N529FE

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING FROM INBOARD CCENTRIC HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING FROM INBOARD ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A. # 1-5750- T0361084 PART 1 STEP 1A. TITLE: WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- ASSY- TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50- 32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZED OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 04 AND E.A. # 1-5750-T0361215 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP- INBD HINGE BRACKET ASSY - CORROSION REPAIR. REPAIR REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

RIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZED OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 04 AND E.A. # 1-5750-T0319469 A PART 2 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT URFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP- INBD HINGE BRACKET ASSY - CORROSION REPAIR. REPAIR REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 61,062 hrs · 14,249 cycles

04 EACH FASTENER HOLES #8, #14, #29 AND #30 FOUND CRACK INDICATION DURING OPEN- HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. LEFT HAND WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. 04 EACH FASTENER HOLES #8, #14, #29 AND #30 REPAIR CARRIED OUT AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. INITIAL INSPECTION TO BE CARRY OUT AT 2000 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2000 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT AND ULTRASONIC INSPECTION PER SRM 57-20-02-2R FIGURE 202 REPAIR 5 TABLE 201.

Part: SKIN — CRACKED (RT WING) · airframe 61,062 hrs · 14,249 cycles

07 EACH FASTENER HOLES #8, #9, #10, #11, #12, #29 AND #32 FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. RIGHT HAND WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. 07 EACH FASTENER HOLES #8, #9, #10, #11, #12, #29 AND #32 REPAIR CARRIED OUT AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL INSPECTION TO BE CARRY OUT AT 2000 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2000 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT CURRENT AND ULTRASONIC INSPECTION PER SRM 57-20-02-2R FIGURE 202 REPAIR 5 TABLE 201.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 61,062 hrs · 14,249 cycles

MAIN DECK CARGO COMPARTMENT - FLOOR PANEL #272EF FROM STATION 1361 TO 1481 FOUND DELAMINATED. DELAMINATED FLOOR PANEL #272EF AT CABIN STATION 1361 TO 1481 REMOVED AS PER AMM 53- 21-04. FLOOR PANEL #272EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #272EF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 61,062 hrs · 14,249 cycles

RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS-893 FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS-893 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 61,062 hrs · 14,249 cycles

MAIN DECK CARGO COMPARTMENT - FLOOR PANEL #271EF FROM STATION 1361 TO 1481 FOUND DELAMINATED. DELAMINATED FLOOR PANEL #271EF AT CABIN STATION 1361 TO 1481 REMOVED AS PER AMM 53- 21-04. FLOOR PANEL #271EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #271EF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 61,062 hrs · 14,249 cycles

MAIN DECK CARGO - CENTER FLOOR PANEL #273JF STATION 1501 TO 5-53 FOUND DELAMINATED. DELAMINATED FLOOR PANEL #273JF AT CABIN STATION 1501 TO STATION 5-53 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #273JF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #273JF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 61,062 hrs · 14,249 cycles

MAIN DECK CARGO COMPARTMENT - FLOOR PANEL #272JF FROM STATION 1481 TO 5-53 FOUND FOUND DELAMINATED. DELAMINATED FLOOR PANEL #272JF AT CABIN STATION 1481 TO STATION 5-53 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #272JF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #272JF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 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-T0319447 A PART 2 STEP 1A AND STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00325 ATTACHED E.A. # 1-5750-T0319447 A PART 2 FOR DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 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 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. # 1-5750-T0319447 A PART 2 STEP 1A AND STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM N00325 ATTACHED E.A. # 1-5750-T0319447 A PART 2 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED 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-T0319447 A PART 2 STEP 1B AND STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD MOUNT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD FORWARD MOUNT LUG HOLE BORE (#6 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-T0319466 A PART 3 STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00475 ATTACHED E.A. # 1-5750-T0319466 A PART 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE 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 CMM 57-44-09 AND E.A. # 1-5750-T0319446 A PART 2 STEP 1A AND STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00326 ATTACHED E.A. # 1-5750-T0319446 A PART 2 FOR DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 09 AND E.A. # 1-5750-T0319446 A PART 2 STEP 1B AND STEP 1, REPAIR REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD FORWARD MOUNT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD FORWARD MOUNT LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER PER MD-11 CMM 57-44-08 AND E.A. # 1-5750-T0319466 A PART 3 STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00475 ATTACHED E.A. # 1-5750-T0319466 A PART 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 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-T0319466 A PART 3 STEP 1, TITLE: WINGS- FLIGHT SURFACES- SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP- INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM CMM 57-44-09 AND E.A. # 1-5750-T0319446 A PART 2 STEP 1C AND STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00326 ATTACHED E.A. # 1-5750-T0319446 A PART 2 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT INBOARD HOLE BORE 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- 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # 1-5750-T0319466 A PART 3 STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP- INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00475 TTACHED E.A. # 1-5750-T0319466 A PART 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM CMM 57-44-08 AND E.A. # 1-5750-T0319466 A PART 3 STEP 1, REPAIR REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00475 ATTACHED E.A. # 1-5750-T0319466 A PART 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # 1-5750-T0319466 A PART 3 STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP- INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00475 A ATTACHED E.A. # 1-5750-T0319466 A PART 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 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 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-T0319466 A PART 3 STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00475 ATTACHED E.A. # 1-5750-T0319466 A PART 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-09 AND FOUND BARREL NUT WALL THICKNESS THICKNESS WITHIN LIMIT BASED THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAXIMUM REWORK LIMITS FOR BARREL NUT HOLE. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. # 1-5750-T0319446 A PART 2 STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP- OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00326 ATTACHED E.A. # 1-5750-T0319446 A PART 2 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM CMM 57-44-09 AND E.A. # 1-5750-T0319446 A PART 2 STEP 1C AND STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00326 ATTACHED E.A. # 1-5750-T0319446 A PART 2 FOR DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 61,062 hrs · 14,249 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 BARREL NUT WALL THICKNESS THICKNESS WITHIN LIMIT BASED THE DIFFERENCE BETWEEN DRAWINGS LIMIT AND CMM MAXIMUM REWORK LIMITS FOR BARREL NUT HOLE. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. # 1-5750-T0319466 A PART 3 STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00475 ATTACHED E.A. # 1-5750-T0319466 A PART 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 cycles

LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED 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- 1-5750-T0319466 A PART 3 STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- WING- OUTBD FLAP- INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00475 ATTACHED E.A. # 1-5750-T0319466 A PART 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 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 CMM 57-44-09 AND E.A. # 1-5750-T0319446 A PART 2 STEP 1A AND STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00326 ATTACHED E.A. # 1-5750-T0319446 A PART 2 FOR DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,062 hrs · 14,249 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 CMM 57-44-08 AND E.A. # 1-5750-T0319466 A PART 3 STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP- INBD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00475 ATTACHED E.A. # 1-5750-T0319466 A PART 3 FOR WORK DETAILS.

Part: COMPUTER — FAILED (BRAKE SYSTEM) · airframe 58,287 hrs · 13,556 cycles

AT CRUISE FL 370 ABOUT 60 MIN INTO FLIGHT, HAD A MOMENTARY "TIRE FAIL" AND ALL TIRES WERE MISSING FROM DISPLAY, THEN THE INDICATIONS RETURNED TO NORMAL. AT FL 250 DESCENDING TO 10,000, WE GOT THE LEVEL 2 "TIRE FAIL" INDICATION WITH THE CAWS ALERT "TIRE FAILURE". WE RAN THE QRH GUIDANCE, AND WHEN WE EXTENDED THE GEAR, THE INDICATIONS DID NOT RETURN TO NORMAL SO WE DECLARED AN EMERGENCY WITH TOWER. LANDING WAS GOOD. 1.14G, 50 FLAPS, FELT NORMAL ON ROLLOUT. FIRE CHIEF INSPECTED TIRES AND NOTIFIED US EVERTHING WAS NORMAL SO WE BLOCKED IN. REMOVED AND REPLACED THE (TIRE PRESSURE/BRAKE TEMPERATURE COMPUTER) IAW PER AMM 32-46-02. RTS TEST PASS. A/C OK FOR SERVICE.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 56,838 hrs · 13,096 cycles

EMPENNAGE - LEFT HAND IN BOARD ELEVATOR TOP SURFACE AT STATION XE=160.5 FOUND DELAM. EMPENNAGE - LEFT HAND IN BOARD ELEVATOR TOP SURFACE REPAIRED AND SMOOTHEN AS PER SRM 55-20-80-2R, REPAIR 2, PARAGRAPH 2A, FIGURE 201 AND THE E.A #1-5520-T0348878 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — GOUGED (BS 1920) · airframe 56,838 hrs · 13,096 cycles

GOUGES ON AFT FUSELAGE UNDER BULK CARGO DOOR SKIN AT BS 1920, BETWEEN LONGERON 49 LEFT AND LONGERON 49 RIGHT, REPAIRED IAW EA 1-5330-T0347135 P2.

