 2 · airframe 57,368 hrs · 9,674 cycles

RT WING OTBD FLAP, FLAP VANE "T' FITTING NR 2 FOUND CORROSION. FITTING REWORKED AS PER EA 1-5750-135649. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 108.

Part: TEE FITTING — CORRODED (FLAP VANE) · corrosion level 2 · airframe 57,368 hrs · 9,674 cycles

RT WING OTBD FLAP, FLAP VANE "T" FITTING FOUND CORROSION. REWORKED AS PER EA 1-5750-135651. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 108.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 57,368 hrs · 9,674 cycles

VERTICAL STABILIZER LT SURFACE FOUND CRACKED AT FWD OF REAR SPAR PLANE AT APPROX ZFR 540 AREA. REPAIR CARRIED OUT ON VERT STAB LT SURFACE SKIN AT FWD OF REAR SPAR PLANE AT APROX ZFR 540 IAW EA 1-5530-135661. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 108.

Part: DOUBLER — CRACKED (MLG WW) · airframe 57,368 hrs · 9,674 cycles

CTR LANDING GEAR WHEEL WELL FWD BULKHEAD RT DOUBLER FOUND CRACKED. DOUBLER REMOVED AND NEW DOUBLER INSTALLED IAW SRM 51-33-01 REV 41. NEW DOUBLER MACHINED IAW DWG EA 0526 REV NC. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 57,368 hrs · 9,674 cycles

LT WING OTBD FLAP OTBD HINGE (WING MOUNTED) ACTUATOR, ATTACHMENT INBD LUG, HOLE FOUND CORROSION. LT OTBD FLAP FWD OTBD HINGE ACTUATOR INBD LUG BORE REWORKED IAW EA NR 1-5750-135629. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-135629. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 57,368 hrs · 9,674 cycles

RT WING OTBD FLAP OTBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT OTBD LUG, HOLE FOUND CORROSION. RT OTBD FLAP HINGE ACTUATOR HOLE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 65. REPAIR FOUND TO BE ACCEPTED IAW EA 1-5750-76656. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REV. 65. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108. REWORK REQUIRED (JPF NR 12) - FINAL BORE DIMENSION IS NOT ACCEPTABLE IAW EA 1-5750-76656.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 57,368 hrs · 9,674 cycles

LT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT INBD BORE FOUND CORRODED. LT OTBD FLAP FWD INBD HINGE UPPER HINGE UPPER MOUNT INBD BORE REMOVED IAW EA 1-5750-135631. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-135631. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 57,368 hrs · 9,674 cycles

RT WING OTBD FLAP OTBD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBD LUG, HOLE FOUND CORROSION. RT OTBD FLAP FWD OTBD ACTUATOR INBD HOLE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV65. REPAIR FOUND TO BE ACCEPTED IAW EA 1-5750-76656 IAW EA 1-5750-76656. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REV 65. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108. REWORK REQUIRED (JPF ITEM NR12) FINAL BORE DIMENSION IS NOT ACCEPTABLE IAW EA 1-5750-76656.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 57,368 hrs · 9,674 cycles

RT WING OTBD FLAP INBD HINGE (WING MOUNTED) LWR ATTACHMENT FWD AND AFT SPOT FACE FOUND CORROSION. RT OTBD FLAP FWD INBD HINGE LWR MOUNT FWD AND AFT SPOTFACE REWORKED IAW EA 1-5750-135630. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: BUSHING — WORN (TE FLAP HINGE) · airframe 57,368 hrs · 9,674 cycles

RT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG INBD BORE BUSHING FOUND WORN. RT INBD FLAP AFT OTBD HINGE PIVOT LUG INBD BORE REWORKED IAW EA 1-5750-135628. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-135628. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 57,368 hrs · 9,674 cycles

LT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG OTBD HOLE FOUND CORROSION. LT INBD FLAP AFT OTBD HINGE PIVOT OTBD HOLE REWORKED IAW EA 1-5750-135627. BUSHING FABRIACTED AND INSTALLED IAW EA 1-5750-135627. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: BUSHING — WORN (ZONE 500) · airframe 57,368 hrs · 9,674 cycles

LT WING OTBD FLAP OTBD HINGE (WING MOUNTED) ACTUATOR OTBD BORE FOUND BUSHING WORN. LT WING OTBD FLAP FWD OTBD HINGE ACTUATOR OTBD BORE REWORKED IAW EA 1-5750-135629. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-135629. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 108.

