N599FE

Part: FRAME — DAMAGED (ZONE 200) · airframe 90,257 hrs · 19,179 cycles

REFERENCE EA T1-5310-T0365005 PART 3, REQUIRES TERMINATING ACTION. HOWEVER ON STEP 1 IS TO REPAIR OR REPLACE AND PART NUMBER GIVEN MANUFACTURE PART NUNBER AEA0213-509 DOES NOT EXIST. REFERENCE EA T1-5310-T0365005 PART 3, TERMINATING ACTION ACCOMPLISHED IAW EA 1-5310-T0365005 A PART 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (200) · airframe 90,257 hrs · 19,179 cycles

CABIN: L3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 - STATION 1315.42 LONGERON 26 LEFT - LONGERON 27 LEFT FOUND CRACK CABIN AT L3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 TO STATION 1315.42 BETWEEN LONGERON 26 LEFT TO LONGERON 27 LEFT, CRACKED SKIN REPAIRED AS PER SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: FLOOR SUPPORT — CRACKED (100) · airframe 90,257 hrs · 19,179 cycles

LOWER AFT WASTE TANK COMPARTMENT CEILING STATION 1977, X=-57 CABIN FLOOR SUPPORT FOUND WITH CRACK. LOWER AFT WASTE TANK COMPARTMENT CEILING AT STATION 1977, X=-57 CRACKED CABIN FLOOR SUPPORT REMOVED AND REPLACED AT STATION 1887 TO STATION 2007, X=-57 AS PER SRM 51-31- 01-0G. FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (200) · airframe 90,257 hrs · 19,179 cycles

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

Part: RIB — CRACKED (RT NR 8 SLAT) · airframe 90,257 hrs · 19,179 cycles

RIGHT HAND WING - #8 SLAT ASSEMBLY STATION XOS 1092.116 INTERNAL RIB CRACKED. RIGHT HAND WING #8 SLAT ASSEMBLY STATION XOS 1092.116 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1928 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 1/9/2023

Part: LONGERON SPLICE — CORRODED (ZONE 100) · airframe 90,257 hrs · 19,179 cycles

LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-70, X 48 LONGERON SPLICE FITTING FOUND WITH CORROTION. LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-70, X 48 CORRODED LONGERON SPLICE FITTING REMOVED AND REPLACED AS PER MD-11 SRM 51-33-01-0G. LONGERON SPLICE FABRICATED AS PER DOUGLAS DRAWING AEA 7653 REVISION C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 1/9/2023

Part: RIB — CRACKED (LT NR 6 SLAT) · airframe 90,257 hrs · 19,179 cycles

LEFT HAND WING - #6 SLAT ASSEMBLY STATION XOS 806.424 INTERNAL RIB CRACKED. LEFT HAND WING #6 SLAT ASSEMBLY STATION XOS 806.424 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1824 REVISION C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 1/9/2023

Part: DOUBLER — CRACKED (RT WING) · airframe 90,257 hrs · 19,179 cycles

RIGHT WING, OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 631 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 631 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. ORIG SUBMISSION DATE: 1/9/2023

Part: RIB — CRACKED (RT NR 6 SLAT) · airframe 90,257 hrs · 19,179 cycles

RIGHT HAND WING - #6 SLAT ASSEMBLY STATION XOS 822.002 INTERNAL RIB CRACKED. RIGHT HAND WING #6 SLAT ASSEMBLY STATION XOS 822.022 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1825 REVISION F. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUBMISSION DATE: 1/9/2023

Part: RIB — CRACKED (RT WING) · airframe 90,257 hrs · 19,179 cycles

RIGHT HAND WING - #6 SLAT ASSEMBLY STATION XOS 816.872 INTERNAL RIB CRACKED.

Part: RIB — CRACKED (RT NR 8 SLAT) · airframe 90,257 hrs · 19,179 cycles

RIGHT HAND WING - #8 SLAT ASSEMBLY STATION XOS 1146.814 INTERNAL RIB CRACKED. RIGHT HAND WING #8 SLAT ASSEMBLY STATION XOS 1146.814 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1954 REVISION N. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 1/9/2023

Part: RIB — CRACKED (LT WING) · airframe 90,257 hrs · 19,179 cycles

LEFT HAND WING - #6 SLAT ASSEMBLY STATION XOS 811.623 INTERNAL RIB CRACKED. LEFT HAND WING #6 SLAT ASSEMBLY STATION XOS 811.623 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1825 REVISION F. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 1/9/2023

Part: DOUBLER — CRACKED (RT WING LE) · airframe 90,257 hrs · 19,179 cycles

RIGHT WING, OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 634 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 634 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUBMISSION DATE: 1/9/2023

Part: RIB — CRACKED (RT WING) · airframe 90,257 hrs · 19,179 cycles

RIGHT HAND WING - #6 SLAT ASSEMBLY STATION XOS 806.424 INTERNAL RIB CRACKED. RIGHT HAND WING #6 SLAT ASSEMBLY STATION XOS 806.424 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1824 REVISION C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUBMISSION DATE 1/9/2023

