N601FE

Part: NONE — NONE (ZONE 800) · airframe 88,676 hrs · 22,905 cycles

UPPER CARGO DOOR,FOUND DOOR SIDE HINGE PART NUMBER ACA7223-523 WITH 18 LOBES WORN. WORN 18 LOBES AT UPPER CARGO DOOR, DOOR SIDE HINGE PART NUMBER ACA7223-523 REWORKED AND FOUND #1 TO #7 LOBE HOLES EXCEED LIMIT AS PER MD-11 SRM 52-30-16-1A FIGURE 101 SHEET 3. OVERSIZE REPAIR BUSHINGS 18 EA FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 52-34-04 REPAIR - GENERAL. PARAGRAPH 2.Y AND E.A .#1-5230- T0365618 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 GMM 6-2-100.

Part: SKIN — CRACKED (200) · airframe 88,676 hrs · 22,905 cycles

MAIN DECK R3 DOOR CUTOUT FORWARD JAMB UPPER SKIN CRACKED AT STATION 1256.750 MAIN DECK AT R3 DOOR CUTOUT FORWARD JAMB CRACKED UPPER SKIN AT STATION 1256.750 REPAIRED AS PER E.A.#: 1-5310-T0365682 P1 , TITLE: FUSELAGE - MAINFRAME - CRACK REPAIR FOR R3 CENTER FUS PAX DOOR JAMB FWD INNER SKIN , STA 1250 - 1256 , L - 15R TO L - 16R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

AGING AIRCRAFT - EXISTING REPAIR AT FWD CARGO DOOR CUTOUT - AFT JAMB SKIN EXTERIOR STATION 1009, LONGERON 39 RIGHT HAND TO 41 RIGHT HAND. EXISTING REPAIR AT FWD CARGO DOOR CUTOUT - AFT JAMB SKIN EXTERIOR STATION 1009, LONGERON 39 RIGHT HAND TO 41 RIGHT HAND EVALUATED AND FOUND NOT REPAIRED IAW SRM 53-00-15-2R REPAIR 8 FIGURE 202. EO 1-5100-7-5001B6 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. EA # 1-5330-T0347600 B PART 4 TITLE : FUSELAGE - PLATES & SKINS - NEW FORWARD CARGO AFT JAMB REPAIR ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

AGING AIRCRAFT - EXISTING REPAIR AT RIGHT HAND WING INBOARD FLAP LOWER SURFACE INBOARD LOWER SEGMENT SKIN STATION XIFH 139. EXISTING REPAIR AT RIGHT HAND WING INBOARD FLAP LOWER SURFACE INBOARD LOWER SEGMENT SKIN STATION XIFH 139 EVALUATED AND FOUND NOT REPAIRED IAW SRM 57-00-00-2R FIGURE 205 REPAIR GENERAL. EA # 1-5750-T0365779 PART 1 TITLE : WING - FLIGHT SURFACES - REPAIR ON RH WING INBD FLAP AFT SEGMENT LOWER SKIN TEE, XIFH 133.9 TO XIFH 147.3 ACCOMPLISHED. EO 1-5100-7-5001B6 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: NONE — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

AGING AIRCRAFT - EXISTING REPAIR AT #1 LEFT PASSENGER DOOR SKIN UPPER AFT CORNER STATION 457. EXISTING REPAIR AT #1 LEFT PASSENGER DOOR SKIN UPPER AFT CORNER STATION 457 EVALUATED AND FOUND REPAIRED NOT IAW SRM 52-10-01-2R REPAIR 3 FIGURE 201. REPAIR CARRIED OUT AT # 1 LEFT PASSENGER DOOR SKIN UPPER AFT CORNER STATION 457 IAW SRM 52-10-01-2R REPAIR 3 FIGURE 201 AND EA # 1-5210-T0365775 PART 1 TITLE : DOORS - PASSENGER / CREW - REPAIR FOR LH N0 #1 FUSELAGE NOSE PASSENGER DOOR ASSY UPPER AFT CORNER. EO 1-5100-7-5001B6 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: NONE — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

LOWER CENTER CARGO COMPARTMENT DOORWAY DOOR CUT OUT STATION 1707, X= -52 FLANGE FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT DOORWAY DOOR CUT OUT CORROSION AT STATION 1707, X= -52 WORK COMPLIED AS PER EA # 1-5310-T0365753 P1 TITLE: FUSELAGE MAINFRAME Ï¿½ ALTERNATE EXTRUSION FOR LOCAL FABRICATION OF CENTER CARGO COMPARTMENT FORWARD JAMP FRAME INSTALLATION TEE PART NUMBER AFA7111-3. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: INTERCOSTAL — CORRODED (BS 426) · airframe 88,676 hrs · 22,905 cycles

AFT OF FORWARD AVIONICS COMPARTMENT 01 EACH INTERCOSTAL AT STATION 426.438 X=2.375 FOUND CORRODED. AFT OF FORWARD AVIONICS COMPARTMENT AT STATION 426.438 X=2.375 INTERCOSTAL CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CORRODED INTERCOSTAL REMOVED AND REPLACED WITH FABRICATED INTERCOSTAL AS PER SRM 51-31-01-0G. INTERCOSTAL FABRICATED AS PER DOUGLAS DRAWING ABA 8678 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: INTERCOSTAL — CORRODED (BS 426-438) · airframe 88,676 hrs · 22,905 cycles

CORROSION WAS FOUND ON THE INTERCOSTAL AFT OF THE FORWARD AVIONICS COMPARTMENT (FAC) STATION 426.438, X= -2.375. AFT OF FORWARD AVIONICS COMPARTMENT AT STATION 426.438 X=-2.375 INTERCOSTAL CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CORRODED INTERCOSTAL REMOVED AND REPLACED WITH FABRICATED INTERCOSTAL AS PER SRM 51-31-01-0G. INTERCOSTAL FABRICATED AS PER DOUGLAS DRAWING ABA 8678 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CRACKED (N/A) · airframe 88,676 hrs · 22,905 cycles

RIGHT WING - OUTER FLAP INBOARD HINGE TENSION STRAP AT STATION XORS 580 FOUND CRACK. CRACKED TENSION STRAP REMOVED AND REPLACED AT STATION XORS 580 AS PER SRM 51-33- 01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. FUEL LEAK CHECK CARRIED OUT AT RIGHT WING OUTBOARD FLAP INBOARD HINGE TENSION STRAP STATION XORS 580 FOUND SATISFACTORY AS PER AMM 12-11-04.

Part: BEAM — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LOWER CENTER CARGO COMPARTMENT STATION 1701, X = 24 FLOOR BEAM . EXISTING REPAIR AT LOWER CENTER CARGO COMPARTMENT STATION 1701, X = 24 FLOOR BEAM EVALUATED AND FOUND NOT REPAIRED IAW SRM 53-00-00-2R FIGURE 203. EXISTING FLOOR BEAM ASSEMBLY AFA0043-3 REMOVED AND REPLACED WITH REWORKED FLOOR BEAM ASSEMBLY IAW SRM 51-31-01-OG AND DOUGLAS DRAWING AFA0043 REVISION Y. EO 1-5100-7-5001B6 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: BEAM — CRACKED (N/A) · airframe 88,676 hrs · 22,905 cycles

LOWER CENTER CARGO COMPARTMENT STATION 1741, X=0 FLOOR BEAM FOUND WITH CRACK. LOWER CENTER CARGO COMPARTMENT STATION 1741, X=0 CRACKED FLOOR BEAM REPAIRED AS PER EA#1-5321-T0365615 PART 1. TITLE: FUSELAGE - CARGO COMP FLOORS - LOWER CENTER CARGO FLOOR BEAM REPAIR, STA 1741, BETWEEN X = 5.500 AND X = -5.500. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (N/A) · airframe 88,676 hrs · 22,905 cycles

LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 613 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 613 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 (N/A) · airframe 88,676 hrs · 22,905 cycles

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

Part: FLOOR SUPPORT — CORRODED (BS 1841) · airframe 88,676 hrs · 22,905 cycles

LOWER AFT CARGO COMPARTMENT STATION 1841, X= 18 WEB FLOOR SUPPORT FOUND WITH CORROSION. LOWER AFT CARGO COMPARTMENT STATION 1841 X= 18 WEB FLOOR SUPPORT CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 REPAIR GENERAL. CORRODED SUPPORT REMOVED AND REPLACED WITH REWORKED SUPPORT AS PER SRM 51- 31-01-0G SUPPORT REWORKED AS PER DOUGLAS DRAWING AGA7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (N/A) · airframe 88,676 hrs · 22,905 cycles

LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 655 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 647. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 647 EVALUATED AND FOUND DOUBLER CRACKED AND NOT REPAIRED PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CARRIED OUT AT LEADING EDGE BEADED DOUBLER STATION XOS 647 LEFT HAND AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO 1-5100-7-5001B6 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: NONE — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 637 . EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 637 EVALUATED AND FOUND DOUBLER CRACKED AND NOT REPAIRED PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CARRIED OUT AT LEADING EDGE BEADED DOUBLER STATION XOS 637 LEFT HAND AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO 1-5100-7-5001B6 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: NONE — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

AGING AIRCRAFT- EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 631. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 631 EVALUATED AND FOUND DOUBLER CRACKED AND NOT REPAIRED PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CARRIED OUT AT LEADING EDGE BEADED DOUBLER STATION XOS 631 LEFT HAND AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO 1-5100-7-5001B6 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: NONE — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

MAIN DECK #L3 PLUG DOOR AFT UPPER #1 BEAM FOUND CRACKED.

Part: TRACK — CRACKED (N/A) · airframe 88,676 hrs · 22,905 cycles

MAIN DECK SEAT TRACK AT STATION 755 X = - 8.5 FOUND CROWN CRACKED. MAIN DECK AT STATION 755 , X = - 8.5 CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES FROM STATION 745 TO STATION 785 X = - 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CRACKED (N/A) · airframe 88,676 hrs · 22,905 cycles

MAIN DECK SEAT TRACK AT STATION 629 , X = - 47.5 CROWN CRACKED. MAIN DECK AT STATION 629 , X = - 47.5 CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES FROM STATION 625 TO STATION 685 , X = - 47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 88,676 hrs · 22,905 cycles

AGING AIRCRAFT- EXISTING REPAIR AT LOWER AFT CARGO COMPARTMENT WEB STATION 1841, X=-10 AND X=-45. EXISTING REPAIR AT LOWER AFT CARGO COMPARTMENT WEB STATION 1841, X=-10 AND X=-45 EVALUATED AND FOUND NOT REPAIRED IAW SRM 53-00-00-2R FIGURE 211 REPAIR GENERAL. WEB REMOVED AND REPLACED WITH FABRICATED WEB AT STATION 1841 FROM X = 0 TO X = -50 IAW SRM 51-31-01-OG. WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REV R. EO 1-5100-7-5001B6 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: FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 88,073 hrs · 22,729 cycles

LH OB FLAP INBD HINGE FAIRING MOUNTING BOLT HOLES TO FLAP, 4 OF 6 SHOW SIGNS OF CORROSION. LH OB HINGE WAS REPAIRED PER MD11 CMM 57-50-04 AND EA 1-5750-T363229 LH OUTBOARD TRAILING EDGE HINGE SUPPORT FITTING-REPAIR OF CORROSION AT FLAP ATTACHMENT SURFACE AND BORES.

Part: GLAND NUT — LEAKING (HYD SYSTEM) · airframe 87,592 hrs · 22,573 cycles

HYD 3 OFF AT FL 340. FLUID AT 2.5 THEN DROP TO 2.1. HYD 3 FAIL CAME ON AFTER GEAR EXTENSION. FLUID DROP TO .9. FOLLOWED QRH FOR HYD 3 FAIL. RH MLG SWIVEL GLAND, AND MAIN LANDING GEAR RETRACT CYLINDER . OPS CK AND LEAK CK OK REF MD11 MM 32-33-21-4, MD11 MM 32-33-20-4.

Part: MANIFOLD — LEAKING (HYD SYSTEM) · airframe 85,963 hrs · 22,114 cycles

LEVEL 1 HYD 1 OFF 36 MINUTES INTO FLIGHT. HYD QUANTITY SHOWING 2.9 GALLONS IN FLIGHT. ON TAXI IN QTY GOT TO 1.2 GALLONS, BUT CAME BACK UP TO 2.7 ON CLEANUP. INSTALLED NR 1 ENG HYD MANIFOLD ASSY, PER AMM 29-12-30. OPS & LEAK CHECK GOOD. OK FOR SERVICE.

Part: SPROCKET — DAMAGED (N/A) · airframe 85,174 hrs · 21,893 cycles

FOUND RH THS DRIVE CHAIN OUTBOARD IDLER SPROCKET DAMAGED AND MISSING BEARING. FOUND DURING HORZ STAB LUBE R&R SPROCKET ASSEMBLY.

Part: SPROCKET — DAMAGED (HORIZ STAB) · airframe 85,174 hrs · 21,893 cycles

FOUND RT THS DRIVE CHAIN OUTBOARD IDLER SPROCKET DAMAGED AND MISSING BEARING, FOUND DURING HORZ STAB LUBE.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 83,730 hrs · 21,461 cycles

LANDING GEAR RIGHT HAND MAIN LANDING GEAR WHEEL WELL UNDERWING BARREL TORQUE BOX APPROXIMATELY STA 1441 FORWARD ANGLE STIFFENER FOUND CRACKED APPROXIMATELY 1" RIGHT HAND MAIN LANDING GEAR WHEEL WELL UNDERWING BARREL TORQUE BOX APPROXIMATELY STA 1441 FORWARD CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. STIFFENER PART NUMBER FXAEA7031-502 FABRICATED AS PER DOUGLAS DRAWING AEA7031 REV A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 83,730 hrs · 21,461 cycles

RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-07 AND E.A. # : 1-5750-T0321648 D PART 3 STEP 1A AND STEP 1C, TITLE : WING- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI. 57500939 FOR WORK DETAILS.

Part: HINGE — CORRODED (RT WING) · airframe 83,730 hrs · 21,461 cycles

RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD- 11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # : 1-5750-T0321648 D PART 3 STEP 1A AND STEP 1C, TITLE : WING- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI. 57500939 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 83,730 hrs · 21,461 cycles

LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-07 AND E.A. # : 1-5750-T0321647 F PART 3 STEP 1A AND STEP 1C, TITLE : WING- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI. 57500938 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 83,730 hrs · 21,461 cycles

LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORROSION. CORROSION AT LEFT HAND WING - INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD- 11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # : 1-5750-T0321647 F PART 3 STEP 1A AND STEP 1C, TITLE : WING- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI. 57500938 FOR WORK DETAILS.

Part: SKIN — CRACKED (ZONE 600) · airframe 83,730 hrs · 21,461 cycles

RIGHT HAND WING LEADING EDGE AT XOS 996 LOWER SKIN CRACKED RIGHT HAND WING LEADING EDGE AT XOS 996 LOWER SKIN CRACKED CARRIED OUT REPAIR AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 9 AND EA # 1-5730-T0350370 PART 1 "TITLE : WINGS - PLATES AND SKINS - RH WING FIXED L.E SKIN, CRACK REPAIR". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (ZONE 500) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT HAND WING - LEADING EDGE CUTOUT STRIP AT STA XOS = 909 FOUND CORROSION LEFT HAND WING - LEADING EDGE CUTOUT STRIP AT STA XOS = 909 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-40-02-2R FIGURE 201 REPAIR 12 AND REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R FIGURE 203 REPAIR 12 AT LEADING EDGE CUTOUT STRIP BETWEEN STA XOS = 899 TO STA XOS = 971. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (LT WING) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT HAND WING - LEADING EDGE CUTOUT STRIP AT STA XOS = 926 FOUND CORROSION LEFT HAND WING - LEADING EDGE CUTOUT STRIP AT STA XOS = 926 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-40-02-2R FIGURE 201 REPAIR 12 AND REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R FIGURE 203 REPAIR 12 AT LEADING EDGE CUTOUT STRIP BETWEEN STA XOS = 899 TO STA XOS = 971. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N00421 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 83,730 hrs · 21,461 cycles

RIGHT HAND WING LEADING EDGE AT XOS 996 LOWER ACCESS PANEL CUTOUT DOUBLER CRACKED RIGHT HAND WING LEADING EDGE AT XOS 996 LOWER ACCESS PANEL CUTOUT DOUBLER CRACKED CARRIED OUT REPAIR AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 9 AND EA # 1- 5730-T0350370 PART 1 "TITLE : WINGS - PLATES AND SKINS - RH WING FIXED L.E SKIN, CRACK REPAIR". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.REFER TO SNRM N01089 FOR WORK DETAILS.

Part: FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING E MOUNT HOLE FOUND WITH CORROSION RIGHT HAND OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. REFER SNRM N00592 FOR WORK DETAIL. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'B' MOUNT HOLE FOUND WITH CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'B' MOUNT HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER SRM 57- 20-02-2R REPAIR 5 FIGURE 201 AND E.A. # 1-5750-T0350242 PART 1 STEP 1A, TITLE : WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTINGS CORROSION REPAIR. AND INSTALLED AS PER AMM 27-50-32-400-801. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING C MOUNT HOLE FOUND WITH CORROSION RIGHT HAND OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. REFER SNRM N00592 FOR WORK DETAIL. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING B MOUNT HOLE FOUND WITH CORROSION RIGHT HAND OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. REFER SNRM N00592 FOR WORK DETAIL. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' MOUNT HOLE FOUND WITH CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' MOUNT HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER SRM 57- 20-02-2R REPAIR 5 FIGURE 201 AND E.A. # 1-5750-T0350242 PART 1 STEP 1A, TITLE : WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTINGS CORROSION REPAIR. AND INSTALLED AS PER AMM 27-50-32-400-801. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NO: N00845 ATTACHED E.A. # 1-5750-T0350242 PART 1 FOR WORK DETAILS.