Part: FRAME — CRACKED (ZONE 200) · airframe 57,368 hrs · 9,674 cycles

MAIN DECK CARGO COMPARTMENT RT SIDEWALL STRUCTURE FRAME CRACKED AT STA 1701, LONGERON 12 RT. UPPER CARGO COMPT. RH SIDEWALL STRUCTURE, CRACKED FRAME REPAIR AT STA 1701, L-12R, REPAIR AS PER SRM 53-00-07 FIG. 201 REPAIR 2 REV. 41. 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 FIG. 201 REPAIR 2 REV. 41. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.

Part: FRAME — DENTED (ZONE 200) · airframe 57,368 hrs · 9,674 cycles

MAIN DECK CARGO COMPARTMENT LT SIDEWALL STRUCTURE FRAME DENTED AT STA 1701, LONGERON 12 LT. MAIN DECK CARGO COMPT, LT SIDEWALL STRUCTURE DENTED FRAME AT STA. 1701 L12L, REPAIR CARRIED OUT AS PER SRM 53-00-07 FIG. 201 REPAIR 2 REV. 41. 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 FIG. 201 REPAIR 2 REV. 41. REPAIR CLASIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 57,368 hrs · 9,674 cycles

RT WING NR 1 SLAT LWR SKIN FOUND DENT. RT WING NR1 SLAT LWR SKIN DENT REPAIR SCHEME CARRIED OUT IAW SRM 57-40-01, REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108. RT WING NR1 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-20-5 REV 64 FOUND SATISFACTORY, TO CARRY OUT VISUAL INITIAL INSP AT NORMAL MX AND REPETITIVE AT NORMAL MX.

Part: SUPPORT FITTING — CORRODED (ZONE 600) · airframe 57,368 hrs · 9,674 cycles

RT WING OTBD FLAP VANE NR 2 TEE SUPPORT FITTING FOUND CORROSION. REPAIR CARRIED OUT IAW EA 1-5750-135646. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 108.

Part: TEE FITTING — CORRODED (RT WING TE FLAP) · airframe 57,368 hrs · 9,674 cycles

RT WING OTBD FLAP VANE NR 4 TEE SUPPORT FITTING FOUND CORRODED. REPAIR CARRIED OUT IAW EA 1-5750-135646. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 108.

Part: BEAM — CRACKED (ZONE 200) · airframe 57,368 hrs · 9,674 cycles

R3 DOOR FWD LOWEST BEAM FWD STOP FITTING CRACKED. R3 DOOR, CRACKED LOWEST BEAM REMOVED AND REPLACED IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 57,368 hrs · 9,674 cycles

CRACK INDICATION FOUND DURING HFEC INSP ON LT OF THE LWR VERTICAL STABILIZER FWD FLANGE OF UPPER REAR SPAR CAP. REPAIR CARRIED OUT ON LT LWR VERTICAL STABILIZER FWD OF UPPER REAR SPAR CAP IAW SRM 55-30-02. REPAIR 3 REV 41 AND EA 1-5530-135661. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 108.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 57,368 hrs · 9,674 cycles