Part: RIB — CRACKED (RT NR 8 SLAT) · airframe 90,257 hrs · 19,179 cycles

RIGHT HAND WING - #8 SLAT ASSEMBLY STATION XOS 1086.832 INTERNAL RIB CRACKED. RIGHT HAND WING #8 SLAT ASSEMBLY STATION XOS 1086.832 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1928 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 1/9/2023

Part: RIB — CRACKED (RT WING) · airframe 90,257 hrs · 19,179 cycles

RIGHT HAND WING - #6 SLAT ASSEMBLY STATION XOS 801.225 INTERNAL RIB CRACKED. RIGHT HAND WING #6 SLAT ASSEMBLY STATION XOS 801.225 INTERNAL CRACKED RIB REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1824 REVISION C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUBMISSION DATE: 1/9/2023

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,257 hrs · 19,179 cycles

LEFT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 619, BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 619 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,257 hrs · 19,179 cycles

LEFT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 752, BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 752 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 90,257 hrs · 19,179 cycles

RIGHT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 683 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 683 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,257 hrs · 19,179 cycles

LEFT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 466, BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 466 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 90,257 hrs · 19,179 cycles

RIGHT WING OTBD FIXED LEADING EDGE COMPARTMENT STATION XOS 695, BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 695 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING LE) · airframe 90,257 hrs · 19,179 cycles

RIGHT WING DROOP LEADING EDGE ASSEMBLEY UPPER SURFACE STATION XDLE 314 CRACKED. RIGHT HAND WING DROOP LEADING EDGE ASSEMBLEY UPPER SURFACE STATION XDLE 314 CRACKED AREA REPAIR CARRIED OUT IAW SRM 57-40-01-2R REPAIR 5 FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,257 hrs · 19,179 cycles

LEFT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 745, BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 745 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,257 hrs · 19,179 cycles

LEFT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 654, BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 654 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 90,257 hrs · 19,179 cycles

RIGHT WING, OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 749 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 749 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 90,257 hrs · 19,179 cycles

LEFT WING, NR 16 SLAT TRACK CUTOUT STATION XOS 1008 CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, REPAIR 7, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (RT WING LE) · airframe 90,257 hrs · 19,179 cycles

RIGHT WING, OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 643 FORMER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT XOS 643 CRACKED FORMER R & R IAW SRM 51-31-01-0G. FORMER FABRICATED IAW DWG ARB 2917 REVISION L. REPAIR CLASSIFIED AS MAJOR IAWGMM 6-2-100.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,816 hrs · 18,815 cycles

DURNING THE LIGHT CHECK WE RECEIVED A FAULT "EMER LT BAT ! LO". REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PER AMM 33-51-01-4. OPS CHECK GOOD. OK FOR SERVICE.

Part: DOUBLER — CRACKED (LT WW BULKHEAD) · airframe 85,075 hrs · 17,838 cycles

FUSELAGE: CENTER LANDING GEAR WHEEL WELL, LEFT HAND BULKHEAD FORWARD DOUBLER APPROXIMATELY AT STATION 1381, X=31.50, FLIGHT CONTROL ROD FEED THROUGH POSITION FOUND CRACKED. FUSELAGE CENTER LANDING GEAR WHEEL WELL LEFT HAND BULKHEAD FORWARD CRACKED DOUBLER APPROXIMATELY AT STATION 1381, X=31.50. REMOVED AND REPLACED, PER MD-11 SRM 51-31-01-0G. FABRICATED DOUBLER MACHINED, PER DOUGLAS DRAWING AEA0526 REVISION NC. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 85,075 hrs · 17,838 cycles

CABIN-UNDER SIDE OF SEAT TRACK FROM STATION 939 TO STATION 979, X=8.5 FOUND CRACK. CABIN-AT STATION 939 TO STATION 979, X=8.5 CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 929 TO EXISTING SPLICE STATION 989 X=8.5, AS PER SRM 53- 00-52 -2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (WW BULKHEAD) · airframe 85,075 hrs · 17,838 cycles

FUSELAGE: CENTER LANDING GEAR WHEEL WELL, RIGHT HAND BULKHEAD FORWARD DOUBLER APPROXIMATELY AT STATION 1381, X= -31.50, FLIGHT CONTROL ROD FEED THROUGH POSITION FOUND CRACKED. FUSELAGE CENTER LANDING GEAR WHEEL WELL RIGHT HAND BULKHEAD FORWARD CRACKED DOUBLER APPROXIMATELY AT STATION 1381, X= -31.50. REMOVED AND REPLACED, PER MD-11 SRM 51-31-01-0G. FABRICATED DOUBLER MACHINED, PER DOUGLAS DRAWING AEA0526 REVISION NC. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: LONGERON — CRACKED (NLG WW) · airframe 85,075 hrs · 17,838 cycles

FUSELAGE: DURING NOSE LANDING GEAR LEFT HAND TRUNNION FITTING REPAIR, FOUND LONGERON 49 LEFT HAND CRACKED AT STATION Y=595. NOSE LANDING GEAR LEFT HAND STATION Y=595 TRUNNION FITTING CRACKED LONGERON 49 LEFT HAND. REMOVED AND REPLACED, AS PER MD-11 SRM 51-33-01-0G AND FABRICATED LONGERON, AS PER DOUGLAS DRAWING ACA3796 REVSION A. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: LONGERON — CRACKED (NLG WW) · airframe 85,075 hrs · 17,838 cycles