Part: FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' MOUNT HOLE FOUND WITH CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' MOUNT HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER SRM 57- 20-02-2R REPAIR 5 FIGURE 201 AND E.A. # 1-5750-T0350242 PART 1 STEP 1A, TITLE : WINGS- FLIGHT SURFACES- LH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTINGS CORROSION REPAIR. AND INSTALLED AS PER AMM 27-50-32-400-801. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NO: N00845 ATTACHED E.A. # 1-5750-T0350242 PART 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE HAD CORROSION. CORROSION REWORKED AND FOUND TO EXCEED LIMITS. BASE THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAXIMUM REWORK LIMIT FOR BARREL NUT HOLE. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08 AND EA 1-5750-T0350113, PART 1, STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (BS 2122-2164) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

EMPENNAGE RIGHT UPPER FUSELAGE SKIN BS 2122 TO 2164, LONGERONS 33-35R, FOUND WITH SURFACE CORROSION. SURFACE CORROSION REMOVED IAW SRM 51-21-01-0G, AND FOUND OUT OF LIMITS IAW SRM 53-70-01-2R, FIGURE 201, REPAIR 3. REPAIRED IAW EA 1-5330-T0350371, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 1841) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LOWER AFT CARGO COMPARTMENT FORWARD BULKHEAD 'L' ANGLE FLOORBEAM FOUND CORRODED AT BS 1841. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-00-2R, FIGURE 205. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1581-1621) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORRODED, BS 1581 - 1621, LBL 8.5. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIG 101. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1571 TO 1631 IAW SRM 53-00-52-2, FIG 201 REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

CORROSION AT WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE NR 3 HOLE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 07. OVERSIZED REPAIR BUSHING FABRICATED AND INSTALLED CMM 57-44-07 AND EA 1-5750-T0321647 F PART 3 STEP 1A AND STEP 1C. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS CMM 57-44- 07. AN OVERSIZED REPAIR BUSHING WAS FABRICATED AND INSTALLED CMM 57-44-07 AND EA 1-5750-T0321648 D PART 3, STEP 1A, AND STEP 1C. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING OUTBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-04. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-04, AND EA 1-5750-76649 A, PART 2, STEP 2, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159802 G, PART 3, STEP 2A, AND STEP 2B. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159802 G, PART 3, STEP 2A, AND STEP 2B. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159801 H, PART 3, STEP 2A, AND STEP 2B. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING, INBOARD FLAP OUTBOARD AFTER HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159801 H, PART 3, STEP 2A, AND STEP 2B. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON — CORRODED (BS 1731) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 47 RIGHT FOUND CORROSION AT STATION 1731. CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 53- 00-00-2R, FIG 205. LONGERON 47 RIGHT AT STATION 1731 CARRIED OUT REPAIR AS PER SRM 53- 00-00-2R , REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (BS 1821) · airframe 83,730 hrs · 21,461 cycles

LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 43 RIGHT FOUND CRACK AT STATION 1821. REMOVED AND INSTALLED FABRICATED LONGERON FITTING AS PER SRM 51-31-01-OG. LONGERON FITTING FABRICATED AS PER DOUGLAS DRAWING AGA 7369 REVISION H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 83,730 hrs · 21,461 cycles

LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 51 RIGHT SPLICE FITTING CRACK AT BETWEEN STATION 5-113 TO 1541. LONGERON SPLICE REMOVED AND INSTALLED A FABRICATED SPLICE IAW SRM 51-33-01-OG. SPLICE FITTING FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 1701) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LOWER CENTER CARGO COMPARTMENT FLOOR BEAM FOUND WITH CORROSION AT STA 1701 X = -34. REPAIR CARRIED OUT AS PER SRM 53-50-51-2R FIGURE 201 REPAIR 1 AND EA # 1-5310- T0350373 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. LOWER CENTER CARGO COMPARTMENT FLOOR BEAM AT STA 1701 X = -34 CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205.

Part: LONGERON — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 44 RIGHT FOUND CORROSION AT STATION 1661 TO 1681. CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 205. LONGERON 44 RIGHT CORROSION AREA CARRIED OUT REPAIR AS PER EA 1-5310-T0350241 PART 1. CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BULKHEAD WEB — CRACKED (BS 1841) · airframe 83,730 hrs · 21,461 cycles

LOWER AFT CARGO COMPARTMENT BILGE AREA FORWARD BULKHEAD FOUND WEB SKIN PUNCTURED AT STA 1841 X = 17. REMOVED AS PER SRM 51-31-01-0G. NEW WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REV R AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED, AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750-T0350013 PART 1 STEP 1 . REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE BORE WAS CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT OUTBOARD HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08 AND EA 1-5750-T0350113, PART 1, STEP 1A, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,730 hrs · 21,461 cycles

LEFT WING BEADED DOUBLER AT XOS 692 FOUND CRACKED. THE DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORRODED BS 5-91, RBL 8.5. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101. THE SEAT TRACK WAS REPAIRED BY SECTIONAL AT EXISTING SPLICES BS 5-63 TO BS 1531, IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD ACTUATOR HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350048, PART 1, STEP 1B, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,730 hrs · 21,461 cycles

LEFT WING BEADED DOUBLER AT STA XOS 763 WAS FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE CORRODED. HOLE NR 3 BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD ACTUATOR HOLE BORE FOUND CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1D, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,730 hrs · 21,461 cycles

RIGHT WING BEADED DOUBLER AT STA XOS 564 WAS FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT OUTBOARD HOLE SURFACE CORRODED. SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD FWD MOUNT BORE WAS CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1B, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE CORRODED. THE NR 7 NUT HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044 PART 1 STEP 1. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350048, PART 1, STEP 1A, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 1581-1641) · airframe 83,730 hrs · 21,461 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK WAS FOUND CRACKED BETWEEN BS 1581 - 1641, RBL 8.5. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICE BS 1571 TO 1651 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED IAW MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT, OUTBOARD HOLE SURFACE CORRODED. OUTBOARD HOLE SURFACE REWORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORRODED. HOLE 4 BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44- 09, AND EA 1-5750-T0350044, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE, WING SIDE, LOWER MOUNT OUTBOARD HOLE SURFACE WAS CORRODED. HOLE SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1C, AND STEP 1. A REPAIR SHIM WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,730 hrs · 21,461 cycles

RIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 643 WAS FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE WAS CORRODED. THE CORROSION WAS REWORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1D, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT INBOARD HOLE SURFACE CORRODED. SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE), OUTBOARD FWD MOUNT HOLE BORE FOUND CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1B, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350048, PART 1, STEP 1B, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 83,730 hrs · 21,461 cycles

LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), UPPER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE, WING SIDE LOWER MOUNT INBOARD HOLE SURFACE CORRODED. HOLE SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1C, AND STEP 1. A REPAIR SHIM WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 675) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSION AT BS 675, RBL 100. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101 ALLOWABLE DAMAGE 1. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, REPAIR 5, FIGURE 201, AND EA 1-5310-T0350372, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT, OUTBOARD NR 3 HOLE BORE CORRODED. THE HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,730 hrs · 21,461 cycles

LEFT WING BEADED DOUBLER AT STA XOS 795 FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE CORRODED. NUT HOLE NR 7 BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 83,730 hrs · 21,461 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), UPPER MOUNT, OUTBOARD HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SCUFF PLATE — DAMAGED (FWD CARGO) · airframe 83,062 hrs · 21,248 cycles

SCUFF PLATE DAMAGED OF THE LOWER FWD CARGO DOOR REPAIRED DAMAGE IN ACCORDANCE WITH EA 1-5330-T0347600 A, PS P2.

Part: DUCT — DAMAGED (NR 3 MANIFOLD) · airframe 82,988 hrs · 21,232 cycles

#3 MANIFOLD FAILURE. SHGN 08JUN19 09:03 KIX INSTALLED NEW DUCT PER AMM 36-14-02-4 AND NO LEAK NOTED. ALSO #3 PNEUMATIC SYSTEM DECAY CHECK W/APU AIR SATISFACTORY PER MD11 JRH. MDC FLOOR BOARD AND SIDEWALL PANEL IN FWD CARGO COMPARTMENT BEING INSTALLED PER AMM 53-21-04-4,25-56-05-4. FACT 08JUN19 10:19 KIX INSTALLED FLOOR PANEL IN MDC AND SIDEWALL PANEL IN FWD CARGO PER AMM 25-56-05-4, 53-21-01-4,53-21-04-4. A/C OK FOR SERVICE.

Part: CABLE — SHORTED (FIRE DETECTION) · airframe 82,922 hrs · 21,211 cycles

PDIS 601 26-10 0334 17MAY19 MEM OPEN U LOGPAGES:2723226 LVL 3 ENG 2 FIRE LIGHT PASSING FL 290. NR 2 ENG. FIRE LOOP "A" DEFERRED. COMPLIED W/ QRH FOUND RIGID CABLE BETWEEN DH7 AND DH8 SHORTED, ALSO FOUND UPP TUR RIGHT A AND B RAIL ASSEMBLY BROKE IN HALF. R&R'D BOTH RIGID CABLES AND UPP TUR RIGHT A AND B RAIL ASSEMBLY REF AMM 26-11-03-4-4, OPS CHECKS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (TIRE) · airframe 82,340 hrs · 21,040 cycles

AFTER LEVEL OFF LEVEL 2 TIRE FAIL ALERT #6 TIRE. REMOVED & REPLACED #5 AND #6 MAIN TIRE WHEEL ASSY PER AMM 32-41-01-4 AND TIRE PRESS CHECK OK AND NO LEAKAGE. T/S PER FIM 32-40-23 AND 32-40-01, PERFORMED R-T-S FOR BTMTP MAINTENANCE MENU, ALL TEST PASSED AND NO EXISTING FAULT NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 81,474 hrs · 20,757 cycles

AFTER TAKE OFF WE RECEIVED LEVEL 1 BRAKE TEMP DIFF ALERT. BRAKE 2 INDICATED PEAK TEMP OF 503 DEGREES. ALL OTHER BRAKES WERE 150 DEGREES OR COOLER. REMOVED AND REPLACED BTMTPI IAW AMM 32-46-02-4 AS A PRECAUTION SINCE THERE IS HISTORY FOR OTHER BRAKE POSITIONS RUNNING HOT, AND MOST CURRENTLY NR 2 MLG BRAKE BEING HOT. OPS CHECK GOOD. ALL R-T-S TESTS PASSED AND ALL INDICATIONS ARE NORMAL.

Part: DETECTOR — MALFUNCTIONED (OVERHEAT SYS) · airframe 80,026 hrs · 20,295 cycles

LEVEL 3 IR MANIFOLD 2 FAIL IN FLIGHT. QRH COMPLIED WITH. RETURN TO DEPARTURE. BLR U NO CURRENT FAULT ON MFC. MFC FAULT REVIEW SHOWS MFC MON RLY. ESC LRU INOPERATIVE. RESET SHOWS PNEU MANIFOLD 2 FAIL. PERFORMED PNEU MANIFOLD 2 DECAY CHECK IAW AMM36-00-01. MANIFOLD 2 DECAY CHECKED GOOD. NO LEAK NOTED. IAW MOCC RAN THE NR 01 & 02 ENGINE AT 40 PERCENT POWER. COULD NOT DUPLICATE THE MANIFOLD FAILURE AT THIS TIME. ENGINE RUN PERFORMED IAW JRH. MFC RTS TEST CHECKED GOOD. REMOVED AND REPLACED MFC, ALL ZONE 11 AND ZONE 17 A AND ZONE 17 B OVERHEAT DETECTORS. PERFORMED MFC RTS TEST AS PER AMM 36-23-01-5.

Part: DUCT — LEAKING (NR 2 ENGINE) · airframe 79,759 hrs · 20,202 cycles

AT APPROXIMATELY 700 FT DURING FINAL, LEVEL 3 ENG 2 FIRE BELL AND WARNING STAYED ON FOR 3-4 SECONDS, THEN WENT OUT. MOVED THROTTLE TO IDLE AFTER SECOND WARNING AT 500FT. WARNING WENT OUT AGAIN. DECIDED TO LAND THE ACFT. IN THE FLARE, THE WARNING OCCURED A THIRD TIME. ROLLOUT NORMAL. AFTER LANDING COMPLETED PHASE 1 AND SHUTDOWN THE NR 2 ENGINE. BLEW THE NR 2 AGENT BOTTLE. NO FURTHER LIGHTS AND WARNINGS. COMPLETED INSTALLATION OF 14 STAGE MANIFOLD DUCTING AND TOLERANCE TAKE UP DUCT ASSY IAW AMM 36-14-03-4-1, WRAPPED DUCT BOSSES AND CLAMPS WITH FOIL AND PERFORMED A LEAK CHECK IAW AMM 36-14-03-5-1. GROUND RAN ENGINE IAW JRH, NO LEAKS, ALL PARAMETERS NORMAL, OK FOR SERVICE.

Part: CIRCUIT BREAKER — FAILED (ADG) · airframe 79,232 hrs · 20,008 cycles

DURING A TEST FLIGHT, DEPLOYED THE ADG FOR TESTING. THE ADG ELECTRIC SWITCH DID NOT CHARGE THE BATTERY, -40 AMPS DISCHARGE DURING ENTIRE TEST. BATTERY VOLTAGE DROPPED TO 27 VOLTS. LEAC AND REAC BUSSES WERE POWERED. THE ADG LEFT EMERGENCY AC BUSS, RCCB B1-1722 REMOVED AND REPLACED IAW AMM 24-50-01-4, AND WDM 24-61-11. GROUND TESTED THE ADG SYSTEM IAW AMM 24-25-00-700-802 AND FOUND SATISFACTORYWITH SMALLER BATTERY DISCHARGE AND POSITIVE CHARGING WAS AVAILABLE. ADG RESTORED IAW AMM 24-25-01-2.

Part: HINGE — WORN (FUSELAGE) · airframe 79,230 hrs · 20,007 cycles

MAIN DECK CARGO DOOR MOST FWD HINGE SECTION ON FUSELAGE SIDE FOUND FWD 12EA HINGE LOBE HOLES WORN EXCEED LIMITS. STA 635- STA 652 WORN EXCEED LIMIT AT MAIN DECK CARGO DOOR MOST FWD HINGE SECTION ON FUSELAGE SIDE FWD 12EA HINGE LOBE HOLES REWORKED. FOUND NR 1 TO NR 6 HOLES EXCEED LIMITS AS PER CMM 52-34-04. OVERSIZE BUSHINGS FABRICATED BY MACHINING AND INSTALLED AS PER EA 1-5310-T0335809 PART 1. MAIN DECK CARGO DOOR JAMB WORN HOLES ON MAIN DECK CARGO DOOR FORWARD SUPPORT HINGE LOBE (FUSELAGE DOOR JAMB SIDE). REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO WRI 53107619 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · corrosion level 2 · airframe 79,230 hrs · 20,007 cycles

AFT FLOOR SUPPORT, BS 1887 - 2007, LBL 2 FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-2R, FIG 206. A NEW FLOOR SUPPORT WAS FABRICATED IAW DWG AGA7081, REV M. REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CHAFED (RT WING LE SLAT) · airframe 79,230 hrs · 20,007 cycles

RIGHT WING, NR 3 LEADING EDGE SLAT LOWER SURFACE FOUND THE EDGE CHAFED AT XOS 482. BLENDED AND SMOOTHENED IAW EA 1-5750-T0335856, PART 1.

Part: SKIN — GOUGED (RT WING) · airframe 79,230 hrs · 20,007 cycles

RIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT, REPAIR DOUBLER, LOWER SURFACE FOUND GOUGED AT XOS 482. THE REPAIR DOUBLER WAS REMOVED IAW SRM 51-31-01-0G. A NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1581) · corrosion level 2 · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1581, RBL 75.25 FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101. THE SEAT TRACK WAS REPLACED FROM BS 1711 TO 1571 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1600) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1600, LBL 47.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1611 TO 1571 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1159) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1159, RBL 8.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1189 TO 6-100 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1701) · corrosion level 2 · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1721, LBL 8.5 FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101. THE SEAT TRACK WAS REPLACED FROM BS 1671 TO 1811 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CHAFED (MAIN DECK) · airframe 79,230 hrs · 20,007 cycles

THE SEAT TRACK AT BS 5-63, RBL 27.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED BETWEEN BS 5-0 TO 5-123 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1801) · corrosion level 2 · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1801, LBL 8.5 FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101. THE SEAT TRACK WAS REPLACED FROM BS 1671 TO 1811 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 1801) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1801, RBL 8.5 FOUND CRACKED. THE SEAT TRACK WAS REPLACED FROM BS 1771 TO 1811 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CHAFED (BS 7115) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 715, LBL 8.5 CRACKED. THE SEAT TRACK WAS REPLACED BETWEEN BS 645 TO 745 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1701) · corrosion level 2 · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1701, RBL 75.25 FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW 53-00-52-1A, FIG 101. THE SEAT TRACK WAS REPLACED FROM BS 1711 TO 1571 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · corrosion level 2 · airframe 79,230 hrs · 20,007 cycles

AFT FLOOR SUPPORT BETWEEN BS 1887 - 2007, LBL 25 FOUND CORRODED. A NEW FLOOR SUPPORT WAS FABRICATED IAW DRAWING AGA7087 REVISION M. REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 715) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 715, RBL 27.5 FOUND CRACKED. THE SEAT TRACK WAS REPLACED BETWEEN BS 705 TO 745 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1914-2007) · corrosion level 2 · airframe 79,230 hrs · 20,007 cycles

AFT FLOOR SUPPORT BETWEEN BS 1914 - 2007, RBL 23 FOUND CORRODED. A NEW FLOOR SUPPORT WAS FABRICATED IAW DRAWING AGA7088, REVISION B. REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1801) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1801, LBL 27.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1811 TO 1751 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · corrosion level 2 · airframe 79,230 hrs · 20,007 cycles

AFT FLOOR SUPPORT BETWEEN BS 1887 - 2007, RBL 2 FOUND CORRODED. A NEW FLOOR SUPPORT WAS FABRICATED IAW DRAWING AGA7080, REVISION S. REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1260) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1260, LBL 27.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1229 TO 1269 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1250-1256) · airframe 79,230 hrs · 20,007 cycles

L3 DOOR FORWARD FRAME LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERONS 26 - 27L, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1420) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1420, RBL 8.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1391 TO 1491 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1305-1315) · airframe 79,230 hrs · 20,007 cycles

R3 DOOR AFT FRAME LOWER WEB BOX AT BS 1305.25 - 1315.42, LONGERON 26 - 27R, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1305-1315) · airframe 79,230 hrs · 20,007 cycles

L3 DOOR AFT FRAME LOWER WEB BOX AT BS 1305.25 - 1315.42, LONGERON 26 - 27L, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1179) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1179, LBL 8.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED BETWEEN BS 1169 TO 1249 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 79,230 hrs · 20,007 cycles