RT WING INBD FLAP UPPER SURFACE AT L/E AREA FOUND DENTED AT APPROX X1FH 183.300 AS MARKED. RT WING INBD FLAP UPPER SURFACE AT L/E APPROX XIFH183.300, DENTED AREA MEASURED, DEPTH = 0.065", LENGTH = 1.5" FOUND WITHIN LIMIT IAW SRM 57-00-00 FIG. 206 REV. 41, HFEC INSP CARRIED OUT IAW DAC NDT SPM REV 13 PART 06-10-01.001 ON DENT AREA AND FOUND NO CRACK EVIDENT. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 53,750 hrs · 8,785 cycles

AFTER T/O R MAIN GEAR SHOWED UNSAFE RAN LIST RECYCLED GEAR NO HELP, INCREASE SPEED AFTER FLAP RETRACT AND AT 225 LIGHT WENT OUT.

Part: UNKNOWN — UNKNOWN (MLG) · airframe 53,750 hrs · 8,785 cycles

AFTER TAKEOFF R MAIN GEAR SHOWED UNSAFE RAN LIST RECYCLED GEAR NO HELP, INCREASE SPEED AFTER FLAP RETRACT AND AT 225 LIGHT WENT OUT.

Part: CYLINDER — MALFUNCTIONED (MLG) · airframe 53,557 hrs · 8,740 cycles

DURING GEAR RETRACTION- RED GEAR INDICATION REMAINED ILLUMINATED FOR RT MAIN GEAR APPROX 5 SECONDS LONGER THAN OTHER GEAR. REMOVED AND REPLACED RETRACT CYL IAW MM 32-33-20-4. REMOVED AND REPLACED RT MLG BUNGEE (UNLOCK) CYL REF MM 32-33-02-4. ACCOMPLISHED DOOR PROX SENSOR RTS IAW MM32-61-15- 5, STEP 3. PERFORMED MLG OPS CK AND TIMIMG CK IAW MM 32-31-00-5. OPS CK GOOD (RT MLG RETRACT TIME 10 SECONDS, MAX IAW MM IS 13 SECONDS). FOUND RT MAIN UP LOCK PROX SENSOR STOP INSTALLED INCORRECT. REPOSITION PROX STOP AND READJUSTED PROX GAP REF MM 32-61-15-5. PERFORMED GEAR SWING OPS CK NORMAL.

Part: CYLINDER — DAMAGED (MLG) · airframe 53,557 hrs · 8,740 cycles

DURING GEAR RETRACTION RED GEAR INDICATION REMAINED ILLUMINATED FOR RIGHT MAIN GEAR APPROXIMATELY FIVE SECONDS LONGER THAN THE OTHER GEAR. REMOVED AND REPLACED RETRACT CYLINDER IAW MM 32-33-20-4. REMOVED AND REPLACED RT MLG BUNGEE (UNLOCK) CYLINDER REF MM 32-33-02-4. ACCOMPLISHED DOOR PROX SENSOR RTS PER MM 32-61-15-5 STEP 3. PERFORMED MLG OPS CK AND TIMING CK PER MM 32-31-00-5. OPS CK GOOD (RT MLG RETRACT TIME 10 SECONDS MAX PER MM IS 13 SECONDS). FOUND RT MAIN UPLOCK PROX SENSOR STOP INSTALLED INCORRECT. REPOSITION PROX STOP AND READJUSTED PROX GAP REF M/M 32-61-15-5. PERFORMED GEAR SWING, OPS CHECK NORMAL, REF SEQ04 W/O 42407.

Part: UNLOCK CYLINDER — MALFUNCTIONED (MLG) · airframe 53,445 hrs · 8,717 cycles

GEAR RETRACT AFTER T/O, RT MAIN UNSAFE A ON PRIMARY AND SECONDARY. TWR STATED RT MAIN GEAR STILL DOWN, OTHERS UP. RAN CHK LIST, NO HELP AFTER GEAR RECYCLE. SETTING UP FOR RTN TO ORIGIN, HEARD SOUND OF GEAR DOOR CLOSING, UNSAFE LIGHT OUT, GEAR NORMAL ON CONFIG SD IN WORK. PERFORMED TEST MAIN GEAR AND GEARWELL DOOR OPERATION AS PER MM 32-31-00-5. PERFORMED THIS TEST 3 TIMES AND 3 TIMES THE RT MLG DID NOT RETRACT. R & R RT MAIN LANDING GEAR UNLOCK CYLINDER AS PER MM 32-33-02-4. PERFORMED TEST MAIN GEAR AND GEARWELL DOOR OPERATION AS PER MM 32-31-00-5. PERFORMED 6 TIMES LANDING GEAR RETRACTION AND EXTENTION AND 6 TIMES THIS TEST WAS OK.

