N594FE

Part: CONTROL VALVE — FAILED (HYD SYSTEM) · airframe 90,013 hrs · 18,933 cycles

ON FINAL, RECEIVED LEVEL 2 HYD 1 FAIL ALERT. RESERVOIR QUANTITY SHOWED 0.8 GALLONS. ***EMERGENCY DECLARED*** REMOVED STAB TRIM CONTROL MODULE IAW MD11 AMM 27-43-40-4 FOR EVIDENCE OF LEAK. LEAKING ISOLATED TO STAB TRIM CONTROL MODULE FLOW CONTROL VALVE.

Part: BRACKET — CORRODED (LT WING) · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND E.A.#1-5750-T0366358 A PART 1 STEP 1F(1) AND STEP 1F(2). REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: SPAR CAP — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

AFTER LEFT HAND OUTBOARD ISLAND REMOVAL FOR ACCESS LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1069 FOUND CORROSION. AFTER LEFT HAND OUTBOARD ISLAND REMOVAL LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1069 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57- 00-10-1A ALLOWABLE DAMAGE 1 FIGURE 101. LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1069 REPAIR CARRIED OUT AS PER EA 1-5710-T0367624 PART 1 TITLE: WINGS - LEFT HAND REAR SPAR - UPPER AFT TANG - CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 500) · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - INBOARD FLAP ASSEMBLY, INBOARD UPPER MID SEGMENT STATION XIFH 160 FOUND OIL CANNING. LEFT HAND WING INBOARD FLAP ASSEMBLY INBOARD UPPER MID SEGMENT DAMAGE SKIN AT STATION XIFH 160 REPAIRED IN ACCORDANCE WITH SRM 57-00-01-2R REPAIR 1 FIGURE 201 AND EA 1-5750-T0307737 A PART 2 TITLE: WINGS - FLIGHT SURFACES - LH WING - INBD FLAP ASSY - CENTER BOX UPPER SKIN REPAIR - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

AFTER LEFT HAND OUTBOARD ISLAND REMOVAL FOR ACCESS LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1049 FOUND CORROSION. LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1049 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-00-10-1A ALLOWABLE DAMAGE 1 FIGURE 101. LEFT HAND WING REAR SPAR UPPER CAP AFT FLANGE XORS = 1049 REPAIR CARRIED OUT AS PER EA 1-5710-T0367624 PART 1 TITLE: WINGS - LEFT HAND REAR SPAR - UPPER AFT TANG - CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND E.A.#1-5750-T0366359 A PART 1 STEP 1F(1) AND STEP 1F(2), TITLE: WINGS- FLIGHT SURFACES - RH WING -INBD FLAP OUTBD FWD HINGE (WING SIDE) REPAIR-PSE 57.55.01.1 INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.(WRI:57505192 FOR DETAILS)

Part: SKIN — NONE (ZONE 500) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING SKIN SPLICE REPAIR FOUND AT LEFT HAND WING INBOARD FLAP CENTER BOX LOWER SURFACE BETWEEN XIFH 249- XIFH 255. EXISTING SKIN SPLICE REPAIR ON LEFT HAND WING INBOARD FLAP CENTER BOX LOWER SURFACE BETWEEN XIFH 249 - XIFH 255 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-50-01-2R REPAIR 2 FIGURE 201. LEFT HAND WING INBOARD FLAP CENTER BOX LOWER SURFACE CARRIED OUT REPAIR FROM XIFH 237.320 TO XIFH 255.590 IN ACCORDANCE WITH EA # 1-5750-T0344949A PART 3. TITLE : WING - FLIGHT SURFACES - LH WING - INBD FLAP ASSY - CENTER BOX LOWER SKIN - SRM REPAIR - RSC TRACKING. EO 1-5100- 7-5001B7 PART1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 - REPAIR IDENTIFICATION & TRACKING REQUIRMENTS 14 CFR 121.707.ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2100.

Part: LUG — CORRODED (ZONE 600) · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND E.A.#1-5750-T0366359 A PART 1 STEP 1F(1) AND STEP 1F(2). REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: LUG — CORRODED (RT WING TE FLAP) · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND E.A.#1-5750-T0366359 A PART 1 STEP 1F(1) AND STEP 1F(2). REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN BETWEEN STATION 383 TO STATION 399 , LONGERON 25 LEFT HAND TO LONGERON 27 LEFT HAND. EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN BETWEEN STATION 383 TO STATION 399 LONGERON 25 TO LONGERON 27 LEFT HAND EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R REPAIR 1 CLASS 1. FUSELAGE SKIN CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5330-T0367805 PART 1 TITLE : FUSELAGE - PLATES & SKINS - FUSELAGE LHS NOSE SECTION SKIN PANEL REPAIR , STA 374-401, Z= -2.9 TO Z= -18.5. EO 1- 5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD - 11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — NONE (ZONE 500) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING DOUBLER REPAIR AT LEFT HAND WING DROOP LEADING EDGE ASSEMBLY . INBOARD AREA XDLE 309.934. EXISTING DOUBLER REPAIR AT LEFT HAND WING DROOP LEADING EDGE ASSEMBLY INBOARD AREA XDLE 309.934 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-00-00- 2R REPAIR GENERAL FIGURE 205. EO 1-5100-7-5001 B7 PART1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (D) ECCENTRIC HOLE CORRODED. HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.#1-5750-T0307725 A PART 2 STEP 3. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE — WORN (ZONE 200) · airframe 90,001 hrs · 18,931 cycles

CABIN-UPPER CARGO DOOR FUSELAGE HINGE FITTING PART NUMBER ACA7223-513 FOUND LOBES #1 TO 15 OUT OF LIMIT. LOBE HOLES #1 TO #15 FROM FORWARD AT CABIN-UPPER CARGO DOOR FUSELAGE HINGE FITTING PART NUMBER:ACA7223-513 REWORKED AND FOUND #1 TO #10 HOLES EXCEED LIMIT,#11 TO#15 HOLES WITHIN LIMIT AS PER MD-11 SRM52-30-16-1A FIGURE 101 SHEET 3. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM52-34-04 REPAIR GENERAL PARAGRAPH 2Y AND EA.#1-5310-T0367683 PART 1 STEP 2 AND STEP 5. TITLE: FUSELAGE-MAINFRAME-MAIN DECK CARGO DOOR JAMB FORWARD SUPPORT HINGE (FUSELAGE SIDE)-WORN HINGE LOBE BORES.REPAIR CLASSIFIED AS MINOR PER GMM6- 2-100.

Part: FITTING — OUT OF LIMITS (ZONE 800) · airframe 90,001 hrs · 18,931 cycles

CABIN-MAIN DECK CARGO DOOR HINGE FITTING PART NUMBER ACA7223-523 FOUND LOBES #1 TO 12 FROM FORWARD OUT OF LIMITS. LOBE HOLES #1 TO #12 FROM FORWARD AT CABIN-MAIN DECK CARGO DOOR HINGE FITTING PART NUMBER:ACA7223-523 REWORKED AND FOUND #1 TO #4 HOLES EXCEED LIMIT,#5 TO#12 HOLES WITHIN LIMIT AS PER MD-11 SRM52-30-16-1A FIGURE 101 SHEET 3. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM52-34-04 REPAIR GENERAL PARAGRAPH 2Y AND EA.#1-5230-T0367637 PART 1 STEP 2 AND STEP 5. TITLE: DOORS- CARGO DOOR /HYD SYS-MAIN DECK CARGO DOOR-2ND MOST FWD HINGE (DOOR SIDE)-WORN SUPPORT HINGE LOBES.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SUPPORT — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (E) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (E) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.#1-5750-T0367755 PART 1 STEP 3 , TITLE: WINGS-FLIGHT SURFACES-LHW FLAP VANE FITTING REWORKED- TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32- 4.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM NUMBER N01002 ATTACHED E.A.#1-5750-T0367755 PART 1 FOR DETAILS.

Part: SUPPORT — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE CORROSION.

Part: SUPPORT — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (C) ECCENTRIC HOLE CORRODED. HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.#1-5750-T0307725 A PART 2 STEP 3. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SUPPORT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.#1-5750-T0307725 A PART 2 STEP 3 , TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-RH WING -OUTBD FLAP VANE ASSEMBLY- NO.1 TRACK SUPPORT FITTING REWORK, AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SUPPORT — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (C) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (C) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.#1-5750-T0367755 PART 1 STEP 3 , TITLE: WINGS-FLIGHT SURFACES-LHW FLAP VANE FITTING REWORKED TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32- 4.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM NUMBER N01002 ATTACHED E.A.#1-5750-T0367755 PART 1 FOR DETAILS.

Part: SUPPORT — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.#1-5750-T0367755 PART 1 STEP 3 , TITLE: WINGS-FLIGHT SURFACES-LHW FLAP VANE FITTING REWORKED- TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-4.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SUPPORT — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (E) ECCENTRIC HOLE CORRODED. HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.#1-5750-T0307725 A PART 2 STEP 3. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SUPPORT — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (D) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (D) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- 50-02-2R REPAIR 5 FIGURE 201. ECCENTRIC OVERSIZED BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.#1-5750-T0367755 PART 1 STEP 3 , TITLE: WINGS-FLIGHT SURFACES-LHW FLAP VANE FITTING REWORKED- TRACK SUPPORT FITTINGS CORROSION REPAIR, AND INSTALLED AS PER AMM 27-50-32-4.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM NUMBER N01002 ATTACHED E.A.#1-5750-T0367755 PART 1 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG BORE(A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND E.A.#1-5750-T0307723 E PART 3 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND E.A.#1-5750-T0307992 D PART 3 STEP 2A AND STEP 2B . REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND E.A.#1-5750-T0366358 A PART 1 STEP 1F(1) AND STEP 1F(2). REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND E.A.#1-5750-T0307992 D PART 3 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 AND E.A.#1-5750-T0366358 A PART 1 STEP 1F(1) AND STEP 1F(2). REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: SUPPORT — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 52-04.OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 52-04 AND EA#1-5750-T0367567 PART 1 STEP 2A, TITLE: WINGS - FLIGHT SURFACES - E0 1-5750- 7-5002 - LH WING OUTBD FLAP, INBD AFT HINGE (FLAP SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD FORWARD HINGE (WING SIDE) BARREL NUT SPOT FACE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP ASSEMBLY . INBOARD FORWARD HINGE (WING SIDE) BARREL NUT SPOT FACE REWORKED AS PER MD-11 CMM57-44-08. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.# : 1-5750-T0307631 A PART 2 STEP 2. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-LH WING - OUTBD FLAP , INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100. REFER TO SNRM NUMBER: N00817 ATTACHED EA. #:1-5750-T0307631 A PART 2 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG BORE (F AND G HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-03 AND E.A.#1-5750-T0307723 E PART 3 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 90,001 hrs · 18,931 cycles

LOWER CENTER CARGO COMPARTMENTSTATION 5-123 LONGERON 39 LEFT HAND SLICE FITTINF FOUND WITH CRACK . SPLICE FITTING REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01- OG. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVSION J . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 90,001 hrs · 18,931 cycles

LOWER CENTER CARGO COMPARTMENT STATION 5-123 LONGERON 50 RIGHT HAND SPLICE FITTING FOUND WITH CRACK . SPLICE FITTING REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01- OG. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVSION J . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — DAMAGED (RT WING) · airframe 90,001 hrs · 18,931 cycles

EXISTING REPAIR FOUND AT RIGHT HAND WING TANK STRINGER END 14 ( UPPER) BETWEEN XORS 506 TO XORS 538. EXISTING REPAIR AT RIGHT HAND WING TANK STRINGER END 14 BETWEEN XORS 506 TO XORS 538 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R REPAIR 5 FIGURE 201. RIGHT HAND WING TANK STRINGER END 14 CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5750-90025A PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — DAMAGED (RT WING) · airframe 90,001 hrs · 18,931 cycles

EXISTING REPAIR FOUND AT RIGHT HAND WING TANK STRINGER END 13 (UPPER) BETWEEN XORS 562 TO XORS 592. EXISTING REPAIR AT RIGHT HAND WING TANK STRINGER END 13 BETWEEN XORS 562 TO XORS 592 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R REPAIR 5 FIGURE 201. RIGHT HAND WING TANK STRINGER END 13 CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5720-90027A PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — DAMAGED (LT WING) · airframe 90,001 hrs · 18,931 cycles

EXISTING REPAIR FOUND AT LEFT HAND WING TANK STRINGER END 14 (UPPER) BETWEEN XORS 506 TO XORS 538 . EXISTING REPAIR AT LEFT HAND WING TANK STRINGER END 14 BETWEEN XORS 506 AND XORS 538 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R REPAIR 5 FIGURE 201. LEFT HAND WING UPPER STRINGER 14 CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5720-90026A PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SKIN — DAMAGED (ZONE 500) · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - INBOARD FLAP ASSEMBLY INBOARD LOWER SEGMENT EXISTING REPAIR INTERNAL DAMAGED. DAMAGE EXISTING REPAIR AT LEFT HAND WING INBOARD FLAP ASSEMBLY INBOARD LOWER SEGMENT BETWEEN XIFH 133.9 AND XIFH 195.3 REMOVED AS PER SRM 51-31-01-0G. REPAIR CARRIED OUT BETWEEN XIFH 133.9 AND XIFH 201.300 IN ACCORDANCE WITH SRM 57-00-01-2R REPAIR 2 FIGURE 201 AND EA 1-5750-T0324501 C PART 3 TITLE: WINGS - FLIGHT SURFACES - LH WING - INBD FLAP ASSY - TRAILING EDGE ASSY UPPER SKIN - SRM REPAIR - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 745 TO STATION 785 X = -8.5.