MAIN DECK LT LONGERON SPLICE 7L AT BS 5-123 FOUND CRACKED. THE LONGERON SPLICE WAS REMOVED IAW SRM 51-33-01-0G. A NEW LONGERON SPLICE WAS FABRICATED IAW DRAWING A5A7112 REVISION D, AND INSTALLED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 898) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 898, LBL 8.5 FOUND CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 869 TO 909 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1282) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK, BS 1282, LBL 47.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1331 TO 1249 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1420) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 1420, RBL 8.5, FOUND THE CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1391 TO 1491 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1250-1256) · airframe 79,230 hrs · 20,007 cycles

R3 DOOR FORWARD FRAME LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26 - 27R, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 820) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK AT BS 820, RBL 27.5, FOUND THE CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 869 TO EXISTING SPLICE IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1149) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK BS 1149, LBL 8.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED BETWEEN BS 6-100 TO 1169 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1282) · airframe 79,230 hrs · 20,007 cycles

SEAT TRACK, BS 1282, LBL 8.5 CROWN DAMAGED. THE SEAT TRACK REPLACED FROM BS 1249 TO 1331 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 79,230 hrs · 20,007 cycles

LEFT WING DROOPED LEADING EDGE UPPER SURFACE SKIN AT XDLE 324 FOUND CRACKED. REPAIRED THE RT WING DROOPED LEADING EDGE UPPER SURFACE SKIN IAW SRM 57-40-01-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,230 hrs · 20,007 cycles

RT WING FIXED LEADING EDGE RIB DOUBLER AT STA XOS 667 FOUND CRACK. RIB DOUBLER AT RH WING FIXED LEADING EDGE XOS 667 REMOVED AS PER SRM 51- 31-01-0G. NEW RIB DOUBLER FABRICATED AS PER DOUGLAS DWG ARB 3954 REV K AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,230 hrs · 20,007 cycles

RT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 760 FOUND CRACK. REPAIR CARRIED OUT AT R/H WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 760 PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,230 hrs · 20,007 cycles

RT WING FIXED LEADING EDGE RIB DOUBLER AT STA XOS 906 FOUND CRACKED. RIB DOUBLER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW RIB DOUBLER PER DOUGLAS DRAWING ARB3954 REV K. INSTALLED NEW RIB DOUBLER AT RH WING FIXED L/E AT XOS 906 PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,230 hrs · 20,007 cycles

LT WING FIXED LEADING EDGE RIB DOUBLER AT STA XOS 667 FOUND CRACK. RIB DOUBLER AT LH WING-FIXED LEADING EDGE STA XOS 667 AREA REMOVED AS PER SRM 51-31-01-0G. NEW RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION K AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LEFT WING) · airframe 79,230 hrs · 20,007 cycles

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

Part: DOUBLER — CRACKED (LT WING) · airframe 79,230 hrs · 20,007 cycles

LT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 731 FOUND CRACK. REPAIR CARRIED OUT AT L/H WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 731 PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,230 hrs · 20,007 cycles

LT WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 581 FOUND CRACK. REPAIR CARRIED OUT AT LH WING-FIXED LEADING EDGE BEADED DOUBLER AT XOS 581 PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 79,230 hrs · 20,007 cycles

LT WING NR 11 SLAT TRACK LOWER SURFACE SKIN CUTOUT INBD CORNER AT STA XOS 715 FOUND CRACK. CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPLICE PLATE — CRACKED (BS 645) · airframe 79,230 hrs · 20,007 cycles

LOWER FWD CARGO CEILING SEAT TRACK BOTTOM ATTACHED PLATE FOUND CRACKED AT BS 645, LBL 47.5. THE SEAT TRACK ATTACH SPLICE PLATE WAS REMOVED IAW SRM 51-35-01-0G. A NEW SPLICE PLATE WAS FABRICATED AND INSTALLED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,230 hrs · 20,007 cycles

RT WING FIXED LEADING EDGE RIB DOUBLER AT STA XOS 789 FOUND CRACK. RIB DOUBLER AT RH WING-FIXED LEADING EDGE STA XOS 789 AREA REMOVED AS PER SRM 51-31-01-0G. NEW RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION K AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 79,230 hrs · 20,007 cycles

LEFT WING DROOPED LEADING EDGE UPPER SURFACE SKIN AT XDLE 314, FOUND CRACKED. REPAIREDTHE LT WING DROOPED LEADING EDGE UPPER SURFACE SKIN IAW SRM 57-40-01-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 79,230 hrs · 20,007 cycles

RIGHT WING NR 14 SLAT TRACK LOWER SURFACE SKIN CUTOUT OUTBD CORNER AT XOS 891 FOUND CRACKED. THE SKIN WAS REPAIRED IAW SRM 57-40-02-2R, FIG 201, REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — SCRATCHED (RT WING LE SLAT) · airframe 78,761 hrs · 19,880 cycles

RIGHT WING, UPPER SURFACE, IN THE AREA OF THE NR 8 SLAT, APPEARS TO HAVE A SCRATCH. REPAIRED IAW EA 1-5730-T0334361, REV A.

Part: IRU — INACCURATE (ALTITUDE) · airframe 77,972 hrs · 19,632 cycles

ALTITUDE MISCOMPARE AFTER TAKEOFF. AT FL270 ALT 1 READ 26940, ALT 2 27010,STBY 27030. REMOVED AND REPLACED CADC-3 IAW AMM 34-16-01-4. OPS CHECKED GOOD IAW AMM 34-16-01-5.

Part: ENGINE — LEAKING (NR 1) · airframe 77,925 hrs · 19,619 cycles

AFTER TO NR 1 ENG OIL QTY STEADILY DECREASED TO TO ZERO. COMPLIED WITH QRH OIL PRESSURE SUBSEQUENTLY DECREASED TO ZERO. COMPLIED WITH QRH NO ENGINE EXCEEDANCES. REMOVED AND REPLACE ENGINE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,220 hrs · 19,406 cycles

EMERGENCY LIGHT BATTERY 1 LOW ALERT DURING AN EMERGENCY LIGHT TEST. R & R PWR SUPPLY IAW AMM: 33-51-01-4, OPS CHECKED GOOD IAW AMM 33-51-01-5.

Part: TIRE — FAILED (MLG) · airframe 75,613 hrs · 18,897 cycles

TIRE NR 9 FAIL, PRESS ZERO. FAILURE OCCURRED ON ROLLOUT APPROX 60 KTS, WHILE AUTO BRAKES WERE ON MEDIUM SETTING. FOUND NR 9 MAIN WHEEL FLAT SPOTTED AND BLOWN. R&R THE NR 9 MAIN WHEEL AS PER MM 32-41-01-4.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 75,526 hrs · 18,871 cycles

LEFT MLG TRUNNION FITTING, INBD UPPER & LOWER SURFACES ARE CORRODED. REMOVED CORROSION IAW SRM 57-20-14-2R & EA 1-3210-T03234600. LANDING GEAR MAIN GEAR & DOORS, LT MLG FITTING CORROSION REPAIR. SEE N00026 FOR ACCOMPLISHMENT OF EA MINOR REPAIR.

Part: FITTING — CORRODED (LT MLG) · airframe 75,526 hrs · 18,871 cycles

LEFT MLG RETRACT CYLINDER, UPPER MOUNT FRAME FITTING IS CORRODED. REPLACED FITTING PN ARB 7170-1. INSTALLED ON NR N00018. MINOR REPAIR.

Part: TRUNNION — CORRODED (LT MLG) · airframe 75,526 hrs · 18,871 cycles

LEFT MLG TRUNNION FITTING UPPER & LOWER HOLE BORES ARE CORRODED. REMOVED CORROSION & BUSHED 4 EACH HOLES ON LT MLG TRUNNION FITTING IAW SRM 57-20-14-2R REPAIR 1. MINOR REPAIR.

Part: INDICATOR — INOPERATIVE (R1 DOOR SLIDE) · airframe 75,509 hrs · 18,864 cycles

R1 DOOR SLIDE PRESSURE INDICATOR LIGHT INOPERATIVE. R & R REMOTE PRESSURE INDICATOR ASSEMBLY IAW AMM 25-61-04-4. R & R EVACUATION SLIDE & RAFT IAW AMM 25-61-01-4. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SWITCH — FAILED (LANDING GEAR) · airframe 750 hrs · 18,720 cycles

AFTER RAISING LG RECEIVED LEVEL ONE TAT PROBE ALERT. AUTOPILOT & THROTTLES DISENGAGED, TAKEOFF WARNING SOUNDED WHEN SLATS RETRACTED. LOST AUTO CABIN PRESSURIZATION. PERFORMED GND SENSOR FAILURE CHECKLIST. LAST LEG FAULTED GND SENSOR SWITCH LT & RT. TROUBLE SHOT IAW FIM 32-40 TASK 842. R & R LT & RT GND SENSOR SWITCH IAW AMM 32-24-01-4. INSPECTED IAW AMM 32-24-01-6. ALL CHECKED GOOD. PERFORMED FCC 1 & FCC 2 AFS R-T-S IAW AMM 22-01-10-5. ALL TESTS PASSED. PERFORMED FUNCTIONAL TEST OF CABIN PRESS CONTROL SYS IAW AMM 21-31-00-5. ALL TESTS PASSED. ACFT OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 750 hrs · 18,719 cycles

MAIN DECK CARGO, UPON REMOVAL OF FLOOR PANEL WITH REF TO SNRM N01299, SEAT TRACK FLANGE BETWEEN STATION 1541 & 1561, X= 47.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1610) · corrosion level 2 · airframe 750 hrs · 18,719 cycles

MAIN DECK CARGO, UPON REMOVAL OF FLOOR PANEL, SEAT TRACK FLANGE AT BS 1610, X= 75.25 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 750 hrs · 18,719 cycles

NOSE LANDING GEAR, UPON REMOVAL OF RT TRUNNION FITTING ASSEMBLY WITH REFERENCE TO SNRM N00831, FOUND LONGERON CRACKED. NLG AT RT TRUNNION FITTING ASSEMBLY AREA CRACKED LONGERON, PN ACA3796-2. R & R IAW SRM 51-31-01-0G. FOR REMOVAL OF LONGERON REFER SNRM N00831 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1541-1561) · corrosion level 2 · airframe 750 hrs · 18,719 cycles

CABIN, UPON REMOVAL OF FLOOR PANEL, ON MAIN DECK CARGO COMPARTMENT FOR ACCESS, LT BS 1541 - 1561, X= 75.25 FOUND CORROSION ON SEAT TRACK FLANGE. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 750 hrs · 18,719 cycles

CENTER LG WW COMPARTMENT, DIAGONAL SUPPORT STRUCTURE AT STATION 1480, X= 31.50 LT, JUST FWD UPPER OF TRUNNION FITTING, FOUND CORROSION. BOOT STRAP R&R AS PER SRM 51-31-01-0G. NEW BOOT STRAP FABRICATED BY MACHINING AS PER DWG AEA 7131. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 750 hrs · 18,719 cycles

CABIN MAIN DECK CARGO COMPARTMENT, CORROSION ON SEAT TRACK FLANGE LT STATION 1781 - 1821, X= 107.25. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 6. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 750 hrs · 18,719 cycles

CABIN MAIN DECK CARGO COMPARTMENT, RT STATION 1289, X= -47.5 SEAT TRACK CROWN AREA FOUND DAMAGED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1248 - 1331, X= -47.5 IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 750 hrs · 18,719 cycles

NOSE LANDING GEAR RT SIDE TRUNNION FITTING, FWD LOWER SECTION FOUND CRACKED. REPAIRED IAW SRM 53-10-14-2R FIG 202 REPAIR 2

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 750 hrs · 18,719 cycles

CABIN MAIN DECK CARGO COMPARTMENT, RT BS 1289, X= -8.5 SEAT TRACK CROWN AREA FOUND DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 750 hrs · 18,719 cycles

AGEING ACFT, EXISTING REPAIR AT CABIN SEAT TRACK STATION 1228, X= -47. EXISTING REPAIR EVALUATED & FOUND CROWN AREA DAMAGED. CABIN SEAT TRACK AT STATION 1209 - 1248, X= -47 CARRIED OUT REPAIR IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1, EO 1-5100-7-5001 B6 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 750 hrs · 18,719 cycles

RIGHT WING LE STATION XOS 615 FORMER CRACKED. CRACKED FORMER REMOVED PER SRM 51-31-01-0G AND REPLACED NEW FORMER AT RH WING LEADING EDGE AT XOS 584 PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 750 hrs · 18,719 cycles

CABIN MAIN DECK CARGO COMPARTMENT, RT STATION 1361, X= -107.25, SEAT TRACK FLANGE FOUND CORROSIONS. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1351 TO 1411, X= -107.25 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO SNRM N00984 FOR WORK DETAILS.

Part: CARGO TRACK — CORRODED (BS 1401) · corrosion level 2 · airframe 750 hrs · 18,719 cycles

CABIN MAIN DECK CARGO COMPARTMENT, RT BS 1411, X -107.25 CARGO TRACK FLANGE FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 750 hrs · 18,719 cycles

RIGHT WING LE STATION XOS 615 FORMER CRACKED. ORMER REMOVED IAW SRM 51-31-01-0G & FABRICATED NEW FORMER IAW DWG ARB 2931 REV H. INSTALLED NEW FORMER AT RT WING LE XOS 584 IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,035 hrs · 18,719 cycles

RIGHT WING LE BEADED DOUBLER AT STATION XOS 669 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LE BEADED DOUBLER AT XOS 669 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 75,035 hrs · 18,719 cycles

LEFT WING LE BEADED DOUBLER AT XOS 593 FOUND CRACKED. REPAIRED IAW SRM 57- 40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,035 hrs · 18,719 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 665 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 75,035 hrs · 18,719 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 646 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CONTROL CABLE — CUT (LE SLAT) · airframe 745 hrs · 18,573 cycles

ON ARRIVAL, WALK AROUND CHECK FOUND LT NR 8 LE SLAT CABLE CUT IN TWO PLACES, SECOND & THIRD TRACK FROM MOST OTBD. R & R LT NR 8 LE SLAT EXTENSION & RETRACTION CABLES & PULLEYS IAW AMM 20-20-07-2, IPC 27-81-27-01 & 20-00-00-0 SMP. COMPLIED LOCKWIRE & LOCK CLIP IAW AMM 20-20-05-2. PERFORMED ADJUSTMENT THE LT OTBD SLAT DRIVE CABLES & FUNCTIONAL TEST OF THE SLAT RANGE OF MOVEMENT IAW AMM 27-80-00-5. ALL SYS WORKS NORMAL. INSTALLED ACCESS PANELS 519DB, 525AB, 527AB, 527DB, 527KB & 527AT. ALL WORKS WITH SASCO 2 AMTS. ACFT OK FOR SERVICE.

Part: BATTERY — DISCHARGED (R1 DOOR) · airframe 742 hrs · 18,487 cycles

R1 DOOR SLIDE PRESS TO TEST INOPERATIVE. REPLACED BATTERIES ON R1 DOOR REMOTE PRESS INDICATOR ASSEMBLY IAW MM 25-61-04-4. FC NOW NORMAL. OK FOR SVC.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 71,958 hrs · 17,717 cycles

AFTER PUSHBACK, LEVEL 1 ALERT FOR EMERGENCY LIGHTS DISARMED. SWITCH POSITION WAS IN ARM. TROUBLESHOT, NO FAULTS FOUND WITH NR 1 DEU OR EMERGENCY LIGHT SWITCH ON OVERHEAD PANEL. NO 30 DAY HISTORY, SYSTEM OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 71,901 hrs · 17,697 cycles

PRIOR TO LANDING LOWERED GEAR HANDLE, ACFT HAD SEVERE SHAKING FOLLOWED BY UNSAFE LT MAIN LANDING. UNSAFE INDICATION ON PRIMARY & SECONDARY INDICATIONS.

Part: SKIN — CRACKED (ZONE 600) · airframe 71,654 hrs · 17,609 cycles

DURING PERFORMANCE OF FCD 1-5710-F0308148, FOUND LARGE CRACK AT RT WING NR 1 SLAT AT INBD SLAT TRACK CUT OUT. CUT OUT CRACK & REMOVED ALL DAMAGE IAW SRM 57-40-02. PERFORMED HFEC INSPECTION IAW NTM 20-00-00 PART 6, NO DEFECTS NOTED. PERFORMED RII INSPECTION FOR DAMAGE REMOVAL, FOUND TO BE IAW SRM 57-40-02 FIGURE 201. INSTALLED NEW SKIN IAW SRM 51-31-01 AND EA 1-5730-T0308398 P1.

Part: SKIN — CRACKED (LT WING) · airframe 71,654 hrs · 17,609 cycles

CRACK IN LOWER LE PANEL ON LT WING JUST INBD OF OTBD SLAT MARKED. INSTALLED REPAIR ON ARB2933-13 IAW EA 1-5710-T0308224 P1. INSTALLED REPAIR ON LE SKIN IAW SRM 57-40-02 REPAIR 7 & EA 1-5710-T0308224 P 1. PAINTED REPAIR AREA IAW SRM 51-51-02.

Part: SKIN — CRACKED (LT WING) · airframe 71,654 hrs · 17,609 cycles

FOUND CRACK ON INBD FWD CORNER OF SLAT DRIVE MECHANISM DOOR CUT OUT LT WING. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6. PERFORMED HFEC INSPECTION IAW NTM 20-00-00 PART 6, NO DEFECTS NOTED. INSPECTED DAMAGE REMOVAL, NOT ACCEPTED. RADIUS ON DAMAGE REMOVAL LESS THAN THE 0.50" MIN RADIUS. DAMAGE REMOVAL INSPECTED IN PREVIOUS SHORT SIGN WAS NOT COMPLETED YET. INSPECTED AGAIN & FOUND TO COMPLY WITH SRM 57-40-02 REPAIR 7 FIGURE 202. PERFORMED HFEC INSPECTION OF DAMAGE REMOVAL IAW NTM CHAPT 20-00-00 PART 6, NO DEFECTS NOTED. REMOVED FASTENERS AT DAMAGE LOCATION IAW SRM 57-40-02 REPAIR 7 FIG 202. FABRICATED DOUBLER FROM MAT PN 6AL4V063. OK TO INSTALL REPAIR IAW SRM 54-40-02.

Part: SUPPORT FITTING — CRACKED (R3 DOOR) · airframe 70,894 hrs · 17,342 cycles

MAIN DECK CABIN DOOR 3 RT, UPPER SUPPORT FITTING FOUND CRACKED.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 70,894 hrs · 17,342 cycles

MAIN DECK CABIN, SEAT TRACK CROWN LOCATION AT STATION 757 LBL 47 INCHES FOUND WORN.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 70,894 hrs · 17,342 cycles

MAIN DECK CABIN, SEAT TRACK CROWN LOCATION AT STATION 752 LBL 9 INCHES FOUND WORN.