Part: UNLOCK CYLINDER — FAILED (RT MLG) · airframe 53,445 hrs · 8,717 cycles

GEAR RETRACT AFTER TAKEOFF, RT MAIN UNSAFE ON PRIMARY AND SECONDARY. TOWER STATED RT MAIN GEAR STILL DOWN, OTHERS UP. RAN CHK LIST, NO HELP AFTER GEAR RECYCLE. SETTING UP FOR RTN TO ORIGINAL, HEARD SOUND OF GEAR DOOR CLOSING, UNSAFE LIGHT OUT, GEAR NORMAL ON CONFIG SD IN WORK. PERFORMED TEST MAIN GEAR AND GEARWELL DOOR OPERATION AS PER MM 32-31-00-5. PERFORMED THIS TEST 3 TIMES AND 3 TIMES THE RT MLG DID NOT RETRACT. REMOVED AND REPLACED RT MAIN LANDING GEAR UNLOCK CYLINDER AS PER MM 32-33-02-4. PERFORMED TEST MAIN GEAR AND GEARWELL DOOR OPERATION AS PER MM 32-31-00-5. PERFORMED 6 TIMES LANDING GEAR RETRACTION AND EXTENSION AND 6 TIMES THIS TEST WAS OK.

Part: PROXIMITY SWITCH — FAILED (RT MLG) · airframe 53,438 hrs · 8,716 cycles

PDIS: AFTER T/O DEL, RT MAIN GEAR UNSAFE INDICATION AFTER RETRACTION ON BOTH PRIMARY AND SECONDARY. CYCLE GEAR PER CK LIST, NO HELP. FELT VIBRATION AT 230KTS WHILE WORKING CK LIST AFTER APPROX 10 MIN VIBRATION STOPPED, INDICATION WENT TO SAFE, LIGHT OUT. CHECK ADJ OF RT MLG UPLATCH. RT MLG DOOR LINK AND BRACKET ASSY PER MM FOUND ON THE LIMITS. ADJUSTMENT MADE AS PRECAUTIONARY MEASURE ONE NOTCH O/B. WIRING, CONNECTORS CHECKED ALL FOUND NORMAL. PSEU FAIL TEST 31-71-04-00 ITEM 4. TEST FAIL. REMOVED AND REPLACED PSEU PER MM 31-71-01, ALL TEST PASS. RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAILED (RT MLG) · airframe 53,438 hrs · 8,716 cycles

AFTER T/O DEL, RT MAIN GEAR UNSAFE INDICATION AFTER RETRACTION ON BOTH PRIMARY AND SECONDARY. CYCLE GEAR PER CK LIST, NO HELP. FELT VIBRATION AT 230KTS WHILE WORKING CK LIST AFTER APPROX 10 MIN VIBRATION STOPPED, INDICATION WENT TO SAFE, LIGHT OUT. CHECK ADJ OF RT MLG UP LATCH. RIGHT MLG DOOR LINK & BRACKET ASSY PER MM FOUND ON THE LIMITS. ADJUSTMENT MADE AS PRECATIONARY MEASURE ONE NOTCH O/B WIRING, CONNECTORS CHECKED ALL FOUND NORMAL. PSEU FAIL TEST 31-71-04-00 ITEM 4. TEST FAIL. REMOVED AND REPLACED PSEU PER MM 31-71-01, ALL TEST PASS. RETURN TO SERVICE.