FUSELAGE: DURING NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING REPAIR, FOUND LONGERON 49 RIGHT HAND CRACKED AT STATION Y=595. NOSE LANDING GEAR RIGHT HAND STATION Y=595 TRUNNION FITTING CRACKED LONGERON 49 RIGHT HAND. REMOVED AND REPLACED, AS PER MD-11 SRM 51-33-01-0G AND FABRICATED LONGERON, AS PER DOUGLAS DRAWING ACA3796 REVSION A. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FWD CABIN) · corrosion level 2 · airframe 85,075 hrs · 17,838 cycles

FORWARD CABIN LEFT HAND SEAT TRACK STATION 430 TO STATION 450, X=85.5 FOUND WITH CORROSION. FORWARD CABIN AT LEFT HAND SEAT TRACK STATION 430 TO STATION 450, X=85.5, CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED, AS PER SRM 51-31-01-0G FROM EXISTING SPLICE STATION 484.784 TO END OF PART STATION 417, X=85.5. REPAIR CLASSIFIED AS MINOR, PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 85,075 hrs · 17,838 cycles

CABIN, FLOOR PANEL NUMBER 231FF FOUND DELAMINATED STATION 595-STA 675. DELAMINATED FLOOR PANEL NUMBER 231FF AT CABIN STATION 595-STATION 675 REMOVED, AS PER AMM 53-21-01-4. FLOOR PANEL NUMBER 231FF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL NUMBER 231FF INSTALLED, AS PER AMM 53-21-01-4. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (FWD CARGO) · airframe 85,075 hrs · 17,838 cycles

FORWARD CARGO COMPARTMENT-LONGITUDINAL SPLICE AT STATION 6-0, LONGERON 39 LEFT FOUND CRACK. FORWARD CARGO COMPARTMENT AT STATION 6-0, CRACKED LONGERON 39 LEFT SPLICE. REMOVED AND REPLACED, AS PER SRM 51-33-01-0G. SPLICE FABRICATED BY MACHINING, AS PER DOUGLAS DRAWING ADA 8424 REVISION A. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 85,075 hrs · 17,838 cycles

CENTER CARGO COMPARTMENT STATION 5-113 TO 1541 RIGHT HAND LONGERON 39 SPLICE END SUSPECT CRACK, CENTER CARGO COMPARTMENT AT STATION 5-113 TO STATION 1541 RIGHT HAND LONGERON 39. CRACKED SPLICE REMOVED AND REPLACED, AS PER SRM 51-33-01-0G. SPLICE FABRICATED BY MACHINING, AS PER DOUGLAS DRAWING A5A 7114 REVISION J. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FITTING — CRACKED (NLG TRUNNION) · airframe 85,075 hrs · 17,838 cycles

FUSELAGE: NOSE LANDING GEAR LEFT HAND TRUNNION FITTING SUSPECTED CRACK. CRACKED NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AT STATION Y=595 REPAIRED, AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 1500 FLIGHT CYCLES, AS PER SRM 53-10-14-2R TABLE 201/REPAIR 2 FIGURE 202/REPAIR 2. REQUIREMENTS, METHOD BY HIGH FREQUENCY EDDY CURRENT OR LIQUID PENETRANT. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FITTING — CRACKED (NLG TRUNNION) · airframe 85,075 hrs · 17,838 cycles

FUSELAGE: NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING SUSPECTED CRACK. CRACKED NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING AT STATION Y=595 REPAIRED, AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 1500 FLIGHT CYCLES, AS PER SRM 53-10-14-2R TABLE 201/REPAIR 2 FIGURE 202/REPAIR 2 REQUIREMENTS. METHOD BY HIGH FREQUENCY EDDY CURRENT OR LIQUID PENETRANT. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 85,075 hrs · 17,838 cycles

DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 REVSION C ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING EXISTING CRACK INDICATION FOUND FROM THIRD FASTENER FROM BELOW TO LOWEST FASTENER AND UNABLE TO PROCEED FURTHER INSPECTION DUE TO WEB BLOCKAGE. RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP STATION 2164 CARRIED OUT REPAIR IN ACCORDANCE WITH EA NR 1-5530-T0358728. PART 1 TITLE: STABILIZERS-VERTICAL STABILIZER-CRACK REPAIR ON VERTICAL STABILIZER REAR SPAR RT FORWARD FLANGE. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 85,075 hrs · 17,838 cycles

MAIN DECK STATION 1841 TO 1853 RIGHT HAND X= -8.5 SEAT TRACK FOUND CORRODED. MAIN DECK AT SEAT TRACK STATION 1841 TO STATION 1853, X= -8.5 CORROSION EVALUATED. FOUND EXFOLIATED AND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 1811 TO END OF PART STATION 1887 X= -8.5, AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REFER TO SNRM N00922 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 85,075 hrs · 17,838 cycles

RIGHT HAND LEADING EDGE FUEL VALVE PANEL CUTOUT DOUBLER AT STATION XOS 906 FOUND CRACKED. RIGHT HAND LEADING EDGE FUEL VALVE PANEL CUTOUT CRACKED DOUBLER AT STATION XOS 906 REPAIR CARRIED OUT, AS PER SRM 57-40-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 85,075 hrs · 17,838 cycles