Part: SKIN — CRACKED (RT WING) · airframe 70,894 hrs · 17,342 cycles

RIGHT HAND WING SLAT TRACK NR 12 CUTOUT LOWER SKIN FOUND CRACKED.

Part: BULB — UNSECURE (TEST LIGHT) · airframe 70,517 hrs · 17,203 cycles

RT LT DOOR SLIDE PRESSURE WILL NOT TEST. SECURED LIGHT IN SOCKET ASSY, TESTED NORMAL IAW MM 25-61-04-5. ACFT OK TO CONTINUE.

Part: WIRE — DAMAGED (FIRE HANDLE) · airframe 69,290 hrs · 16,797 cycles

SHORTLY AFTER STARTING APU AUTO SHUTDOWN WITH FIRE HANDLE ILLUMINATED. NO AURAL WARNING. NO INDICATION OF ACTUAL FIRE. REPAIRED WIRING INSULATION IAW SWPM 20-10-01. OPS AND LEAK CHECKED GOOD. FIRE WARNING TEST OF APU GOOD.

Part: FAIRING — BROKEN (NR 2 A/C PACK) · airframe 69,150 hrs · 16,751 cycles

LOUD AND VIOLENT VIBRATION IN AIRFRAME STARTING AT 220KTS WHILE RETRACTING SLATS. FELT AS IF IT WAS UNDER CAPTINS SEAT. VIBRATION STOPPED AFTER SLOWING BELOW 220KIAS AND DID NOT RETURN. ONCE LEVELED OFF AND SLOWED TO 190 VIBRATION WAS NOT PRESENT FOR REMAINDER OF FLIGHT, RETURNED AND LANDED WITHOUT INCIDENT. INSPECTED PACK INLETS, FOUND DEFLECTOR FAIRING ON NR 2 PACK BROKE AT ATTACH POINTS AND HANGING IN AIRSTREAM R & R FAIRING ASSY REF MM 21-55-01-4-2. OPS CHECK GOOD NO DEFECTS NOTED.

Part: COMPUTER — MALFUNCTIONED (MLG) · airframe 68,737 hrs · 16,618 cycles

ON FINAL, LOWERED GEAR AND GOT LEVEL 1 TIRE PRESS LO ALERT. SD SHOWED NUMEROUS GEAR YELLOW AND LOW PRESS INDICATIONS, OTHER GEAR WERE "BLANKED." EXECUTED GO AROUND. CONSULTED QRH AND MOCC ON SATCOMM. HISTORY, SHOWED THIS IS A REPEAT. RETURNED AND RELEASED FOR SERVICE. R & R BTM/TPI COMPUTER IAW AMM 32-46-02-4.

Part: BRAKE — FAILED · airframe 68,471 hrs · 16,534 cycles

AFTER LANDING, RECEIVED LEVEL 2 TIRE FAIL ALERT. TIRE NR 9 SHOWED AMBER W/"0" PRESSURE. ADVISE MX AND WAS TOWED TO THE GATE. REMOVED AND INSP NR 9 AND NR 10 CENTER MAIN WHEEL ASSY IAW MM 32-41-01-4. LEAK CK OK. REMOVED AND INSPECTED NR 9 BRAKE ASSY IAW MM 32-43-20-4, REPLACED NR 10 BRAKE FLEX HYD HOSE AND PERFORMED BRAKE TEST IAW MM 32-43-20, TEST OK.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 67,729 hrs · 16,290 cycles

IN CLIMB TO ABOUT 12,000 FT AND DESCENT BELOW 17,000 FT THERE IS AN ACRID ODOR IN COCKPIT. PERFORMED OPS CHECK OF PACK OPERATION, FLIGHT COPMARTMENT HEATING AND COOLING IN REF TO AMM 21-40-00 AND 21-50-00, NO DEFECTS NOTED AND NO ODOR PRESENT. UNABLE TO DUPLICATE ON GROUND.

Part: FIRE DETECTOR — FALSE ACTIVATION (NR 1 NACELLE) · airframe 67,448 hrs · 16,211 cycles

NR 1 FIRE INDICATION WITH BELL AT MAX POWER DURING TAKE OFF. INITIATED REJECTION AT 120KIAS. SHUTDOWN ENGINE AND FIRED AGENT BOTTLE. FIRE INDICATION QUIT AFTER THROTTLES RETARDED TO IDLE. R & R A & B UPPER TURB LOOPS AND RAIL ASSY IAW MM. REF 26-11-03-4, IAW FDCU1 ADJ/TEST IAW MM REF 26-11-02-5 AND CLEARED A LOOP FAULT. FDCU1 STILL SHOWS 'UP RT FIRE DET ASSY B'. T/S IAW FIM 26-11 AND VERIFIED RESISTANCE, FIG 103, SH2 AT 1450 OHMS BETWEEN PINS J & K, ALSO CONTINUITY BTWEEN J & K TO GROUND. CONTINUED SHAKE AND FOUND A PREVIOUSLY REPAIRED WIRE HARNESS SHOWING ERRATIC 'B' LOOP CONTINUITY. READING DURING SHAKE. PERFORMED RTS ON FDCU1 ALL TESTS GOOD ON LOOP A.

Part: PANEL — MISSING (ZONE 600) · airframe 66,697 hrs · 16,018 cycles

MISSING PANEL ON TOP OF RT WING FWD OF OTBD AILERON, REF IPC 57-54-05-01, ITEM 253. REPAIRED IAW EA EA 1-5750-161180

Part: SKIN — CRACKED (RT WING) · airframe 66,346 hrs · 15,919 cycles

RIGHT NR 12 SLAT TRACK CUTOUT FOUND CRACKED. CRACKED AREA REPAIRED IAW EA 1-5730-154295. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 114.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RT WING - UPPER WING SURFACE FOUND CORRODED AT STA XORS 264. REPAIRED IAW EA 1-5730-154297. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 114.

Part: SUPPORT — CORRODED (MLG WW) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

LT MLG WW T/E ADJACENT AREA OF TRAPEZOIDAL FITTING SUPPORT STRUCTURE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5710-154299. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV114

Part: SUPPORT — CORRODED (RT MLG WW) · airframe 66,346 hrs · 15,919 cycles

MLG RT W/W T/E ADJACENT AREA OF TRAPEZOIDAL FITTING STRUCTURE SUPPORT FOUND WITH CORROSION. REPAIR CARRIED OUT IAW EA 1-5710-154300. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — WORN (LT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

LEFT WING FLAP SIDE INBD FLAP HINGE INBD PIVOT HOLE BUSHING WORN. REPAIRED IAW EA 1-5750-159801, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RT WING - ACFT SIDE OTBD FLAP HINGE LOWER MOUNT AFT SURFACE FOUND CORRODED. REMOVED CORROSION IAW EA 1-5750-76663B PART 3.

Part: BUSHING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RT WING, FLAP SIDE INBD FLAP HINGE INBD PIVOT HOLE BUSHING WORN. REPAIRED AS PER EA#1-5750-159802. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 114.

Part: FLOORBEAM — CORRODED (BS 595) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

CORROSION ON FLOORBEAM AT STA 595 X=-47 TO -75. REPAIRED IAW EA 1-5310-154298. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RT WING OTBD FLAP VANE FITTING C ECCENTRIC BOLT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-150432, PART 1. EXISTING HOLE SIZE: 0.880" X 0.625" FINAL HOLE SIZE 0.956" X 0.658" . BUSHING INSTALLED IAW EA1-5750-150432. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: VANE — CORRODED (RT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

RT WING OTBD FLAP VANE FITTING E ECCENTRIC BOLT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-150432, PART 1. EXISTING HOLE SIZE: 0.923" X 0.606" FINAL HOLE SIZE 0.973" X 0.668" MAX ALLOWABLE LIMIT 0.940" X 0.670". BUSHING INSTALLED IAW EA. REPAIR CLASSIFIED MAJOR AS IAW GMM 6-2-100, REV 114.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

DURING FPI INSPECTION ON LEFT WING INBD FLAP, FLAP SIDE INBD PIVOT HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-159801. EXISTING HOLE DIA 1.253" FINAL HOLE DIA 1.255'. MAXIMUM HOLE DIA 1.220' . BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-159801, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

DURING FPI INSPECTION ON RT WING INBD FLAP, FLAP SIDE INBD PIVOT HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-157802 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: FLOORBEAM — CORRODED (BS 460) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

CABIN FLOORBEAM FOUND CORRODED AT STA 460 X= 48 TO X =53. REMOVED IAW SRM 51-31-01, REV 48 AND INSTALLED NEW FLOORBEAM IAW AMM 20-50-02, REV 70.2. NEW FLOORBEAM REPLACED IAW DWG ACA7364-1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114

Part: BUSHING — WORN (LT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

LEFT WING, WING SIDE OTBD FLAP INBD HINGE PIVOT HOLE BUSHING WORN OUT. REPAIRED IAW EA1-5750-76665A PART 2. NEW BUSHING FABRICATED AND INSTALLED IAW EA1-5750-76665A PART 2, STEP 6 . REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RIGHT WING, FLAP SIDE, INBD FLAP HINGE, OTBD PIVOT HOLE BUSHING WORN. REPAIRED IAW EA 1-5750-159802, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

LEFT WING, WING SIDE OTBD FLAP INBD HINGE LOWER MOUNT FWD AND AFT SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5750-76665A, STEP 3 AND 4 PART 2. INBD EXISTING THICKNESS :0.447" INBD FWD MATERIAL REMOVED:0.008" REMAINING THICKNESS: 0.439" OTBD EXISTING THICKNESS: 0.417", OTBD FWD MATERIAL REMOVED: 0.008", REM THICKNESS: 0.409"MINIMUM ALLOWABLE THICKNESS ;0.423". SHIM FABRICATED AND INSTALLED IAW EA NR 1-5750-76665A, PT 2, STEP 7 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

LEFT WING, WING SIDE OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. EXISTING HOLE DIAMETER 1.222", FINAL HOLE DIAMETER 1.253", MAX HOLE DIAMETER 1.220". BUSHING FABRICATED AND INSTALLED IAW EA1-5750-76015A PART 2, STEP 6. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

LEFT WING, WING SIDE OTBD FLAP INBD HINGE LOWER MOUNT AFT SURFACE FOUND CORROSION. REPAIRED IAW EA 1-5750-76665A PART 2, STEP 3 AND 4. OTBD AFT EXISTING THICKNESS :0.439", MATERIAL REMOVED 0.015", REMAINING THICKNESS 0.424". INBD AFT EXISTING THICKNESS :0.409', MATERIAL REMOVED 0.025" REMAINING THICKNESS 0.384'. MINIMUM ALLOWABLE THICKNESS 0.423". REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

LEFT WING, WING SIDE OTBD FLAP OTBD HINGE LOWER MOUNT AFT SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. INBD AFT EXISTING THICKNESS;0.414" MATERIAL REMOVED : 0.008" REMAINING THICKNESS : 0.406" OTBD AFT EXISTING THICKNESS : 0.399" MATERIAL REMOVED: 0.010" REMAINING THICKNESS : 0.389". REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (LT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

LEFT WING, WING SIDE OTBD FLAP INBD HINGE ACTUATOR HOLE OTBD HOLE BUSHING WORN OUT. REPAIRED IAW EA 1-5750-76665A, PART 2, STEP 6. EXISTING HOLE DIA 1.221" MAX. ALLOWABLE HOLE DIA 1.220". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76665A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (LT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

LEFT WING, FLAP SIDE INBD FLAP HINGE OTBD PIVOT HOLE BUSHING WORN. REPAIRED IAW EA 1-5750-159801, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

LEFT WING, WING SIDE, OTBD FLAP, OTBD HINGE LOWER MOUNT FWD AND AFT SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A, STEP 3 AND 4 PART 2. INBD EXISTING THICKNESS :0.416" INBD FWD MATERIAL REMOVED :0.002" REMAINING THICKNESS:0.414" OTBD EXISTING THICKNESS:0.401", OTBD FWD MAT REMOVED:0.002" REMAINING THICKNESS:0.399" MINIMUM ALLOWABLE THICKNESS ;0.408", REMAINING THICKNESS INBD:0.406", OTBD : 0.389". REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (LT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

LEFT WING, WING SIDE OTBD FLAP INBD HINGE ACTUATOR HOLE INBD HOLE BUSHING WORN OUT. REPAIRED IAW EA1-5750-76665A, PART 2, STEP 6. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76665A, PART 2, STEP 6. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

LEFT WING, WING SIDE OTBD FLAP OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. UPPER EXISTING THICKNESS;0.401" MATERIAL REMOVED: 0.002" REMAINING THICKNESS : 0.399" LOWER EXISTING THICKNESS : 0.417" MATERIAL REMOVED: 0.002" REMAINING THICKNESS : 0.415" . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — CORRODED (TE FLAP HINGE) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

LEFT WING - WING SIDE FLAP OTBD HINGE, OTBD ACTUATOR HOLE FOUND CORROSION. REWORKED IAW EA 1-5750-76015A. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76015A . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114. EXISTING HOLE DIA 1.222" FINAL HOLE DIA 1.220".

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RT WING, WING SIDE OTBD FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. CORROSION REMOVED IAW CMM 20-11-02, REV 72. EXISTING THICKNESS :0.434" MATERIAL REMOVED :0.002" REMAINING THICKNESS : 0.432". FOUND WITHIN LIMITS IAW DWG ARC0502 SHEET 4, REV BN REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RIGHT WING OTBD FLAP OTBD HINGE LOWER MOUNT FWD AND AFT SURFACE FOUND CORRODED. CORROSION REMOVAL ACCOMPLISHED IAW EA 1-5750-76663B PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (RT WING TE FLAP) · airframe 66,346 hrs · 15,919 cycles

RT WING WING SIDE OTBD FLAP, INBD HINGE PIVOT HOLE BUSHING WORN OUT. R & R WITH NEW BUSHING IAW EA 1-5750-76664A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RT WING OTBD FLAP, OTBD HINGE LOWER MOUNT, OTBD HOLE FOUND CORRODED. CORROSION REMOVAL ACCOMPLISHED IAW EA1-5750-76663B PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RT WING OTBD FLAP OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. RT WING - ACFT SIDE OTBD FLAP, OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORROSION. CORROSION REMOVED IAW EA 1-5750-76663B PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76663B.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RT WING OTBD FLAP, OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. CORROSION REMOVED IAW EA 1-5750-76663B, PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: BUSHING — WORN (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RIGHT WING OTBD FLAP, OTBD HINGE PIVOT HOLE BUSHING WORN OUT. BUSHING REPAIRED IAW EA 1-5750-76663B, PART 3. EXISTING HOLE DIA 2.331" MAX ALLOWABLE DIA 2.3135". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76663B, PART 3, STEP 6 AND 11. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

RT WING OTBD FLAP, OTBD HINGE SIDE LOAD FITTING LOWER HOLE FOUND CORRODED. CORROSION REMOVED IAW EA 1-5750-76663B, PART 3. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (BS 675-695) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

CORROSION ON SEAT TRACK FLANGE AT BS 675 - 695 X= -27. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52 FIG 201 REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 66,346 hrs · 15,919 cycles

RT WING L/E LOWER SURFACE ACCESS PANEL 619CB CUTOUT FWD INBD CORNER FOUND SUSPECTED CRACK. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

FWD CARGO COMPT STA 6-50-STA 6-73. DURING REPAIR OF LONGERON 52 FOR CORROSION FOUND SPLICE FITTING REPAIR WITH CORROSION. REMOVED AND CARRIED OUT REPAIR IAW SRM 53-00-05, FIG 202, REPAIR 1, REV 48. NEW REPAIR LONGERON SPLICE FABRICATED IAW SRM 53-00-05, FIG 202, REPAIR 1, REV 48 AND INSTALLED NEW REPAIR LONGERON SPLICE IAW SRM 51-33-01, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 66,346 hrs · 15,919 cycles

SEAT TRACK LOPE AT STA 635 X=-47 WORN. TRIMMED OUT AND CARRIED OUT REPAIR IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 66,346 hrs · 15,919 cycles

SEAT TRACK LOPE AT BS 635 RBL 8 WORN. REMOVED AND REPLACED WITH A NEW REWORKED SEAT TRACK IAW SRM 53-00-52, FIG 201, REPAIR 1 REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (ZONE 500) · airframe 66,346 hrs · 15,919 cycles

SKIN AROUND FOUR FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND 713.6. REPAIR CARRIED OUT IAW EA 1-5710-154293, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (ZONE 600) · airframe 66,346 hrs · 15,919 cycles

SKIN AROUND SIX FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS =683.4 AND 713.6. REPAIR CARRIED OUT IAW EA 1-5710-154294, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: FLOOR SUPPORT — CRACKED (BS 405) · airframe 66,346 hrs · 15,919 cycles

BS 405 , X 44 LT UPPER CABIN FLOOR SUPPORT FOUND CRACKED . FLOOR SUPPPORT R & R IAW SRM 51-31-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON — CRACKED (BS 1219-1239) · airframe 66,346 hrs · 15,919 cycles

LONGERON 27 LT FOUND CRACKED AT BS 1219 - 1239. LONGERON R & R IAW SRM 51-31-01, REV 48, NEW LONGERON FABRICATED IAW EA 1-5310-154296. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (BS 625-675) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

CORROSION ON SEAT TRACK FLANGE AT STA 625-675 X =-27. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CHAFED (RT WING) · airframe 66,346 hrs · 15,919 cycles

RIGHT WING TELESCOPIC DUCT CUTOUT FOUND CHAFED. REPAIRED AREA IAW SRM 51-31-01, REV 48. DOUBLER FABRICATED SRM 57-40-01, REPAIR 10 FIG 201, REV 48. FABRICATED DOUBLER INSTALLED IAW SRM 57-40-01. REPAIR 10, FIG 201, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON — CRACKED (BS 595 L49L) · airframe 66,346 hrs · 15,919 cycles

FOUND ATTACHED LONGERON 49L FASTENER HOLE COMMON TO NLG TRUNNION FITTING CRACKED (APPROX 0.025"). CRACKED LONGERON REMOVED IAW SRM 51-35-01, REV 48 AND REPLACED WITH A NEW LONGERON IAW SRM 51-35-01, REV 48 AND SRM 51-33-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