Part: TRUNNION — CORRODED (ZONE 700) · corrosion level 2 · airframe 53,160 hrs · 8,652 cycles

DURING CENTER LANDING GEAR REMOVAL FOR REPLACEMENT, THE RIGHT TRUNNION FITTING AFT ATTACHMENT BOLT HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5310-122488, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (BS 1371) · corrosion level 2 · airframe 53,160 hrs · 8,652 cycles

AFTER REMOVAL OF LEFT OVERWING FLOOR PANELS FOR WIRING INSPECTION ACCESS FOUND CENTER WING TANK LEFT UPPER TORQUE BOX SKIN APPROXIMATELY AT STA Y1371, XCW113 WITH EXFOLIATION CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA NR 15710-122479, TITLE: WINGS CENTER WING AFT UPPER SKIN CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — DAMAGED (ZONE 200) · airframe 53,160 hrs · 8,652 cycles

MAIN DECK CARGO DOOR SPOOL FITTING NR 4 MOUNTING BOLT HOLES "B" AND "C" FOUND WITH CRACK FREE CONDITION AFTER REAMED TO MAXIMUM ALLOWABLE DIAMETER 0.52". MAIN DECK CARGO DOOR SPOOL FITTING NR 4 MOUNTING BOLT HOLES CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 53,160 hrs · 8,652 cycles

MAIN DECK CARGO DOOR SPOOL FITTING NR 3 FOUND 3RD LAYER CRACK INDICATIONS AT ALL FITTING MOUNTING BOLT HOLES. MAIN DECK CARGO DOOR SPOOL FITTING NR 3. REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 53,160 hrs · 8,652 cycles

CENTER CARGO DOOR LOWER AFT CUTOUT FOUND CHAFED. CHAFED MARK AT CENTER CARGO DOOR LOWER AFT CUTOUT REPAIRED AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 53,160 hrs · 8,652 cycles

MAIN DECK SEAT TRACK AT STA 525, X = -8 FOUND HOLE ELONGATED. DAMAGED SEAT TRACK AT MAIN DECK STA 525 TO STA 555, X = -8 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 53,160 hrs · 8,652 cycles

MAIN DECK CARGO DOOR SPOOL FITTING NR 6 FOUND 3RD LAYER CRACK INDICATION AT FITTING MOUNTING BOLT HOLE C. MAIN DECK CARGO DOOR SPOOL FITTING NR 6 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 53,160 hrs · 8,652 cycles

MAIN DECK CARGO DOOR SPOOL FITTING NR 2 FOUND 3RD LAYER CRACK INDICATIONS AT FITTING MOUNTING BOLT HOLES A, C, AND D. MAIN DECK CARGO DOOR SPOOL FITTING NR 2 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 53,160 hrs · 8,652 cycles

MAIN DECK CARGO DOOR SPOOL FITTING NR 1 FOUND 3RD LAYER CRACK INDICATIONS AT ALL FITTING MOUNTING BOLT HOLES. MAIN DECK CARGO DOOR SPOOL FITTING NR 1 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (BS 1009) · airframe 53,160 hrs · 8,652 cycles

FORWARD CARGO DOOR CUTOUT LOWER AFT FOUND WITH CHAFFING. CHAFFED MARK ON FORWARD CARGO DOOR CUTOUT LOWER AFT SKIN EDGE BLENDED OUT AND FOUND WITHIN LIMIT AS PER SRM 53-50-00 FIGURE 17 VOLUME I. MATERIAL REMOVED AT EDGE 0.023 INCH. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 53,160 hrs · 8,652 cycles

MAIN DECK CARGO DOOR SPOOL FITTING NR 7 FOUND 3RD LAYER CRACK INDICATIONS AT ALL FITTING MOUNTING BOLT HOLES. MAIN DECK CARGO DOOR SPOOL FITTING NR 7 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 53,160 hrs · 8,652 cycles