Part: SEAT TRACK — DAMAGED (BS 490) · airframe 56,838 hrs · 13,096 cycles

MAIN DECK FLOOR CURVE SEAT TRACK AT STATION 490 X = - 75.25 FOUND CROWN DAMAGED . MAIN DECK FLOOR AT CURE SEAT TRACK STATION 490 X = - 75.25 , 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 458 TO STATION 525 X = - 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 6 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (RT WING) · airframe 56,838 hrs · 13,096 cycles

RIGHT HAND LEADING EDGE CAVITY RIB DOUBLER AT XOS 667 FOUND CRACKED . RIGHT HAND LEADING EDGE CAVITY, CRACKED RIB DOUBLER AT XOS 667, REMOVED AND REPLACED WITH FABRICATED RIB DOUBLER AS PER SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DRAWING ARB 3954 REVISION K. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — WORN (BS 895) · airframe 56,838 hrs · 13,096 cycles

EXISTING REPAIR AT FUSELAGE SKIN FORWARD CARGO FORWARD JAMB CUTOUT STA 895.700 BETWEEN LONGERON 39 RIGHT TO LONGERON 42 RIGHT. EXISTING REPAIR AT FUSELAGE SKIN FWD CARGO FWD JAMB CUTOUT STA 895.700 BETWEEN L39R TO L42R EVALUATED AND FOUND EXISTING REPAIR DOUBLER WORN. SKIN REPAIRED AS PER EA 1-5330-T0303487B PT5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (BS 1305-1315) · airframe 56,838 hrs · 13,096 cycles

MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 TO STATION 1315.42 LONGERON 26 RIGHT TO LONGERON 27 RIGHT FOUND CRACKED . REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1305-1315) · airframe 56,838 hrs · 13,096 cycles

MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT BS 1305.25 TO STATION 1315.42 LONGERON 26 TO 27 LEFT FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R FIGURE 201 REPAIR 3 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (LT WING) · airframe 56,838 hrs · 13,096 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 763-XOS 768 FOUND CRACKED LEFT HAND WING LEADING EDGE CAVITY, CRACKED BEADED DOUBLER AT XOS 763-XOS 768, REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 56,838 hrs · 13,096 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 584-XOS 589 FOUND CRACKED LEFT HAND WING LEADING EDGE CAVITY, CRACKED BEADED DOUBLER AT XOS 584-XOS 589, REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1441) · corrosion level 2 · airframe 56,838 hrs · 13,096 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1441 X = 8.5 FOUND CORROSION . MAIN DECK FLOOR SEAT TRACK AT STATION 1441 X = 8.5 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONALSEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION1431 TO 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: SEAT TRACK — DAMAGED (BS 1282) · airframe 56,838 hrs · 13,096 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 47.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 47.5 , 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 SECTIONA SEAT TRACK REPLACEMENT FROM STATION 1269 TO EXISTING SPLICE STATION 1331 X = 47.5 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 56,838 hrs · 13,096 cycles

RIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 728 - XOS 734 FOUND CRACKED. RIGHT HAND WING LEADING EDGE CAVITY, CRACKED BEADED DOUBLER AT XOS 728 - XOS 734, REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 56,838 hrs · 13,096 cycles

DURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE RIGHT HAND FORWARD FLANGE OF LOWER VERTICAL STABILIZER REAR SPAR CAP AT STATION Y = 2164 , FOUND 01EA CRACK WITH LENGTH APPROXIMATELY 1.5" BETWEEN THE FIRST AND THIRD FASTENER FROM BELOW. VERTICAL STABILIZER REAR SPAR CAP RIGHT HAND FORWARD FLANGE AT STATION Y = 2164 CRACKED APPROXIMATELY 1.5" BETWEEN THE FIRST AND THIRD FASTENER FROM BELOW TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAIR 5, REPAIR CARRIED OUT AS PER SRM 55- 30-02-2R FIGURE 204 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT EVERY 5,400 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2,700 FLIGHT CYCLES AS PER SRM 55-30-02-2R TABLE 203 REPAIR 5. METHOD OF INSPECTION BY ULTRASONIC AND HIGH FREQUENCY EDDY CURRENT PER SN10550000.

Part: DOUBLER — CRACKED (LT WING) · airframe 56,838 hrs · 13,096 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 626 - XOS 629 FOUND CRACKED LEFT HAND WING LEADING EDGE CAVITY, CRACKED BEADED DOUBLER AT XOS 626 - XOS 629, REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1282) · airframe 56,838 hrs · 13,096 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 47.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 47.5 , 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 1269 TO EXISTING SPLICE STATION 1331 X = - 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (BS 1282) · airframe 56,838 hrs · 13,096 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 8.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR AT SEAT TRACK STATION 1282 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 1311 TO EXISTING SPLICE STATION 1229 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 (RT WING) · airframe 56,838 hrs · 13,096 cycles

RIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 763 - XOS 767 FOUND CRACKED RIGHT HAND WING LEADING EDGE CAVITY, CRACKED BEADED DOUBLER AT XOS 763 - XOS 767, REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 56,838 hrs · 13,096 cycles

RIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 636 - XOS 643 FOUND CRACKED. RIGHT HAND WING LEADING EDGE CAVITY, CRACKED BEADED DOUBLER AT XOS 636 - XOS 643, REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1282) · airframe 56,838 hrs · 13,096 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 8.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1282 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 1269 TO STATION 1331 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 56,838 hrs · 13,096 cycles

LEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 542-XOS 547 FOUND CRACKED LEFT HAND WING LEADING EDGE CAVITY, CRACKED BEADED DOUBLER AT XOS 542-XOS 547, REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,838 hrs · 13,096 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 5-11 X = - 47.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR AT SEAT TRACK STATION 5-11 X = - 47.5 , 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 AT EXISTING SPLICES STATION 5-0 TO STATION 5-63 X = - 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: TRUNNION — CRACKED (BS 595) · airframe 56,838 hrs · 13,096 cycles

NOSE LANDING GEAR WHEEL WELL LEFT TRUNNION FITTING SUSPECTED CRACKED AT BS 595, REPAIRED IAW SRM 53-10-14-2R, FIGURE 202, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 56,317 hrs · 12,954 cycles

MDIS 529 33-50 6878 17MAY19 MEM FACT U DURING EMERGENCY LIGHT TEST, RECIEVED EMER BATT LOW (1). R/I 17MAY19 17:32 MEM U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 60-4411-5 POS: ONL SRL: 0163 TAG NBR: 4G9021 ON MPN: 60-4411-5 CPN: 3300197 SRL: 0636 TAG NBR: 0898F2 FACT 17MAY19 17:32 MEM U REMOVED AND REPLACED NR 1 EMERGENCY LIGHT POWER SUPPLY IAW MM 33-51-01-4. EMERGENCY LIGHTS TEST PASSED. A/C OK FOR SERVICE.

Part: STRUT — CRACKED (LT MLG) · airframe 56,019 hrs · 12,846 cycles

QC DETECTED A CRACK WHILE INSPECTING THE LEFT MAIN GEAR AND THE WORK CARD IS CALLING FOR A GEAR CHANGE. REPLACED LH MLG STRUT

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 55,509 hrs · 12,692 cycles

L1 DOOR EVACUATION SLIDE/RAFT FELL OUT. INSTALLED L1 DOOR EVAC SLIDE/RAFT REF AMM 25-61-15-4. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 55,267 hrs · 12,610 cycles

NOSEWHEEL STEERING ONLY WAS APPROX. 50% EFFECTIVE. TILLER WOULD GO TO FULL THROW LEFT OR RIGHT BUT NOSEWHEEL WOULD ONLY MAKE A GRADUAL TURN - MUCH TO LARGE OF A RADIUS - WITHOUT STEPPING ON INBOARD BRAKE. NOSE STRUT IS EXTENDED MORE THAN NORMAL ACCORDING TO GROUND CREW. OUR ZFCG IS 30.1, TOCG 32.3 - NEAR AFT LIMITS. FOUND NLG STRUT EXTENDED TO 10.5". CHECKED NLG STRUT PRESSURE IAW AMM 32-21-01-3. NO DEFECTS NOTED. MOVED WEIGHT(LOAD) TO MORE FWD CG. NLG STRUT EXTENSION IS NOW 5.25". OK FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (NR 2 ENGINE) · airframe 54,559 hrs · 12,373 cycles

LEVEL 3 ALERT FOR THE NR 2 ENGINE ANTI-ICE DUCT FAILURE, COMPLIED WITH QRH. REMOVED AND REPLACED THE NR 2 ENGINE ANTI- ICE VALVE IAW AMM 30-22-01, AND THE PRESSURE SWITCH IAW AMM 30-22-02. THE NR 2 ENGINE ANTI-ICE SYSTEM OPERATED NORMAL AND NO LEAKS FOUND IN DUCTING, OR VALVE ASSY.

Part: DUCT — LEAKING (ANTI-ICE) · airframe 54,304 hrs · 12,287 cycles

RECIEVED A NR 2 ENGINE A-DUCT WARNING, DURING CLIMBOUT, FOLLOWED SHORTLY BY A LEVEL 1 NR 2 ENGINE ANT-ICE OFF ALERT. LANDED AT NEAREST SUITABLE AIRPORT DUE TO WARNINGS. NO ENGINE EXCEEDANCES DURING THE NR 2 ENGINE WINDMILLING AND SHUTDOWN. INSTALLED A SERVICEABLE DUCT ASSEMBLY.

Part: TIRE — BLOWN (MLG) · airframe 54,170 hrs · 12,242 cycles

CLIMBING OUT OF CDG, TIRE PRESS LO ALERT CONFIG PAGE SHOWED NR 5 TIRE PRESS DECREASING ALSO NR 6 WAS AMBER BUT NOT DECREASING. LATER TIRE FAIL ALERT ON NR 5 WHEN PRESS WENT BELOW 50 PSI. AFTER NR 5 PRESS WENT TO 0 PSI , NR 5 TIRE DISAPPEARED FROM DISPLAY. NR 6 RETURNED TO NORMAL. IAW MM 05-51-02-6 NO SPECIAL INSPECTION REQUIRED, FOR ONLY 1 BLOWN TIRE. REMOVED AND REPLACED NR 5 TIRE AND WHEEL ASSY IAW MM 32-41-01-4.