FWD CARGO BAY BILGE AREA BETWEEN STA 6-50 - 6-73, LONGERON 52 (UNDER SPLICE REPAIR) FOUND CORRODED. CORROSION REMOVED AND CARRIED OUT REPAIR IAW SRM 53-00-05, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — WORN (BS 635) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

SEAT TRACK LOPE FOUND WORN AT STA 635 X=27. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — WORN (BS 635) · airframe 66,346 hrs · 15,919 cycles

SEAT TRACK LOPE FOUND WORN AY STA 635 X=47. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (BS 505-515) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

CORROSION ON SEAT TRACK FLANGE AT STA 505-515 X=-75. SEAT TRACK REPAIRED IAW EA 1-5310-159803 AND SRM 53-00-52, FIG 201. REPAIR 1, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CHAFED (LT WING LE) · airframe 66,346 hrs · 15,919 cycles

LEFT WING FIXED L/E ANTI-ICE DUCT CUTOUT FOUND CHAFED. CUTOUT AREA IAW SRM 51-31-01, REV 48. DOUBLER FABRICATED IAW SRM 57-40-01. REPAIR 10, FIG 201, REV 48. FABRICATED DOUBLER INSTALLED IAW SRM 57-40-01. REPAIR 10, FIG 201, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (BS 635-675) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

CORROSION ON SEAT TRACK FLANGE AT BS 635-675 X=-47. TRIMMED OUT AND CARRIED OUT REPAIR IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (BS 595-605) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

CORROSION ON SEAT TRACK FLANGE AT STA. 595-605 X=-75. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (BS 645-655) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

SEAT TRACK FLANGE CORRODED AT STA 645-655 X= -75. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 66,346 hrs · 15,919 cycles

RIGHT WING INBD AILERON L/E EXTERIOR SURFACE FOUND CHAFING. REPAIR CARRIED OUT IAW EA 1-5750-154291. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (BS 615-625) · corrosion level 2 · airframe 66,346 hrs · 15,919 cycles

CORROSION ON SEAT TRACK FLANGE AT BS 615-625 X=-27. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 66,346 hrs · 15,919 cycles

LEFT WING INBD AILERON LOWER L/E PANEL INBD AND OTBD EDGE FOUND CHAFED. REPAIR CARRIED OUT IAW EA 1-5750-154290. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: TRUNNION — CRACKED (NLG) · airframe 66,346 hrs · 15,919 cycles

NLG LEFT SIDE TRUNNION FITTING FOUND CRACKED. CARRIED OUT REPAIR IAW SRM 53-10-14. REPAIR 2, FIG 202, REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (ZONE 100) · airframe 66,346 hrs · 15,919 cycles

FUSELAGE SKIN CRACKED. REPAIR CARRIED OUT IAW SRM 53-20-15, FIG 201, REPAIR 3 REV 48 . CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: O-RING — FAILED (NR 2 HYD SYS) · airframe 66,060 hrs · 15,836 cycles

HYD 2 OFF LEVEL 1 ALERT. RESERVOIR QUANTITY 2.7 GAL, RESERVOIR TEMP 74 DEG-C. RESERVOIR TEMP CONTINUED TO RISE WHEN RESERVOIR TEMP REACHED 96 DEG. DIVERTED AND LANDED. FOUND HYD LEAK FROM NR 2 HYD PRESSURE TRANSMITTER ON NR 2 HYD MANIFOLD. R & R O-RING IAW MM 29-12-46-2-0. SERVICED HYD FLUID TO PROPER LEVEL IAW MM12-13-02-3-0. LEAK CHECKED AND NO LEAKS NOTED IAW JRH. PERFORMED HSC R-T-S AND ALL PASSED IAW MM29-08-01-5-0. ACFT OK FOR SERVICE.

Part: PBE — WORN (COCKPIT) · airframe 64,887 hrs · 15,533 cycles

COCKPIT PORTABLE BREATHING EQUIPMENT (PBE) BLUE INDICATOR FADED OUT. REMOVED AND REPLACED PBE WITH SERVICEABLE 1 IAW AMM 25-60-00-0. RELEASED ACFT FOR SERVICE. CLOSED.

Part: INDICATOR — INOPERATIVE (L1 DOOR SLIDE) · airframe 64,551 hrs · 15,456 cycles

L1 DOOR SLIDE TEST LIGHT INOPERATIVE. REPLACED REMOTE SLIDE PRESSURE INDICATOR ASSY IAW M/M 25-61-04-4, F/C NOW NORMAL. OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 64,185 hrs · 15,388 cycles

EMERGENCY LIGHT TEST FAILED. PERFORMED TEST OF EMERGENCY LIGHT PER MM 33-51-01-5 AND GOT ALERT "EMER LT BAT 1 LO". R & R EMERGENCY LIGHT BATTERY POWER SUPPLY PER MM 33-51-01-4. TEST AND FUNCTIONED NORMAL.

Part: SHEAR TIE — MISREPAIRED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

WHILE ACCOMPLISHING REMOVAL OF EXISTING REPAIR AT STA 5-33 CROWN AREA FOUND SHEAR TIE WITH EXISTING REPAIR NOT IAW ANY SRM REPAIR. MAIN DECK STA 5-33 CROWN AREA SHEAR TIE REPAIRED IAW SRM 53-00-06, FIG 201. REPAIR 1, REV 43. EO NR 1-5100-7-5001A4, PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: LONGERON — CRACKED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

UPON ACCOMPLISHMENT OF SNRM N00646, CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 1 EACH FASTENER HOLE AT STA 5-53 LONGERON 1L. CRACK AT 1 EACH FASTENER HOLE STA 5-53 LONGERON 1L REPAIRED IAW SRM 53-00-05 FIG 202. REPAIR 1 REVISION 43. INTERCOSTAL R & R IAW SRM 51-31-01, REV 43. NEW INTERCOSTAL FABRICATED IAW DWG AFA 3121 SHEET 2, REV AV. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 109.

Part: BUSHING — WORN (SPOILER HINGE) · airframe 60,845 hrs · 14,595 cycles

RT WING NR 5 SPOILER OTBD HINGE FWD SUPPORT FITTING BUSHING FOUND WITH PLAY. BUSHING REMOVED IAW CMM 20-20-07 REV 66. BOTH HOLES REWORKED IAW EA NR 1-5740- 137924, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SHEAR TIE — MISREPAIRED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

WHILE ACCOMPLISHING REMOVAL OF EXISTING REPAIR AT STA 5-53 CROWN AREA FOUND SHEAR TIE WITH EXISTING REPAIR NOT IAW ANY SRM REPAIR. SHEAR TIE REPAIRED IAW SRM 53-00-06, FIGURE 201. REPAIR 1 REV 43, EO 1-5100-7-5001A4 PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: HINGE BRACKET — WORN (NR 2 SPOILER) · airframe 60,845 hrs · 14,595 cycles

LT WING NR 2 SPOILER INBD HINGE LINK WITH PLAY. REPAIR CARRIED OUT IAW EA NR 1-5740-137923, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 109.

Part: BUSHING — WORN (SPOILER HINGE) · airframe 60,845 hrs · 14,595 cycles

RT WING NR 3 SPOILER OTBD HINGE FWD SUPPORT FITTING BUSHING WITH PLAY. RT WING NR 3 SPOILER OTBD HINGE FWD SUPPORT FITTING BUSHING. REMOVED IAW CMM 20-20-07 REV 66. REPAIR CARRIED OUT IAW EA 1-5740-137922, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 109.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 60,845 hrs · 14,595 cycles

CRACK FOUND APPROX 1.5 INCH ON VERTICAL STABILIZER RT SIDE FWD FLANGE OF NR 4 BANJO FITTING RADIUS. REPAIR CARRIED OUT IAW EA NR 1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 60,845 hrs · 14,595 cycles

02 CRACKS APPROX .3125 INCH AND .1875 INCH AT 5:00 AND 7:00 O'CLOCK RESPECTIVELY ON FASTENER HOLE OF VERTICAL STABILIZER LT SIDE FWD FLANGE OF NR 4 BANJO FITTING. REPAIR CARRIED OUT IAW EA NR 1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: FITTING — CRACKED (NR 4) · airframe 60,845 hrs · 14,595 cycles

CRACK FOUND PROPAGATED 1.3 INCH UPWARD FROM STOP DRILL HOLE ON LT NR 4 BANJO AFT FLANGE OF REAR SPAR. REPAIR CARRIED OUT IAW EA NR 1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 60,845 hrs · 14,595 cycles

02 CRACKS APPROX .1250 INCH AND .1875 INCH AT 1:00 AND 7:00 O'CLOCK RESPECTIVELY ON FASTENER HOLE OF VERTICAL STABILIZER RT SIDE FWD FLANGE OF NR 4 BANJO FITTING. REPAIR CARRIED OUT IAW EA NR1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 60,845 hrs · 14,595 cycles

CRACK FOUND PROPAGATED 0.4 INCH DOWNWARD FROM STOP DRILL HOLE ON RT NR 4 BANJO AFT FLANGE OF REAR SPAR. REPAIR CARRIED OUT IAW EA NR 1-5530-132370, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — CORRODED (LT WING) · airframe 60,845 hrs · 14,595 cycles

CORROSION - LT WING STA XORS279 AT UPPER SURFACE DOUBLER AREA. REPAIRED IAW EA NR 1-5730-137933, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: STRUCTURE — CRACKED (ZONE 600) · airframe 60,845 hrs · 14,595 cycles

RT WING - UPPER PYLON BOX OTBD LOWER EDGE FOUND CRACKED.

Part: SKIN — CORRODED (CENTER WING) · airframe 60,845 hrs · 14,595 cycles

RT STA 1234 XCW = -57 TO XCW = -62 CTR WING UPPER PANEL FOUND CORROSION. REPAIR CARRIED OUT IAW EA NR 1-5710-132367, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 109.

Part: SKIN — CORRODED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

CABIN - RT STA 1229 XCW = -67 TO XCW = -74 CTR WING UPPER PANEL FOUND CORROSION. REPAIR CARRIED OUT IAW EA NR 1-5710-132367, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 109.

Part: SKIN — CORRODED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

CABIN - RT STA 1229 XCW = -20 CTR WING UPPER PANEL FOUND CORROSION. REPAIR CARRIED OUT IAW EA NR 1-5710-132367, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - RT WING INBD FLAP REPAIR PATCH FOUND AT LOWER SKIN AT XIFH 195 UPPER SEGMENT AREA. EXISTING REPAIR AT RT WING INBD FLAP LOWER SKIN AT XIFH 195 UPPER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR PATCH REMOVED IAW SRM 51-31-01 REVISION 42 AND REPAIR CARRIED OUT IAW SRM 57-50-01 FIG 201, REPAIR 2 REV 42. REFER TO SNRM N00445 FOR WORK DETAILS. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

CABIN - LT STA 5-23 X = 75.5 SEAT TRACK FOUND CORROSION.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

CABIN - LT STA 5-75 X = 8.5 SEAT TRACK FOUND CORROSION.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 149 UPPER SEGMENT AREA. EXISTING REPAIR AT LT WING INBD FLAP UPPER SKIN AT XIFH 149 UPPER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING REPAIR PATCH REMOVED IAW SRM 51-31-01 REV 42 AND REPAIR CARRIED OUT IAW SRM 57-00-01, FIG 201, REPAIR 1, REV 42. EO NR 1-5100-7- 5001A4, PART 1, TITLE: STRUCTURES - REPAIR CATALOG -IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

CABIN - LT STA 5-35 X = 107 SEAT TRACK FOUND CORROSION.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 226 LOWER SEGMENT AREA. EXISTING REPAIR AT LT WING INBD FLAP UPPER SKIN AT XIFH 226 LOWER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR PATCH REMOVED IAW SRM 51-31-01 REV 42 AND REPAIR CARRIED OUT IAW SRM 57-00-01, FIGURE 201, REPAIR 1 REV 42. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

CABIN - LT STA 5-05 X = 8.5 SEAT TRACK FOUND CORROSION.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

CABIN - RT STA 1482 X = -107 SEAT TRACK FOUND CORROSION.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - LT WING NR3 SLAT REPAIR PATCH (2 EACH) FOUND ON INBD OUTER SKIN AREA. EXISTING REPAIR (2 EACH) AT LT WING NR 3 SLAT ON INBD OUTER SKIN AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR PATCH (2 EACH) REMOVED IAW SRM 51-31-01 REVISION 42 AND REPAIR CARRIED OUT IAW SRM 57-40-01 FIG 201 REPAIR 7 REV 42. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - RT WING INBD FLAP REPAIR PATCH FOUND AT LOWER SKIN AT XIFH 183 UPPER SEGMENT AREA. EXISTING REPAIR AT RT WING INBD FLAP LOWER SKIN AT XIFH 183 UPPER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR PATCH REMOVED IAW SRM 51-31-01, REV 42 AND REPAIR CARRIED OUT IAW SRM 57-50-01, FIG 201, REPAIR 2 REV 42. EO NR 1-5100-7-5001A4, PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - LT WING INBD FLAP OTBD UPPER SURFACE FOUND WITH REPAIR PATCH AT STA XIFH 279 TO YIFH 8.5. EXISTING REPAIR AT LT WING INBD FLAP OTBD UPPER SURFACE STA XIFH 279 TO YIFH 8.5 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR PATCH REMOVED IAW SRM 51-31-01 REV 42 AND FASTENERS RE-INSTALLED IAW DWG ARC2258 REVISION AF. EO 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - RT WING L/E AT SLAT TRACK NR 6 UPPER SKIN REPAIR PATCH FOUND. EXISTING REPAIR AT RT WING L/E SLAT TRACK NR 6 UPPER SKIN EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING PATCH REPAIR REMOVED IAW SRM 51-35-01, REV 42 AND NEW REPAIR CARRIED OUT IAW EA NR 1-5730-137927, TITLE: WINGS - PLATES AND SKIN - RT FIXED L/E SKIN REPAIR AT STA XOS 430. EO 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (BS 1023) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR FOUND AT LOWER FUSELAGE STA 1023 AFT OF FWD CARGO LOWER SCUFF PLATE. EXISTING REPAIR AT LOWER FUSELAGE STA 1023 AFT OF FWD CARGO LOWER SCUFF PLATE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-31-01 REVISION 42 AND REPAIR CARRIED OUT IAW EA NR 1-5330-137931, TITLE: FUSELAGE - PLATES AND SKIN - FUSELAGE SKIN DAMAGE AT STA 1019 AT LONGERON 42R. EO NR1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 201 UPPER SEGMENT AREA. EXISTING REPAIR AT LT WING INBD FLAP UPPER SKIN AT XIFH 201 UPPER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING PATCH REPAIR REMOVED IAW SRM 51-31-01 REV 42 AND REPAIR CARRIED OUT IAW SRM 57-00-01 FIGURE 201, REPAIR 1, REV 42. EO NR 1-5100-7-5001A4, PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.

Part: SKIN — CRACKED (ZONE 600) · airframe 60,845 hrs · 14,595 cycles

CRACK FOUND ON NR 34 FASTERNER HOLE ON RIGHT HAND SIDE OUTER WING LOWER SKIN PANEL ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND XORS 713.6. REPAIR CARRIED OUT AS PER E.A. 1-5710-137915, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 109.

Part: SKIN — NONE (ZONE 500) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - REPAIR DOUBLER FOUND ON LT WING L/E UPPER SKIN AT XIS 247. EXISTING REPAIR - AT LT WING L/E UPPER SKIN STA XIS 247 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-40-02 FIGURE 201, REPAIR 8 REV 42. CHAFED DOUBLER REMOVED IAW SRM 51-31-01 REV 42. NEW DOUBLER FABRICATED AND INSTALLED IAW SRM 57-40-02, FIG 201, REPAIR 8, REV 42. EO 1-5100-7-5001A4, PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.

Part: FRAME — CRACKED (VERTICAL STAB) · airframe 60,845 hrs · 14,595 cycles

CRACK - VERTICAL STABILIZER LOWER ACCESS PANEL NR 364QR CUTOUT AFT. CRACK AT VERTICAL STABILIZER LOWER ACCESS PANEL NR 364QR CUTOUT R & R AS PER SRM 51-31-01 REVISION 43. NEW FRAME FABRICATED AS PER EA NR 1-5530-137929, REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 109.

Part: FAIRING — DENTED (HORIZONTAL STAB) · airframe 60,845 hrs · 14,595 cycles

DENT MARK - HORIZONTAL STABILIZER LT L/E FAIRING NR 331BT.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR FOUND AT FWD CARGO DOOR CUTOUT FWD JAMB STA 888, JUST ABOVE LOWER SCUFF PLATE. EXISTING REPAIR AT FWD CARGO DOOR CUTOUT FWD JAMB STA 888, JUST ABOVE LOWER SCUFF PLATE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01 REVISION 42 AND REPAIR CARRIED OUT IAW SRM 53-00-15 FIG 202, REPAIR 8, REV 42 AND EA NR1-5330-137914, TITLE: FUSELAGE - PLATES ANS SKIN - FWD CARGO DOOR, FWD JAMB REPAIR AT STA 895. REPETITIVE INSP TO BE CARRIED OUT AS PER MD11 ALI, INITIAL INSPECTION AT 12,600 FLIGHT CYCLES AND SUBSEQUENT INSPECTION AT 6,300 FLIGHT CYCLES. EO NR 1-5100-7- 5001A4, PART 1, TITLE: STRUCTURES - REPAIR CATALOG - IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR FOUND AT UPPER FUSELAGE EXTERIOR CROWN AREA AT APPROXIMATELY STA 1295. EXISTING REPAIR AT UPPER FUSELAGE EXTERIOR CROWN AREA AT APPROXIMATELY STA 1295 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER AND INTERNAL DOUBLER REMOVED AS PER SRM 51-31-01. REVISION 42 AND REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 43. FEDEX EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 109.