Part: FORMER — CRACKED (ZONE 600) · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 584 FORMR FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 584 FORMER CRACKED REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISION H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: NONE — NONE (N/A) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND ON WEB AT CENTER CARGO COMPARTMENT AFT BULKHEAD STATION 1841 X = 17 . EXISTING REPAIR DOUBLER ON WEB AT CENTER CARGO COMPARTMENT AFT BULKHEAD STATION 1841 X = 17 EVALUATED AND FOUND WEB WITH DAMAGE AND EXCEEDED LIMIT AS PER SRM 53 -00-00-2R REPAIR GENERAL FIGURE 202. DAMAGED WEB REMOVED AND REPLACED BY FABRICATION IN ACCORDANCE WITH DOUGLAS DRAWING # AGA 7170 REVISION : R AND SRM 51- 31-01-0G . EO 1-5100-7-5001 B7 PT 1. CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (MAIN DECK) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 745 TO STATION 783 X = 27.5. EVALUATED AND FOUND SEAT TRACK NOT REPAIRED IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201 . SEAT TRACK REPAIR CARRIED OUT FROM STATION 745 TO STATION 799 X= 27.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201 . EO 1-5100-7-5001B7 PART1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 600) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 288.14 EXISTING REPAIR DOUBLER AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 288.14 EVALUATED AND FOUND REPAIR DOUBLER DAMAGED AND EXCEEDED LIMIT AS PER SRM 57-00-00-2R FIGURE 201 REPAIR GENERAL. RIGHT HAND WING INBOARD FLAP LOWER SEGMENT CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5750-T0324527 A PART 2 TITLE : WINGS - FLIGHT SURFACES - EO 1-5100-7-5001 - RH WING - INBD FLAP ASSY - EXISTING REPAIRS - RSC TRACKING. EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD -11- REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 600) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 261.69. EXISTING REPAIR DOUBLER AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT UPPER SKIN XIFH 261.69 EVALUATED AND FOUND EXISTING REPAIR DOUBLER DAMAGED AND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 57-00-00-2R FIGURE 201 REPAIR GENERAL. RIGHT HAND WING INBOARD FLAP LOWER SEGMENT CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5750-T0324527 A PART 2 TITLE : WINGS - FLIGHT SURFACES - EO 1-5100-7-5001 - RH WING - INBD FLAP ASSY - EXISTING REPAIRS - RSC TRACKING . EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS - 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SKIN — CRACKED (LT NR 8 SLAT) · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING # 8 SLAT INTERIOR SURFACE FOUND CRACK. LEFT HAND WING #8 SLAT INTERIOR SURFACE AT STATION XOS 1146.814 CRACKED AREA REPAIR CARRIED OUT AS PER EA 1-5750-T0367711 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (ZONE 600) · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 542 STIFFENER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 542 CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB 2918 RIVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (ZONE 500) · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING LOWER STIFFENER AT APPROXIMATELY XOS 542 FOUND CRACK. LEFT HAND WING LOWER AT APPROXIMATELY XOS 542 CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB 2918 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 789 RIB DOUBLER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 789 RIB DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-0-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 3954 REVISION K. REPAIR CALSSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING LE) · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING FIXED LEADING EDGE AT APPROXIMATELY XOS = 789 FORMER FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE AT APPROXIMATELY XOS = 789 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2930 REVISION F. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING LE) · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING UPPER FORMER AT APPROXIMATELY XOS 912 FOUND CRACKED. LEFT HAND WING UPPER COMPARTMENT FIXED LEADING EDGE APPROXIMATELY XOS 912 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2921 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CAP — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING REAR SPAR LOWER CAP AFT FLANGE XORS = 1051 FOUND CORROSION LEFT HAND WING REAR SPAR LOWER CAP AFT FLANGE XORS = 1051 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-00-10-1A FIGURE 101 ALLOWABLE DAMAGE 1. LEFT HAND WING REAR SPAR LOWER CAP AFT FLANGE XORS = 1051 REPAIR CARRIED OUT AS PER SRM 57-20-10-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 670 BEADED DOUBLER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 670 BEADED DOUBLER CRACKED AREA 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 (600) · airframe 90,001 hrs · 18,931 cycles

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

Part: TRACK — NONE (ZONE 200) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 1481 TO STATION 5-0 , X = 27.5 . EXISTING REPAIR ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 1481 TO STATION 5-0 X = 27.5 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. SEAT TRACK REPAIR CARRIED OUT AT STATION 1471 TO STATION 5-0 X = 27.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO 1-5100- 7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — NONE (ZONE 200) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT STATION 5-0, X = 8.5. EXISTING REPAIR ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT STATION 5-0 X = 8.5 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. SEAT TRACK REPAIR CARRIED OUT AT STATION 5-0 TO STATION 5-42 X=8.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD11- REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: TRACK — NONE (ZONE 200) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT STATION 5-0 , X = 47.5. EXISTING REPAIR ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT STATION 5-0 X = 47.5 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. SEAT TRACK REPAIR CARRIED OUT AT STATION 5-0 TO STATION 5-63 X= 47.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B7 PART1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED . REPAIR CLASSIFED AS MAJOR PER GMM 6-2- 100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750-T0307630 B PART 3 STEP 1C, REPAIR CLASSIFIED AS MINOR PER GMM6-2- 100.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE (HOLE #8) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA.#:1-5750-T0307629 A PART 3 STEP 2B. TITLE: WINGS - FLIGHT SURFACES- EO1-5750-7-5002-RH WING -OUTBD FLAP, OUTBD FWD HINGE (WING SIDE)-CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM NUMBER : N00850 ATTACHED EA.#:1-5750-T0307629 A PART 3 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE (HOLE #7) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#: 1-5750-T0367603 PART 1 STEP 2B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#: 1-5750-T0367603 PART 1 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.# : 1-5750-T0307631 A PART 2 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD SPOT FACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM57- 44-08 AND EA.#: 1-5750-T0367603 PART 1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA#:1-5750-T0307631 A PART 2 STEP 2B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA.#:1-5750-T0307629 A PART 3 STEP 2A. TITLE: WINGS - FLIGHT SURFACES-EO1-5750-7-5002-RH WING -OUTBD FLAP, OUTBD FWD HINGE (WING SIDE)- CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM NUMBER : N00850 ATTACHED EA.#:1-5750-T0307629 A PART 3 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#: 1-5750-T0367603 PART 1 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.# : 1-5750-T0307631 A PART 2 STEP 2B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE (HOLE #4) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA.#:1-5750-T0307629 A PART 3 STEP 2B. TITLE: WINGS - FLIGHT SURFACES- EO1-5750-7-5002-RH WING -OUTBD FLAP, OUTBD FWD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM NUMBER : N00850 ATTACHED EA.#:1-5750-T0307629 A PART 3 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE (HOLE #7) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#: 1-5750-T0367603 PART 1 STEP 2B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT BORE (HOLE #7) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA.#:1-5750-T0307629 A PART 3 STEP 2B. TITLE: WINGS - FLIGHT SURFACES- EO1-5750-7-5002-RH WING -OUTBD FLAP, OUTBD FWD HINGE (WING SIDE)- CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM NUMBER : N00850 ATTACHED EA.#:1-5750-T0307629 A PART 3 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT BORE (HOLE #7) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA.#:1-5750-T0307629 A PART 3 STEP 2B. TITLE: WINGS - FLIGHT SURFACES- EO1-5750-7-5002-RH WING -OUTBD FLAP, OUTBD FWD HINGE (WING SIDE)- CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM NUMBER : N00850 ATTACHED EA.#:1-5750-T0307629 A PART 3 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. INBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. INBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE(HOLE #4) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#: 1-5750-T0367603 PART 1 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.# : 1-5750-T0307631 A PART 2 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD 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 CMM57-44-09 AND E.A.#1-5750-T0307630 B PART 3 STEP 1A, 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 N00770 ATTACHED E.A. #1-5750-T0307630 B PART 3 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750-T0307630 B PART 3 STEP 1C, REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750-T0307630 B PART 3 STEP 1B, REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA.#:1-5750-T0307629 A PART 3 STEP 2A. TITLE: WINGS - FLIGHT SURFACES-EO1-5750-7-5002-RH WING -OUTBD FLAP, OUTBD FWD HINGE (WING SIDE)-CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM NUMBER : N00850 ATTACHED EA.#:1-5750-T0307629 A PART 3 FOR DETAILS.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE (HOLE #8) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA.#:1-5750-T0307629 A PART 3 STEP 2B. TITLE: WINGS - FLIGHT SURFACES- EO1-5750-7-5002-RH WING -OUTBD FLAP, OUTBD FWD HINGE (WING SIDE)-CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: CAP — NONE (ZONE 600) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE STATION XOS 906. EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE STATION XOS 906 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-40-03-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,001 hrs · 18,931 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750-T0307630 B PART 3 STEP 1B, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 90,001 hrs · 18,931 cycles

RIGHT HAND WING INBOARD FIXED LEADING EDGE STATION XIS247 UPPER SURFACE CRACKED. RIGHT HAND WING INBOARD FIXED LEADING EDGE STATION XIS247 UPPER SURFACE CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 8 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — NONE (ZONE 200) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON FRAME AT MAIN DECK CARGO COMPARTMENT STATION 535 LONGERON 19 LEFT HAND. EXISTING REPAIR ON FRAME AT MAIN DECK CARGO COMPARTMENT STATION 535 LONGERON 19 LEFT HAND EVALUATED AND FOUND EXISTING REPAIR ANGLES WITH DEEP CHAFFED MARK. MAIN DECK FRAME AT STATION 535 LONGERON 19 LEFT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-20-07-2R REPAIR 1 FIGURE 202. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — NONE (ZONE 200) · airframe 90,001 hrs · 18,931 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON FRAME AT MAIN DECK CARGO COMPARTMENT STATION 535 LONGERON 24 LEFT HAND. EXISTING REPAIR ON FRAME AT MAIN DECK CARGO COMPARTMENT STATION 535 LONGERON 24 LEFT HAND EVALUATED AND FOUND EXISTING REPAIR ANGLES WITH DEEP CHAFFED MARK . MAIN DECK FRAME AT STATION 535 LONGERON 24 LEFT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-20-07-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSFIED AS MAJOR PER GMM 6-2- 100

Part: NONE — FAILED (N/A) · airframe 90,001 hrs · 18,931 cycles

ON PREFLIGHT LEVEL 1 EMER LTS BAT 1LO WHILE TESTING THE EMERGENCY LIGHTS. R&R THE EMERGENCY LIGHTING BATTERY POWER SUPPLY AND DID OPERATIONAL TEST THE BATTERY PACK, TEST PASSED PER AMM 33-51-01-4.