LEFT HAND WING LEADING EDGE LOWER SURFACE DOUBLER AT FUEL VALVE DOOR FOUND CRACK APPROXIMATELY STATION XOS 906. LEFT HAND WING LEADING EDGE LOWER SURFACE CRACKED DOUBLER AT FUEL VALVE DOOR APPROXIMATELY STATION XOS 906 REPAIR CARRIED OUT, AS PER SRM 57-40-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: STOP FITTING — CRACKED (RT WING TE FLAP) · airframe 85,075 hrs · 17,838 cycles

RIGHT HAND OUT BOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED AT XOVH 537.324. CRACKED FITTING REMOVED AND REPLACED AT RIGHT HAND OUT BOARD FLAP, AS PER SRM 51-33-01-0G AT XOVH 537.324. REPAIR CLASSIFIED AS MINOR, PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 85,075 hrs · 17,838 cycles

LEFT HAND WING LEADING EDGE LOWER SURFACE NR 15 SLAT TRACK CUTOUT APPROXIMATELY STATION XOS 994 SKIN FOUND CRACK. LEFT HAND WING LEADING EDGE LOWER SURFACE NR 15 SLAT TRACK CUTOUT APPROXIMATELY STATION XOS 994 SKIN REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 85,075 hrs · 17,838 cycles

CABIN, FLOOR PANEL NUMBER 241DF FOUND DELAMINATED STATION 755-STATION 795. DELAMINATED FLOOR PANEL NUMBER 241DF AT CABIN STATION 755-STATION 795 REMOVED, AS PER AMM 53-21-01-4. FLOOR PANEL NUMBER 241DF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL NUMBER 241DF INSTALLED, AS PER AMM 53- 21-01-4. REPAIR CLASSIFIED MAJOR. AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 85,075 hrs · 17,838 cycles

CABIN FLOOR PANEL NUMBER 241EF FOUND DELAMINATED STATION 735-STATION 755. DELAMINATED FLOOR PANEL NUMBER 241EF AT CABIN STATION 735-STATION 755 REMOVED, AS PER AMM 53-21-01-4. FLOOR PANEL NUMBER 241EF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL NUMBER 241EF INSTALLED, AS PER AMM 53-21-01-4. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 85,075 hrs · 17,838 cycles

CABIN FLOOR PANEL NUMBER 231LF FOUND DELAMINATED STATION 675-STATION 735. DELAMINATED FLOOR PANEL NUMBER 231LF AT CABIN STATION 675-STATION 735 REMOVED, AS PER AMM 53-21-01-4. FLOOR PANEL NUMBER 231LF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL NUMBER 231LF INSTALLED, AS PER AMM 53-21-01-4. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 85,075 hrs · 17,838 cycles

CABIN-FLOOR PANEL NUMBER 231HF FOUND DELAMINATED STATION 595-STATION 675. DELAMINATED FLOOR PANEL NUMBER 231HF AT CABIN STATION 595-STATION 675 REMOVED, AS PER AMM 53-21-01-4. FLOOR PANEL NUMBER 231HF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL NUMBER 231HF INSTALLED, AS PER AMM 53- 21-01-4. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 85,075 hrs · 17,838 cycles

CENTER CARGO COMPARTMENT STATION 5-113 TO 1541 RIGHT HAND LONGERON 51 SPLICE FOUND CRACK CENTER CARGO COMPARTMENT STATION 5-113 TO 1541 RIGHT HAND LONGERON 51. CRACKED SPLICE REMOVED AND REPLACED, AS PER SRM 51-33-01-0G. FABRICATED SPLICE, AS PER DRAWING A5A 7114 REVISION J BY MACHINING. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 85,075 hrs · 17,838 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 545 FOUND CRACK. RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 545 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 85,075 hrs · 17,838 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 554 FOUND CRACK. RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 554 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 85,075 hrs · 17,838 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 766 FOUND CRACK. RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 766 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 85,075 hrs · 17,838 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 789 FOUND CRACK. RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 789. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 85,075 hrs · 17,838 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 770 FOUND CRACK. RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 770 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FRAME — DENTED (CABIN) · airframe 85,075 hrs · 17,838 cycles

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

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 85,075 hrs · 17,838 cycles

CENTER CARGO COMPARTMENT STATION 5-113 TO 1541 RIGHT HAND LONGERON 49 SPLICE FOUND CRACK CENTER CARGO COMPARTMENT AT STATION 5-113 TO STATION 1541. CRACKED LONGERON 49 RIGHT SPLICE REMOVED AND REPLACED, AS PER SRM 51-33-01-0G. LONGERON 49 RIGHT SPLICE FABRICATED, AS PER DOUGLAS DRAWING A5A 7114 REVISION J BY MACHINING. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 85,075 hrs · 17,838 cycles

LEFT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 583, FOUND CRACK LEFT HAND WING LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 583. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 85,075 hrs · 17,838 cycles

LEFT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 659 FOUND CRACK, LEFT HAND WING LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 659. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 85,075 hrs · 17,838 cycles