Part: SKIN — NONE (ZONE 500) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 149 LOWER SEGMENT AREA. EXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 149 LOWER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-01, FIGURE 201 REPAIR 1 REVISION 42. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SKIN — NONE (ZONE 100) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR FOUND AT FWD CARGO DOOR EXTERIOR AFT LOWER CORNER. EXISTING REPAIR AT FWD CARGO DOOR EXTERIOR AFT LOWER CORNER EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW EA 1-5230-90809 REV A, TITLE: DOORS - FWD CARGO DOOR - LOWER CORNER, STA Y = 997 - PERMANENT REPAIR. EO 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: STRUCTURE — MISREPAIRED (CARGO DOOR) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR FOUND AT CTR CARGO DOOR EXTERIOR FWD LOWER CORNER. EXISTING REPAIR AT CTR CARGO DOOR EXTERIOR FWD LOWER CORNER EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01 REV 42 AND REPAIR CARRIED OUT IAW SRM 52-30-16, FIG 201, REV 42. EO NR 1-5100-7-5001A4 PART 1, SRM REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS, 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (BS 2140-2150) · airframe 60,845 hrs · 14,595 cycles

LOWER FUSELAGE EXTERIOR, FOUND EXISTING SKIN DOUBLER REPAIR JUST OTBD OF ACCESS DOOR NR 317CB AND FWD OF DRAIN MAST. EXISTING REPAIR AT LOWER FUSELAGE EXTERIOR JUST OTBD OF ACCESS DOOR NR 317CB AND FWD OF DRAIN MAST EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01, REV 42 AND REPAIR CARRIED OUT IAW EA NR 1-5330-137925, TITLE: FUSELAGE - PLATES AND SKIN - FUSELAGE SKIN DAMAGE AT STA 2140 BETWEEN LONGERON 41L AND LONGERON 43L. EO NR 1-5100-7-5001A4, PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR FOUND AT UPPER FUSELAGE EXTERIOR CROWN AREA AT APPROXIMATELY STA 5-53. EXISTING REPAIR AT UPPER FUSELAGE EXTERIOR CROWN AREA AT APPROXIMATELY STA 5-53 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01 REVISION 43 AND REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 43. FEDEX EO NR 1-5100-7- 5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 109.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR AT MAIN DECK CARGO LT STA 535 9G NET LOWER SUPPORT YOKE EVALUATED AND FOUND NOT CARRIED OUT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR R & R CARRIED OUT IAW EA 1-5310-137920, TITLE: FUSELAGE - MAIN FRAME - FRAME DAMAGE AT STA 535 BETWEEN LONGERON 18L AND LONGERON 21L, AND BETWEEN LONGERON 22L AND LONGERON 25L REPAIR. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR AT MAIN DECK CARGO RIGHT STA 535 9G NET UPPER SUPPORT YOKE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AS PER SRM 51-31-01 REVISION 42 AND REPAIR CARRIED OUT PER EA NR 1-5310-137921, TITLE: FUSELAGE - MAIN FRAME - FRAME DAMAGE AT STA 535 BETWEEN LONGERON 18R AND LONGERON 21R, AND BETWEEN LONGERON 22R AND LONGERON 25R REPAIR. FEDEX EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 109.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR AT MAIN DECK CARGO RIGHT STA 535 9G NET LOWER SUPPORT YOKE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AS PER SRM 51-31-01 REVISION 42 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-137921, TITLE: FUSELAGE - MAIN FRAME, FRAME DAMAGE AT STA 535 BETWEEN LONGERON 18R AND LONGERON 21R, AND BETWEEN LONGERON 22R AND LONGERON 25R REPAIR. FEDEX EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 109.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR FOUND AT LOWER FUSELAGE EXTERIOR STA 435. EXISTING REPAIR FOUND AT LOWER FUSELAGE EXTERIOR STA 435 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AS PER SRM 51-35-01 REVISION 42 AND NEW REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-137932, TITLE: FUSELAGE - PLATES AND SKIN, FUSELAGE SKIN DAMAGE AT STA 436.15 AT X = 0.00. FEDEX EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 109.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR FOUND AT LOWER FUSELAGE STA 1807, LONGERON 37R. EXISTING REPAIR AT LOWER FUSELAGE STA 1807, LONGERON 37R EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01 REVISION 42 AND REPAIR CARRIED OUT AS PER SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 42. EO NR 1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 109.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 60,845 hrs · 14,595 cycles

EXISTING REPAIR AT MAIN DECK CARGO LT STA 535 9G NET UPPER SUPPORT YOKE EVALUATED AND FOUND NOT CARRIED OUT IAW ANY SRM REPAIR. EXISTING REPAIR REMOVED IAW SRM 51-31-01 REV 42 AND NEW REPAIR CARRIED OUT IAW EA NR1-5310-137920, TITLE: FUSELAGE - MAIN FRAME - FRAME DAMAGE AT STA 535 BETWEEN LONGERON 18L AND LONGERON 21L, AND BETWEEN LONGERON 22L AND LONGERON 25L. REPAIR EO NR1-5100-7-5001A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: FITTING — DAMAGED (ZONE 200) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 1 FOUND HOLES A, B, C AND D OVERSIZED TO 0.520 INCH.

Part: FITTING — DAMAGED (ZONE 200) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 2 FOUND HOLES A, B, C AND D OVERSIZED TO 0.520 INCH.

Part: FITTING — DAMAGED (ZONE 200) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 5 FOUND HOLES A, C AND D OVERSIZED TO 0.520 INCH.

Part: SKIN — DAMAGED (LT WING) · airframe 55,741 hrs · 13,425 cycles

11 FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT.

Part: SKIN — CRACKED (ZONE 600) · airframe 55,741 hrs · 13,425 cycles

05 FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT.

Part: SEAT TRACK — CORRODED (BS 1281-1361) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK SEAT TRACK FLANGE AT STA 1281 TO STA 1361, X = -75.5 UPPER SURFACE FOUND CORROSION.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK SEAT TRACK FLANGE UPPER SURFACE AT STA 1159, X = 8 FOUND CORROSION.

Part: SUPPORT FITTING — CRACKED (BS 757) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND 2ND LAYER BEAM WITH CRACK INDICATION AT HOLE D. REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5310-122531, TITLE: FUSELAGE MAIN CARGO DOOR LOWER JAMB BORE HOLES AT APPROXIMATE STA = 737 AND 757 REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRAP — CRACKED (ZONE 500) · airframe 55,741 hrs · 13,425 cycles

LEFT WING OUTBOARD FLAP INBOARD FORWARD FLAP HINGE TENSION STRAP FOUND CRACKED. LEFT WING OUTBOARD FLAP INBOARD FLAP HINGE TENSION STRAP REMOVED AND REPLACED AS PER FEDEX EO NR 1-5750-7-5004 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (BS 737) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND 3RD LAYER CRACK INDICATION AT HOLE A, B, C AND D. MAIN DECK CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 6 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHINGS FABRICATED AND INSTALLED AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND 2ND LAYER BEAM WITH CRACK INDICATION AT HOLE B. REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5310-122531, TITLE: FUSELAGE MAIN CARGO DOOR LOWER JAMB BORE HOLES AT APPROXIMATE STA = 737 AND 757, REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (BS 666) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND 3RD LAYER CRACK INDICATION AT HOLE A, C AND D. MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (BS 757) · airframe 55,741 hrs · 13,425 cycles

MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND 3RD LAYER CRACK INDICATION AT HOLE A, B, C AND D. MAIN DECK CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 7 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHINGS FABRICATED AND INSTALLED AS PER SRM 53-50-00 FIGURE 10, VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CHAFED (T/E FLAP) · airframe 51,298 hrs · 12,413 cycles

LT WING I/B FLAP L/E AT O/B HINGE AREA FOUND CHAFED. REPAIR CARRIED OUT AS PER SRM 57-00-01 FIG. 7 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CORRODED (FUEL TANK) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO CENTER FUEL TANK UPPER SURFACE FOUND CORROSION AT STA 1218, X=75.25. COMPLIED WITH FEDEX EA 1-5710-105629. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO DOOR JAMB UNDER CENTERING GUIDE AREA FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5310-106596. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO FLOOR SEAT TRACK FOUND CORRODED AT STA 5-0 TO 5-10, X=-8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO FRAME FOUND DENT AT STA 1641. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG. 1 VOL.I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES TO BE CARRIED OUT AND THEREAFTER 9500 CYCLES AS PER SRM 53-30-00 FIG.1. VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM CHAPTER 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NO. 309719.

Part: SPAR CAP — CORRODED (ZONE 500) · airframe 51,298 hrs · 12,413 cycles

LT WING REAR SPAR LWR CAP XORS=1050 FOUND UPPER SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5720-106594. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 500) · airframe 51,298 hrs · 12,413 cycles

LT WING REAR SPAR TOP CAP TAPER FILLER AT XORS=480 FOUND UPPER SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5720-106599. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1508, X=-8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 5-0 TO 5-53, X=-75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1521-1528) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1521-1528, X=8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: UNKNOWN — CORRODED (ZONE 100) · airframe 51,298 hrs · 12,413 cycles

CENTER CARGO BETWEEN STA 1561 TO STA 1581 STR 48R FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-10- 00 FIG. 2 VOL.I. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1505, X= 75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1495 - 1510, X=-75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 600) · airframe 51,298 hrs · 12,413 cycles

RT WING, REAR SPAR CAP FOUND TOP SURFACE AT XORS=1048 CORRODED. COMPLIED WITH FEDEX EA 1-5720-106595. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1328, X=75.25. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,298 hrs · 12,413 cycles

MAIN DECK CARGO, FLOOR SEAT TRACK FOUND CORROSION AT STA 1521, X=8.5. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: ANGLE — CRACKED · airframe 51,298 hrs · 12,413 cycles

FOUND CENTER UNDERWING TANK LT SIDE APPROX STA 1305 TO 1321 SUSPECT CRACK ON CORNER ANGLE SPLICE. COMPLIED WITH FEDEX EA 1-5310-106592. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 300) · airframe 51,298 hrs · 12,413 cycles

EMPENNAGE, AFT FUSELAGE COMPARTMENT APPROX STA 2023 LONGERON 45L FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5310-106597, FUSELAGE MAINFRAME LONGERON 45 (L/H). REPAIR AT BODY STATION Y = 2007 - Y = 2033/STANDARD REPAIR DRAWING (NR SR10530090) EMBODIMENT. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRUCTURE — CRACKED (ZONE 600) · airframe 51,298 hrs · 12,413 cycles

RIGHT WING L/E TELESCOPING DUCT PASSAGE CUTOUT FOUND TOP I/B CORNER EDGE CRACKED. REPAIRED AS PER SRM 57-10-00 FIG. 42 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 10 (XORS 760) IN LEFT TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 09 (XORS 819) IN LEFT TANK. REPAIR CARRIED OUT PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 13 (XORS 577) IN LEFT TANK. CARRIED OUT REPAIR AT LT WING STRINGER 13 AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 12 (XORS 642) IN LEFT TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 44 (XORS 523) IN LEFT TANK. COMPLIED WITH FEDEX EA 1-5720-106593. REPAIR CLASSIFIED AS MINOR ALTERATION AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 40 (XORS 747) IN LEFT TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 13 (XORS 577) IN RIGHT TANK. CARRIED OUT REPAIR AT RT WING STRINGER NR 13 (XORS 577) AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 51,298 hrs · 12,413 cycles

LEFT WING ANTI-ICING TELESCOPING DUCT DOOR CUTOUT FOUND CRACKED. LT WING ANTI-ICING TELESCOPIC DUCT CUTOUT CRACK REPAIRED AS PER SRM 57-10-00 FIG. 42 VOL.I. (TR) REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 12 (XORS 642) IN RIGHT TANK. CARRIED OUT REPAIR AT RT WING STRINGER NR 12 (XORS 642) AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 14 (XORS 521) IN RIGHT TANK. CARRIED OUT REPAIR AT RT WING STRINGER 14R (XORS 521) AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 51,298 hrs · 12,413 cycles

DURING HFEC INSPECTION, CRACK FOUND AT STRINGER 09 (XORS 819) IN RIGHT TANK. REPAIR CARRIED OUT PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: TIRE — DETACHED (NLG) · airframe 50,727 hrs · 12,278 cycles

LANDING ROLLOUT KJFK RWY 22L. WINDS 260/05 KTS FLAPS 35 DEG, LEFT NOSE TIRE ASSEMBLY DETACHED. REMOVED AND REPLACED LT NOSE TIRE ASSY, HUB CAP AND TORSION LINK LOCKING SCREW AS PER MM 32-42-01-4. RT NOSE TIRE REPLACED UNDER WRI 32-41/2850. PERFORMED SHOCK STRUT NOSE LANDING GEAR INSP CK AS PER MM 32-21-01-6 AND TORQUE LINKS NOSE LANDING GEAR INSP CHECK AS PER MM 32-21-12-6. A/C LANDING GEAR AND AXEL OK FOR INSPECT, RII AND OK FOR SERVICE. DUE TO LT NOSE TIRE DEPARTING NOSE GEAR SEE WRI 32-41/2848. LT NOSE TRANSDUCER WAS RIPPED APART. REMOVED AND REPLACED LT NOSE TIRE PRESS TRANSDUCER AS PER MM 32-46-04. GROUND OPS CK OK.

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 49,146 hrs · 11,926 cycles

DURING DEPARTURE FROM KIX, GOT AMBER BOXED EVM OF 5.0 ACCOMPLISHED BY MODERATE VIBRATION FELT IN AIRFRAME AND RUDDER PEDALS. N1 DROPPED TO 83 PERCENT N2 GOT AMBER INDICATION OF 113.3 EGT WAS IN WARNING RANGE. GOT CONFIRM ENG OUT PROMPT ON MCDU. DID PRECAUTIONARY IN FLIGHT ENG SHUT DOWN. RETURNED TO KIX. AFTER FUEL DUMP. INSPECTED INTAKE/N1 BLADES, FOUND NORMAL. INSPECTED EXHAUST, FOUND BROKEN BLADES. SENT DAMAGE PICS TO MOCC. WAITING ENG AND TOOLS FOR ENG CHANGE.

Part: FIRE LOOP — MALFUNCTIONED (NR 1 NACELLE) · airframe 48,400 hrs · 11,734 cycles

NR 1 ENGINE FIRE ALARM - BELL AND LIGHT IN FUEL LEVER. PULLED THROTTLE TO IDLE INDICATIONS WENT AWAY. SHUT ENGINE DOWN AND FIRED ONE FIRE BOTTLE, IN ACCORDANCE WITH QRH. DIVERTED TO SEA. REMOVED AND REPLACED NR 1 ENG NR 2 FIRE BOTTLE & UPPER RIGHT LOOP RAIL. DURING FOIL WRAP CHECK FOUND UPPER LEFT BLEED DUCT FOIL BLOWN. RETORQUED AND REFOILED JOINT. PERFORMED POWER ASSURANCE CHECK PER JRH. ALL PARAMETERS WITHIN LIMITS AND FIRE WARNING SYSTEM GOOD. OPENED NR 1 ENGINE AFTER RETURN TO BLOCKS AND VERIFIED FOIL INTACT ON ABOVE JOINT.

Part: SKIN — DAMAGED (LT SLAT) · airframe 47,611 hrs · 11,563 cycles

PDIS: AFTER LANDING IN NARITA, THE MECHANIC AND THE NEW BOARDING OUTBOUND CREW REPORTED A HOLE IN THE LEADING EDGE OF THE LEFT SLAT OUTBOARD OF NUMBER ONE ENGINE. THE AIRPLANE FLEW AND FELT FINE ON A HAND FLOWN APPROACH TO 34L. PANEL MISSING ON OUTBOARD NR 1 ENGINE. REPAIRED AND 3 LEFT SLAT BY DOUBLER REPAIR PER SRM 57-00-01. INSTALLED MISSING PANEL 438EL ON NR 1 ENGINE. INSPECT AND OPS CHECK PER MM.

Part: ATTACH BRACKET — BROKEN (NLG DOOR) · airframe 46,822 hrs · 11,378 cycles

DURING CLIMB PASSING 1200FT ACCELLERATING THROUGH 270KTS.LOUD BANG FOLLOWED BY SEVERE VIBRATION. NO ALERTS IN COCKPIT. ON POST FLT, FOUND NLG LEFT DOOR ACTUATION RODS DETACHED FROM DOOR FRAME AND NOSE GEAR CASE. R & R FWD LT NOSE GEAR DOOR AND FWD DOOR DRIVE LINK PER MM 32-23-03-4. R & R AFT LT NOSE GEAR DOOR AND NOSE GEAR SIDE BRACE ATTACH BRACKET PER MM 32-23-05-4. JACKED A/C NOSE PER MM 07-11-00-2 AND PERF.NOSE GEAR OPS CHK. ALL ADJUSTMENTS AND MEASURES ARE WITHIN MM LIMITS. R & R NOSE GEAR WHEEL WELL INSULATION BLANKET PER SRM.

Part: VANE — DELAMINATED (ZONE 500) · airframe 46,432 hrs · 11,291 cycles

LT WING - DELAMINATION FOUND AT LOWER SURFACE, INBOARD FLAP VANE 17 INCHES FROM INBOARD FLAP, CENTER TRACK. COMPLIED WITH FEDEX EA 1-5750-89965

Part: SLEEVE — MISSING (ZONE 700) · airframe 46,432 hrs · 11,291 cycles

LEFT MAIN GEAR, TRUCK BEAM AFT OUTBOARD LUBE HOLE FOUND PIVOT BORE SLEEVE CHIPPED OFF. REMOVED AND RE-INSTALLED AS PER MM 32-12-20-4 AND RE-INSPECTED LEFT HAND TRUCK BEAM AFT OUTBOARD PIVOT BORE SLEEVE AREA FOUND THE CHIPPED OUT IS ACTUALLY GREASE AS PER DRAWING ARG7029.

Part: COVER — DAMAGED (ZONE 700) · airframe 46,432 hrs · 11,291 cycles

LEFT MAIN LANDING GEAR DOOR, DURING REPLACE, FORWARD AND UPPER COVER ASSEMBLY FOUND EXTRA FASTENER HOLES ON THE DOOR OUTER SKIN. LEFT HAND MAIN LANDING GEAR DOOR OUTER SKIN EXTRA FASTENER HOLES AREA REPAIR CARRIED OUT AS PER SRM 52-00-01 FIGURE 7 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2 -100.

Part: SLEEVE — DAMAGED (MLG) · airframe 46,432 hrs · 11,291 cycles

RIGHT MAIN GEAR, TRUCK BEAM AFT INBOARD LUBE HOLE FOUND PIVOT BORE SLEEVE CHIPPED OFF. REMOVED AND RE-INSTALLED AS PER MM 32-12-20-4 AND RE-INSPECTED RIGHT HAND TRUCK BEAM AFT INBOARD PIVOT BORE SLEEVE AREA FOUND THE CHIPPED OFF IS ACTUALLY A GREASE GROOVE AS PER DRAWING ARG7029.