Part: CABLE — FROZEN (RUDDER) · airframe 53,088 hrs · 11,921 cycles

ENROUTE, RUDDER PEDALS AND TRIM WHEEL BECAME FROZEN/LOCKED. UNUSABLE UNTIL TAT REACHED 10 DEGREES. OPENED PANEL 364AR AND REMOVED ABOUT 1 INCH OF POOLED WATER INSIDE COMPARTMENT. CLEANED AND LUBRICATED BOTH TRIM AND RUDDER CABLES INSIDE COMPARTMENT IAW AMM 20-20-06-2 AND TSI 27-20/4645.

Part: CONTROL VALVE — FAILED (TE FLAPS) · airframe 52,190 hrs · 11,660 cycles

AFTER TAKE OFF, RECEIVED A LEVEL 2 FLAP DISAGREE. MATCHED FLAPS BACK TO 10'. RAN QRH INBOARD FLAPS WOULD NOT MOVED PAST 10'. MADE A FLAPS 10'. LANDED AT THE NEAREST SUITABLE AIRPORT. INSTALLED A NEW INBOARD WING FLAP CONTROL VALVE IAW AMM 27-52-03-4. PERFORMED AN OPS CHECK IAW AMM 27-50-00-710-801. RAN NR 1 AND 2 ENGINES IAW JRH AND MOVED FLAPS 20-10 AND 10-0 SEVERAL TIMES AND WAS UNABLE TO DUPLICATE PROBLEM. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 51,990 hrs · 11,591 cycles

DURING HFEC INSPECTION, FOUND ONE FASTENER HOLE 31 HAD A CRACK INDICATION AT RIGHT WING LOWER PANEL OUTER WING ACCESS DOOR AT XORS 696.730. REPAIRED IAW SRM 57-20-02-2R, FIG. 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 51,990 hrs · 11,591 cycles

DURING AN HFEC INSPECTION, FOUND TWO FASTENER HOLES 31 AND 34 WITH CRACK INDICATIONS, AT THE RIGHT WING LOWER PANEL OUTER WING ACCESS DOOR AT XORS 696.730. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1671) · corrosion level 2 · airframe 51,990 hrs · 11,591 cycles

MAIN DECK SEAT TRACK AT BS 1671, RBL 27.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SUPPORT — CRACKED (LT WING) · airframe 51,990 hrs · 11,591 cycles

LEFT WING LEADING EDGE LOWER SURFACE SUPPORT FORMER AT XOS 1084 FOUND CRACKED. REMOVED IAW SRM 51-31-01-0G. A NEW SUPPORT FORMER FABRICATED IAW DRAWING ARB2920, REV BB, AND INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1169) · corrosion level 2 · airframe 51,990 hrs · 11,591 cycles

MAIN DECK SEAT TRACK AT BS 1169, LBL 8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1451) · corrosion level 2 · airframe 51,990 hrs · 11,591 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1451, RBL 8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 795) · airframe 51,990 hrs · 11,591 cycles

MAIN DECK SEAT TRACK AT BS 795, LBL 75.25 CROWN FOUND DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,990 hrs · 11,591 cycles

MAIN DECK SEAT TRACK AT STATION 5-75, RBL 47.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 710) · airframe 51,990 hrs · 11,591 cycles

MAIN DECK SEAT TRACK AT BS 710, LBL 75.25 CROWN FOUND DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1306) · airframe 51,990 hrs · 11,591 cycles

MAIN DECK SEAT TRACK AT BS 1306, RBL 75.25, FOUND THE CROWN DAMAGED. REPLACED FROM BS 1263 TO 1390, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING RIB) · airframe 51,990 hrs · 11,591 cycles

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

Part: FORMER — CRACKED (RT WING) · airframe 51,990 hrs · 11,591 cycles

RIGHT WING-FIXED LEADING EDGE FORMER ASSEMBLY AT XOS 801 FOUND CRACKED. THE FORMER WAS REMOVED IAW SRM 51-31-01-0G. A NEW FORMER FABRICATED IAW DRAWING ARB2922 REV B, AND INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING RIB) · airframe 51,990 hrs · 11,591 cycles

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

Part: SKIN — CRACKED (RT WING) · airframe 51,990 hrs · 11,591 cycles

DURING HFEC INSPECTION, FOUND A CRACK ON THE RIGHT WING FIXED LEADING EDGE SKIN, APPROX. 1/2 INCH IN LENGTH AT CORNER NR 11 FUEL ACCESS DOOR FORWARD INBOARD CORNER. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 18. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: LONGERON — CORRODED (BS 1531-1641) · airframe 49,381 hrs · 10,709 cycles

LOWER FUSELAGE AFT OF LOWER BEACON, RIVET HEAD POPPED & SKIN BULGING. REPLACE FACTORY SPLICE & LONGERON.

Part: COVER — LOOSE (ZONE 200) · airframe 49,107 hrs · 10,618 cycles

R1 DOOR EMER EXIT LIGHT COVER, TAB IS BROKEN ON BACK OF COVER. REMOVED AND REPLACED R1 DOOR EMERGENCY EXIT LIGHT COVER IN REF AMM 33-27-05-4-0.

Part: VALVE — MALFUNCTIONED (ANTI ICE SYS) · airframe 479 hrs · 10,214 cycles

DURING CLIMB OUT WE GOT A LEVEL 1 ENG 2 ANTI-ICE OFF. THE MEL WE WERE OPERATING UNDER HAD NR 2 ENG ANTI-ICE VLV SECURED OPEN, THIS INDICATED A POSSIBLE PNEUMATIC LEAK IN NR 2 ANTI-ICE DUCT. DIVERTED & LANDED WITHOUT INCIDENT. R & R NR 2 INLET COWL ANTI-ICE SHUTOFF VALVE IAW MM 30-22-01-4-1. FACTED ON WRI 30-20-1424.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 478 hrs · 10,155 cycles

TAXI OUT BRAKING RESPONSE GOOD & NORMAL, AFTER FIRST OFFICER LANDING USING MEDIUM AUTO BRAKES, INITIAL BRAKE APPLICATION WAS VERY INEFFECTIVE UNTIL APPLIED HEAVY PRESS TO BEGIN SLOWING THE ACFT FROM 20 KTS GND SPEED. INSPECTED ALL MAIN & CTR LG BRAKES IAW AMM 32-43-20-6, CHECKED NORMAL. INSPECTED MAIN BRAKE CONTROLS, INCLUDES BRAKE PEDAL CONTROL, CABLES & LINKAGES IAW AMM 32-44-00-5, NO ABNORMALITY FOUND. PERFORMED THE IBCV INPUT PUSHRODS ADJUSTMENT & IBCV OPERATIONAL TEST IAW AMM 32-44-00-5, TESTED NORMAL. BLEED THE MLG & CTR LANDING GEAR BRAKES IAW AMM 32-43-20-2.

Part: DOUBLER — CRACKED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING LE COMPARTMENT AT APPROX STATION XOS 789, FOUND WITH CONTOUR LONGITUDINAL FRAME DOUBLER CRACKED. LONGITUDINAL FRAME DOUBLER REMOVED IAW SRM 51-31-01-0G, NEW FRAME DOUBLER FABRICATED IAW DWG ARB3954 REVISION K. NEW FRAME DOUBLER INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING LE AT APPROX STATION XOS 602, FOUND PANEL SUPPORT FRAME DOUBLER WITH SIGNS OF CRACK. REMOVED IAW SRM 51-31-01-0G, NEW FRAME DOUBLER FABRICATED IAW DWG ARB2933 REVISION T SHEET 2. NEW DOUBLER INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 478 hrs · 10,154 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE, SURFACE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.711", MATERIAL REMOVED 0.006", REMAINING THICKNESS 0.705", MINIMUM ALLOWABLE THICKNESS 0.720". REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0319681 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 478 hrs · 10,154 cycles

LEFT WING, FLAP SIDE, OTBD FLAP, INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-04. EXISTING DIAMETER =1.149", FINAL DIAMETER =1.190", MAXIMUM ALLOWABLE DIAMETER =1.150". REPAIR ACCOMPLISHED IAW EA 1- 5750-T0319468 PART 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100. REFER TO WRI 57501276 FOR WORK DETAILS.