LEFT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 530 FOUND CRACK LEFT HAND WING LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 530. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 85,075 hrs · 17,838 cycles

LEFT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 577, FOUND CRACK LEFT HAND WING LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 577. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 85,075 hrs · 17,838 cycles

LEFT HAND WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 440 FOUND CRACK, LEFT HAND WING LEADING EDGE DOUBLER AT APPROXIMATELY STATION XOS 440. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 84,619 hrs · 17,719 cycles

DURING PREFLIGHT TEST OF EMERGENCY LIGHT SYSTEM GOT LEVEL 1 "EMER LT BAT 1 LO" ALERT. REMOVED & REPLACED EMERGENCY LIGHTING BATTERY/POWER SUPPLY, PER AMM 33-51-01-4. SDR INFO: GRIMES, RECHARGEABLE BAT POWER SUPPLY P/N 60-4411-5, S/N 1172.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 83,685 hrs · 17,491 cycles

L1 DOOR WILL NOT ARM. REPOSITIONED GIRT BAR. OPS CHECK GOOD REF AMM 25-61-15-4.

Part: HYDRAULIC LINE — CRACKED (ZONE 100) · airframe 82,969 hrs · 17,306 cycles

PDIS 599 29-02 3267 28FEB20 DWC OPEN U LOGPAGES:3166387 DURING CRUISE COMPLETE LOSS OF NUMBER 2 HYDRO REFER WRI 29-02 3262. NO.2 HYDRAULIC SUPPLY LINE PIPE FROM NO..2 RESERVOIR TO FIRE SHUT OFF VALVE FRACTURED (HAIR LINE) AT FLANGE OF THE PIPE WHICH CONNECTS TO THE RESERVOIR SUPPLY FITTING. THIS CAUSED IMMEDIATE LOSS OF NO.2 HYDRAULIC FLUID QUANTITY. REMOVED AND REPLACED NO.2 ENG INLET SUPPLY PIPE REFER MD11 IPC 29-12-72-01 ITEM 330. REPLACED L/H AND R/H ENGINE DRIVEN PUMPS. REMOVED AND REPLACED 4 HYDRAULIC FILTERS. NO.2 HYDRAULIC SYSTEM BLED AND RE-SERVICED. FUNCTIONAL TEST OF SYSTEM. ENGINE RUN CARRIED OUT ON NO.2 ENGINE PER JRH.. L/H & R/H EDP'S CHECKED FOR OPERATION AND FUNCTIONALITY ALL TESTS PASSED

Part: LAMP — INOPERATIVE (TEST SWITCH) · airframe 82,883 hrs · 17,284 cycles

L1 DOOR REMOTE BOTTLE PRESSURE TEST SWITCH WILL NOT TEST. RELAMPED AND OPS CHECKED GOOD I.A.W. M.M. 25-61-04-5-0.

Part: SWITCH — FAILED (R1 DOOR LIGHT) · airframe 81,681 hrs · 16,937 cycles

R1 PRESSURE TEST LIGHT INOP. R&R'ED R1 DOOR "PRESS TO TEST" LIGHT SWITCH IAW REF: AMM 25-61-04-4. OPS CH'D GOOD.

Part: BULKHEAD — DAMAGED (RT MLG WW) · airframe 81,112 hrs · 16,771 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD BULKHEAD. COMPLY WITH EA 1-5310-T0347293, REV NO. POS. P1 REPAIRED AREA IN REF. TO E.A 1-5310-T0347293.

Part: BULKHEAD — DAMAGED (RT MLG WW) · airframe 81,112 hrs · 16,771 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD BULKHEAD REIN COMPLY WITH E..A. 1-5310-T0347293 REV NO. POS. P1 REPAIRED AREA IN REF. TO E.A 1-5310-T0347293

Part: ELBOW — DAMAGED (NR 2 ENGINE) · airframe 80,740 hrs · 16,646 cycles

AT CRUISE 20 MIN INTO THE FLIGHT HYD 2 LEFT AND RIGHT PUMPS FAULTED WITH AN AMBER T ABOVE THEM. HYD 2 QTY WAS 7.7 BUT THE TEMP OF THE HYD FLUID STARTED CLIMBING AND WAS BOXED AMBER. MAX TEMP WAS 120C. WHEN CONFIGURING FOR LANDING HYD 2 SYS. SLOWY CAME BACK TO NORMAL. REMOVED DAMAGED HIGH PRESSURE TURB AIR ELBOW PER IPC REF 75-23-05-01 AND INSTALLED NEW. PERFORMED ALL SYSTEM CHECKS OF NR 2 ENGINE AS THOUGH THE ENTIRE ENGINE WAS REPLACED PER MM 71-00-00-5-1, ALL CHECKS PASSED. RAN NR 2 ENG AT IDLE FOR LEAK AND OPS CHECK AND ALSO AT HIGH POWER PER JRH, ALL TEMPERATURES, AND INDICATIONS NORMAL. ANTI-ICE SYSTEM CHECKS NORMAL AND HYDRAULIC TEMPERATURES ALSO SHOW NORMAL PER OPERATING LIMITS. A/C OK FOR CONTINUED SERVICE.