AFTER REAMED TO MAXIMUM ALLOWABLE DIAMETER 0.52 INCH ON MAIN DECK CARGO DOOR SPOOL FITTING NR 2 MOUNTING BOLT HOLE "D" FOUND 2ND LAYER OF DOOR JAMB WITH CRACK INDICATION. REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5310-122486, TITLE: FUSELAGE MAIN CARGO DOOR LOWER JAMB BORE HOLE AT STA = 645 - REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 53,160 hrs · 8,652 cycles

MAIN DECK CARGO DOOR SPOOL FITTING NR 5 FOUND 3RD LAYER CRACK INDICATION AT FITTING MOUNTING BOLT HOLE D. MAIN DECK CARGO DOOR SPOOL FITTING NR 5 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 48,114 hrs · 7,528 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 48,114 hrs · 7,528 cycles

RIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD CENTER BOLT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 48,114 hrs · 7,528 cycles

RIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER CMM 57-52- 04. FLAP ADJUSTMENT REFER TO FEDEX EO 1-5720-7-5001 PT2, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 48,114 hrs · 7,528 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 48,114 hrs · 7,528 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 48,114 hrs · 7,528 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107762, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 48,114 hrs · 7,528 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD CENTER HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107762, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 48,114 hrs · 7,528 cycles

RIGHT WING TELESCOPIC DUCT CUTOUT FOUND CRACKED. CRACK AREA ON THE RIGHT WING TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I AND FEDEX EA NR 1-5710-107767, TITLE: WINGS, RIGHT WING ANTI-ICING TELESCOPIC DUCT DOOR CUTOUT REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,114 hrs · 7,528 cycles

CABIN RIGHT STA 1701 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CABIN RIGHT STA 1701 BETWEEN LONGERON 12 TO LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,114 hrs · 7,528 cycles

CABIN, LEFT STA 1641 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND DENT. CABIN, LEFT STA 1641 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,114 hrs · 7,528 cycles

CABIN LEFT STA 1681 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND DENT. CABIN LEFT STA 1681 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,114 hrs · 7,528 cycles

CABIN RIGHT STA 1681 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CABIN, RIGHT STA 1681 BETWEEN LONGERON 12 TO LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLE WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 48,114 hrs · 7,528 cycles

CABIN LEFT STA 1661 BETWEEN LONGERON 12 AND LONGERON 14 FRAME FOUND CRACKED. CABIN LEFT STA 1661 BETWEEN LONGERON 12 AND LONGERON 14 FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 500) · airframe 48,114 hrs · 7,528 cycles

LEFT WING TELESCOPIC DUCT OUTBOARD CUTOUT FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 42 VOLUME I AND FEDEX E.A. #1-5710-107766, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 48,114 hrs · 7,528 cycles

CABIN STA 755 X = -8.5 SEAT TRACK LOWER FLANGE FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,114 hrs · 7,528 cycles

DURING HFEC INSPECTION AT THE RIGHT WING TANK, CRACK WAS FOUND AT THE END OF STRINGER 14 (XORS 521) WITH APPROX 11" IN LENGTH. TRIMMED OUT AND REPAIRED WITH SPLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,114 hrs · 7,528 cycles

DURING HFEC INSPECTION ON THE LEFT WING TANK, CRACK WAS FOUND AT THE END OF STRINGER 14 (XORS 521) WITH APPROX 13" IN LENGTH. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,114 hrs · 7,528 cycles

DURING HFEC INSPECTION ON THE LEFT WING TANK, CRACK WAS FOUND AT THE END OF STRINGER 13 (XORS 577) WITH APPROX 8" IN LENGTH. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEARING — WORN (MLG PUSH ROD) · airframe 43,586 hrs · 6,518 cycles