Part: HINGE — CORRODED (TE FLAP) · airframe 478 hrs · 10,154 cycles

RIGHT WING, FLAP SIDE, OTBD FLAP INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-04. EXISTING DIAMETER =1.150", FINAL DIAMETER =1.158", MAXIMUM ALLOWABLE DIAMETER =1.150". REPAIR ACCOMPLISHED IAW EA 1- 5750-T0319469 PART 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 478 hrs · 10,154 cycles

LEFT WING, FLAP SIDE, INBD FLAP OTBD HINGE, OTBD PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER = 1.328", FINAL DIAMETER =1.338", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-T0319470 PART 1. REFER TO WRI 57501290 FOR WORK DETAILS. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 478 hrs · 10,154 cycles

RIGHT WING, FLAP SIDE, INBD FLAP OTBD HINGE, INBD PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIAMETER = 1.256", FINAL DIAMETER =1.260", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-T0319472 PART 1. REFER TO WRI 57501291 FOR WORK DETAILS. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 478 hrs · 10,154 cycles

RIGHT WING, FLAP SIDE, INBD FLAP OTBD HINGE, OTBD PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIAMETER = 1.256", FINAL DIAMETER =1.260", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-T0319472 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING, WING SIDE OTBD FLAP, INBD HINGE LOWER MOUNT INBD HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 0.703", FINAL HOLE DIAMETER =0.723", MAXIMUM ALLOWABLE HOLE DIAMETER =0.709". REPAIRED BUSHING, FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319466 PART 1 STEP 1B. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100. REFER TO WRI 57501280 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING, WING SIDE OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 0.643", FINAL HOLE DIAMETER =0.721", MAXIMUM ALLOWABLE HOLE DIAMETER =0.709". REPAIRED BUSHING, FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319466 PART 1 STEP 1B. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, BARREL NUT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED, FOUND WITHIN LIMITS. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING, WING SIDE, OTBD FLAP OTBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER =2.3105", FINAL HOLE DIAMETER =2.334", MAXIMUM ALLOWABLE HOLE DIAMETER =2.3135". REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319446 PART 1 STEP 1B. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100. REFER TO WRI 57501279 FOR WORK DETAILS.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 478 hrs · 10,154 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 750 X= 8 FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. CORROSION AT HOLE NR 3, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER = 0.580", FINAL HOLE DIAMETER =0.595", MAXIMUM ALLOWABLE HOLE DIAMETER =.584". REPAIR ACCOMPLISHED IAW EA 1-5750-T0319447 PART 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING, WING SIDE OTBD FLAP, INBD HINGE INBD ACTUATOR HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 1.215", FINAL HOLE DIAMETER =1.254", MAXIMUM ALLOWABLE HOLE DIAMETER =1.220". REPAIRED BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319466 PART 1 STEP 1C. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100. REFER TO WRI 57501280 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, OTBD ACTUATOR HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (LE DROOP) · airframe 478 hrs · 10,154 cycles

LEFT WING LE DROOP PANEL, UPPER SURFACE SKIN FOUND CRACKED FROM STATION XDLE 329.774 - XDLE 325.114. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING, WING SIDE, OTBD FLAP INBD HINGE, OTBD ACTUATOR HOLE BORE, FOUND CORROSIONS. CORROSION AT HOLE 8, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 1.219", FINAL HOLE DIAMETER =1.252", MAXIMUM ALLOWABLE HOLE DIAMETER =1.220". REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319466 PART 1 STEP 1C.

Part: HINGE — CORRODED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING, WING SIDE, OTBD FLAP INBD HINGE, SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE, FOUND CORRODED. REPAIRED IAW CMM 57-44-08. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 478 hrs · 10,154 cycles

RIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. CORROSION AT HOLE 3, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER = 0.580", FINAL HOLE DIAMETER =0.595", MAXIMUM ALLOWABLE HOLE DIAMETER =0.584". REPAIR ACCOMPLISHED IAW EA 1-5750-T0319447 PART 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING, WING SIDE OTBD FLAP, INBD HINGE PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER =2.309", FINAL HOLE DIAMETER =2.336", MAXIMUM ALLOWABLE HOLE DIAMETER =2.3135". REPAIRED BUSHING, FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319466 PART 1 STEP 1A. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100. REFER TO WRI 57501280 FOR WORK DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 478 hrs · 10,154 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 5 - 5, X= 8, FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING LE AT APPROX STATION XOS 425, FOUND INTERIOR BEADED DOUBLER CRACKED. LEFT WING LE REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING, WING SIDE, OTBD FLAP HINGE SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE FOUND CORRODED. FOUND WITHIN LIMITS. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1199) · airframe 478 hrs · 10,154 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1199, LBL 8 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: MOUNT — CORRODED (LT WING) · airframe 478 hrs · 10,154 cycles

LEFT WING, WING SIDE OTBD FLAP HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER =0.591", FINAL HOLE DIAMETER =0.599", MAXIMUM ALLOWABLE HOLE DIAMETER =0.584". AIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319446 PART 1 STEP 1A. CORROSION REPAIRED. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100. REFER TO WRI 57501279 FOR WORK DETAILS.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 478 hrs · 10,154 cycles

MAIN DECK RT FRAME AT STATION 535, LONGERON 19R FOUND DAMAGED. MAIN DECK DAMAGE REPAIRED IAW SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 478 hrs · 10,154 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1406, X= 8 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 478 hrs · 10,154 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1199, X= -27.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 478 hrs · 10,154 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 750, X= -8, FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 478 hrs · 10,154 cycles

MAIN DECK RT FRAME AT STATION 535, LONGERON 24R FOUND DAMAGED. MAIN DECK DAMAGE REPAIRED IAW SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: GCU — MALFUNCTIONED (NR 1) · airframe 477 hrs · 10,133 cycles

AFTER TAKEOFF AS GEAR WAS RETRACTING CAPTAIN`S 1, 2 & 3 DU'S WENT DARK. MULTIPLE LEVEL 1 & 2 ALERTS, SOME WERE TRANSITORY. THOSE WE WORKED WERE GEN 1 OFF, AC BUS TIE 1, EMER POWER & BATTERY DISCHARGE. CLEANED UP CAC IAW MM 05-50-02. INSPECTED & FOUND NR 1 GCU FAULTED. R & R NR 1 GCU IAW MM 24-21-03-4. PERFORMED OPERATIONS CHECK IAW 24-21-03-5. ALL CHECKED GOOD. GND RAN ALL 3 ENGS IAW JRH CHAPTER 5. SWAPPED POWER FROM ENG TO APU GND. ALL CHECKED GOOD. ACFT OK FOR SERVICE.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 472 hrs · 9,986 cycles

AFTER TAKEOFF & GEAR RETRACTION, HAD NOSE GEAR UNSAFE LIGHT ON PRIMARY. NOTED VERY UNUSUAL AIR NOISE FROM BELOW FUSELAGE, NOSE GEAR AREA. CHECK OF CONFIG PAGE SHOWED NOSE GEAR WAS UP. RED TABS REVIEWED FOR UNSAFE INDICATIONS. MOCC CONSULTED & DUE TO LOUDER THAN NORMAL NOSE GEAR NOISE, RETURNED. RED PRIMARY UNSAFE REMAINED AFTER GEAR PLACED DOWN. RED TABS REVIEWED, SECONDARY SHOWED GREEN DOWN LOCKED. CONFIRMED BY ATC PRIOR TO LANDING. REMOVED AND REPLACED NOSE GEAR PRIMARY PROX SENSOR D1-40 REF MD-11 AMM 32-61-17- 4. REQUIRES NEW SENSOR WIRES TO BE PULLED THROUGH CONDUIT, TERMINATED, AND ATTACHED TO TERMINAL STRIP INSIDE NR 3 PACK BAY. REF WDM 32-61-02, RAN SENSOR D1-40 SENSOR WIRING THRU CONDUIT AND TERMINATED AT S3-623. D1-40 SENSOR INSTALLATION IS COMPLETE. SHROUD OVER TERMINAL STRIP S3-623 IN PACK BAY IS REINSTALLED. PERFORMED OPS CHECK OF PRIMARY SENSOR REF MD-11 AMM 32-61-17-4. OPS CHECK NORMAL AT THIS TIME. PERFORMED FUNCTIONAL TEST OF PSEU REF AMM 31-71-01-2 WITH NO FAULTS FOUND AT THIS TIME. JACKED NOSE OF A/C REF AMM 07-11-00-2, AND PERFORMED TWO SUCCESSFUL NOSE GEAR EXTENTION AND RETRACTIONS REF AMM 32-31-00-5 WITH NO ABNORMAL NOISE NOTED. ALL INDICATIONS ON PRIMARY AND SECONDARY INDICATIONS NORMAL AT THIS TIME.

Part: INDICATOR — INOPERATIVE (EVAC SLIDE) · airframe 468 hrs · 9,896 cycles

ON LAYOVER, CHECK EVACUATION SLIDE REMOTE PRESSURE, PRESS TO TEST, INDICATING SYS INOPERATIVE. PRESS TO TEST SWITCH INOPERATIVE. FOUND INCORRECT LAMPS INSTALLED IN INDICATOR ASSEMBLY. INSTALLED CORRECT LAMPS AND OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EVAC SLIDE) · airframe 45,386 hrs · 9,462 cycles

L1 DOOR EVAC SLIDE WILL NOT TEST. RELEASED FOR SERVICE IAW MEL 25-61-02. L1 EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-02. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQUATE ONCE EACH FLIGHT DAY. RESECURED BROKEN WIRE AT BATTERY TERMINALS. ALL OPERATIONAL CHECKS NORMAL.

Part: FMU — INOPERATIVE (NR 3 ENGINE) · airframe 44,637 hrs · 9,238 cycles

REJECTED TAKEOFF FOR AN ENGINE FAIL LIGHT. NR 3 ENGINE WOULD NOT FULLY SPOOL UP. PERFORMED GVI FOR BOTH ENGINE INTAKE & EXHAUST AREA, FOUND NO DEFECTS. NO FAULTS STORED ON ALL EEC. PERFORMED FADEC INTERFACE TEST ON BOTH FCC-1 & FCC-2. ALL TEST PASSED IAW MM 22-01-10-5. DEU NR 3 HAS NO FAULT. ENGINE PRESSURE RATIO INDICATOR INOPERATIVE & AUTO THROTTLES INOPERATIVE. ACFT CATII. RAN NR 1 & NR 3 ENG IAW JRH, FOUND NORMAL ENGINE INDICATION. DUE TO HISTORY FOR NR 3 ENG EPR IND SPLIT AT TAKEOFF POWER ASSURANCE TABLE ON AMM 71-02-09-5-2. ACFT OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 44,497 hrs · 9,189 cycles

NR 3 ENG WOULD NOT ADVANCE TO MAX POWER, EPR OF 1.61, AUTO THROTTLES ADVANCED ENGINES 1 & 2 TO 1.61 EPR, NR 3 STOPPED AT 5% - 6% BELOW 1 & 2. THROTTLE NR 3 STOPPED 1/2 KNOB BEHIND NR 1 & 2. MANUALLY ADVANCED NR 3 THROTTLE UP, EPR & N1 SETTINGS WOULD NOT ADVANCE. INITIATED A LOW SPEED RTO AT 70 KNOTS. ACCOMPLISHED HIGH POWER RUN OF ALL 3 ENGINES, ALL PARAMETERS NORMAL & THROTTLE KNOBS EVEN. RAN ENGINES IAW JRH. IAW POWERPLANT CHECKED NR 3 ENGINE FUEL FILTER, FOUND NO DISCREPANCY. IAW POWERPLANT, PRECAUTIONARY CHANGE OF THE FUEL PUMP ACCOMPLISHED IAW MM 73-12-01-4-2. LEAK & OPS CHECKED NORMAL. RAN ENGINES AGAIN WITH SAME RESULTS. ACFT OK FOR SERVICE.