Part: COMPUTER — FAILED (COCKPIT) · airframe 80,739 hrs · 16,645 cycles

ON DECENT INTO PHNL, THRU 6000' AURAL WARNING OF TIRE FAIL REPEATED 3 TIMES. LEVEL 3 BOXED TIRE FAIL ON EAD. CYCLED BETWEEN "TIRE FAIL" TO TIRE PRESSURE LOW. THIS WAS THE NR 7 AND NR 8 TIRES. THE ALERTS CLEARED AND NORMAL TIRE TEMP & PRESSURE RESUMED. REPLACED BRAKE TEMPERATURE MONITOR /TIRE PERSSURE INDICATING COMPUTER AS PER AMM 32-46-02-4, NO FAULTS NOTED. OK FOR SERVICE.

Part: HYDRAULIC LINE — LEAKING (MLG) · airframe 80,251 hrs · 16,492 cycles

PDIS 599 32-30 1847 04JAN19 BOM OPEN U LOGPAGES:3061325 AFTER T/O HANDLE WOULD NOT MOVE TO UP POSITION COMPLIED WITH QRN PART 04JAN19 10:11 MC1 U IDENTIFIED PARTS MLG HYD TRIM CYL MPN: AE1011181H0342 CPN: 3210706 QTY: 1 PART 04JAN19 10:12 MC1 U ORDER PART MPN: AE1011181H0342 CPN: 3210706 QTY: 1 MSN: 1950590 PART 04JAN19 10:48 MC1 U IDENTIFIED PARTS FUSE ASSY MPN: K3210483K2 CPN: 3215850 QTY: 1 (W/KIT) WHLWELL HYD PIPIN MPN: 6360-2 CPN: 3210483 QTY: 1 PART 04JAN19 10:49 MC1 U ORDER PART MPN: 6360-2 CPN: 3210483 QTY: 1 MSN: 1950592 FACT 04JAN19 16:57 BOM FOUND LEAK IN LEFT HAND TRUCK TRIM CYL DOWN LINE HOSE. REMOVED LINE AND INSTALLED ALT HOSES MPN 170141-8CR0240 AND MPN BACH30M080120 PER AMM 20-40-01-2, LEAK CHECK C/W, NO LEAK FOUND. OPS CHK C/W PER 32-37-10-4. BLEED HYD SYS PER AMM 32-37-10-4.

Part: TIRE — FAILED (ZONE 700) · airframe 80,225 hrs · 16,480 cycles

PDIS 599 32-42 1829 30DEC18 DWC FACT U LOGPAGES:3061310 NR 6 TIRE PRESS LO ALERT FOLLOWED BY TIRE FAIL. DECLARED EMERGANCY - DIRECTED TO DIVERT TO OMDW AFTER ARRIVAL NR 6 TIRE FOUND DEFLATED. PERFORMED VISUAL INSP - NO DAMADE NOTED. NR 6 TIRE REPLACED PER AMM 32-41-01-4. ACFT OK TO CONTINUE.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 80,099 hrs · 16,447 cycles

LEFT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE). INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE (HOLE #4) 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 EA # 1-5750-63187 E PART 3 STEP 1.F(1) AND STEP 1.F(3) TITLE: WINGS - FLIGHT SURFACES - LH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 INSPECTION - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57101164 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE HOLE (HOLE #4) 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 EA #: 1-5750-T0329602 B PART 1 STEP 1.F(1) AND STEP 1.F(3) TITLE: WINGS - FLIGHT SURFACES - RH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57501171 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE (HOLE #4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-07 AND EA #: 1-5750-T0329602 B PART 1 STEP 1.F(1) AND STEP 1.F(3) TITLE: WINGS - FLIGHT SURFACES - RH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. RFER TO WRI: 57501171 FOR WORK DETAILS.

Part: FINGER DOUBLER — DETACHED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING TRAILING EDGE INBOARD ISLAND UPPER SKIN FINGER DOUBLER AT XORS 449 FOUND DETACHED. RIGHT WING - TRAILING EDGE INBOARD ISLAND UPPER AT XORS 449 DAMAGED SKIN AREA REPAIRED AS PER SRM 57-50-01-2R FIGURE 202 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 80,099 hrs · 16,447 cycles

EMPENNAGE, DURING REMOVAL ACCESS FOR BANJO FITTING REPAIR, RIGHT HAND SIDE LOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL FOUND CRACK. INTERCOSTAL AT STATION 2164 REPAIR CARRIED OUT AS PER SRM 55-30-02-2R FIGURE 204 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 80,099 hrs · 16,447 cycles

LOWER CENTER CARGO DOOR FORWARD LOWER EDGE CRACKED AT STATION XIFH 1713.9. REPAIRED AS PER EA 1-5230-T0343643 P1. FWD LOWER CORNER OUTER SKIN CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RAIL — CORRODED (CARGO BAY) · airframe 80,099 hrs · 16,447 cycles

LOWER CENTER CARGO COMPARTMENT DURING UPON ACCOMPLISH EA 1-5310-T0338224 P3 TO CARRY OUT PERMANENT REPAIR CENTER CARGO JAMB RAIL AT STATION 1717. REPAIRED AS PER EA #: 1-5310-T0338224 A P3 TITLE: FUSELAGE - MAINFRAME - CENTER CARGO DOOR LOWER JAMB - CORROSION AT OUTER AND INNER RAILS BETWEEN STA 1710 AND STA 1725. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. REFER TO WRI: 53101196 FOR DETAILS.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 80,099 hrs · 16,447 cycles