Part: SKIN — CHAFED (ZONE 600) · airframe 46,432 hrs · 11,291 cycles

RIGHT WING, FIXED LEADING EDGE UPPER SURFACE FOUND CHAFED MARK AT OUTBOARD OF NR 19 SLAT TRACK. CHAFED MARKED REMOVED FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE UPPER SURFACE AREA AT OUTBOARD OF NR 19 SLAT TRACK AS PER SRM 57-10-00 FIGURE 14 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 46,432 hrs · 11,291 cycles

CENTER ACCESSORY COMPARTMENT LONGERON 51L, STA 1112 SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. LONGERON FABRICATED AS PER DRAWING AAA7088 AND FEDEX EA 1-5310-89966.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 46,432 hrs · 11,291 cycles

CENTER CARGO - UPPER DECK SEAT TRACK X = -75.25 FROM STA 5-73 TO STA 1681 FOUND METAL CLIP NUTS AND SURROUNDING STRUCTURE WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 46,432 hrs · 11,291 cycles

CENTER CARGO - UPPER DECK FLOOR PANEL SUPPORT AT STA 1561 X = 58 FOUND CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 46,432 hrs · 11,291 cycles

MAIN DECK SEAT TRACK X = 8.5 FROM STA 5-73 TO STA 1681 FOUND METAL CLIP NUTS AND SURROUNDING STRUCTURE CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,432 hrs · 11,291 cycles

CENTER CARGO - UPPER DECK SEAT TRACK X = -8.50 FROM STA 5-73 TO STA 1681 FOUND METAL CLIP NUTS AND SURROUNDING STRUCTURE CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 46,432 hrs · 11,291 cycles

AFT CARGO - RIGHT SEAT TRACK AT STA 1954 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 46,432 hrs · 11,291 cycles

CENTER CARGO CEILING UPPER DECK SEAT TRACK RBL 8.0 FOUND CORRODED AT STA 1561. REPAIR CARRIED OUT AS PER SRM 53-70-00.

Part: SKIN PANEL — CHAFED (ZONE 600) · airframe 46,432 hrs · 11,291 cycles

RIGHT WING - DROOP L/E SKIN PANEL OUTBOARD EDGE FOUND CHAFED MARK. FOUND WITHIN LIMITS AS PER SRM 57-00-01. TRIMMED AND FIGURE 1A VOLUME I. MATERIAL REMOVED 0.375 FROM EDGE. NDT INSPECTED AND VERIFIED CRACK FREE CONDITION. OPERATION CHECKED AND FOUND 'SAT' AS PER AMM 27-80-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 46,432 hrs · 11,291 cycles

UPPER CARGO SEAT TRACK RBL 47 CORRODED AT STATION 1441. CARRIED OUT REPAIR AS PER SRM 53-70-00.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 46,432 hrs · 11,291 cycles

UPPER CARGO SEAT TRACK RBL 47 CRACKED AT STATION 6-20. UPPER CARGO SEAT TRACK RBL 47 CRACKED AT STATION 6-20 REPAIRED AS PER SRM 53- 70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 46,432 hrs · 11,291 cycles

UPPER CARGO SEAT TRACK LBL 11 CORRODED AT STA 1791. CORROSION REMOVED AS PER SRM 51-21-01.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,432 hrs · 11,291 cycles

UPPER CARGO SEAT TRACK RBL 47 CRACKED AT STA 1309. REPAIRED AS PER SRM 53-700-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 46,432 hrs · 11,291 cycles

MAIN DECK, SEAT TRACK LBL 11 CORRODED AT STA 859.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 46,432 hrs · 11,291 cycles

UPPER CARGO SEAT TRACK LBL 11 CRACKED AT STA 633. UPPER CARGO SEAT TRACK LBL 11 AT STA 633 CARRIED OUT REPAIR AS PER SRM 53-70- 00 VOLUME I FIGURE 1. REPAIR IS CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 46,432 hrs · 11,291 cycles

UPPER CARGO SEAT TRACK RBL 47 CORRODED AT STA 1696. CARRIED OUT REPAIR AS PER SRM 53-70-00.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,432 hrs · 11,291 cycles

MAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 939. REPAIR CARRIED OUT AS PER SRM 53-70-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 46,432 hrs · 11,291 cycles

MAIN DECK, SEAT TRACK RBL 11 CORRODED AT STA 795 TO STA 879. CORROSION REMOVED AS PER SRM 51-21-01.

Part: COMPUTER — MALFUNCTIONED (FCC) · airframe 45,541 hrs · 11,088 cycles

ON DEPARTURE FROM MEM NEVER GOT AUTOPILOT ON, OR AUTOTHROTLES ON. HAD TO FLY BELOW RVSM DUE TO NO AUTOPILOT. PERFORMED DETAILED AFS SYSTEM CHECK, ALL TESTS PASSED, CHECKED FCC NR 1 AND FCC NR 2 PROFORMED AUTO FLIGHT SYSTEM TEST. REF MD-11 M/M 22-01-10-5. ALL TEST PASSED. A/C OK FOR SERVICE. A/C CAT STATUS DOWN GRADED TO NOT CAT II A/P NR 1 AND NR 2 ARE CHECK CAT II. REMOVED AND REPLACED GLARESHIELD CONTROL PANEL PRECAUTIONARY. REF MD-11 M/M 22-00-04-5. OPS CHECK NORMAL. OK FOR SERVICE.

Part: BRACKET — CORRODED (T/E FLAP) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT I/B FLAP O/B HINGE, O/B STRAP PIVOT HOLE FOUND WITH MINOR CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651 - WINGS - TRAILING EDGE FLAPS, LT & RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR.

Part: SUPPORT FITTING — DAMAGED (T/E FLAP) · airframe 42,327 hrs · 10,353 cycles

LEFT I/B FLAP DRIVE FITTING AFT MOST TOP ROLLER BRACKET-F O/B BUSHING BORE FOUND ELONGATED. COMPLIED WITH FEDEX EA 1-5750-75933, WINGS - LEFT INBOARD FLAP, ROLLER UPPER AFT FITTING ASSEMBLY.

Part: SUPPORT FITTING — CHAFED (T/E FLAP) · airframe 42,327 hrs · 10,353 cycles

LEFT I/B FLAP DRIVE FITTING AFT MOST TOP ROLLER BRACKET-F O/B FWD EDGE FOUND WITH CHAFE MARKS. COMPLIED WITH FEDEX EA 1-5750-75933 - WINGS - LEFT INBOARD FLAP, ROLLER UPPER AFT FITTING ASSEMBLY.

Part: HINGE — CRACKED (T/E FLAP) · airframe 42,327 hrs · 10,353 cycles

RIGHT O/B FLAP, I/B HINGE FITTING TENSION STRAP SUPPORTS FOUND EXISTING CRACK ON HINGE HOLES BIGGER IN SIZE COMPARE TO EO 1-5750-7-5004 01 PT2 AS CALL OUT ON STEP 1B. COMPLIED WITH FEDEX EA 1-5750-75942 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE, TENSION STRAP FASTENER HOLES.

Part: FASTENER — SHEARED (RT WING) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING LOWER SURFACE, ONE FASTENER HEAD FOUND SHEARED OFF FORWARD OF PANEL 641KB. RIGHT WING LOWER SURFACE, ONE FASTENER FORWARD OF PANEL 641KB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.

Part: FASTENER — SHEARED (RT WING) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING LOWER SURFACE, ONE FASTENER HEAD FOUND SHEARED OFF FORWARD OF O/B FLAP I/B HINGE. RIGHT WING LOWER SURFACE - ONE FASTENER FORWARD OF O/B FLAP I/B HINGE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.

Part: FASTENER — SHEARED (LT WING) · airframe 42,327 hrs · 10,353 cycles

LT WING LOWER SURFACE I/B AREA, ONE FASTENER HEAD FOUND SHEARED OFF. LT WING LOWER SURFACE I/B AREA, ONE FASTENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2.

Part: SPLICE — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

FWD CARGO COMPARTMENT STA 1119 - 6-10 LONGERON 44 RT SPLICE FOUND CRACKED. FWD CARGO COMPARTMENT STA 1119 - 6-10 LONGERON 44 RT SPLICE REMOVED AS PER SRM 51-33-01 VOL II AND INSTALLED NEW SPLICE AS PER SRM 51-33-01 VOL II.

Part: SPLICE — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON 44R SPLICE FOUND CRACKED.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 42,327 hrs · 10,353 cycles

FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL 2.

Part: SPLICE — CORRODED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE FOUND CORROSION. FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.

Part: SPLICE — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL 2.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 42,327 hrs · 10,353 cycles

FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE FOUND CORROSION. FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

FWD CABIN STA 427 RBL 8.5 FLOOR PANEL SUPPORT CORRODED. FWD CABIN STA 427 RBL 8.5 FLOOR SUPPORT REMOVED AND REPLACED IAW SRM 51-33-01 VOL II.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 42,327 hrs · 10,353 cycles

CENTER CARGO COMPARTMENT, LEFT TUNNEL AT STA 5-113 TO STA 1541, STR 40 LONGERON SPLICE FOUND CRACKED. CENTER CARGO COMPARTMENT, LONGERON SPLICE REMOVED AS PER SRM 51-31-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2.

Part: LONGERON — CORRODED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

CENTER CARGO COMPARTMENT AT STA 5-123 - 1561 LT LONGERON 48 FOUND CORROSED. CENTER CARGO COMPARTMENT AT STA 5-123 - 1561 LT LONGERON 48 REMOVED AND INSTALLED NEW LONGERON AS PER SRM 51-33-01 VOL II.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

FWD CABIN, STA 442 RBL 30 FOUND FLOORBEAM CORRODED. **** S/D COMING ****

Part: SPLICE — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

FWD CARGO COMPARTMENT RT TUNNEL STR 38 AT STA 1119 - STA 6-10 LONGERON SPLICE FOUND CRACKED. **** S/D COMING ****

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

FWD CABIN STA 442 RBL 30, FOUND FLOORBEAM CORRODED. FWD CABIN STA 442 RBL 30 FLOORBEAM REMOVED AND INSTALLED AS PER SRM 51-33-01 VOL II AND DWG ABA8305.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

CABIN SEAT TRACK CORRODED STA 1830 & STA 1671 LBL 27. CABIN SEAT TRACK CUT AND REMOVED AT STA 1651 TO STA 1887 LBL 27.5. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I.

Part: LONGERON — CORRODED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

CENTER CARGO COMPARTMENT. AT STA 5-123 TO STA 1561 LT LONGERON 48, FOUND CORROSION. **** S/D COMING****

Part: SPLICE — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

FWD CARGO COMPARTMENT, RIGHT TUNNEL STR 38 AT STA 1119 - STA 6-10 LONGERON SPLICE FOUND CRACKED. FWD CARGO COMPARTMENT, RIGHT TUNNEL STR 38 AT STA 1119 - STA 6-10 LONGERON CRACKED SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,327 hrs · 10,353 cycles

FWD CABIN STA 427 RBL 8.5 FLOOR PANEL SUPPORT CORRODED. FWD CABIN STA 427 RBL 8.5 FLOOR SUPPORT REMOVED AND REPLACED IAW SRM 51-33-01 VOL 2.

Part: SPLICE — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

CENTRE CARGO COMPARTMENT, LT TUNNEL AT STA 5-113 TO STA 1541, STR 38 LONGERON SPLICE FOUND CRACKED. **** S/D COMING ****

Part: SPLICE — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

CENTER CARGO COMPARTMENT, LT TUNNEL AT STA 5-113 - 1541, STR 38 SPLICE FOUND CRACKED. CENTER CARGO COMPARTMENT LT TUNNEL AT STA 5-113 - 1541, STR 38 SPLICE REMOVED AS PER SRM 51-31-01 VOL II AND INSTALLED NEW SPLICE AS PER SRM 51-33- 01 VOL II.

Part: SPLICE — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

CENTER CARGO COMPARTMENT, LT TUNNEL AT STA 5-113 TO STA 1541, STR 40 LONGERON SPLICE FOUND CRACKED. CENTER CARGO COMPARTMENT LONGERON SPLICE REMOVED AS PER SRM 51-31-01 VOL II AND REPLACED AS PER SRM 51-33-01 VOL II.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,327 hrs · 10,353 cycles

CABIN SEAT TRACK CORRODED STA 1830 & STA 1671 LBL 27. CABIN SEAT TRACK CUT AND REMOVED AT STA 1651 TO STA 1887 LBL 27.5. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

FWD CABIN, STA 442 - STA 447 LBL 87 FOUND FLOOR CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

FWD CABIN, STA 442 - 447 LBL 87 FOUND SEAT TRACK CORRODED. FWD CABIN SEAT TRACK AT STA 442 - 447 LBL 87 REMOVED AND INSTALLED IAW SRM 51-33-01 VOL II AND DWG NBA6022.

Part: VANE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT I/B FLAP VANE I/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION.CORROSION REMOVED AS PER SRM 51-21-01 VOL II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005.

Part: VANE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT I/B FLAP VANE O/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005.

Part: VANE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT I/B FLAP VANE O/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED PER CMM57-52-03.

Part: VANE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT I/B FLAP VANE I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED PER CMM57-52-03.

Part: VANE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT I/B FLAP VANE O/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT O/B FLAP FWD I/B HINGE O/B SIDE SURFACE AROUND THE FWD MOUNT AREA FOUND RUSTY AND PAINT WORK DETERIORATED. CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC 0502 SHEET 2.

Part: VANE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT I/B FLAP VANE I/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT O/B FLAP FWD I/B HINGE O/B SIDE SURFACE AROUND THE BRACE FITTING FOUND RUSTY AND PAINT WORK DETERIORATED. CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND REFER TO THE DWG TOLERANCE OF ARC0502 SHT 1.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

FWD CABIN STA 427 LBL 53 - LBL 76 FOUND FLOOR SUPPORT BEAM CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BEAM AS PER AMM 20-50-02.

Part: VANE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT I/B FLAP VANE I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED AS PER CMM57-52-03.

Part: HINGE — CHAFED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT O/B FLAP FWD I/B HINGE O/B SIDE ABOVE PIVOT BORE SURFACE FOUND WITH CHAFE MARKS. CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC0502 SHEET 1.

Part: HINGE — CHAFED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT O/B FLAP FWD I/B HINGE O/B SIDE ABOVE PIVOT BORE SURFACE FOUND WITH CHAFE MARKS. CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC0502 SHEET 1.

Part: VANE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RT I/B FLAP VANE O/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED PER CMM57-52-03.

Part: SPLICE — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

CENTER CARGO COMPARTMENT AT STA 5-123 RIGHT STR 49 LONGERON SPLICE FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.

Part: SKIN — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

AFT FUSELAGE RT EXTERIOR SKIN FOUND WITH CORROSION AT STA Y 2007-2015 LONGERON STR 27. COMPLIED WITH FEDEX EA 1-5310-76666. REMOVAL AT RT FUSELAGE STATION 1997.75 LONGERON L-27R CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING O/B FLAP O/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING O/B FLAP O/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. WING TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING O/B FLAP O/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. WING TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING O/B FLAP O/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. WING TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING O/B FLAP I/B HINGE PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR.

Part: BRACE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP I/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: VANE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT O/B FLAP VANE, NR 5 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75931. LEFT AND RIGHT OUTBOARD FLAP NR 5 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: VANE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT O/B FLAP VANE, NR 2 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75928. LEFT AND RIGHT OUTBOARD FLAP NR 2 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: VANE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT O/B FLAP VANE, NR 3 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75929. LEFT AND RIGHT OUTBOARD FLAP NR 3 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP O/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING O/B FLAP I/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP I/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. REMOVED AND REPAIRED AS PER CMM 57-44-08 AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC0502 SHT 4.

Part: VANE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT O/B FLAP VANE, NR 4 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75930. LEFT AND RIGHT OUTBOARD FLAP NR 4 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: VANE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT O/B FLAP VANE, NR 2 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75928, LT AND RT OUTBOARD FLAP - NR 2 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP I/B HINGE PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING O/B FLAP I/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR.

Part: VANE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT O/B FLAP VANE, NR 1 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75927. LEFT AND RIGHT OUTBOARD FLAP NR 1 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP I/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: VANE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT O/B FLAP VANE, NR 5 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75931. LEFT AND RIGHT OUTBOARD FLAP NR 5 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP O/B HINGE PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP O/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: VANE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT O/B FLAP VANE, NR 4 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75930. LEFT AND RIGHT OUTBOARD FLAP NR 4 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING O/B FLAP I/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR.

Part: VANE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT O/B FLAP VANE, NR 1 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75927. LEFT AND RIGHT OUTBOARD FLAP NR 1 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP O/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP O/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING O/B FLAP I/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. REMOVED AND REPAIRED AS PER CMM 57-44-08. FOUND REMAINING THICKNESS WITHIN TOLERANCE AS PER DWG ARC0502 SHT4.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING O/B FLAP I/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: VANE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT O/B FLAP VANE, NR 3 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75929. LT AND RT OUTBOARD FLAP NR 3 FITTING SUPPORT VANE TO TRACK CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, I/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

FORWARD CABIN FLOOR SUPPORT FOUND CORRODED STA 465 LBL 27.5. SEAT TRACK CORROSION REMOVED AND FOUND CRACKED THROUGH EXCEED LIMIT IAW SRM 53-70-00 FIG 3 VOL 1. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL1.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

FWD CABIN STA 475 CBL FOUND FLOORBEAM CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BEAM ON FWD CABIN STA 475 CENTER BUTTOCK LINE AS PER AMM 53-21-04.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

AFT CARGO COMPARTMENT, RIGHT MOST O/B FLOOR SUPPORT UPPER & LOWER SURFACE FOUND WITH SEVERAL PLACES CORROSION. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.