Part: SENSOR — MALFUNCTIONED (MLG) · airframe 87,118 hrs · 18,079 cycles

INTERMITTENT GEAR UNSAFE CENTER GEAR PERFORMED GO AROUND CONSULTED QRH LANDED UNEVENTFUL. PERFORMED MSC FAULT REVIEW OF LEG 01, NO FAULTS SHOWN. PERFORMED SELF TEST OF PSEU, IAW FIM 32-30-08-05, FIGURE 109, NO FAULTS NOTED OR OBSERVED. WILL CONTINUE TO T/S, IAW TSI. R & R CENTER GEAR LOCKED SENSORS D1-69 AND D1-184, REF MD-11 MM 32-61-16 AND WDM 32-61-02/32-61-03. OPERATIONS CHECKS GOOD, REF TSI 32-60/3604. PERFORMED CENTER LANDING GEAR RETRACTION AND EXTENTION CHECKS, IAW MD11 AMM 32-38-00-2. ALL INDICATIONS NORMAL.

Part: FITTING — CORRODED (RT HORIZ STAB) · airframe 85,567 hrs · 17,651 cycles

RT HORIZONTAL L/E I/B LOWER ATTACH HOLES HAVE RIFELING AND CORROSION. REPAIRED RT HORIZONTAL L/E I/B LOWER ATTACH HOLES REF EA T1-5510-T0354193 05/22/20 SEE ATTACHMENT FOR JPF.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,567 hrs · 17,651 cycles

UPPER CARGO COMPARTMENT - SEAT TRACK STA.755/RBL-8.5 - LOBE DAMAGED (MARKED).

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,567 hrs · 17,651 cycles

UPPER CARGO COMPARTMENT - SEAT TRACK STA.755/LBL-27.5 - LOBE DAMAGED (MARKED).

Part: FITTING — CRACKED (FUSELAGE) · airframe 85,567 hrs · 17,651 cycles

UPPER FUSELAGE LEFT SIDE STA 1381 FILLET PANEL SUPPORT RIB, LOWER CLIP IS CRACKED. REMOVED LOWER CLIP (ANB7142-7) CLIP AND INSTALLED NEW FABRICATED ANB7142-7 CLIP REF SRM 51-31-01-0G.

Part: FITTING — CRACKED (FUSELAGE) · airframe 85,567 hrs · 17,651 cycles

UPPER FUSELAGE LEFT SIDE STA1401 FILLET PANEL SUPPORT RIB, LOWER CLIP IS CRACKED. REMOVED AND REPLACED LOWER CLIP (ANB7143-11) AT LEFT SIDE STA 1361 REF SRM 51-31- 01-0G.

Part: STRUCTURE — WORN (DROOP LE) · airframe 85,567 hrs · 17,651 cycles

RH WING, DROOP L/E INBD SIDE HAS DEEP WEAR MARKS INSTALLED REPAIR DOUBLER PER SRM 57-40-01 REPAIR 15

Part: SKIN — CANNING (TE FLAP) · airframe 85,567 hrs · 17,651 cycles

R/H I/B FLAP TOP FORWARD CENTER SKIN IS OIL CANNING. SUSPECT DELAM. REPAIRED R/H IB FLAP REF. SRM 57-00-01-2R REPAIR 1. REF. EA 1-5750-T0353561. R/H INBD FLAP UPPER SURFACE - DENT, RSC TRACKING. MAJOR REPAIR

Part: SPAR — CRACKED (RT PYLON) · airframe 85,567 hrs · 17,651 cycles

RT TAIL PYLON UPPER SPAR ASSY HAS A .100 INCH CRACK AT STA YID=408.5 AT THE OUTSIDE RADIUS. TRIMMED OUT NOTED AREA OF RT NR 2 PYLON UPPER SPAR ASSY AS REQUIRED TO REMOVE ALL EVIDENCE OF CRACK REF SRM 54-00-00-2R.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 85,567 hrs · 17,651 cycles

LOWER FWD CARGO DOOR UPPER AFT CORNER HAS A CRACK INDICATION AT THE UPPER FASTENER HOLE. (MARKED) FASTENER HOLE OVERSIZED TO .213 TO REMOVE CRACK. NDT VERIFIED CRACK REMOVED REF SRM 51-31-01-0G

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 85,567 hrs · 17,651 cycles

MAIN DECK SEAT TRACK HAS A CRACK, AT STA. 2007 RBL 111" (DOT #2) (DOT #2, CRACK IS VIEWABLE THROUGH AFT WASTE TANK COMPARTMENT ZONE 189) REMOVED AND REPLACED SEAT TRACK FROM STA 1868 - 2007 PER SRM 53-00-52-2R FIG 201. REPAIR 1. "MARJOR REPAIR".

Part: SKIN — CRACKED (LT WING) · airframe 85,567 hrs · 17,651 cycles

L/H LOWER WING SKIN AT FUEL ACCESS DOOR CUTOUT (XORS 697) HAS CRACK INDICATIONS IN BOLT HOLES #7, 13, 14, AND 36. (MARKED) REPAIRED BOLT HOLES #7,13, 14 AND 36 AT L/H LOWER WING SKIN AT FUEL ACCESS DOOR CUTOUT XORS 697 REF. SRM 57-20-02-2R PG. 30

Part: SKIN — CRACKED (RT WING) · airframe 85,567 hrs · 17,651 cycles

R/H LOWER WING SKIN AT FWD INBD CORNER OF PANEL 618FB (SLAT ACTUATOR ACCESS DOOR HAS .300 INCH CRACK REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-40-02-2R FIG 202 SHEET 1

Part: SKIN — CRACKED (RT WING) · airframe 85,567 hrs · 17,651 cycles

R/H LOWER WING SKIN AT FWD INBD CORNER OF PANEL 618FB (SLAT ACTUATOR ACCESS DOOR HAS .300 INCH CRACK

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO DECK, FLOOR PANEL AT ENTRANCE OF R1 DOOR IS SPONGY REMOVED AND REPLACED FLOOR BOARD, MAIN CARGO DECK AT R1, #221JF, REF-AMM-53-21-00- 0

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 85,567 hrs · 17,651 cycles

MAIN CABIN UNDER FLOORBOARD AT STATION 735 LT SIDE LBL 100, NR 2 PNUEMATIC DUCT TURN BUCKLE ATTACH BRACKET. TWO EACH FASTENERS SHEARED FROM FLOORBEAM. MKD 585184 05-MAY-2020 12:06. REMOVED AND REPLACED TWO SHEARED HI-LOKS, MAIN CABIN UNDER FLOORBOARD AT STATION 735 LT SIDE, LBL 100 PNEUMATIC DUCT TURN BUCKLE ATTACH BRACKET IAW SRM 51-33-01. REF EA 1-5310-T0352924, FUSELAGE MAINFRAME CRACK INDICATION 2 HOLES IN FLOORBEAM LBL STATION 735. SEE ATTACHMENT FOR JPF.

Part: SEAT TRACK — BENT (FUSELAGE) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO DECK ENTRY AREA RH BTM CORNER AT APROX STA 758 LBL 111 SEAT TRACK BENT 585184: JACKSON, SENIAE M - 12-MAR-2020 13:11 REPLACED IAW SRM 53-00-52 FIG 201 SHEET 213 03/11/20 SEE ATTACHMENT FOR JPF.

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN DECK AT APROX STA 1680 BTWN RBL 51 & RBL 79 FLOOR BOARD PUNCHERED SEVERAL AREAS (MARKED) REPAIRED FLOOR BOARD 282DF RBL 68 & 73 ON STA 1677 PER SRM 53-00-50-2R FIG 206 REPAIR 2 SHT 1.

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1531 (18C) PUNCTURED IN SEVERAL AREAS REPAIRED FLOOR BOARD 273 JF ON CENTERLINE AT STA 1501, 1504, 1507, 1510, 5-9, 5-21, 5-48, 5-51, 5-82 PER SRM 53-00-50-2R FIG 206 REPAIR 2 SH 1

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN DECK FLOOR PANEL AT CNTR AISLE APPROX STA 950 (8C) PUNCTURED IN SEVERAL AREAS (MARKED) REPAIRED FLOOR BOARD 251 GF ON CENTERLINE AT STA 1003, 1011, 1053, 1056. 1098 PER SRM 53-00-50-2R REPAIR 2 FIG 206 SH1

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1870 PUNCTURED (MARKED) REPAIRED FLOORBOARD 293 KF AT STA 1882 & CENTERLINE PER SRM 53-00-50-2R FIG 206 REPAIR 2 SH 1

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1730 (21C) PUNCTURED IN SEVERAL AREAS (MARKED) REPAIRED FLOOR BOARD 283 EF ON CENTERLINE AT STA 1605, 1608, 1632, 1635, 1640, 1643 PER SRM 53-00-50-2R FIG 206 REPAIR 2 SH 1

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1790 (22C) PUNCTURED IN SEVERAL AREAS (MARKED) REPAIRED FLOOR BOARD 283 HF ON CENTERLINE AT STA 1774 & 1761 PER SRM 53-00-50-2R

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN DECK FLOOR PANEL AT CNTR AISLE APPROX STA 850 (6C) PUNCTURED IN SEVERAL AREAS (MARKED) REPAIRED FLOOR BOARD 245 DF ON CENTERLINE, STA 925, 930, 971, & 974 PER SRM 53-00-50- 2R FIG 206 REPAIR 2 SH 1

Part: SKIN — CRACKED (LT WING) · airframe 85,567 hrs · 17,651 cycles

L/H LOWER WING SKIN AT AFT OUTBOARD CORNER OF THE #12 SLAT TRACK CUTOUT HAS A .300 IN. CRACK. (MARKED) REPLACED NOTED SLAT TRACK CUTOUT PER SRM 57-40-02-2R REPAIR 7 FIG 201 SHT 1.

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1219 (C12- C13) PUNCTURED IN SEVERAL AREAS REPAIRED FLOOR BOARD 263BF ON CENTERLINE, STA 1162, 1166, 1205, 1210, 1239, & 1254 PER SRM 53-00-50-2R FIG 206 REPAIR 2 SH 1

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1350 (C14) PUNCTURED IN SEVERAL AREAS REPAIRED FLOOR BOARD 263EF ON CENTERLINE AT STA 1331, 1337, & 1387 PER SRM 53-00-50- 2R FIG 206 REPAIR 2 SH 1

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1840 (13C) PUNCTURED IN SEVERAL AREAS (MARKED) REPAIRED FLOOR BOARD 293JF ON CENTERLINE AT STA 1836 & 1852 PER SRM 53-00-50-2R FIG 206 REPAIR 2 SH 1

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN DECK FLOOR PANEL AT CNTR AISLE APPROX STA 1140/6-0 (9C-10C) PUNCTURED IN SEVERAL AREAS (MARKED) REPAIRED FLOOR BOARD 253HF ALONG CENTERLINE AT STA-1101, STA-1130, STA-1135, STA-1164, STA-1178, REF SRM 53-00-50-2R, FIG-206, REPAIR-2, SH-1.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN DECK FLOOR PANEL AT CNTR AISLE APPROX STA 1199 (11C) PUNCTURED IN SEVERAL AREAS (MARKED) REPAIRED FLOOR BOARD 252 SF ON CENTERLINE AND STA 6-91, 6-93, 6-95, & 1151 PER SRM 53- 00-50-2R

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1299 PUNCTURED IN SEVERAL AREAS REPAIRED FLOOR BOARD 263BF ON CENTERLINE, STA 1288 PER SRM 53-00-50-2R FIG 206 REPAIR 2 SH 1

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1630 PUNCTURED (MARKED) REPAIRED FLOOR BOARD 283BF ON CENTERLINE AT STA 1605, 1608, 1632, 1635, 1640, 1643 PER SRM 53-00-50-2R SIG 206 REPAIR 2 SHT 1.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN DECK FLOOR PANEL AT CNTR AISLE APPROX STA 730 (5C) PUNCTURED IN SEVERAL AREAS (MARKED) REPAIRED FLOOR PANEL 245BF ALONG CENTERLINE AT STA-794, STA-796, STA-837, STA-849, STA-878, STA-883 REF SRM-53-00-50-2R, FIG-206, REPAIR-2, SH-1.