NR 1 RAM AIR EXHAUST CUTOUT DOUBLER SUSPECT CRACKED STATION 561 LONGERON 48 LEFT. CRACKED DOUBLER REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-35-01-0G. NEW DOUBLER FABRICATED AS PER DRAWING ACA 3850 REVISION AA. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 428) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

FORWARD CABIN FLOOR SEAT TRACK AFT OF LAVATORY MODULE STATION 428 X = -27" FOUND WITH CORROSION. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED FROM STATION 421 TO STATION 485 X = -27.5 AS PER SRM 51-31-01-0G. NEW SEAT TRACK FABRICATED AS PER DRAWING ABA7684 REV G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

FORWARD CABIN FLOOR SEAT TRACK AT STATION 440 X = 18" FOUND WITH SURFACE CORROSION. CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED FROM STATION 440 TO STATION 495 X= 19 AS PER SRM 51-31-01-0G. NEW SEAT TRACK FABRICATED AS PER DRAWING SP11530031 REVISION NEW. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (LT TWING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

LEFT WING OUTBOARD FLAP VANE NO. 4 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSIONS. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343882 PART 1 STEP 1A. TRACK SUPPORT FITTINGS CORROSION REPAIR AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (LT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

LEFT WING OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSION. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343882 PART 1 STEP 1A. TRACK SUPPORT FITTINGS CORROSION REPAIR AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION CORROSIONS AT RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND EA #: 1-5750-T0329602 B PART1 STEP 1.F(1) AND STEP 1.F(3) TITLE: WINGS - FLIGHT SURFACES - RH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57501171 FOR WORK DETAILS.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONS. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. REPAIR BUSHING FABRICATED AS PER EA 1-5750-T0343705 P1 STEP 1A. TRACK SUPPORT FITTINGS CORROSION REPAIR AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSION. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. REPAIR BUSHING FABRICATED AS PER EA 1-5750-T0343705 P1 STEP 1A. TRACK SUPPORT FITTINGS CORROSION REPAIR AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 80,099 hrs · 16,447 cycles

RIGHT MAIN DECK COMPARTMENT FRAME AT STATION 1641 FOUND DENTED AT LONGERON 12 RIGHT. FRAME REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE FOUND CORROSION CORROSIONS AT RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUND PIVOT BORE SPOTFACE REMAINING THICKNESS: 0.457" (INBOARD) WITHIN LIMIT AS PER EA #: 1-5750-T0329602 B PART 1 STEP 1E FIGURE 2 TITLE: WINGS - FLIGHT SURFACES - RH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57501171 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND EA #: 1- 5750-63187 E PART 3 STEP 1.F(1) AND STEP 1.F(3) TITLE: WINGS - FLIGHT SURFACES - LH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 INSPECTION - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57101164 FOR WORK DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1359 X = -8.75 FOUND WITH CORROSION AS MARK. SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1331 TO STATION 1371 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND EA # 1-5750-63187 E PART 3 STEP 1.F(1) AND STEP 1.F(3) TITLE: WINGS - FLIGHT SURFACES - LH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 INSPECTION - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57101164 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUND PIVOT BORE SURFACE REMAINING THICKNESS: 0.443" (I/B) BEYOND REWORK LIMIT AS PER EA #: 1-5750-63187 E PART 3 STEP 1.E FIGURE 2 TITLE: WINGS - FLIGHT SURFACES - LH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 INSPECTION - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57101164 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND EA #: 1-5750-T0343678 P1 STEP 2.C AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750- T0343678 P1 AND SNRM N00323 FOR WORK DETAILS. (WRI: 57-50/1730)

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

RIGHT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT INBOARD LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 4-08 AND EA #: 1-5750-T0343678 P1 STEP 2.B AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750-T0343678 P1 AND SNRM N00323 FOR WORK DETAILS (WRI: 57-50/1730)

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. ACTUATOR LUG HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5740-63186 A P2 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

RIGHT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND EA #: 1-5750-T0343678 P1 STEP 2.C AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750- T0343678 P1 AND SNRM N00323 FOR WORK DETAILS. (WRI: 57-50/1730)

Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 80,099 hrs · 16,447 cycles

RIGHT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSIONS. CORROSION AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-4-08 AND EA #: 1-5750-T0343678 P1 STEP 2.B AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750-T0343678 P1 AND SNRM N00323 FOR WORK DETAILS (WRI: 57-50/1730)