Part: STRINGER — CRACKED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

CENTER CARGO COMPARTMENT STA 1782 RIGHT STR 46 FOUND CRACKED. REPAIR ON LONGERON 46R BY BETWEEN STATION 1781 AND 1787.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 42,327 hrs · 10,353 cycles

AFT CARGO COMPARTMENT, LEFT MOST O/B FLOOR SUPPORT UPPER & LOWER SURFACE FOUND WITH SEVERAL PLACES OF CORROSION. FLOOR SUPPORTS REMOVED AND REPLACED AS PER SRM 53-00-01 FIG 9 AND DWG AGA3857.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, I/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, I/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, CORROSION REMOVAL & REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, I/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT I/B FLAP, O/B HINGE PIVOT BORE AREA FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76659. TRAILING EDGE FLAPS RIGHT INBOARD FLAP FORWARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT I/B FLAP, O/B HINGE PIVOT BORE AREA FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76012. WING TRAILING EDGE & TRAILING EDGE DEVICES. LT INBOARD FLAP. OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT I/B FLAP, O/B HINGE I/B LUG PIVOT HOLE FOUND WITH CORROSION. REPAIRED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT I/B FLAP, O/B HINGE O/B STRAP PIVOT HOLE FOUND WITH MINOR CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651. TRAILING EDGE FLAPS LT & RT INBOARD FLAP OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT I/B FLAP, O/B HINGE I/B STRAP PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651. TRAILING EDGE FLAPS LT & RT INBOARD FLAP OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, O/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, O/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, O/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT I/B FLAP, O/B HINGE O/B LUG PIVOT HOLE FOUND WITH CORROSION. REPAIRED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, O/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, O/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT I/B FLAP, O/B HINGE I/B STRAP PIVOT HOLE FOUND WITH CORROSION. REPAIRED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, I/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, O/B HINGE INNER SURFACE OF O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, I/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, O/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649. WING LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, O/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, I/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AND REPAIRED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, O/B HINGE INNER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT I/B FLAP, O/B HINGE I/B LUG PIVOT HOLE FOUND WITH CORROSION. REPAIRED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT I/B FLAP, O/B HINGE O/B STRAP PIVOT HOLE FOUND WITH CORROSION. REPAIRED.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AND REPAIRED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, O/B HINGE INNER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649,CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT AFT O/B FLAP, I/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AND REPAIRED.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, O/B HINGE INNER AND OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT O/B FLAP, O/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT AFT I/B FLAP, O/B HINGE O/B LUG PIVOT HOLE FOUND WITH CORROSION. CORROSION REPAIRED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 755 RBL 29 FOUND CRACKED. SEAT TRACK AT STA 745 TO STA 816 RBL 27.5 CUT AND REMOVED, CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 VOL 1.

Part: FITTING — CRACKED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT OUTBOARD FLAP NR 2 FLAP UP STOP BOLT FITTING SUSPECT CRACK AT THE STOP BOLT BARREL NUT AREA. REMOVED AS PER SRM 51-31-01 VOL II AND NEW STOP FITTING INSTALLED AS PER SRM 51-33-01 VOL II AND DRAWING ARC4125.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 755 LBL 29 FOUND CRACKED. SEAT TRACK AT STA 745 TO STA 785 LBL 27.5 CUT AND REMOVED, CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL 1.

Part: FITTING — CRACKED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

LEFT OUTBOARD FLAP NR 2 FLAP UP STOP BOLT FITTING FOUND CRACK AT THE STOP BOLT BARREL NUT AREA AT TWO PLACES. REMOVED IAW SRM 51-31-01 VOL II AND INSTALLED NEW FITTING IAW SRM 51-33-01 VOL II AND DWG ARC4125.

Part: SKIN — CRACKED (ZONE 200) · airframe 42,327 hrs · 10,353 cycles

FUSELAGE PAX DOOR 3 OFF CRACK ON INTERNAL PRIMARY DOUBLER OF LOWER FWD CORNER APPROXIMATELY .1875 INCH. CLEANED UP IAW SRM 53-00-01 FIG 1A VOL I. AND CARRIED OUT AS PER DAC NDT SPM PART 06-10-01-001 REV 11 AND FOUND NO CRACK EVIDENT.

Part: PANEL — CORRODED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RIGHT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH SEVERAL BULGES. COMPLIED WITH FEDEX EA 1-5710-76644 - WINGS - LEFT AND RIGHT HAND WING AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR.

Part: PANEL — CORRODED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH BULGE. COMPLIED WITH FEDEX EA 1-5710-76644. LEFT AND RIGHT HAND WING - AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR.

Part: TRACK — CRACKED (ZONE 400) · airframe 42,327 hrs · 10,353 cycles

NR 3 ENG RIGHT REVERSER COWL OF TRANSLATING COWL MOST UPPER TRACK END FOUND WITH CRACK. NR 3 ENG RT REVERSER TRANSLATING COWL REMOVED AS PER AMM 78-31-16-4. REPAIRED AS PER FAA 8130-3/FA2004/0118, & REINSTALLED AS PER AMM 78-31-16-4.

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 42,327 hrs · 10,353 cycles

LEFT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. LT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 42,327 hrs · 10,353 cycles

RT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. RT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 40,335 hrs · 9,900 cycles

HYDRAULIC 3 FAILURE DURING FLIGHT. REMOVED AND REPLACED UPPER AND LOWER ENG DRIVEN HYD PUMP ASSY AS PER MM 29- 11-20-4, FOR LEAK CHK AND OPS CHK. REMOVED AND REPLACED PER MOCC REQUEST FOR PRECAUTIONARY.

Part: DISPLAY — INOPERATIVE (FUEL SYSTEM) · airframe 39,656 hrs · 9,745 cycles

CLIMBING THRU 18,000 FT BOTH "TIP LOW" (1 AND 3) LEVEL ONE ALERTS CAME ON SHORTLY AFTER FUEL SYSTEM SELF CORRECTED. UPON REACHING CRUISE FL 370 NOTICED FUEL DECREASING AT AN ABNORMAL RATE. ONE MINUTE LATER "FUEL QTY/USED CHK" LEVEL 2 ALERT CAME ON. AT THAT TIME TOTAL FUEL WAS 10,000 #S BELOW PLANNED WITH FUEL STILL DECREASING (ALL TANKS EQUALLY). ENROUTE KOAK TO KSEA DIVERTED TO KSMF. FUEL SYSTEM INDICATED WE HAD LOST 12,000#S. AFTER LANDING AT KSMF. "MEL 28-01-01-02: TANK NO. 2_ FUEL TANK SYN OPTIC QTY DISPLAY- INOP.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INTERIOR , FOUND BARREL 27TH NUT HOLE AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INTERIOR, NR 16 RT BARREL NUT HOLE CORRODED. R&R HORIZ STABILIZER PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 35 AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INT, BARREL NUT HOLE 32R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STAB PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INT, BARREL NUT HOLE NR 26R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INT, BARREL NUT HOLE NR 23L AFTER CORROSION BLEND OUT, OUT OF SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INT BARREL NUT HOLE NR 24R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INT, BARREL NUT HOLE NR 20R EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER 1-5510-66415.

Part: STRUCTURE — DAMAGED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 14L OUT OF SB LIMIT. R&R HORIZ STAB PER EA 1-5510-66415.

Part: STRUCTURE — DAMAGED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 19R BOTTOM SURFACE EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415.

Part: STRUCTURE — DAMAGED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 9R BOTTOM SURFACE EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415.

Part: STRUCTURE — DAMAGED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB EXTERIOR, FOUND BARREL NUT HOLE NR 14R ELONGATED. R&R STAB HORIZ PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

HORIZ STAB INTERIOR FOUND BARREL NUT HOLE NR 21 L BOTTOM SURFACE LOCAL BLENDOUT CORROSION EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

AFTER CORROSION REMOVAL ON BARREL NUT HOLE NR 36 RT, BOTTOM SURFACE AND SIDEWALL BLEND OUT EXCEEDED LIMIT AS PER SB MD11-55-023. R&R HORIZ STAB PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,446 hrs · 9,244 cycles

AFTER CORROSION REMOVAL ON BARREL NUT HOLE NR 36 LT, BOTTOM SURFACE BLENDOUT EXCEEDED LIMIT AS PER SB MD11-55-023. R&R HORIZ STABILIZER PER EA 1-5510-66415.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 37,448 hrs · 9,245 cycles

CORROSION ON HORIZONTAL STABILIZER. R&R HORIZONTAL STABILIZER PER ME 11-55-023.

Part: STRUCTURE — SCRATCHED (RT WING) · airframe 37,446 hrs · 9,244 cycles

FUSELAGE RIGHT SIDE LWR SURFACE OF WING ROOT AT WING TO BODY FILLET (154AB) SCRATCHED. REMOVED & REPLACED SKIN PER EA. 1-5330-66000.

Part: WIRE — DAMAGED (RT WING) · airframe 34,544 hrs · 8,579 cycles

WIRE BUNDLES IN RT WING ROOT LEADING EDGE BURNT.

Part: PUMP — BURNED (HYDRAULIC SYS) · airframe 34,107 hrs · 8,469 cycles

BOTH NR 1 & 2 HYD AUXILIARY PUMPS FOUND BURNT/DAMAGED DURING RT MLG WHEEL WELL CLEANING. REMOVED AND REPLACED BOTH PUMPS.

Part: FIRE DETECTOR — INTERMITTENT (NR 1 ENGINE)

ON ARRIVAL INTERMITTENT ENG 1 FIRE (AURAL ALSO) WARN. SHOW AS LEVEL 1 ALERT. REMOVED AND REPLACED UPPER RIGHT FIRE DETECTOR ASSY PER MM 26-11-03-4. OPS CK OK. CLOSED COWLING.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 29,765 hrs · 7,492 cycles

SNRM 587 CRACK AT LT SIDE FWD RADIUS. SNRM 588 RT SIDE FWD RADIUS. *S/D* REMOVED AND REPLACED PER SRM 55-20-00 FIG 3 VOL 1 AND EA 1-5530-49647.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 29,765 hrs · 7,492 cycles

SNRM 456 & 590 MAIN DECK, SEAT TRACK CRACKED AT BS 635 X = 27.5 RT. *S/D* REWORKED SEAT TRACK PER SRM 53-70-00 FIG 1 VOL 1.

Part: THROTTLE — FAILED (COCKPIT)

99-288 - ON T/O FROM LFPG, MISC DISPLAY IND NO AUTOLAND AND AUTOPILOT 1 AND 2 WOULD NOT ENGAGE. GOT AILERON DISAGREE ALERT. PERF FCC NR 1 AND 2 RTS PER MM 22-00-00-5, (TASK 22-00-00-701-801). ALL RTS PASSED DUE TO PREVIOUS HISTORY. CAT 2 PRECAUTIONARY AND DEFERRED AILERON IND INOP.

Part: PILLOW BLOCK — CORRODED (RT MLG)

PILLOW BLOCK ASSY ON RT CENTER LANDING GEAR HAS CORROSION ON A/C STRUCTURE PAD, BOLT HOLES AND ALIGNMENT PIN HOLE. *S/D* REMOVED CORROSION FROM CENTER LANDING GEAR, SHEAR PIN AND ATTACH BOLT HOLES PER SRM 53-40-00. DIMENSIONS ARE WITHIN SRM 53-40-00 REPAIR LIMITS.

Part: PILLOW BLOCK — CORRODED (LT MLG)

PILLOW BLOCK ASSY ON LT CTR LAND GEAR HAS CORROSION ON A/C STRUCTURE PAD, BOLT HOLES AND ALIGNMENT PIN HOLE. *S/D* REPAIRED LT PILLOW BLOCK MOUNTING PAD SURFACE AND BORES PER SRM 53-40-00 ON CTR GEAR ASSY.

Part: SKIN — CORRODED (CENTER WING)

CENTER WING UPPER SKIN ROUND WITH EXFOLIATION CORROSION AT BS 1229 STR 13, BS 1256 STR 14 AND BETWEEN BS XCW 118 AND XCW 100 RT SIDE AT BS 1273 STR 10 AND BS 1289 STR 5-SNRM 0358. RBL 18 AT BS 1160 AND BS 1219-SNRM 0455. RT AREA OF BS 1293 AND BS 1315-SNRM 0456. PANEL (P/N APB7447-), (P/N APB7441), (APB7445-1). *S/D* REMOVED AND REPLACED CENTER WING UPPER AUX TANK UPPER PANEL STRUCTURE AS PER SRM 57-20-00 FIG 12 VOL 1 AND EA 1-5730-40268.

Part: DUCT — BLOWN (NR 1 ENGINE)

NR 1 ENG FIRE WARN AND IND. SHUT ENGINE DOWN IAW CKLIST. DISCHARGED NR 1 FIRE BOTTLE. FOUND HIGH PRESSURE TURBINE COOL DUCT BLOWN. REMOVED AND REPLACED DUCT, NR 1 FIRE BOTTLE AND SQUIB. RAN ENGINE, LEAK CHECK GOOD.

Part: CIRCUIT BREAKER — TRIPPED (ACCESSORY COMPT)

DURING FUEL SYS STATUS CK WORKCARD 28B1301, L/TAIL TANK TRANSFER PUMP C/B TRIPPED. FIRE STARTED IN AFT ACCESSORY SECTION DURING FUEL TRANSFER TEST. C/W REPAIR IAW EA 1-2800-38210 AND WDM 28-22-05.

Part: BOLT — SHEARED (NR 3 PYLON)

NR 3 PYLON INSIDE ACCESS PANEL 488HL BS YN 342, BULKHEAD TO UPPER SPAR WEB FWD END 3 ATTACH BOLTS HAVE SHEARED AND THE OTHERS ARE LOOSE. * S/D* HFEC BOLT HOLES NO CRACK INDICATIONS NOTED. INSTALLED AND TORQUED NEW BOLTS PER M/M 20-50-02. RETORQUED REMAINING BOLTS PER M/M 20-50-02. 10/24/97.

Part: BOLT — SHEARED (NR 1 PYLON)

NR 1 PYLON INSIDE ACCESS PANEL 438HL STA YN 342, BULKHEAD TO UPPER SPAR WEB FWD END 1 ATTACH BOLT HAS SHEARED AND SEVERAL OTHER BOLTS ARE LOOSE. *S/D* HFEC INSPECTED AREA OF SHEARED AND LOOSE FASTNERS, NO CRACK INDICATIONS NOTED. INSTALLED NEW BOLT PER M/M 20-50-02 AND RE-TORQUED ALL BOLTS. INSTALLED ACCESS PANELS, M/M 54-00-01. 10-22-97

Part: BOLT — BROKEN (LT TE FLAP)

LT WING TRAILING EDGE FLAP, INBOARD HINGE SUPPORT FITTING TO FWD CLEVIS BRACKET, INBOARD LOWER ATTACH BOLT IS SHEARED OFF AND INBOARD UPPER ATTACH BOLT CONICAL WASHER MISSING. OUTBOARD UPPER BOLT CONICAL WASHER IS BROKEN. *S/D* REPLACED BOLT WITH NEW SERVICEABLE BOLT PER DAC DRAWING ARC0501 AND M/M 57-53-01-4. (NOTE: ALL FOUR BOLTS AND WASHERS WERE REPLACED.) 10-22-97.

Part: WASHER — BROKEN (RT TE FLAP)

RT WING TRAILING EDGE FLAP, INBOARD HINGE SUPPORT FITTING TO FWD CLEVIS BRACKET, INBOARD UPPER ATTACH BOLT CONICAL WASHER IS BROKEN. * S/D* REMOVED FITTING, INSPECTED AND CLEANED BOLT HOLES, NO CORROSION NOTED. INSTALLED SERVICEABLE CLEVIS FITTING WITH NEW ATTACH BOLTS PER DAC DRAWING ARC0501 AND M/M 57-53-01-4.

Part: DUCT — FAILURE (NR1 ENGINE)

NRT: AFTER T/O SMOKE OF UNKNOWN ORIGIN APPEARED IN COCKPIT; DID AIR TURNBACK AND RETURNED TO NRT. SMOKE APPEARED TO BE COMING FROM AIR CONDITIONING. FOUND DIRTY OIL IN COALESER OF WATER SEPARATOR IN THE NR 1 PACK AND WET OIL IN NR 1 ENG STATER PNEU DUCT IN THE NR 1 ENG. ALSO, FOUND HOLE BY CHAFING BY HYD LINE (MAINTENANCE REV HALF OPEN MECH) ON THE NR 1 ENG BLEED DUCT. THEN CLEANUP INSIDE OF NR 1 PACK WATER SEPARATOR AND R/R COALESER ALSO BLEED DUCT.

Part: CASTING — BROKEN (L/WING)

SNRM 5020 THE L/H WING, O/B FLAP, I/B HINGE FITTING SUPPORT CASTING IS BROKEN OUT AT THE WING REAR SPAR, LOWER TANG, WING STA XORS 560 APPROX. ******S/D ******* REPLACED L/FLAP TENSION STRAP SUPPORT WITH NEW ONE, PER MDC SB 57-0-10 CONDITION II DATE C.W 8-12-96.

Part: STRAP — CRACKED (RT WING)

RIGHT WING OUTBOARD FLAP, INBOARD HINGE TENSION STRAP SUPPORT CRACKED AT LOWER ATTACH BOLT HOLE, LOWER SURFACE (EXTERNAL) STA X ODRSX562390. REPLACED RIGHT FLAP TENSION STRAP SUPPORT WITH NEW PART PER MDC SB 57-0-10 CONDITION II AND C/W EA 1-5710-29039.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. ACCOMPLISHED CHECKLIST AND LANDED. WE HAD NOSE WHEEL STEERING AVAILIABLE IN FLT AND THE AUTOPILOT AND THE FCP WORKED NORMALLY. RESET AND SAFTIED MLG TRIM CYLINDER INTERLOCK CYL FUSE PER MM 32-37-00. JACKED A/C AND PERFORMED 3 SUCCESSFUL GEAR SWINGS.

Part: ACTUATOR — MALFUNCTIONED (RT AILERON)

UPON FLAP/SLAT RETRACTION FOLLOWING T/O, AILERON DEFLECT DISAGREE LEVEL 2 LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST IN RED BOOK PAGE 2-5-13 AND IAW CHECKLIST DUMPED FUEL AND RETURNED FOR LANDING. FOUND RT O/B AILERON FULLY DEFLECTED AND LT O/B AILERON IN DROOP NEUTRAL POSITION. C/W MXP 27-2 AND DEFERRED AILERON DEFLECTION SYSTEM. DEFERRED PER MEL 27-2 AND FINAL FIX TO BE DONE IN TPE 12-3-95. REPLACED RT O/B AILERON CONTROL LINEAR ACT, OPS CK'D GOOD PER MM 27-16-02 AND FCC-1 AND FCC-2 RTS. ALL PASSED DMI CLEARED.

Part: DOOR FRAME — CRACKED (LT MLG)

THE LEFT HAND CENTERLINE LANDING GEAR DOOR FRAME IS CRACKED ALONG THE FWD, INBOARD CORNER, CRACK IS APPOX 3.5 INCHES LONG C-CK N/R 7004. REMOVED LT FWD CENTERLINE DOOR AND INSTALLED NEW FRAME. P/N ANB 7387-1 PER SRM 53-00-01.