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

MAIN CARGO FLOOR BOARD AT CNTR AISLE APPROX STA 1430 (C15- C17) PUNCTURED IN SEVERAL AREAS REPAIRED FLOOR BOARD 273 EF ON CENTERLINE AT STA 1384, 1410, 1412, 1427, 1456, 1464 PER SRM 53-00-50-2R FIG 206 REPAIR 2 SH 1

Part: SKIN — CRACKED (RT WING) · airframe 85,567 hrs · 17,651 cycles

R/H LOWER WING SKIN AT AFT INBOARD CORNER OF THE #10 SLAT TRACK CUTOUT HAS A .250 IN. CRACK. (MARKED) INSTALLED DOUBLER REPAIRED PER SRM 57-40-02 FIG 201

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 85,567 hrs · 17,651 cycles

FLOOR PANEL # 231HF APRX STA 615 TO 675, SHOW 1/2 IN HOLE PUNCHED TO PANEL AND MUNEROUS WORN SPOTS SURFACE. REPAIRED FLOOR PANEL 231 HF AT LBL 76 STA 620 PER SRM 53-00-50-2R FIG 206 REPAIR 2 SH 1

Part: SKIN — CRACKED (RT WING) · airframe 85,567 hrs · 17,651 cycles

R/H LOWER WING SKIN AT AFT OUTBOARD CORNER OF THE #15 SLAT TRACK CUTOUT HAS A .750 IN. CRACK. (MARKED) INSTALLED DOUBLER REPAIR PER SRM 57-40-02

Part: SKIN — CRACKED (RAM AIR DOOR) · airframe 85,567 hrs · 17,651 cycles

FUSELAGE L/H:AFT RAM AIR DOOR CRACKED AT UPPER AFT CORNER MARKED RED. REPAIRED PER SRM 53-20-15-2R FIG 201 REPAIR # 3

Part: SKIN — CORRODED (BS 2140-2163) · corrosion level 2 · airframe 84,751 hrs · 17,373 cycles

AFT ACCESSORY COMPARTMENT HAS CORROSION ON R/H SIDE WALL REPAIR IN REF. TO MD-11 SRM 53-70-01-2R; FIG. 201.

Part: FUSE — LEAKING (LANDING GEAR) · airframe 83,173 hrs · 16,928 cycles

HYD 3 FAIL, RESERVOIR HYD AUANITY 0.0. UPON INITIAL CONFIGURATION CHECK. RNR'D TRIM CYL INTERLOCK FUSE MM 32-37-06-4. SERVICED NR 3 HYD SYS MM 12-13-02-3, BLED HYD SYS MM 29-03-00-2. BLED INTERLOCK FUSE MM 32-37-06-4 AND ADJ/TEST TRUCK BEAM TRIM INTERLOCK CYL MM 32-37-00-5 - OPS CK NML. NO LEAKS NOTED. ENG RUN PER JRH WITH FULL FLIGHT CONTROL ROLL OUT-NO ANOMOLIES NOTED. A/C OK FOR SERVICE

Part: TRANSPONDER — INOPERATIVE (NR 1) · airframe 82,392 hrs · 16,697 cycles

AT 1 30 HRS INTO FLIGHT, RECEIVER LEVEL 1 TRANSPONDER 1 FAIL. SWITCHED TO TRANS 2 AND RECEIVED TRNSP 2 FAIL. BOTH TRANSPS INTERMITTENTLY FAILED REMAINING FLIGHT. TRANSPORTER 1 REPLACED SYSTEM 1 AND 2 FIM TASK 34-54-00-1, TEST OK. NO FAULTS REV NOV 1/2010. REPLACED AS PER AMM REMOVAL/ INSTALLATION TASK 34-54-01-000-811 REV 91.6, TEST PASSED. OK FOR SERVICE P/N 7517800-10400 S/N OUT 99082485 S/N INXSE09117.

Part: TRANSPONDER — FAILED (VOR) · airframe 82,392 hrs · 16,697 cycles

PDIS 594 34-54 1175 25NOV18 ATH FACT U LOGPAGES:3042743 AT 1 30 HRS INTO FLIGHT RECIEVER LEVEL 1 TRANSPORNDER 1 FAIL.SWITCHED TO TRANS 2 AND RECIEVED TRNSP 2 FAIL.BOTH TRANSPS INTERMITENTLY FAILED REMAINING FLIGHT . FACT 25NOV18 10:37 ATH U TRANSPORTER 1 REPLACED SYSTEM 1 AND 2 FIM TASK 34-54-00-1 TEST O.K NO FAULTS REV NOV 1/2010 INFO SEE LIG 3042746

Part: SUPPORT — CORRODED (LT WING) · airframe 81,531 hrs · 16,445 cycles

LT WING MLG SUPPORT ASSY P/N ARB7118 UPPER PAD HAS PITTING CORROSION. REMOVED CORROSION PER SRM 57-20-14-2R REPAIR 4(B).

Part: SUPPORT — CORRODED (LT MLG) · airframe 84,061 hrs · 17,183 cycles

LT WING MLG SUPPORT ASSY P/N ARB7118 LOWER PAD HAS PITTING CORROSION. REMOVED CORROSION PER SRM 57-20-14-2R REPAIR 4(B).

Part: SUPPORT — CORRODED (LT WING) · airframe 81,531 hrs · 16,445 cycles

LT WING MLG SUPPORT ASSY P/N ARB7118 LOWER PAD HAS PITTING CORROSION. REMOVED CORROSION PER SRM 57-20-14-2R REPAIR 4(B).

Part: SUPPORT — CORRODED (LT MLG) · airframe 84,061 hrs · 17,183 cycles

LT WING MLG SUPPORT ASSY P/N ARB7118 UPPER PAD HAS PITTING CORROSION. REMOVED CORROSION PER SRM 57-20-14-2R REPAIR 4(B).

Part: SUPPORT — CORRODED (LT MLG) · airframe 84,061 hrs · 17,183 cycles

LT MLG RETRACT ACT. ATTACH SUPPORT (A) FRAME A/C ATTACH HOLES ARE CORODED REAMED TWO LOWER MOUNTING HOLES AND ONE UPPER FWD HOLE TO 1.064 DIA. REAMED ONE UPPER AFT MOUNTING HOLE TO 1.068 DIA. PER SRM 57-20-14-2R REPAIR 2.

Part: SUPPORT — CORRODED (LT MLG) · airframe 81,531 hrs · 16,445 cycles

LT MLG RETRACT ACT ATTACH SUPPORT (A) FRAME A/C ATTACH HOLES ARE CORRODED. REAMED TWO LOWER MOUNTING HOLES AND ONE UPPER FWD HOLE TO 1.064 DIA. REAMED 1 UPPER AFT MOUNTING HOLE TO 1.068 DIA PER SRM 57-20-14-2R REPAIR 2.

Part: FRAME — CORRODED (LT MLG) · airframe 81,531 hrs · 16,445 cycles

LEFT MLG 'A' FRAME HAS RUST BY TOP AFT MOUNT BOLT REMOVED AND REPLACED PER DWG.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 81,147 hrs · 16,326 cycles

2.5 HRS IN FLIGHT RECEIVED "HYD 2 OFF" ALERT. NR 2 PUMPS OFF, QTY AT 2.7 GAL ON APPROACH EXTENDING SLATS, HSC TURNED 3/2 RMP ON, PRESSURIZED HYD 2 SYS. ONCE FLAPS WERE EXTENDED NR 2 QTY WENT TO 2.0 GAL, RECEIVED "QTY 2 LO" ALERT, AND HYD 2 FAIL ALERT. FOUND LEAK ON NR 2 ENGINE UPPER HYDRAULIC MODULE. REPLACED O-RING SEAL ON HYD PRESS MODULE UNION TO LEFT HYD PUMP AND PRESS LINE FROM HYD PRESS MODULE TO LEFT PUMP (UPPER) PER MM 29-11-20-4-2 AND MM 29-12-30-2-1. RAN ENG PER JRH CHAPT-6. ALL CHECK GOOD.

Part: TIRE — FAILED (MLG) · airframe 80,538 hrs · 16,140 cycles

AFTER LANDING, RECEIVED A LEVEL 2 TIRE FAIL ALERT WITH TIRE NR 6 INDICATING ZERO PSI. RECEIVED A LEVEL 2 ANTI-SKID FAIL ALERT. THE BRAKE TEMP ALERT APPEARED LATER WITH BRAKE NR 6 INDICATING ABOUT 200-300 DEGREES COOLER THAN OTHER BRAKES. REMOVED AND REPLACED THE NR 6 TIRE ASSY. REMOVED AND REPLACED NR 5 TIRE ASSY DUE TO NR 6 TIRE FAILURE IAW AMM 32-41-01-4. FOUND 5 BRAKE LINES ON LH GEAR THAT WERE ROUTED TO THE INCORRECT SUPPLY LINE. REPOSITIONED THESE LINES TO THE CORRECT POSITION. OPS CHECKS NORMAL

Part: SKIN — CRACKED (RT WING) · airframe 80,454 hrs · 16,120 cycles

DURING ACCOMPLISHMENT OF HFEC INSPECTION ON RIGHT WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUTS AND ACCESS DOORS, FOUND ONE CRACK INDICATION, XOS 470 TAI DUCT CUTOUT CORNER NR 2 APPROXIMATELY .20 INCH IN LENGTH, REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1761-1781) · corrosion level 2 · airframe 80,454 hrs · 16,120 cycles

MAIN DECK CARGO TRACK FOUND CORRODED BETWEEN BS 1761 - 1781, LBL 8.5. THE CORROSION WAS REMOVED, AND FOUND TO OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE CARGO TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1641-1661) · corrosion level 2 · airframe 80,454 hrs · 16,120 cycles

MAIN DECK CARGO TRACK FOUND CORRODED BETWEEN BS 1641 - 1661, RBL 8.5. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE CARGO TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (BS 775) · airframe 80,454 hrs · 16,120 cycles

- MAIN DECK CARGO TRACK CROWN AREA FOUND DAMAGED AT BS 775, LBL 75.25. THE CARGO TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON — CORRODED (BS 1953) · corrosion level 2 · airframe 80,454 hrs · 16,120 cycles

LOWER AFT CARGO BAY, LONGERON 44R, BS 1953 FOUND CORRODED. REPAIRED THE LONGERON BETWEEN BS 1937 - 1972 IAW EA 1-5310-T0338480, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (BS 535) · airframe 80,454 hrs · 16,120 cycles

MAIN DECK CARGO FRAME REPAIR CHAFED AT BS 535, LONGERON 24L. THE REPAIR ANGLE WAS REMOVED IAW SRM 51-33-01-0G. A NEW REPAIR ANGLE WAS FABRICATED, AND INSTALLED IAW SRM 53-20-07-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (BS 535) · airframe 80,454 hrs · 16,120 cycles

MAIN DECK CARGO, FRAME REPAIR CHAFED AT BS 535, LONGERON 19L. THE REPAIR ANGLE WAS REMOVED IAW SRM 51-33-01-0G, AND A NEW REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,454 hrs · 16,120 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 702, FOUND CRACKED. REPAIRED PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,454 hrs · 16,120 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 760, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,454 hrs · 16,120 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 628, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,454 hrs · 16,120 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 698, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,454 hrs · 16,120 cycles

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

Part: DOUBLER — CRACKED (LT WING) · airframe 80,454 hrs · 16,120 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 882 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,454 hrs · 16,120 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 769, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1556) · corrosion level 2 · airframe 80,454 hrs · 16,120 cycles

MAIN DECK CARGO BAY, CORROSION FOUND ON THE SEAT TRACK BS 1556, LBL 8.5. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,454 hrs · 16,120 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 649, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,454 hrs · 16,120 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 652, FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,454 hrs · 16,120 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 612, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,454 hrs · 16,120 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 634, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1830-1850) · corrosion level 2 · airframe 80,454 hrs · 16,120 cycles

MAIN DECK CARGO, CORROSION ON THE SEAT TRACK AT BS 1850 - 1830, LBL 8.5. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6 -2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,454 hrs · 16,120 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 730, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: INDICATOR — FALSE INDICATION (MLG) · airframe 80,340 hrs · 16,074 cycles

DURING GEAR EXTENSION FOUR RED UNSAFE LIGHTS ON PRIMARY AND SECONDARY INDICATIONS. EXECUTED GO AROUND AND CONSULTED QRH. ALL FOUR GEAR DOWN AND LOCKED AFTER GEAR HANDLE MOVEMENT. TROUBLESHOT IAW FIM 32-30-05-01. ALL INDICATIONS NORMAL. NO DEFECTS FOUND. ACFT OK FOR SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 78,907 hrs · 15,639 cycles

DURING CRUISE, THE HYD 3 PRESSURE HIGH ALERT. HYD 3 OFF. TEMP WENT TO 120 DEGREE C AND PRESS TO 3720. THEN IN SERVICE QTY HYD 3 WENT TO O PSI. LEAK APPEARS TO BE FROM THE NR 3 HYD PRESSURE LINE FROM PYLON UNDER 617AB. REMOVED AND INSPECTED RT ENGINE CASE DRAIN FILTERS. NO DEBRIS NOTED. INSTALLED NEW FILTERS. NEEDS LEAK CHECK. IAW AMM 29-12-30-2-1. CHECKED THE NR 3 ENGINE CASE DRAIN FILTERS IAW AMM 29-12-42-6, AND LEAKED CHECKED IAW 29-00-00-6. NO LEAKS NOTED. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (L1 DOOR) · airframe 77,561 hrs · 15,235 cycles

ON PREFLIGHT, THE L1 SLIDE LIGHT IN DOOR WOULD NOT TEST. R & R L1 SLIDE REMOTE PRESSURE INDICATOR BATTERIES.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 76,742 hrs · 14,940 cycles

L1 DOOR ELECTRIC, SLIDE, CONTINUITY LIGHT INOPERATIVE. MEL 31AUG16 13:55, MEM U RELEASED FOR SERVICE IAW MEL: 25-61-02, CATEGORY: C, EXPIRATION : 10SEP16, MEL 25-61-02: L1, EVAC SLIDE REMOTE PRESSURE INDICATOR INOPERATIVE IAW MEL 25-61-02, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESSURE ADEQUATE ONCE EACH FLIGHT DAY. MEL 25-61-02, REQUIRES EVAC SLIDE SYS PRESSURE CHECK ONCE EACH FLIGHT DAY. L1 SYS PRESSURE VERIFIED IAW MEL 25-61-02. ACFT OK FOR SERVICE.