Part: BATTERY PACK — MISINSTALLED (L1 DOOR SLIDE) · airframe 44,026 hrs · 9,035 cycles

L1 SLIDE INDICATOR LIGHT INOPERATIVE. FOUND BATTERIES INSTALLED INCORRECTLY, REPOSITIONED BATTERIES & OPS CHECKED GOOD.

Part: CONTACT — DIRTY (LAMP SOCKET) · airframe 43,931 hrs · 9,002 cycles

L1 DOOR EVACUATION SLIDE REMOTE PRESSURE, PRESS TO TEST LIGHT INOPERATIVE. FOUND LAMP CONTACTS DIRTY, CLEANED IAW SMP. OPS TESTED GOOD. ACFT OK FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (ANTI-ICE SYS) · airframe 43,793 hrs · 8,960 cycles

WITH ANTI-ICE ON, RECEIVED WING ANTI-ICE LT DISAGREE. LT ANTI-ICE VLV SHOWED DISAGREE ON SYNOPTIC & BLEED PRESS ON SYS 1 WENT TO ZERO. SECURED ANTI-ICE IAW QRH & BLEED PRESS RETURNED TO NORMAL. DIVERTED AND LANDED MSP WITHOUT INCIDENT. REMOVED AND REPLACED L ANTI-ICE PRESS DIFF SWITCH REF M/M 30-11-02-4 AND PERFORMED WING ANTI-ICE ADJ/TEST REF M/M 30-11-00-5. CHECKS GOOD, A/C OK FOR SERVICE.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 43,771 hrs · 8,951 cycles

EMERGENCY EXIT LIGHT OVER L1 DOOR INOPERATIVE WITH EMERGENCY LIGHT SWITCH AT ON POSITION. FOUND POWER WIRE TO LIGHT ASSY. PULLED OUT OF SPLICE, RESPLICED WIRE PER MM 20-30-03-2, LIGHT OPS CHECKED GOOD.

Part: DEU — FAILED (NR 1) · airframe 43,444 hrs · 8,833 cycles

MASTER CAUTION & MASTER WARNING, WITH ASSOCIATED AUDIBLE WARNING, CONTINUOUSLY WENT ON FOR ENTIRE FLIGHT TILL APPROXIMATELY 2000' ON FINAL. DEU 1 FAILED ON CLIMB OUT. REPLACED NR 1 DEU IAW MD11 AMM 34-61-02-4, CHECKED GOOD.

Part: HANDLE — BROKEN (L1 DOOR) · airframe 43,395 hrs · 8,814 cycles

DOOR L1 EMERGENCY HANDLE BROKEN ON AFT BRACKET FOUND L1 DOOR EMERGENCY HANDLE, MANUAL LIFT BAR UNCLIPPED. CLIPPED & STOWED HANDLE. ACFT OK FOR CONTINUED SERVICE.

Part: STRUCTURE — CORRODED (FUEL CELL) · airframe 43,191 hrs · 8,725 cycles

BS 1321, XCW= 106 CENTER WING FUEL TANK SURFACE FOUND WITH CORRODED. REPAIRED IAW EA 1-5730-T0303574 PART 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 118.

Part: STRUCTURE — CORRODED (FUEL CELL) · airframe 43,191 hrs · 8,725 cycles

BS 1301, XCW= 107, CENTER WING FUEL TANK FOUND CORRODED. REPAIRED IAW EA 1-5730-T0303436 PART 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 118.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 43,191 hrs · 8,725 cycles

HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON MAIN DECK CARGO DOOR FUSELAGE LOWER FRAME SUPPORT FITTING, NR 6 HOLE B AND D FOUND WITH CRACK INDICATION AND HOLE DIAMETER REACHED 0.560". SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 43,191 hrs · 8,725 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON MAIN DECK CARGO DOOR LOWER FRAME SUPPORT FITTING, NR 7 HOLE A AND B FOUND CRACKED AND HOLE DIAMETER REACHED 0.560". SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 43,191 hrs · 8,725 cycles

HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON MAIN DECK CARGO DOOR FUSELAGE LOWER FRAME SUPPORT FITTING, NR 1 HOLE NR A, B AND C FOUND CRACKED AND HOLE DIAMETER REACHED 0.560". SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 43,191 hrs · 8,725 cycles

BS 1259, LONGERON 26R, R3 DOOR FORWARD FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 43,191 hrs · 8,725 cycles

MAIN DECK BS 635 RBL 8.5 SEAT TRACK FOUND CRACKED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 43,191 hrs · 8,725 cycles

LEFT WING FIXED L/E BEAD DOUBLER AT LWS 666 FOUND CRACKED. REPAIRED IAW SRM 57-40-02, REPAIR 15 FIGURE 203 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.

Part: STRAP — CRACKED (RT WING TE FLAP) · airframe 43,191 hrs · 8,725 cycles

RIGHT WING OTBD FLAP, INBD HINGE TENSION STRAP AT WS 486.603, FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,191 hrs · 8,725 cycles

BS 1014, LBL 8.5, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 969 TO 1029 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: SKIN — CHAFED (ZONE 100) · airframe 43,191 hrs · 8,725 cycles

FORWARD CARGO DOOR CUT OUT FORWARD SIDE FOUND EXISTING BLEND OUT AT BS 888, LONGERON 40 - 41 RT. REPAIRED IAW SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 53. EA 1-5330-T0303487 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: SKIN — CHAFED (ZONE 100) · airframe 43,191 hrs · 8,725 cycles

FORWARD CARGO DOOR CUT OUT AFT SIDE FOUND EXISTING BLEND OUT AT BS 1009, LONGERON 40 - 41R. REPAIRED IAW SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 53. EA 1-5330-T0303487 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 42,703 hrs · 8,566 cycles

HYD 1 OFF ALERT, TWO HOURS INTO FLT AT F360, SYS PRESSURE 40 PSI (AFTER ISOLATED), 39 DEGREES AND 8.6 GAL AT RESERVOIR, 30 MINUTES LATER QTY 0.3, HYD 1 FAIL ALERT. PUMPS SHUTOFF TWO HRS INTO FLT AND DIDN'T COME BACK ON. R & R NR 1 ENG DRIVEN HYD PUMP ASSY IAW MM 29-11-20-4-2. SOLENOID VALVE HAD DAMAGE ELEC RECEPTACLE, IAW MM 29-11-21-4. DRY MOTORED, LEAK CHECKED GOOD. R & R HYD FILTERS REF AMM 29-12-41-2. LEAK CHECKED GOOD.

Part: WARNING SYSTEM — FALSE INDICATION (FUEL SYSTEM) · airframe 41,960 hrs · 8,332 cycles

TIP TANK FUEL TRAPPED LT WING. PERFORMED TESTS IN REF TO FIM 28-14-16-00, ALL TESTS PASS. FQBU TEST RESULTED IN NO FAULTS, AND ALL FLOAT SWITCH TESTS PASS. ACFT OK FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (BATTERY CHARGER) · airframe 40,647 hrs · 7,960 cycles

BATTERY DISCHARGING LEVEL 1, ALERT. INTERMITTENT AT FIRST, THEN CONTINUOUS. BATTERY VOLTAGE SHOWED 30V-34V. R & R EPCU REF AMM24-08-01-4, OPS CHECKED NORMAL. ALL TROUBLESHOOTING PERFORMED IAW FIM 24-30-03-00. NO FAULTS NOTED, SYSTEM OPS CHECKS NORMAL.

Part: BATTERY — UNKNOWN · airframe 40,365 hrs · 7,886 cycles

BATTERY DISCHARGE ILLUMINATED SEVERAL TIMES STAYED ON FOR APPROX 2 MIN LAST DURATION THEN EXTINGUISHED. EPCU FAULT REVIEW SHOWED "COOLING VALVE 3/ INTFC", BATTERY CHARGER FAULT DISPLAY SHOWED "CHARGER FAIL, BATT FAIL, BUSS OK". TROUBLE SHOT IAW MM 24-30-00-2, CHECKED WIRES AND PINS FROM CHARGER TO BATTERYS ALL CHECKS NORMAL. FOUND SOME CORROSION AT BATTERY GROUND 4027R, CLEANED IAW SMP, REPLACED BATTERY 1 AND 2 IAW MM 24-34-02-4, AND BATTERY CHARGER IAW MM 24-30-00-2. ALL TESTS PASSED, OK FOR SERVICE.