UPON GEAR EXTENSION DURING APPROACH ALL FOUR GEARS INDICATED UNSAFE AND NO EXTENSION. GEAR HANDLE RECYCLED UP AND DOWN AGAIN WITH GEAR EXTENSION BEING ABOUT ONE FOURTH THE SPEED OF NORMAL GEAR EXTENSION. SEQUENCE OF DOWN AND LOCKED INDICATIONS WERE NOSE, CENTER, LEFT, THEN RIGHT. REMOVED AND REPLACED RT MAIN GEAR DOOR POSITION FOLLOW UP PUSH ROD BEARING PER REF TO MD-11 MM CHAPTER 25 SMP. CYCLED GEAR SEVERAL TIMES PER REF TO MD-11 MM CHAPTER 32-31-00-5. ALL INDICATIONS NORMAL. REFERENCE PREVIOUS SHORT SIGN OCT 5 2005 AT 0012Z. FOR REMOVAL AND REPLACEMENT OF LT AND RT MAIN LANDING GEAR FOLLOW LINKS.

Part: SKIN — DELAMINATED (TE FLAPS) · airframe 42,941 hrs · 6,370 cycles

RIGHT WING, INBOARD FLAP, FLAP VANE INBOARD LOWER SKIN FOUND DELAMINATED. DELAMINATION MEASURES 40.00 INCHES IN LENGTH BY 17.00 INCHES IN WIDTH. REPAIRED IN ACCORDANCE WITH FEDEX EA 1-5750-87555.

Part: FRAME — CHAFED (THRUST REVERSER) · airframe 42,941 hrs · 6,370 cycles

NR 1 ENGINE, RIGHT HAND THRUST REVERSER COWL T-FRAME AT LOWER 2 BUMPER AREA FOUND WITH CHAFING MARK. CARRIED OUT REPAIR PER FEDEX EA 1-7830-87557. ENGINE THRUST REVERSER - NR 1 ENGINE, RIGHT HAND TEE FRAME WEAR AT 4 AND 5 O' CLOCK POSITIONS - REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STATIC PORT — FAILED (FUSELAGE) · airframe 42,941 hrs · 6,370 cycles

FUSELAGE INTERIOR, LT PRIMARY STATIC PORT FAILED WAVINESS TEST. REMOVED AND REPLACED AS PER AMM 34-11-03-4.

Part: NOSE COWL — DAMAGED (NR 3 ENGINE) · airframe 42,941 hrs · 6,370 cycles

NR 3 ENGINE, NOSE INLET COWL INNER BARREL FROM 6 TO 9 O' CLOCK POSITION FOUND WITH CORROSION. NR 3 ENGINE, NOSE INLET COWL REMOVED AND REPLACED PER AMM 71-11- 01-4.

Part: NOSE COWL — DAMAGED (NR 1 ENGINE) · airframe 42,941 hrs · 6,370 cycles

NR 1 ENGINE, NOSE INLET COWL INNER BARREL FROM 3, 9 AND 12 O' CLOCK POSITION FOUND DOUBLER WITH SHEARED RIVETS. NR 1 ENGINE, NOSE INLET COWL REMOVED AND REPLACED AS PER AMM 71- 11-01-4.

Part: FRAME — DENTED (ZONE 200) · airframe 42,941 hrs · 6,370 cycles

RT MAIN DECK AFT FUSELAGE FRAME AT STA 1641, BETWEEN LONGERONS L12 AND L13 FOUND WITH DENT. REPAIRED PER SRM 53-30-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,941 hrs · 6,370 cycles

MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= - 8.5 FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFID AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,941 hrs · 6,370 cycles

MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= -27 FOUND WITH CRACKED APPROXIMATELY 3 INCHES LONG. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSLEAGE) · airframe 42,941 hrs · 6,370 cycles

MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= 47 FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: SEAT TRACK — ELONGATED (ZONE 200) · airframe 42,941 hrs · 6,370 cycles

MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK CROWN AT STA 645, X= -47 FOUND ELONGATED.