Part: PIN — SHEARED (NLG) · airframe 76,102 hrs · 14,716 cycles

AFTER EXITING RNWY, ATTEMPTED NORMAL 90 DEGREE LT TURN, CREW HEARD THUMP & LOST LT TURN AUTHORITY. INITIAL EVALUATION REVEALED BOLT & PIN ATTACHING LT STEERING ACTUATOR TO STEERING COLLAR TO BE MISSING. TOP HALF OF SHEARED BOLT & PIN WAS RECOVERED ON THE TAXIWAY BY THE PORT AUTHORITY. IDENTIFIED PARTS INSPECTED NOSE STRUT STEERING CYLINDERS AREA. STARTED NOSE GEAR LT STEERING CYLINDER REMOVAL IAW AMM 32-52-30-4 UP TO STEP C 8 WITH THE EXCEPTION OF STEP C 7 NLG SWIVEL GLAND REMOVAL. SWIVEL GLAND WAS NOT REMOVED JUST DISCONNECTED & CAPPED. UPON FURTHER INSPECTION FOUND NOSE GEAR LT GLIDESLOPE ANTENNA MOUNTING BRACKET DAMAGED. REMOVED SAME FOR REPLACEMENT IAW AMM 32-52-30-4. REPLACED LT NOSE STEERING COLLA

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 76,102 hrs · 14,716 cycles

L1 LIFE RAFT & SLIDE CIRCUIT CONTINUITY TEST LIGHT DOES NOT ILLUMINATE. RE-LAMPED L1 SLIDE PTT & LOW PRESS INDICATOR.

Part: STIFFENER — CRACKED (LT WING) · airframe 75,885 hrs · 14,628 cycles

AGEING ACFT, UPON REMOVAL OF STIFFENER AT LT WING LE STATION XOS 542, FOR ACCESS FOUND CRACKED. REFER SNRM N00744. R&R STIFFENER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (FUSELAGE) · airframe 75,886 hrs · 14,628 cycles

CABIN MAIN DECK CARGO COMPARTMENT, FRAME CHAFED AT RT STATION 535, LONGERON 24R. REPAIRED IAW SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (TE FLAP) · airframe 75,886 hrs · 14,628 cycles

AGEING ACFT, EXISTING REPAIR AT LT WING, INBD FLAP LOWER SEGMENT, UPPER SKIN STATION, XIFH 153.30 - XIFH 195.30. EXISTING REPAIR EVALUATED & FOUND REPAIR SKIN WITH NEW DAMAGE. REPAIR CARRIED OUT IAW SRM 57-00-01 REPAIR 2 FIG 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57507224 FOR WORK DETAILS.

Part: FRAME — CHAFED (FUSELAGE) · airframe 75,886 hrs · 14,628 cycles

CABIN MAIN DECK CARGO COMPARTMENT, FRAME CHAFED AT RT STATION 535, LONGERON 19R. REPAIRED IAW SRM 53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,886 hrs · 14,628 cycles

AGEING ACFT, EXISTING REPAIR AT FWD CARGO, FUSELAGE DOOR CUT OUT, FWD JAMB SKIN STATION 895.7, LONGERON 40RT - 41RT. EXISTING REPAIR EVALUATED & FOUND DAMAGED. REPAIR CARRIED OUT IAW EA 1-5330-T0324500A P 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53307226 FOR WORK DETAILS.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 75,886 hrs · 14,628 cycles

CABIN MAIN DECK CARGO COMPARTMENT. R3 DOOR FWD FUSELAGE JAMB LOWER WEB CRACKED AT RT STATION 1256, LONGERON 26R. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 75,886 hrs · 14,628 cycles

CABIN MAIN DECK CARGO COMPARTMENT. L3 DOOR FWD FUSELAGE JAMB, LOWER WEB CRACKED AT LT STATION 1256, LONGERON 26L. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 75,886 hrs · 14,628 cycles

CABIN MAIN DECK CARGO COMPARTMENT. L3 DOOR AFT FUSELAGE JAMB, LOWER WEB CRACKED AT LT STATION 1310, LONGERON 26L. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 75,886 hrs · 14,628 cycles

AGEING ACFT, EXISTING REPAIR AT MAIN DECK FRAME LT STATION 535, LONGERON -19 TO -21 AREA. EXISTING REPAIR EVALUATED & FOUND DAMAGED. REPAIR CARRIED OUT IAW SRM 53-20-07-2R FIG 202 REPAIR 1 EO 1-5100-7-5001 B6 PT 1. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,886 hrs · 14,628 cycles

AGEING ACFT, EXISTING REPAIR AT FWD CARGO FUSELAGE DOOR CUT OUT, AFT JAMB SKIN STATION 1002.3, LONGERON -40R TO -41R. EXISTING REPAIR AT FWD CARGO FUSELAGE DOOR CUT OUT, AFT JAMB SKIN EVALUATED & FOUND DAMAGED REPAIR CARRIED OUT AT FWD CARGO IAW EA -5330-T0324460 P 1. REPLACE DAMAGED REPAIR EO 1-5100-7-5001 B6 P T 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53307208 FOR WORK DETAILS.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 75,886 hrs · 14,628 cycles

CABIN MAIN DECK CARGO COMPARTMENT. R3 DOOR AFT FUSELAGE JAMB, LOWER WEB CRACKED AT RT STATION 1310, LONGERON 26R. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1741) · airframe 75,886 hrs · 14,628 cycles

MDCC SEAT TRACK CORRODED AT RT BS 1741, X=-8.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1741) · airframe 75,886 hrs · 14,628 cycles

MDCC FRAME DENTED AT RT BS 1741, LONGERON 12R. FRAME REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,886 hrs · 14,628 cycles

LEFT WING LE BEADED DOUBLER, AT XOS 653 - 658, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,886 hrs · 14,628 cycles

RIGHT WING LE BEADED DOUBLER, AT XOS 636 - 643, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 75,886 hrs · 14,628 cycles

NOSE LANDING GEAR, LT WEB TRUNNION FITTING HAS A SUSPECTED CRACK AT BS 583. REPAIRED IAW SRM 53-10-14-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,886 hrs · 14,628 cycles

RIGHT WING LE BEADED DOUBLER, AT XOS 625 - 629, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ACCESS DOOR — CRACKED (RT WING) · airframe 75,886 hrs · 14,628 cycles

HFEC INSPECTION CARRIED OUT ON RT WING LE & FOUND ONE EACH CRACK APPROXIMATELY 1.0 INCH INCH LENGTH, AT THE FWD INBD CORNER OF THE FUEL ACCESS DOOR, AT XOS 610.844. REPAIRED IAW SRM 57-40-01-2R FIG 201 REPAIR 18. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (BS 1009) · airframe 75,886 hrs · 14,628 cycles

CABIN MAIN DECK CARGO TRACK CROWN DAMAGED, AT LT BS 1009, X 27.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 75,886 hrs · 14,628 cycles

RIGHT WING LE FORMER, AT XOS 1025, FOUND CRACKED. FORMER REMOVED IAW SRM 51-31-01-0G & FABRICATED NEW FORMER IAW DWG ARB2920 REV BB. INSTALLED NEW FORMER IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,886 hrs · 14,628 cycles

LEFT WING LE BEADED DOUBLER, AT XOS 662 - 667, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (A/C PACK ACCESS) · airframe 743 hrs · 14,096 cycles

CRACK AT THE RIGHT PACK BAY ACCESS DOOR, UPPER AFT, FUSELAGE SKIN CUT OUT. COMPLIED WITH EA 1-5310-T0318923. RIGHT PACK DOOR, CORNER SKIN CRACKED. SEALED, PAINTED & INSTALLED PACK DOOR IAW SRM 51-21-02 & AMM 52-42-01-4.

Part: SKIN — CRACKED (A/C ACCESS DOOR) · airframe 743 hrs · 14,096 cycles

NR 3 PACK ACCESS DOOR OUTER SKIN CRACKED AT TOP EDGE. INSPECTED SUSPECT AREA IAW NTM 20-20-06, VERIFIED CRACK. CRACK EXTENDS PAST RIVET TOWARD THE AFT OF DOOR. REPAIRED CRACK IN AIR CONDITIONING COMPARTMENT DOOR SKIN IAW SRM 52-40-01-2R REPAIR 1 PAGE 1 - 10.

Part: HANDLE — DETACHED (L1 DOOR) · airframe 71,078 hrs · 13,151 cycles

L1 DOOR MANUAL LIFTING HANDLE IS DETACHED ON RT SIDE. REATTACHED L1 DOOR MANUAL LIFTING HANDLE IAW AMM 52-11-02-4. ACFT OK FOR SERVICE.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

RIGHT WING OTBD FLAP VANE HORN FITTING CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02 REPAIR 5 FIGURE 201 REVISION 55. REPAIRED IAW SRM 57-50-02 REPAIR 5 FIGURE 201 REVISION 55 AND EA 1-5750-T0307725 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

DURING ACCOMPLISHMENT OF FPI INSPECTION, RT INBD FLAP SIDE HINGE PIVOT FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03 REVISION 78. REPAIRED IAW CMM 57-52-03 REVISION 78 AND EA 1-5750-T0307723 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 70,942 hrs · 13,112 cycles

LEFT WING INBD FLAP UPPER SKIN CRACKED. REPAIRED AS PER EA 1-5750-T0307737 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: MOUNT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

RIGHT WING OTBD FLAP INBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307627 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: MOUNT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

LEFT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0307630 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: MOUNT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

LEFT WING OTBD FLAP OTBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0307630 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: MOUNT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

LEFT WING OTBD FLAP OTBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0307630 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: MOUNT — DAMAGED (LT WING TE FLAP) · airframe 70,942 hrs · 13,112 cycles

LEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR MOUNT OUT OF LIMITS AFTER BUSHING REMOVAL IAW CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307631 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: MOUNT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

LEFT WING OTBD FLAP OTBD FWD HINGE LOWER MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0307630 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: MOUNT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

LEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307631 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 121.

Part: MOUNT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

RIGHT WING OTBD FLAP INBD FWD HINGE ACTUATOR MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307627 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: BRACKET — DAMAGED (RT WING TE FLAP) · airframe 70,942 hrs · 13,112 cycles

RIGHT WING OTBD FLAP OTBD FWD HINGE ACTUATOR OTBD HOLE FOUND EXCEED LIMIT DURING BUSHING REMOVAL. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0307629 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: MOUNT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

RIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0307627 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: MOUNT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 70,942 hrs · 13,112 cycles

RIGHT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT CORRODED. MOUNT REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. NEW BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND E.A. 1-5750-T0307627 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 121.

Part: CARGO TRACK — CHAFED (BS 755) · airframe 70,942 hrs · 13,112 cycles

MAIN DECK CARGO TRACK FOUND INNER EDGE CROWN CHAFED AT BS 755, X = -8.5. REPAIRED BS 745-783, IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 69,969 hrs · 12,811 cycles

VERY RANCID ODORS EMANATING FROM A/C PACKS. INSPECTED SYS & FOUND ALL 3 COALESCER BAGS TO BE DIRTY. R & R THE COALESCER BAGS & OPERATIONS CHECKED OK. ACFT IS OK FOR CONTINUED SERVICE.