Part: RELAY — INOPERATIVE (BATTERY CHARGER) · airframe 40,064 hrs · 7,810 cycles

APPROX 6.5 HRS INTO FLIGHT BATTERY DISCHARGING ALERT ILLUMINATED IAW QRH, DIVERTION INITIATED, AFTER 5-7 MINUTES THE ALERT WENT OUT. ELECTED TO PROCEED TO DESTINATION. VOLTAGE WAS CONSTANT 33 VOLTS DURING AND AFTER THE ALERT. ILLUMINATED AGAIN ON SHORT FINAL FOR APPROX 10 SECONDS. REPLACED RELAYS R2-5142 & R2-5145 REF ESPM 7 WDM 24-62-11. BATTERY CHARGER RELAY ADJUSTMENT AND TEST SATISFACTORY REF MM 24-34-01-2.

Part: INDICATOR — INOPERATIVE (ESCAPE SLIDE) · airframe 38,251 hrs · 7,356 cycles

DOOR ESCAPE SLIDE LOW PRESSURE INDICATOR LIGHT WILL NOT PRESS TO TEST. R & R LENS, LAMP RETAINER AND BULBS, IAW AMM 25-61-04-4-0. OPS CHECKED NORMAL. RETURNED TO SERVICE.

Part: DOUBLER — CRACKED (LT WING) · airframe 38,187 hrs · 7,337 cycles

LT WING BEADED DOUBLER FOUND CRACKED. REPAIRED IAW EA 1-5730-154256. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.

Part: SKIN — CRACKED (LT WING) · airframe 38,187 hrs · 7,337 cycles

LEFT WING L/E AT XOS 928 SKIN FOUND CRACKED UPON REMOVAL OF FORMER. REPAIRED IAW EA 1-5730-154256. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.

Part: FITTING — LOOSE (VERTICAL STAB) · airframe 38,187 hrs · 7,337 cycles

AFTER REMOVAL OF FIREWALL ACCESS PANEL, VERTICAL STABILIZER BANJO FITTING AFT SIDE CENTER FASTENER FOUND SHEARED OFF. FASTENER R & R IAW SRM 51-31-01, REV 48 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.

Part: FITTING — LOOSE (VERTICAL STAB) · airframe 38,187 hrs · 7,337 cycles

VERTICAL STABILIZER RT SIDE BANJO FITTING AFT SIDE FOUND LOOSE. R & R FASTENER IAW EA 1-5530-154251, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: FITTING — LOOSE (VERTICAL STAB) · airframe 38,187 hrs · 7,337 cycles

VERTICAL STABILIZER LT SIDE BANJO FITTING AFT SIDE HAS A FASTENER LOOSE. FASTENER R & R IAW EA 1-5530-154251 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: SEAT TRACK — CORRODED (BS 1059-1079) · corrosion level 2 · airframe 38,187 hrs · 7,337 cycles

CORROSION ON SEAT TRACK CROWN AND CHANNEL AT BS 1059 -1079 X=-8. REPAIRED IAW SRM 53-00-52, FIG 201, REVISION 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 36,143 hrs · 6,856 cycles

TOTAL LOSS OF NR 2 HYD. FOUND UPPER RUDDER NON REV PUMP SHUTOFF VALVE LEAKING. REPLACED VALVE . REPLACED BOTH NR 2 ENG DRIVEN PUMP CASE DRAIN FILTERS. NO CONTMINATION NOTED. FOUND FLUID IN NR2 RESERVIOR AND BOTH CASE DRAIN FILTERS. RAN NR 2 ENG HYD PUMPS OP CK NORMAL. NO LEAKS NOTED. ACFT OK FOR SVC.

Part: ACCESS DOOR — MISSING (LT WING) · airframe 32,785 hrs · 6,072 cycles

ON POST FLT WALKAROUND FOUND ACCESS DOOR MISSING FROM LT WING INBD T/E FAIRING, DOOR IS 541CL AND IS SHOWN ON MM 06-35-00-0, FIG 12/SHEET 1. REPLACED ACCESS DOOR MISSING FROM LT WING INBD T/E FAIRING IAW SRM 51-00-00.

Part: FRAME — CHAFED (ZONE 200) · airframe 32,171 hrs · 5,929 cycles

CABIN - LT STA 1741 BETWEEN LONGERON 11 LT AND LONGERON 12 LT FOUND CHAFED. REPAIRED IAW SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 42. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT AS IAW SRM 53-00-07 FIGURE 201 REPAIR 2, REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 108. .

Part: SKIN — CORRODED (BS 1210) · airframe 32,171 hrs · 5,929 cycles

CABIN - RT STA 1210, XCW = -107 CTR WING UPPER PANEL FOUND CORROSION. REPAIRED IAW EA NR 1-5710-135667, THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REVISION 108.

Part: SKIN — CORRODED (BS 1229) · airframe 32,171 hrs · 5,929 cycles

CABIN - RT STA 1229, XCW = -105 CTR WING UPPER PANEL FOUND CORROSION. REPAIRED IAW EA NR 1-5710-135667, THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 108.

Part: ENGINE — POWER LOSS (NR 3) · airframe 30,362 hrs · 5,458 cycles

ENG NR 3 FLAMED OUT IN FLIGHT. FL 320. LOUD BANG & SHUDDER WITH HIGH EGT INDICATION. DUMPED 59K LBS OF FUEL. LOUD COMPRESSOR STALL SOUND AND LOOKS LIKE EGT WENT TO 680 DEG C. ENGINE APPEARED TO ROLL BACK. HE CONSIDERED A RESTART BUT HIGH EGT PROMPTED SHUTDOWN. THEY DID NOT BLOW THE BOTTLE. FIRE HANDLE IS STILL PULLED. C/W ENG FAILURE OVERLOAD CONDITION INSP. CHECK. "A" CHECK INSP. ONLY FOR NR 3 ENG PYLON. NO DEFECTS NOTED. PER M/M 05-51-09-6. NR 3 ENGINE CHANGE WORK CARD 71T0903-PW C/W. NO DEFECTS NOTED AFTER ENGINE CHANGE. ACFT OK FOR FLIGHT.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 27,866 hrs · 4,893 cycles

LEFT WING, LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACKED. REMOVED CRACKED RIB DOUBLER AS PER SRM 51-31-01, VOL. II. FABRICATED NEW RIB DOUBLER AS PER DRAWING ARB3954. INSTALLED NEW RIB DOUBLER AT LT WING LEADING EDGE AT XOS 667 AS PER SRM 51-33-01, VOL.II. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 27,866 hrs · 4,893 cycles

LEFT WING ANTI-ICE TELESCOPIC DUCT DOOR CUT OUT CORNER FOUND CRACKED AT STATION XOS 464 AND XOS 470. REPAIR CARRIED OUT AS PER SRM 57-10-00, FIG.43, VOL.I AND EA 1-5710-122715, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 27,866 hrs · 4,893 cycles

RT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT TOP INBOARD AND OUTBOARD CORNER FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1721 L12L) · airframe 27,866 hrs · 4,893 cycles

AFT CABIN AT APPROXIMATELY STATION 1721 LEFT SIDE LONGERON 12 LEFT FOUND FRAME DENTED. CARRIED OUT REPAIR AS PER SRM 53-30-00, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1701 L12R) · airframe 27,866 hrs · 4,893 cycles

AFT CABIN AT APPROXIMATELY STATION 1701 RIGHT SIDE LONGERON 12 RIGHT TO LONGERON 13 RIGHT FOUND FRAME DENTED. AFT BS 1701 FRAME RT LONGERON 12 TO 13 RT CARRIED OUT REPAIR AS PER SRM 53-30-00, FIG.1, VOL.I. DUE TO CAT B REPAIR, INITIAL INSPECTION TO BE CARRIED OUT AT 14,500 CYCLE WITH REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLE AS PER SRM 53-30-00, FIG.1, VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1761 L12L) · airframe 27,866 hrs · 4,893 cycles

AFT CABIN AT APPROXIMATELY STATION 1761 LEFT SIDE LONGERON 12 LEFT FOUND FRAME DENTED. BS 1761 LT LONGERON 12 LT FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00, FIG.1, VOL.I. DUE TO CAT B REPAIR, INITIAL INSPECTION TO BE CARRIED OUT AT 14,500 CYCLE, WITH REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLE AS PER SRM 53-30-00, FIG.1, VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

DURING ACCOMPLISHING EO, NEW EXTERNAL SKIN (P/N ADA 7030Y1) FOUND WITH 2 MISDRILLED HOLES AND 11 EXTRA HOLES BEING TRANSFERRED AFTER TRANSFERRED HOLES FROM EXISTING EXTERNAL HOLES AT STA 853 TO STA 875, L-37R TO L-41R. REPAIR CARRIED OUT PER STEP 31 AND 32 OF E.A 1-5330-104764. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 24,609 hrs · 3,922 cycles

CENTER CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.040" REMAINING THK 0.300". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 24,609 hrs · 3,922 cycles

CENTER CARGO DOOR HINGE AT FUSELAGE AREA FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.028" REMAINING THK 0.312". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 24,609 hrs · 3,922 cycles

AFT CARGO DOOR HINGE AT FUSELAGE SIDE FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.020" REMAINING THK 0.320". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 24,609 hrs · 3,922 cycles

FWD CARGO DOOR HINGE FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.025" REMAINING THK 0.315". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 24,609 hrs · 3,922 cycles

AFT CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.035" REMAINING THK 0.305". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 24,609 hrs · 3,922 cycles

FWD CARGO DOOR HINGE AT FUSELAGE AREA FOUND WITH CORROSION. CORROSION ON FUSELAGE CARGO DOOR HINGE ASSY REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.021" REMAINING THK 0.319". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 300) · airframe 24,609 hrs · 3,922 cycles