Part: SKIN — CRACKED (ZONE 500) · airframe 42,941 hrs · 6,370 cycles

RT WING, LEADING EDGE SKIN AT STA XORS 797 FOUND WITH 17 IN CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 VOLUME I, FIGURE 37.

Part: RIB — CRACKED (RT WING) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING - NR 16 SLAT TRACK INBOARD RIB SUSPECTED CRACK AS MARKED. RIGHT WING - NR 16 SLAT TRACK INBOARD RIB REMOVED AND REPLACED AS PER SRM 51-31-01, VOL 2.

Part: HINGE — CORRODED (RT WING) · airframe 38,490 hrs · 5,369 cycles

RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, BARREL NUT BOLT BORE SPOTFACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (RT WING) · airframe 38,490 hrs · 5,369 cycles

RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658.

Part: SKIN — DENTED (L/E SLAT) · airframe 38,490 hrs · 5,369 cycles

LT WING DENT MARK FOUND ON OUTBOARD NOSE SURFACE AREA OF SLAT NR 6. DENTED AREA AT LH WING OUTBOARD NOSE SURFACE OF SLAT NR 6 TRIMMED AS PER SRM 57-00-01, FIG.7, VOL. I. REPAIR PARTS FABRICATED & INSTALLED AS PER SRM 57-00-01, FIG.7, VOL.I & SRM 51-35-01, VOL.II.

Part: HINGE — CORRODED (RT WING) · airframe 38,490 hrs · 5,369 cycles

RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658.

Part: FITTING — CORRODED (T/E FLAP VANE) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING OUTBOARD FLAP VANE T-FITTING (SECOND FROM INBOARD SIDE) FOUND WITH HOLES CORRODED. TEE FITTING (SECOND FROM INBOARD SIDE) REPAIRED AS PER EA 1-5750-76008.

Part: HINGE — CORRODED (RT WING) · airframe 38,490 hrs · 5,369 cycles

RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, LOWER MOUNT SPOTFACE FOUND CORRODED. LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502, SHT.4, ZONE 40.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, BARREL NUT BOLT HOLE AREA SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD UPPER MOUNT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WINGS OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD UPPER MOUNT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 AND REPAIRED AS PER EA 1-5750-76657 PART 1. INBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (FLAP SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

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

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, LOWER MOUNT SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DRAWING ARC0502, SHT.4, ZONE 40.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, BARREL NUT BOLT BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643, TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, BARREL NUT BORE SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD LOWER MOUNT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.

Part: LONGERON — CRACKED (ZONE 100) · airframe 38,490 hrs · 5,369 cycles

CENTER CARGO COMPARTMENT CRACKED ON LONGERON SPLICE 51L, STA 5- 123. CRACKED LONGERON SPLICE REMOVED AND REPLACED PER SRM 51-33- 01 VOL II

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1, LT OUTBOARD FLAP INBD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BUSHINGS. CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CROSSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654, LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654 LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RT WING AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIRED.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1, LT OUTBOARD FLAP INBD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BUSHINGS. CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CROSSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654 . LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CROSSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76003.

Part: STOP FITTING — CRACKED (ZONE 600) · airframe 38,490 hrs · 5,369 cycles

RIGHT WING STOP FITTING ASSEMBLY ON OUTBOARD FLAP CRACKED AT BARREL NUT BORE AREA. CRACKED STOP FITTING ASSY ON OUTBOARD FLAP AT RT WING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.

Part: STOP FITTING — CRACKED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LT WING STOP FITTING ASSEMBLY ON OUTBOARD FLAP CRACKED AT BARREL NUT BORE AREA. CRACKED STOP FITTING ASSY ON OUTBOARD FLAP AT LT WING REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II.

Part: RIB — CRACKED (ZONE 500) · airframe 38,490 hrs · 5,369 cycles

LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 16 FOUND CRACKED. LT WING LEADING EDGE RIB AT SLAT TRACK NR 16 REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II.