Part: SOCKET — MISINSTALLED (R1 DOOR SLIDE) · airframe 69,488 hrs · 12,643 cycles

ON POST FLIGHT CHECK, R1 DOOR EVACUATION SLIDE PTT LIGHT WILL NOT TEST. FOUND R1 DOOR SLIDE REMOTE PRESS TO TEST SOCKET CLOCKED IMPROPERLY. CLOCKED PER MM 25-61-04-4 AND OPS CHECKED GOOD IAW MM 25-61-04-5. OK FOR SERVICE.

Part: CONNECTOR — MISINSTALLED (DOOR SLIDE) · airframe 69,493 hrs · 12,644 cycles

ON POST FLIGHT, CHECK R1 DOOR EVAC SLIDE PTT LIGHT WILL NOT TEST. REPLACED LAMPED AND CHANGED BATTERIES, OPS CHECK STILL NO GOOD. FOUND R1 DOOR SLIDE REMOTE PRESS TO TEST SOCKET CLOCKED IMPROPERLY. CLOCKED IAW MM 25-61-04-4 AND OPS CHECKED GOOD IAW MM 25-61-04-5. OK FOR SERVICE.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 66,377 hrs · 11,697 cycles

CENTER CARGO DOOR FWD FRAME ADJACENT TO RUB PLATE, FOUND CRACKED. REPAIR ACCOMPLISHED IAW EA 1-5230-160969. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SUPPORT — CRACKED (LT WING ACCESS) · airframe 66,377 hrs · 11,697 cycles

LT WING LOWER L/E INBD OF ACCESS PANEL NR 526DB FWD SUPPORT AT STA XORS 799, FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-03, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: STRUCTURE — CRACKED (MLG WW) · airframe 66,377 hrs · 11,697 cycles

CENTER LANDING GEAR WHEEL WELL - INTERIOR RT SPLICE BEHIND TRUNNION FITTING, FOUND SUSPECTED CRACK. R & R IAW SRM 51-33-01, REV 49 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — CRACKED (LT WING) · airframe 66,377 hrs · 11,697 cycles

LT WING LOWER FIXED L/E AT NR 14 SLAT TRACK CUTOUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02, REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — CRACKED (ZONE 600) · airframe 66,377 hrs · 11,697 cycles

SKIN AROUND FASTENER HOLES HAVE CRACK INDICATIONS. FOUND DURING HFEC OPEN HOLE INSPECTION ON RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6. REPAIRED IAW EA 1-5710-160968, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — CRACKED (RT WING) · airframe 66,377 hrs · 11,697 cycles

RT WING LOWER FIXED L/E AT NR 11 SLAT TRACK CUTOUT FOUND CRACKED. CRACKED AREA AT RT WING LOWER FIXED L/E AT NR 11 SLAT TRACK CUTOUT REPAIRED IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 49, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: FLOOR SKIN — CRACKED (COCKPIT) · airframe 66,377 hrs · 11,697 cycles

FORWARD CABIN FLOOR WEB BELOW 1ST OBSERVER SEAT FOUND CRACKED. REPAIRED IAW SRM 53-10-51, FIG 201. REPAIR 1 REV 49, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — CRACKED (LT WING) · airframe 66,377 hrs · 11,697 cycles

SKIN AROUND FASTENER HOLES HAVE CRACK INDICATIONS. FOUND DURING HFEC OPEN HOLE INSPECTION ON LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6. REPAIRED IAW EA 1-5710-160967, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115

Part: CARGO TRACK — CRACKED (BS 635) · airframe 66,377 hrs · 11,697 cycles

FORWARD CARGO ABOVE CEILING SEAT TRACK AT STA 635, X=-27.5 FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 66,377 hrs · 11,697 cycles

FORWARD CARGO ABOVE CEILING SEAT TRACK AT STA 635, X=27.5 FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR GMM 6-2-100, REV 115.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 66,377 hrs · 11,697 cycles

FORWARD CARGO ABOVE CEILING SEAT TRACK AT STA.635, X=-8.5 FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR AS GMM 6-2-100, REV 115.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 66,377 hrs · 11,697 cycles

FORWARD CARGO ABOVE CEILING SEAT TRACK AT STA.635, X=-47.5 FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR AS GMM 6-2-100, REV 115.

Part: SKIN — CRACKED (RT WING) · airframe 66,377 hrs · 11,697 cycles

RT WING LOWER FIXED L/E AT NR 14 SLAT TRACK CUTOUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02, REPAIR 7, FIG 201, REV 49, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — CRACKED (RT WING) · airframe 66,377 hrs · 11,697 cycles

RT WING LOWER FIXED L/E AT NR 12 SLAT TRACK CUTOUT FOUND CRACKED. CRACKED AREA AT RT WING LOWER FIXED L/E AT NR 12 SLAT TRACK CUTOUT REPAIRED IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 49, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — CRACKED (LT WING) · airframe 66,377 hrs · 11,697 cycles

LT WING LOWER FIXED L/E AT NR 16 SLAT TRACK CUTOUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: FLOOR SUPPORT — CORRODED (BS 421) · airframe 66,377 hrs · 11,697 cycles

FWD CABIN -STA 421, X=70 (APPROX) ON REMOVAL OF FLOOR PANEL NR 221GF, FOUND FLOOR SUPPORT CORRODED AND CRACKED. REMOVED IAW SRM 51-31-01, REV 49. NEW FLOOR SUPPORT FABRICATED IAW DWG ABA8303, REV A . FLOOR SUPPORT INSTALLED IAW AMM 20-50-02, REV 72.0. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SEAT TRACK — CORRODED (BS 455) · airframe 66,377 hrs · 11,697 cycles

ADJACENT TO L1 DOOR SILL PLATE , CURVE SEAT TRACK, BS 455 FOUND CORRODED. REPAIRED IAW EA 1-5310-160963 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 66,377 hrs · 11,697 cycles

FORWARD CARGO ABOVE CEILING SEAT TRACK AT BS 635, X=47.5 FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: FLOOR SUPPORT — CRACKED (BS 415) · airframe 66,377 hrs · 11,697 cycles

FORWARD CABIN - DURING COURIER MODULE REMOVAL, BS Y 415 - X 19 FLOOR SUPPORT FOUND CRACKED. REMOVED AND INSTALLED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: INDICATOR — INOPERATIVE (ESCAPE SLIDE) · airframe 66,340 hrs · 11,691 cycles

RT PASSENGER DOOR PUSH TO TEST "SLIDE LIGHT" WILL NOT ILLUMINATE WHEN PUSHED. REPLACED R1 DOOR INDICATOR ASSY IAW MM 25-61-04-4. OPS CHECK ED OK.

Part: BATTERY PACK — INOPERATIVE (LIGHT PTT) · airframe 65,548 hrs · 11,480 cycles

R1 DOOR, EVAC SLIDE REMOTE PRESSURE PRESS TO TEST LIGHT INOPERATIVE. R & R REMOTE PTT SWITCH BATTERIES IAW AMM 25-61-04-4-0. OPS CHECKED GOOD.

Part: INDICATION SYS — INOPERATIVE (R1 DOOR SLIDE) · airframe 65,193 hrs · 11,401 cycles

ON PRE-FLIGHT L1 DOOR SLIDE PRESS TO TEST INDICATION SYS INOPERATIVE. R & R L1 DOOR SLIDE REF MM 25-61-15-4. OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (L1 DOOR SLIDE) · airframe 65,178 hrs · 11,394 cycles

AFTER ACFT BLOCKED IN, FOUND L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYS INOPERATIVE. REPLACED BATTERIES ON L1 DOOR REMOTE. OPS CHECKED GOOD IAW AMM 25-61-04. OK FOR SERVICE

Part: ACCELEROMETER — MALFUNCTIONED (NR 1 ENGINE) · airframe 64,731 hrs · 11,289 cycles

REJECTED TAKE OFF, DUE TO NR1 ENGINE EVM COMPRESSO AMBER BOX ILLUMINATED AT APPROX 5.0 THEN EXTINGUISHED, FOLLOWED BY ILLUMINATION OF THE NR 1 ENGINE EVM TURBINE AMBER BOX AT APPROX 4.4. NO PHYSICAL VIBRATION. PER FIM 77-32 INSPECTED NR 1 ENG FOR DAMAGE. NO PROBLEMS FOUND, ALL CHECKED OK. SUSPECT BAD EVM BOX. R & R EVM COMPUTER PER MM 77-32-02-4-1 AND TESTED PER MM 77-32-02-5-1. NO FAULTS OCCURED. ACCOMPLISHED ENGINE VIBRATION SURVEY, ADJUSTMENT TESTED PER MM 71-00-00-5-1 & JRH AND FOUND AT GROUND IDLE INDICATION, COMPRESSOR 0.4, TURBINE 0.3, MPA SETTINGS TURBINE READS 0.5 & COMPRESSOR 0.2. WHEN RETARDING THROTTLES TO IDLE, BOTH TURBINE AND COMPRESSOR GO ANYWHERE FROM 0.0-3.4 UNITS. NO VIBRATION FELT DURING TEST. PERFORMED NR 1 ENGINE RUN PER JRH & EVM SHOWED COMPRESSOR 0.2, TURBINE 0.2 AT IDLE, COMPRESSOR 0.1, TURBINE 0.8 AT N2 80%. DURING ADVANCEMENT OF THROTTLE, TURBINE MOMENTARY SHOWED 2.3 AT N2 75%. CHECKED WIRING WITH WIRE SHAKE, ENGINE SIDE BETWEEN P1-8163 & R5-1091A IAW WDM 77-32-01, FOUND NORMAL & NO SHORTED TO GROUND. R & R CORE VIBRATION ACCELEROMETER PER MM 77-32-03-4. RAN EVM R-T-S TEST IAW MM 77-32-02-5 & TEST PASSED. RAN NR 1 ENGINE AT IDLE & N2 80%. EVM SHOWED COMPRESSOR 0.2, TURBINE 0.3 AT IDLE & COMPRESSOR 0.3, TURBINE 0.5 AT N2 80%.

Part: WIRE — SHORTED (E/E BAY FAN) · airframe 63,998 hrs · 11,098 cycles

AVIONICS RACK FAN "2" POPPED. REF TO ORIGNAL WRI 46-00/0454. FOUND WIRE B115-280-14B SPLICE SHORTED TO ACCESS PANEL UNDER FIRST OBSERVER TABLE. INSPECTED ALL OTHER WIRES ON SAME BUNDLE REF AMM 20-30-00 AND FOUND NO OTHER DEFECTS. RE-SPLICED WIRE B115-280-14B REF WDM 21-26-02. AVIONICS RACK FAN 2 CIRCUIT BREAKER STAYS CLOSED AND OPS CHECKS NORMAL REF AMM 21-26-02-2-2.

Part: UNKNOWN — SPARKS (COCKPIT) · airframe 63,998 hrs · 11,098 cycles

ON LANDING ROLLOUT, HEARD NOISES AND SAW SPARKS COMING FROM BELOW DESK AT FIRST OBSERVERS SEAT. SPARKS CEASED ALMOST IMMEDIATELY WITH LITTLE SMOKE. SPARKS AND SMOKE ARE ADDRESSED IN WRI 21-26/0458.

Part: ENGINE — FAILED (NR 1) · airframe 61,779 hrs · 10,555 cycles

CLIMBING OUT OF 7000, NR1 ENG FAILED WITH A FIRE INDICATION. QRH PROCEDURES, SHOT BOTH BOTTLES, FIRE INDICATION REMAINED. N1, N2, NEAR ZERO. R&R NR 1 ENG IAW WORK CARDS. REF WORK CARDS, OK FOR SERVICE.

Part: FRAME — CHAFED (BS 535) · airframe 60,831 hrs · 10,312 cycles

MAIN DECK CARGO LT UPPER AND LOWER SUPPORT YOKE AREA FRAME FOUND CHAFED. FRAME REPAIRED AS PER DWG SG10530002 REV 0 NEW. REFER TO SNRM N00199 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 60,831 hrs · 10,312 cycles

RT WING INBD FLAP OTBD LOWER SURFACE FOUND WITH DENTS AT STA XIFH 293.910 TO XIFH 299.680. REPAIR CARRIED OUT AT RT WING INBOARD FLAP OUTBOARD LOWER SEGMENT AS PER SRM 57-50-01 FIG 201 REV 43. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 110.