LT HORIZONTAL STAB LEADING EDGE O/B SECTION NR 331FT FOUND WITH DENT ON O/B EDGE. FOUND OUT OF LIMIT AS PER SRM 55-00-01 VOL. I. DEPTH= 0.080", WIDTH= 2". REPAIR CARRIED OUT AS PER SRM 55-20-00 FIG. 5 VOL. I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — DAMAGED (FUSLEAGE) · airframe 24,609 hrs · 3,922 cycles

DURING FUSELAGE SKIN REPLACEMENT PER EA 1-5330-104764 PT.1 FOUND 01 HOLE SIZE 1/4 AT STA 979 LONGERON 48R, ORIGINAL SIZE 3/16. DIAMETER HOLE ON NEW SKIN PICKED-UP AND 01 EA. FASTENER ON NEW SKIN INSTALLED AS PER SRM 51-35-01 VOL.II. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FRAME — CRACKED (ZONE 600) · airframe 24,609 hrs · 3,922 cycles

DURING PROGRESSION OF REPAIR PER EO 1-5100-7-50001A PT.1 FOUND FRAME CRACKED AT RIGHT I/B NR 1 SLAT AT STA XIS 185.453. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL.II AND SRM 51-33-01 VOL.II. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 24,609 hrs · 3,922 cycles

RT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. ORIGINAL 1.2555" FINAL 1.2555" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-5750-106570. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 24,609 hrs · 3,922 cycles

FOUND RHW O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-09 PG. 402-408 AND FOUND WITHIN DAC DWG ARC 0503 LIMIT. ORIGINAL THK I/B 0.484" O/B 0.484" REMAINING THK I/B 0.481" O/B 0.481" MATERIAL REMOVED I/B 0.003" O/B 0.003". REPAIR CARRIED OUT AS PER CMM 57-44-09 AND CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 24,609 hrs · 3,922 cycles

RHW O/B FLAP I/B HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.469" O/B 0.486" REMAINING THK I/B 0.460" O/B 0.481" MATERIAL REMOVED I/B 0.009" O/B 0.005". REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 24,609 hrs · 3,922 cycles

LHW I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. LT FWD I/B FLAP O/B HINGE PIVOT HOLE SPOTFACE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07 PG. 403-404. ORIGINAL THK I/B 0.491" O/B 0.443" REMAINING THK I/B 0.489" O/B 0.443", MATERIAL REMOVED I/B 0.002" MIN ALLOWABLE THK 0.450". REPAIR CARRIED OUT AS PER E.A. 1-5750-106573 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 24,609 hrs · 3,922 cycles

RHW O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG. 621-622. ORIGINAL THK 1.151" FINAL 1.151" MAX. ALLOWABLE THK 1.150". BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-04 IAW REFERENCE E.A.1-5754-90387. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: RIB — CRACKED (BULKHEAD) · airframe 24,609 hrs · 3,922 cycles

FOUND CENTER LANDING GEAR WHEEL WELL RT BULKHEAD FWD RIB CUTOUT SUSPECT CRACKED. CENTER LANDING GEAR WHEEL WELL R/H BULKHEAD FWD RIB CUTOUT REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 24,609 hrs · 3,922 cycles

RHW I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. RT AFT I/B FLAP O/B HINGE PIVOT I/B BORE CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. ORIGINAL THK 1.2555" FINAL 1.2555" MAXIMIUM ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-5750-106570. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (BULKHEAD) · airframe 24,609 hrs · 3,922 cycles

CENTER LANDING GEAR WHEEL WELL LT BULKHEAD FWD RIB CUTOUT SUSPECT CRACKED. CRACKED RIB CUTOUT REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 800-840) · airframe 24,609 hrs · 3,922 cycles

FWD CABIN SEAT TRACK RIGHT FLANGE AND CROWN UPPER SURFACE FOUND CORROSION AT STA 800-840, RBL 27.5. REMOVED AS PER SRM 51-31-01 VOL.II AT STA 745 TO STA 869 X=27.5 R/H. NEW SEAT TRACK FABRICATED AS PER DRAWING ADA 7321-519, FASTENER HOLES PICKED UP AS PER SRM 51-31-01 VOL.II AND INSTALLED AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 24,609 hrs · 3,922 cycles

RHW O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-08 PG. 612-615 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.441" O/B 0.425" REMAINING THK I/B 0.438 O/B 0.432" MATERIAL REMOVED I/B 0.003" O/B 0.003". REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 24,609 hrs · 3,922 cycles

LHW O/B FLAP O/B HINGE (WING SIDE), LOWER ATTACHMENT I/B BORE FOUND CORRODED. LT FWD O/B FLAP O/B HINGE LOWER MOUNT I/B BORE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG. 402-408. ORIGINAL THK 0.518" FINAL 0.591" MAXIMUM ALLOWABLE 0.584". BUSHING FABRICATED AND INSTALLED AS PER E.A.1-5750-106566 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 24,609 hrs · 3,922 cycles

RHW I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5750-106574 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 24,609 hrs · 3,922 cycles

LHW O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP O/B HINGE BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PG. 402-408 AND FOUND WITHIN DRAWING ARC 0503 LIMIT. ORIGINAL THK I/B 0.498" O/B 0.498", REMAINING THK I/B 0.495" O/B 0.495", MATERIAL REMOVED I/B 0.003" O/B 0.003". REPAIR CARRIED OUT AS PER CMM 57-44-09 AND CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 24,609 hrs · 3,922 cycles

LHW I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER E.A.1-5750-106569. ORIGINAL 1.300" FINAL 1.328" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-5750-106569. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 24,609 hrs · 3,922 cycles

LHW O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP I/B HINGE LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CMM 57- 44-08 PG. 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.476" O/B 0.476" REMAINING THK I/B 0.473" O/B 0.473" MATERIAL REMOVED I/B 0.003" O/B 0.003" MIN ALLOWABLE THK 0.720". REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED MINOR PER GMM 6-2- 100.

Part: SKIN — DENTED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

FWD CARGO DOOR CUTOUT AFT DOOR JAMB FX SKIN WITH DENT AT L-32R TO L-35R. DAMAGED AREA TRIMMED AS PER SRM 53-50-00 FIG.16 VOL.I. REPAIR DOUBLER FABRICATED AND INSTALLED AS PER 53-50-00 FIG.16 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 24,609 hrs · 3,922 cycles

LHW O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-08 PG. 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.476" O/B 0.476" REMAINING THK I/B O.473" O/B 0.473" MATERIAL REMOVED I/B 0.003" O/B 0.003" MIN ALLOWABLE THK 0.720". REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED MINOR PER GMM 6-2- 100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 24,609 hrs · 3,922 cycles

LHW O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-08 PG. 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.476" O/B 0.476" REMAINING THK I/B 0.473" O/B 0.473" MATERIAL REMOVED I/B 0.003" O/B 0.003" MIN ALLOWABLE THK 0.720". REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED MINOR PER GMM 6-2- 100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 24,609 hrs · 3,922 cycles

LHW O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57- 44-08 PG. 602-607 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.476" O/B 0.476" REMAINING THK I/B 0.473" O/B 0.473" MATERIAL REMOVED I/B 0.003" O/B 0.003" MIN ALLOWABLE THK 0.720". REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED MINOR PER GMM 6-2- 100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 24,609 hrs · 3,922 cycles

LHW O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP I/B HINGE BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 PG. 612-615 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.445" O/B 0.440", REMAINING THK I/B 0.442" O/B 0.437", MATERIAL REMOVED I/B 0.003" O/B 0.003". REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 24,609 hrs · 3,922 cycles

HORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 02 CORROSION REWORK FOUND EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — GOUGED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

CTR CARGO DOOR CUTOUT FUSELAGE SKIN ON AFT DOOR JAMB FOUND WITH SCRATCHES ON L-38R TO L-40R. SCRATCHES ON CENTER CARGO DOOR CUTOUT AFT JAMB OF FUSELAGE SKIN L38R TO L40R REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 16 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: FRAME — DAMAGED (TAILCONE) · airframe 24,609 hrs · 3,922 cycles

LEFT FWD TAILCONE FRAME ALIGNMENT PIN HOLE (CTR POS) ELONGATED. DAMAGED FRAME AT L/H FWD TAILCONE REMOVED AS PER SRM 51-31-01 VOL.II. HOLES ON NEW FRAME PICKED-UP AS PER SRM 51-31-01 VOL.II AND DWG AKC 7520. NEW FRAME AT L/H FWD TAILCONE INSTALLED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 24,609 hrs · 3,922 cycles

HORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 19 CORROSION REWORK FOUND OUT OF LIMIT PER EO 1-5510-7-5000 D1 PT1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1179-1301) · airframe 24,609 hrs · 3,922 cycles

CABIN, SEAT TRACK STA 1179 TO STA 1301 X=75.5 (LT) FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: TANK — CORRODED (BS 1360) · airframe 24,609 hrs · 3,922 cycles

CABIN, UNDER FLOOR AREA, OVERWING TANK TOP SURFACE STA 1360 X=-75.0 (RT) FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 57-00-01 FIG.1A VOL.I. ORIGINAL THK 0.076" REMOVED 0.007" REMAINING THK 0.069" AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG.12 VOL.I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: FRAME — CRACKED (TAILCONE) · airframe 24,609 hrs · 3,922 cycles

RT FWD TAILCONE FRAME ALIGNMENT PIN HOLE (CTR POS) FOUND WITH CRACK. REPAIRED AS PER SRM 53-00-01 FIG.9 VOL. I AND SRM 53-30-00 FIG.12 VOL.I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

CABIN SEAT TRACK AT STA 990 TO STA 1079 X=-8.5 (RT) FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