Part: FRAME — MISREPAIRED (BS 535) · airframe 60,831 hrs · 10,312 cycles

MAIN DECK FRAME STA535 LH, 9G NET SUPPORT YOKE. EXISTING REPAIR AT MAIN DECK FRAME STA 535 LT, 9G NET SUPPORT YOKE EVALUATED AND FOUND FEDEX DRAWING SRZ-53-503 REV A BUT NOT EFFECTIVE TO MD11 ACFT. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED AS PER REPAIR DRAWING SG10530002 REV - (NEW). EO 1-5100-7-5001A4-PT1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 110.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 60,831 hrs · 10,312 cycles

PATCH REPAIR FOUND AT RT WING INBOARD FLAP LOWER SEGMENT LOWER SKIN STA XIFH 172. EXISTING PATCH REPAIR AT RIGHT HAND WING INBOARD FLAP LOWER SEGMENT LOWER SKIN STA XIFH 172 EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. RT WING INBOARD FLAP LOWER SEGMENT LOWER SKIN STA XIFH 172 REPAIRED IAW SRM 57-00-00 FIGURE 205 REPAIR GENERAL REVISION 43. E.O. 5100-7-5001 A4 PART 1, REPAIR CLASSIFIED AS MAJOR PER MM 6-2-100 REVISION 110.

Part: LONGERON — DAMAGED (BS 535 L25L) · airframe 60,831 hrs · 10,312 cycles

MAIN DECK CARGO STATION 535 LONGERON 25L STRINGER FOUND DAMAGED. DAMAGED LONGERON AT MAIN DECK CARGO STATION 535 LONGERON 25L REMOVED AND REPLACED WITH NEW FABRICATED LONGERON AS PER DWG ACA3017 REV L AND INSTALLED AS PER SRM 51-31-01 REV 43. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 100.

Part: SKIN — MISREPAIRED (BS 383-399) · airframe 60,831 hrs · 10,312 cycles

LEFT FUSELAGE SKIN BS 383-399 BETWEEN L25-27L. EXISTING REPAIR EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR. NEW REPAIR CARRIED OUT IAW SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 43 AND REPAIR BUSHING INSTALLED AS PER SRM 51-73-00 FIGURE 1 REVISION 43. EO 1-5100-7-5001 A4 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 110.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 60,831 hrs · 10,312 cycles

DELAMINATION - LT WING INBD FLAP VANE LOWER SURFACE. REMOVED AND REPLACED AS PER AMM 27-50-22 REV 66 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-830-801 REV 66.

Part: TRANSDUCER — FAILED (WHEEL SPEED) · airframe 56,582 hrs · 9,356 cycles

PRIOR TO 100 KTS, VERY LOUD AURAL TONE OVERPOWERED RADIO XMSNS & TIRE FAILURE WARNINGS. REJECTED TAKEOFF. CKD ACFT, FOUND SHREDDED CENTER MLG TIRE & HYD FLUID LEAKING. STATUS INDICATED ANTI-SKID FAULT. FOUND NR 9 TIRE BLOWN. NR 9 & 10 BRAKES DAMAGED. NR 9 HUB CAP BROKEN. NR 10 FWD BRAKE LINE FITTING PULLED OUT. ASCU SHOWS IN CURRENT FAULTS NR 9 WHEEL NOT TURNING. CLEARED MESSAGE. REPLACED TIRES & BRAKES, BRAKE TEMP SENSOR, HUB CAP & WHEEL SPEED XDUCER, ASCU & CENTER GEAR A/S CONTROL VALVES. REPAIRED BRAKE LINE FITTING. INSPECT CENTER AXELS OK. CENTER ANTI-SKID WIRING CKS OK. RETORQUED TRUNNION BOLTS, PERFORMED WHEEL SPEED TEST, HI DRAG LOAD SIDE LOAD INSP & CENTER MLG RETRACT TEST, ALL OK. ACFT RTS.

Part: SPAR — CRACKED (ZONE 600) · airframe 55,178 hrs · 9,009 cycles

RIGHT WING, TRAILING EDGE REAR SPAR AT STA XORS = 197.20 LANDING GEAR BRACE SUPPORT ROD LOWER FITTING 02 EACH CRACK FOUND NEAR FASTENER. RIGHT WING TRAILING EDGE REAR SPAR AT STA XORS = 197.20 LANDING GEAR BRACE SUPPORT ROD LOWER FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II, AND FUEL LEAK CHECK CARRIED OUT AS PER AMM 12-11-04 AND FOUND SATISFACTORY.

Part: FRAME — DAMAGED (ZONE 200) · airframe 55,178 hrs · 9,009 cycles

MAIN DECK CARGO AT STA 1661 JUST BELOW LONGERON 12 RIGHT HAND FRAME FOUND DAMAGED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTION AT EVERY 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 100) · airframe 55,178 hrs · 9,009 cycles

FUSELAGE EXTERIOR FOUND FORWARD CARGO DOOR CUTOUT FORWARD LOWER EDGE CHIPPED. CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 7 VOLUME I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-20-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 55,178 hrs · 9,009 cycles

WASTE COMPARTMENT, AT ABOUT STA 1986 LONGERON 48 LEFT SPLICE FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 100) · airframe 55,178 hrs · 9,009 cycles

FUSELAGE EXTERIOR FOUND FORWARD CARGO DOOR CUTOUT AFT LOWER EDGE CHIPPED. CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 7 VOLUME I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FRAME — DAMAGED (ZONE 200) · airframe 55,178 hrs · 9,009 cycles

MAIN DECK CARGO AT STA 1701 JUST BELOW LONGERON 12 RT FRAME FOUND DAMAGED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INPSECTION REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 55,178 hrs · 9,009 cycles

LT WING INBOARD FLAP VANE INBOARD OF MID WAY TO TRAILING EDGE AREA FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,178 hrs · 9,009 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,178 hrs · 9,009 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, C AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 1 SUPPORT FITTING R & R AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,178 hrs · 9,009 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING R&R AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 55,178 hrs · 9,009 cycles

LT WING - LEADING EDGE AT SLAT NR 3, NR 8 TRACK AREA, 01 EA EDGE CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 55,178 hrs · 9,009 cycles

RT WING INBOARD FLAP VANE LOWER SURFACE INBOARD OF MID WAY TO LEADING EDGE AREA FOUND DELAMINATED. REPAIRED IAW EA 1-5750-124362, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,178 hrs · 9,009 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A AND B. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 2 SUPPORT FITTING R & R AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,178 hrs · 9,009 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION, ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,178 hrs · 9,009 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,178 hrs · 9,009 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NO.4 SUPPORT FITTING AT HOLES A, C AND D.

Part: LANDING GEAR — MALFUNCTIONED · airframe 54,187 hrs · 8,801 cycles

AFTER TAKEOFF RIGHT MAIN LANDING GEAR INDICATED UNSAFE AFTER RETRACTION ON BOTH THE LANDING GEAR INDICATOR AND ON THE SYNOPTIC DISPLAY. COMPLIED WITH QRH WHICH CALLED FOR ONE RECYCLING OF THE LANDING GEAR. IT WAS SUCCESSFUL ,

Part: SKIN — PUNCTURED (ZONE 500) · airframe 50,115 hrs · 7,893 cycles

LT WING I/B FLAP LOWER SEGMENT UPPER SKIN FOUND PUNCTURED. LT WING I/B FLAP LOWER SEGMENT REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 35, VOL I AND FEDEX EA 1-5750-106610, WINGS TRAILING EDGE AND TRAILING EDGE DEVICES, LT INBD FLAP UPPER SKIN REPAIR. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 50,115 hrs · 7,893 cycles

MAIN DECK CARGO, FRAME FOUND DENT AT STA 1721 L12 LT. REPAIR CARRIED OUT AT MAIN DECK CARGO FRAME AT STA 1721 L12 LT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 50,115 hrs · 7,893 cycles

MAIN DECK CARGO FRAME, FOUND DENT AT STA 1661 L12 LT. REPAIR CARRIED OUT AT MAIN DECK CARGO FRAME AT STA 1661 L12 LT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 500) · airframe 50,115 hrs · 7,893 cycles

LT WING FIXED L/E COMPT FOUND TELESCOPING DUCT PASSAGE CUTOUT ON EXTERNAL UPPER SURFACE CORNER CRACKED. REPAIR CARRIED OUT ON PASSAGE CUTOUT EXTERNAL UPPER SURFACE CORNER OF THE LT WING FIXED L/E COMPT TELESCOPING DUCT AS PER SRM 57-10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOOR — CRACKED (ZONE 700) · airframe 50,115 hrs · 7,893 cycles

RIGHT MLG FLAPPER DOOR FWD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND MLG FLAPPER DOOR FWD CORNER AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 46,666 hrs · 7,112 cycles

CRUISE 340 ALL AI ON. AP AND AT DISCONNECTED, FOLLOWING ALERTS SEL ELEV MAN, SEL FLAP LIMIT OVERRIDE, IAS COMPL, WIND SHEAR DET FAIL, NO FD PITCH BAR. RAN AIRSPEED LOST. SUSPECT OR ERRATIC CK LIST, INDICATES NR 1 CADC PROBLEM. DIVERTED TO KSEA ON CADC 2. REPLACED NR 1 CADC PER AMM 34-16-01, OPS CHECKED PER AMM 34-16-01-5 ALL TESTS PASSED. A/C DOWN GRADED TO CHECK CAT 2. PREMATURE REMOVAL/INSTALLATION OFF MFG 4059060-901.

Part: VALVE — UNKNOWN (MLG) · airframe 45,989 hrs · 6,971 cycles

PDIS: HAD UNSAFE GEAR INDICATION ON ALL 4 GEAR ON BOTH PRIMARY AND SECONDARY INDICATORS. EXECUTED MISSED APPROACH AND COMPLIED W/QRH. GEAR RECYCLED ON OUTSIDE DOWNWIND IAW/QRH AND WE RECEIVED 4 DOWN AND LOCKED INDICATIONS ON PRIMARY AND SECONDARY INDICATORS. LANDED UNEVENTFULLY. JACKUP A/C. REPLACED LANDING GEAR SELECTOR VALVE AND HANDLE POSITION SWITCH H S1-431. PERFORMED LANDING GEAR EXTENSION/RETRACTION TEST IAW MM. RETURNED AIRCRAFT TO SERVICE.

Part: FIRE WARNING — FALSE INDICATION (NR 1 ENGINE) · airframe 45,870 hrs · 6,946 cycles

ON T/O GOT NR 1 ENG FIRE INDICATION. REJECTED 60KTS/FIRED NR 1 BOTTLE. INDICATION WENT OUT WHEN THROTTLES WERE RETARDED TO IDLE OPENED NR 1 ENG COWLING FOUND SEVERAL COUPLINGS MISSING FOIL. NR 1 FIRE BOTTLE REPLACED, SEE WRI 26-20/4535. FOUND SEVERAL CLAMPS SUSPECT FOWARD OF THE HP VALVE. SECURED SAME REF AMM 36-11-03-4. CHECKED OTHER PNEU DUCTS AND LINES FOR SECURITY. ALL SEEM IN GOOD CONDITION. REAPPLIED FOIL AROUND ALL PNEU DUCT CLAMPS AND CONNECTIONS. RAN NR 1 ENG AT POWER WITH NO FIRE WARNING, IAW JRH. AFTER RUN, OPENED NR 1 ENG COWL AND INSPECTED ENG. NO EVIDENCE OF OF DUCT LEAKS.

Part: SKIN — DAMAGED (ZONE 600) · airframe 44,798 hrs · 6,693 cycles

RIGHT WING UPPER SURFACE AFT OF NR 7 SLAT, 2 EACH LOCKBOLT HEAD FOUND FUEL LEAK, SKIN PLANK FOUND TO HAVE AN ELONGATED BORE. CARRIED OUT REPAIR AS PER FEDEX EA 1-5710-90018.

Part: BUSHING — WORN (ZONE 700) · airframe 44,798 hrs · 6,693 cycles

NOSE LANDING GEAR, GROUND SENSING CRANK ASSY, FOUND WITH PLAY. CARRIED OUT BUSHING REPAIR AS PER FEDEX EA 1-3220-90020.

Part: FITTING — CORRODED (ZONE 600) · airframe 44,798 hrs · 6,693 cycles

RIGHT WING, OUTBOARD FLAP INBOARD AFT HINGE FITTING AFT MOUNT AFT HOLE (FLAP SIDE) CORRODED. REMOVED AS PER EO 1-5750-7-5008.