AFT FUSELAGE COMPT UPPER TORQUE BOX WEB AT STA 2007 FOUND WITH CRACK. STOP DRILLED AS PER SRM 53-40-00 FIG.23 VOL.I. REPAIR FILLER AND DOUBLER FABRICATED AS PER SRM 53-40-00 FIG.23 VOL.I USING MATERIAL 7075T6-.032" AND MIL-T-9046-0.032". REPAIR FILLER AND DOUBLER INSTALLED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

AFT CABIN, AFT PRESSURE BULKHEAD LOWER T-CHORD AT STA 2007 FOUND EXISTING REPAIR DOUBLER AT RBL 27.5. SNRM N01258: REFER TO SNRM N00806 AND SRM 51-31-01 VOL II FOR WORK CARRIED OUT. AFT CABIN, AFT PRESSURE BULKHEAD LOWER T-CHORD AT STA 2007 REMOVED AS PER SRM 51-31-01 VOL II NEW T-CHORD HOLES PICKED-UP AND REPROTECTED AS PER SRM 51-31-01 AND SRM 51-21-01 VOL.II. NEW T-CHORD INSTALLED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 24,609 hrs · 3,922 cycles

HORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 30 CORROSION REWORK FOUND EXCEEDED LIMITS PER EO1-5510-7-5000 D1 PT 1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

CABIN SEAT TRACK AT STA 6-0 TO STA 6-30 X=27.5 (LT) FOUND WITH CORROSION. CORROSION CRACK REMOVED AND SECTIONAL REPAIR PERFORMED AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 24,609 hrs · 3,922 cycles

HORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 28 CORROSION REWORK FOUND EXCEEDED LIMITS PER EO1-5510-7-5000 D1 PT 1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

CABIN SEAT TRACK AT STA 824 TO STA 840 X=8.5 LT FOUND WITH CORROSION. CORROSION CRACK REMOVED AND SECTIONAL REPAIR PERFORMED AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

CABIN SEAT TRACK AT STA 808 TO STA 859 X=27.5 LT FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

FOUND CABIN SEAT TRACK AT STA 845 TO STA 899 X=75.25 RT FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

CABIN SEAT TRACK AT STA 6-100 TO STA 1199 X=27.5 RT FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

CABIN SEAT TRACK AT STA 899 TO STA 1099 X=27.5 RT FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL. I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

CABIN SEAT TRACK AT STA 899 TO STA 962 X=8.5 RT FOUND WITH CORROSION. REPAIR CARRIED OUT PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 24,609 hrs · 3,922 cycles

HORIZONTAL STAB CONSTANT SECTION LT BARREL NUT HOLE NR 17 REWORK FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 D1 PT 1. REPAIRED AS PER E.A. 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

CABIN SEAT TRACK AT STA 890 TO STA 979 X=27.5 LT FOUND WITH CORROSION. REPAIR CARRIED OUT PER SRM 53-70-00 FIG.1 VOL. I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

LT WING NR 16 SLAT TRACK CUTOUT I/B RIB SUSPECT CRACK. LT WING NR 16 SLAT TRACK CUTOUT I/B CRACK RIB REMOVED AND INSTALLED NEW RIB AS PER SRM 51-31-01 VOL.II REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 24,609 hrs · 3,922 cycles

HORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 6 REWORK FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 D1 PT 1. REPAIRED AS PER E.A.1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: BULKHEAD — DAMAGED (TEE FRAME) · airframe 24,609 hrs · 3,922 cycles

AFT CABIN, AFT PRESSURE BULKHEAD LOWER T-CHORD AT STA 2007 FOUND EXISTING REPAIR DOUBLER AT LBL 27.5. SNRM N00806: AFT CABIN AFT PRESSURE BULKHEAD LOWER T-CHORD AT STA 2007. REMOVED AS PER SRM 51-31-01 VOL II. NEW T-CHORD HOLES PICKED-UP AND REPROTECTED AS PER SRM 51-31-01 AND 51-21- 01 VOL II. NEW T-CHORD AT AFT PRESSURE BULKHEAD STA 2007. INSTALLED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SPAR — DAMAGED (HORIZ STAB) · airframe 24,609 hrs · 3,922 cycles

HORIZONTAL STAB CONSTANT SECTION RT SIDE BARREL NUT HOLE NR 1 REWORK FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 D1 PT.1. HORIZONTAL STAB CONSTANT SECTION R/H BARREL NUT HOLE NR 1 REPAIRED AS PER E.A.1-5510-106546 ATTACHMENT 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: NUT PLATE — DAMAGED (STROBE LIGHT) · airframe 24,609 hrs · 3,922 cycles

LOWER ANTI-COLLISION STROBE LIGHT 14 MOUNTING NUT PLATE FOUND DAMAGED. REPAIRED IAW EA 1-5330-106553. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

FOUND CABIN SEAT TRACK AT STA 935 TO STA 1025 X=8.5 LT FOUND WITH CORROSION. CORROSION CRACK REMOVED AND SECTIONAL REPAIR PERFORMED AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 24,609 hrs · 3,922 cycles

COCKPIT, DENT MARKS ON FLOOR PANEL 216BF. COCKPIT FLOOR PANEL #216BF REMOVED AS PER AMM 53-21-02. FLOOR PANEL FABRICATED AS PER DRAWING ABA 8675, NEW FLOOR PANEL PAINTED AS PER SRM 51-21-01 AND INSTALLED AS PER AMM 53-21-02. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 10" IN LENGTH DURING HFEC INSPECTION ON RT WING TANK AT THE END OF STRINGER 13 XORS 577. REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 1 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 10" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 14 XORS 521. REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 1 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 44 XORS 523. REPAIRED AS PER SRM 57-20-00 FIG. 10 OPT 2 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 0.25" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 41 XORS 685. REPAIRED AS PER SRM 57-20- 00 FIG. 10 OPT 2 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 0.25" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 9 XORS 819. REPAIRED AS PER SRM 57-20-00 FIG. 10 OPT 1 VOL.I. THIS REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 43 XORS 565. REPAIRED AS PER E.A.1-5720-106552.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 4" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 38 XORS 877. REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 2 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 42 XORS 642. LT WING TANK AT THE END OF STRINGER 42 XORS 642 CRACK REPAIRED AS PER E.A.1-5720-106551 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 8.5 IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 11 XORS 704. REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 3 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 7.5" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 10 XORS 760. REPAIRED AS PER SRM 57-20-00 FIG. 10 OPT 3 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 24,609 hrs · 3,922 cycles

CRACK FOUND APPROX 13" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 13 XORS 577. REPAIRED AS PER SRM 57-20-00 FIG. 10 OPT 1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (L/E SLAT) · airframe 24,609 hrs · 3,922 cycles

EXISTING REPAIR FOUND AT LT WING NR 1 SLAT LOWER SKIN STA XIS200. EXISTING REPAIR AT L/H WING NR 1 SLAT LOWER SKIN STA XIS 200, NEW SKIN REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG.10 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — UNKNOWN (CARGO DOOR) · airframe 24,609 hrs · 3,922 cycles

EXISTING REPAIR FOUND AT AFT CARGO DOOR LWR FWD CORNER, SNRM N00411: AFT CARGO DOOR LOWER FWD CORNER FASTENERS REMOVED AS PER SRM 51-35-01 VOL.II. DAMAGED AREA TRIMMED OFF AS PER SRM 52-10-00 FIG 17 VOL I. NEW REPAIR DOUBLER AND FILLER REWORKED AS PER SRM 52-10-00 FIG 17 VOL I AND SRM 51-31-01 VOL II AND INSTALLED AS PER SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (L/E SLAT) · airframe 24,609 hrs · 3,922 cycles

EXISTING REPAIR FOUND AT RT WING NR 1 SLAT UPPER SKIN LOWER AFT EDGE STA XIS 349.035.

Part: BULKHEAD — DAMAGED (ZONE 100) · airframe 24,609 hrs · 3,922 cycles

EXISTING REPAIR FOUND AT CENTER CARGO COMPT STA 1841 BULKHEAD WEB LT SNRM N00405: EXISTING REPAIR AT CENTER CARGO COMPT STA 1841 BULKHEAD WEB LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENGINEERING REPAIR/AUTHORIZATION 381015-14, EO 1-5100-7-5001A PT.1 TITLE: "REPAIR CATALOG-MD-11-REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (L/E SLAT) · airframe 24,609 hrs · 3,922 cycles

EXISTING REPAIR FOUND AT LT WING NR 2 SLAT LOWER SKIN STA XIS 349.035. EXISTING REPAIR FOUND AT LT WING NR 2 SLAT LOWER SKIN STA XIS 349.035 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 10 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,609 hrs · 3,922 cycles

EXISTING REPAIR FOUND AT FUSELAGE SKIN AFT LAVATORY EXHAUST PORT STA 1937 AND STA 1959. REWORK CARRIED OUT AS PER E.A.1-5330-105642.

Part: SKIN — DAMAGED (ZONE 100) · airframe 24,609 hrs · 3,922 cycles

REMOVED AND REPLACED FUSELAGE SKIN AND DOUBLERS PER DIRECTION OF AIRCRAFT ACQUISITION ENGINEERING. SKIN REPLACEMENT IS TO ELIMINATE PREVIOUS REPAIR AT STATIC PORT; RT FUSELAGE, FWD OF FWD LOWER CARGO COMPT DOOR. SNRM S00005: REFER TO EA 1-5330-104764 FOR WORK ACCOMPLISHED. TITLE:" FUSELAGE, PLATES AND SKINS, BODY STATION Y= 765.000 THROUGH Y= 1129.000, LONGERONS 36 THROUGH 48 RIGHT SKIN PANEL ASSY REPLACEMENT. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.