Part: FITTING — CORRODED (ZONE 500) · airframe 44,798 hrs · 6,693 cycles

LEFT WING, OUTBOARD FLAP INBOARD AFT HINGE FITTING FORWARD MOUNT OUTBOARD AFT HOLE (FLAP SIDE) CORRODED. REMOVED AND REPLACED AS PER AMM 27- 50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-00.

Part: FITTING — CORRODED (ZONE 600) · airframe 44,798 hrs · 6,693 cycles

RIGHT WING, OUTBOARD FLAP INBOARD AFT HINGE FITTING OUTBOARD MOUNT HOLE (HINGE SIDE) CORRODED. CARRIED OUT BUSHING REPAIR AS PER FEDEX EA #1-5750- 90023.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,798 hrs · 6,693 cycles

CRACK INDICATION AT END OF STRINGER 10 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. CRACKED AREA REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 44,798 hrs · 6,693 cycles

CRACK INDICATION AT END OF STRINGER-13 WAS FOUND DURING HFEC INSPECTION AT RIGHT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIG 10, VOL I. NEW STRINGER CLIP FABRICATED AS PER FEDEX EA 1-5720-90027, THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 44,798 hrs · 6,693 cycles

CENTER CARGO, LONGERON SPLICE AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON-52 LEFT BRIM AREA FOUND CRACK. CRACK LONGERON SPLICE AT CENTER CARGO - LONGERON STATION 5-113 TO STATION 1541 LONGERON 52 REMOVED AND REPLACED WITH NEW LONGERON AS PER SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,798 hrs · 6,693 cycles

CRACK INDICATION AT END OF STRINGER-43 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,798 hrs · 6,693 cycles

CRACK INDICATION AT END OF STRINGER 14 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIGURE 10 VOLUME I. STRINGER REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 44,798 hrs · 6,693 cycles

CENTER CARGO, LONGERON SPLICE AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON -51 LT BRIM AREA FOUND CRACK. CRACK LONGERON SPLICE REMOVED AS PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 44,798 hrs · 6,693 cycles

CRACK INDICATION AT END OF STRINGER 09 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. REPAIR CARRIED OUT AT LT WING TANK AT STRINGER 9 AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIR ANLGES AS PER SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 44,798 hrs · 6,693 cycles

CRACK INDICATION AT END OF STRINGER-12 WAS FOUND DURING HFEC INSPECTION AT RIGHT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIG 10, VOL I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 44,798 hrs · 6,693 cycles

CRACK INDICATION AT END OF STRINGER-14 WAS FOUND DURING HFEC INSPECTION AT RIGHT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIG 10, VOL I. NEW STRINGER CLIP FABRICATED AS PER FEDEX EA 1-5720-90025, THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 44,798 hrs · 6,693 cycles

CENTER CARGO, LONGERON SPLICE AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON-49 RIGHT BRIM AREA FOUND CRACK. LONGERON SPLICE REMOVED AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON-49 RT AS PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 100) · airframe 44,798 hrs · 6,693 cycles

CENTER CARGO - LONGERON SPLICE ADJACENT TO STA 1541 L-40 LEFT HAND BRIM AREA FOUND CRACK. LONGERON SPLICE ADJACENT TO STA 1541 LLONGERON 40 LEFT HAND BRIM AREA REMOVED AS PER SRM 51-33-01 VOL II. NEW LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 100) · airframe 44,798 hrs · 6,693 cycles

CENTER CARGO - LONGERON SPLICE ADJACENT TO STA 1541 L-38 RIGHT BRIM AREA FOUND CRACK. STA 1541 LONGERON 38 RT CRACK LONGERON SPLICE REMOVED AS PER SRM 51-33-01 VOL II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CHIPPED (ZONE 100) · airframe 44,798 hrs · 6,693 cycles

CENTER CARGO - DOOR AFT CUTOUT EDGES EXTERIOR EXISTING REPAIR DOUBLER PATCH CHIPPED EDGES. DAMAGED EXISTING REPAIR DOUBLERS ON CENTER CARGO, DOOR AFT CUTOUT AREA REMOVED AS PER SRM 51-33-01 VOLUME II. AND NEW REPAIR DOUBLERS FABRICATED AS PER SRM 53-50- 00 FIGURE 16 VOLUME I. NEW REPAIR DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.

Part: FRAME — NICKED (ZONE 200) · airframe 44,798 hrs · 6,693 cycles

MAIN DECK - DVI CARRIED OUT ON INTERIOR FUSELAGE, NICK FOUND ON FRAME 535 LEFT HAND AT G-NET CAUSED BY SUPPORT YOKES. MAIN DECK STATION 535 LEFT HAND FRAME REPAIRED AS PER DWG SRZ-53-503. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 100) · airframe 44,798 hrs · 6,693 cycles

CENTER CARGO LONGERON SPLICE BRIM AREA SUSPECT CRACK AT STA 1541 ADJACENT TO LONGERON 37 RIGHT HAND. SPLICE REMOVED AS PER SRM 51-33-01 VOL II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 44,798 hrs · 6,693 cycles

CABIN - SEAT TRACK ADJACENT TO STA 635 X-11 LOWER FLANGE FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 100) · airframe 44,798 hrs · 6,693 cycles

CENTER CARGO LONGERON SPLICE FOUND CRACK AT STA 1541 L-32 LEFT HAND. NEW LONGERON SPLICE FABRICATED AS PER DRAWING A5A7112. CRACKED LONGERON SPLICE ON STA 1541 LONGERON 32 REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: ROD END — DAMAGED (ELEV FEEL ACT) · airframe 41,452 hrs · 5,947 cycles

ON T/O, THE ACFT ROTATED EXTREMELY SLOW DUE TO ABNORMALLY HEAVY NOSE. CONTACTED GOC TO VERIFY LOAD. AFTER DISCUSSION WITH MX IT WAS DETERMINED THAT PAST HISTORY OF JET SUGGESTED FLT CONTROL PROBLEM. EMERGENCY DECLARED, FUEL DUMPED TO LANDING WEIGHT, CONTROL CHECK ACCOMPLISHED. FOLLOWED BY AUTOLAND. REMOVED AND REPLACED THE DUPLEX ACT ROD END BOLT PER 27-32-01-4, CKD CLEARANCE OF THE ELEV LOAD FEEL ACT ROD END BOLT AND MECH IN ALL POS REF MD11MM 27-32-01-4. ALL CHK GOOD. ADJ THE AG CAM MARK WITH THE AH LEG PER MM 27-30-00-5 FOR THE BUS TUBE ASSY. RII C/W R/R FCC 1 AND FCC 2 PRECAUTIONARY. FCC RTS'S C/W. C/W THE CAT3B RTS. REF MD11 AMM 22-00-00-5.

Part: PNEUMATIC SYSTEM — MALFUNCTIONED (PNEUMATIC SYSTEM) · airframe 41,188 hrs · 5,885 cycles

ON CLIMB OUT FROM ZSPD GOT LEVEL 3 ALERT AIR MANF 2 FAIL. COMPLIED /W QRH, DUMPED FUEL, LANDED RJBB. ACN RELEASED FOR SERVICE IAW MEL/CDL: 36-10-02-A CATEGORY: C EXPIRATION: 03OCT04) MEL 36-10-02-A: PNEUMATIC SUPPLY SYS NR 2 INOPERATIVE.**** S/D COMING****

Part: FRAME — DENTED (ZONE 200) · airframe 40,324 hrs · 5,659 cycles

MAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1661 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I.

Part: FRAME — DENTED (ZONE 200) · airframe 40,324 hrs · 5,659 cycles

MAIN CABIN LT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1701 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR: 1-2520-7-3308 PART I.

Part: FRAME — DENTED (ZONE 200) · airframe 40,324 hrs · 5,659 cycles

MAIN CABIN LEFT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1741 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I.

Part: FRAME — DENTED (ZONE 200) · airframe 40,324 hrs · 5,659 cycles

MAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1681 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR: 1-2520-7-3308 PART I.

Part: FRAME — DENTED (ZONE 200) · airframe 40,324 hrs · 5,659 cycles

MAIN CABIN LT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1681 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I.

Part: FRAME — DENTED (ZONE 200) · airframe 40,324 hrs · 5,659 cycles

MAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1621 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 PG. 402-407 ORIG. DIAM.:1.187 FINAL DIAM.: 1.222. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76724 WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS =0.446, MATERIAL REMOVED =0.003, REMAINING THICKNESS =0.443, WITHIN LIMIT AS PER DWG NR ARC0503.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.220. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND LOWER MATING SURFACE CORRODED. SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS= 0.464, MATERIAL REMOVED= 0.031, REMAINING THICKNESS= 0.433. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.

Part: PRESSURE PANEL — CANNING (FUSELAGE) · airframe 40,324 hrs · 5,659 cycles

RIGHT HAND WHEEL WELL - OIL CANNING FOUND AT STA: Y= 1395-1401, Z= -90 TO -100, DEPTH= 0.0549 INCH Y= 1401-1411, Z= -90 TO -100, DEPTH= 0.0941 INCH Y= 1411-1421, Z= -90 TO -100, DEPTH= 0.0921 INCH Y= 1421-1431, Z= -90 TO -100, DEPTH= 0.0976 INCH Y= 1431-1441, Z= -70 TO -90, DEPTH= 0.1430 INCH. COMPLIED FEDEX EA 1-5310-76719, FUSELAGE - MAINFRAME - KEEL WEB / CENTER LANDING GEAR INSPECTION REQUIRMENTS, PART I.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.221. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 PG. 402-407. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.222, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76724 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER =1.188, FINAL DIAMETER =1.217. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76721, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS= 0.418, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.416. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER =1.188, FINAL DIAMETER =1.252. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76721, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS =0.426, MATERIAL REMOVED =0.002, REMAINING THICKNESS =0.424, WITHIN LIMIT AS PER DWG NR ARC0503.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG. 402-407. ORIG. THK.: 0.415, MATERIAL REMOVED: 0.004, REMAINING THK.: 0.411. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND LOWER MOUNT MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG. 402-404. ORIG. THK.: 0.514, MATERIAL REMOVED: 0.008, REMAINING THK.: 0.506. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PG. 402-407. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.221, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND OUTBOARD ACTUATOR HOLE OUTBOARD CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PG. 402-404. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.222, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.397, MATERIAL REMOVED: 0.002, REMAINING THK. OF LUG: 0.395. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.091. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.512, MATERIAL REMOVED= 0.003, REMAINING THICKNESS= 0.409. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.062, FINAL DIAM.: 1.093, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.402, MATERIAL REMOVED: 0.002, REMAINING THK.OF LUG: 0.400. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.508, MATERIAL REMOVED= 0.001, REMAINING THICKNESS= 0.507. COMPLIED WITH FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.092. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.503, MATERIAL REMOVED= 0.005, REMAINING THICKNESS= 0.498. COMPLIED WITH FEDEX EA #1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP AFT INBOARD HINGE FOUND OUTBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.510, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.508. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.492, MATERIAL REMOVED: 0.002, REMAINING THK.OF LUG: 0.490. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR. HOLE OUT SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.390, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.388. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.409, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.407. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.410, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.408. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG.THK. OF LUG: 0.504, MATERIAL REMOVED: 0.007, REMAINING THK.OF LUG: 0.497. REPAIR CARRIED - OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.403, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.401. COMPLIED WITH FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.125. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.507, MATERIAL REMOVED= 0.006, REMAINING THICKNESS= 0.501. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.093, FINAL DIAM.: 1.125, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.129. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.140. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RT WING - OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.400, MATERIAL REMOVED = 0.002, REMAINING THICKNESS= 0.398. COMPLIED WITH FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. DIA: 1.062, FINAL DIA: 1.191. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.094. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.506, MATERIAL REMOVED : 0.007, REMAINING THICKNESS OF LUG: 0.506. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LT WING OB FLAP AFT OB HINGE, FOUND OB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.062, FINAL DIAM.: 1.196, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LT WING - OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - L/H OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

LT WING OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.400, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.398. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR

Part: HINGE — CORRODED (T/E FLAP) · airframe 40,324 hrs · 5,659 cycles

RIGHT WING - INBOARD FLAP AFT OUTBOARD HINGE - FOUND INBOARD PIVOT BORE HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 - 443. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.252. COMPLIED WITH FEDEX EA 1-5750-76714, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBOARD FLAP HINGE BRACKET REPAIR.