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 80,099 hrs · 16,447 cycles

MAIN DECK CARGO COMPARTMENT LEFT HAND 9G NET SUPPORT YOKE FRAME AT STATION 535, LONGERON 24 LEFT, EXISTING REPAIR CHAFED. CHAFED EXISTING REPAIR REMOVED AS PER SRM 51-33-01-0G AND REPAIR CARRIED OUT AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) PIVOT BORE HOLE FOUND CORROSIONS. HINGE HOLE BORE (HOLE 4) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0343678 P1 STEP 2A AND STEP 2. INBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACK. DOUBLER REMOVED AS PER SRM 51-31-01-0G AND REPLACED WITH NEW RIB DOUBLER AS PER SRM 51-33-01-0G. FABRICATED RIB DOUBLER AS PER DWG ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FOUND CORROSION. CORROSIONS AT LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. OVERSIZED SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-09 AND EA #: 1-5750-T0343728 P1 STEP 2A AND STEP 2 TITLE: WING - FLIGHT SURFACES - EO 1-5750-7-5002 - LH WING - OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. CORROSIONS AT LEFT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND EA #: 1- 5750-T0343675 PART 1 STEP 2.B AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7- 5002 - LH WING - OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSIONS AT RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 03 AND EA #: 1-5750-127487 E PART 5 STEP 2 AND STEP 3 TITLE: WINGS - FLIGHT SURFACES - RH WING INBOARD FLAP OUTBOARD FWD HINGE (FLAP SIDE) REPAIR - PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57501736 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSIONS AT RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER MD-11CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-09. REPAIR EVALUATED AND FOUND BARREL NUT MATING SURFACE REMAINING THICKNESS OF UPPER: 0.423" AND LOWER: 0.434" WITHIN LIMIT BASE THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAX REWORK LIMITS FOR BARREL NUT HOLE. MINIMUM THICKNESS: 0.3765". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,099 hrs · 16,447 cycles

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

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

LEFT HAND INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE ( FLAP SIDE ) INBOARD PIVOT LUG HOLE BORE ( HOLE G AND F ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND EA#1-5750-63117 D PART 6 STEP 2 AND STEP 3. TITLE: WINGS - FLIGHT SURFACES - LEFT HAND WING INBOARD FLAP OUTBOARD HINGE ( FLAP SIDE ) REPAIR PSE 57 . 55 . 01 . 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57501740 FOR WORK DETAILS.

Part: FORMER — CRACKED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING FIXED LEADING EDGE UPPER FORMER AT XOS 584 FOUND CRACK. FIXED LEADING EDGE UPPER AT XOS 584 , NEW FORMER FABRICATED AS PER DOUGLAS DRAWING ARB2931 REVISION H. CRACKED FORMER REMOVED AND REPLACED WITH NEW FORMER AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 80,099 hrs · 16,447 cycles

LEFT WING FIXED LEADING EDGE UPPER FORMER AT XOS 584 FOUND CRACK. A NEW FORMER FABRICATED AS PER DOUGLAS DRAWING ARB2931 REVISION H. CRACKED FORMER REMOVED AND REPLACED WITH NEW FORMER AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSIONS AT LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND EA #: 1-5750-T0343728 P1 STEP 2B AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7-5002 - LH WING - OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750- T0343728 P1 AND SNRM N00127 FOR WORK DETAILS (WRI: 57-50 / 1733).

Part: DOUBLER — CRACKED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 639 FOUND CRACK.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSIONS AT RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND EA #: 1-5740-63186 A P2 STEP 1A AND STEP 1 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP OUTBD HINGE (WING SIDE) - CORROSION REPAIR. REAPIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5740- 63186 A P2 AND SNRM NO. N00287 FOR WORK DETAILS (WRI: 57-40 / 1732).

Part: DOUBLER — CRACKED (RT WING) · airframe 80,099 hrs · 16,447 cycles

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

Part: DOUBLER — CRACKED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 841 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 467 FOUND CRACK. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 80,099 hrs · 16,447 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 80,099 hrs · 16,447 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSIONS AT LEFT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-08 AND EA #: 1-5750-T0343675 PART 1 STEP 2.A AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7-5002 - LH WING - OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750- T0343675 PART1 AND SNRM N00156 FOR WORK DETAILS (WRI: 57-50 / 1731).

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

LEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE ( FLAP SIDE ) OUTBOARD PIVOT LUG HOLE BORE ( HOLE B AND A ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND EA#1-5750-63117 D PART 6 STEP 2 AND STEP 3. TITLE: WINGS - FLIGHT SURFACES - LEFT HAND WING INBOARD FLAP OUTBOARD HINGE ( FLAP SIDE ) REPAIR PSE 57 . 55 . 01 . 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57501740 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSIONS AT RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE (HOLE A ND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND EA #: 1-5750-127487 E PART 5 STEP 2 AND STEP 3. TITLE: WINGS - FLIGHT SURFACES - RH WING INBOARD FLAP OUTBOARD FWD HINGE (FLAP SIDE) REPAIR - PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57501736 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,099 hrs · 16,447 cycles

RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 618 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 80,099 hrs · 16,447 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSIONS AT LEFT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-08 AND EA #: 1-5750-T0343675 PART 1 STEP 2.A AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7-5002 - LH WING - OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750- T0343675 PART1 AND SNRM N00156 FOR WORK DETAILS (WRI: 57-50 / 1731).

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 80,099 hrs · 16,447 cycles

DURING HFEC INSPECTION CARRIED OUT AT LOWER VERTICAL STABILIZER UPPER REAR SPAR CAP LEFT FORWARD FLANGE AND FOUND 01 EACH CRACK WITH LENGTH OF APPROXIMATE 5/8" LONG. AT STATION 2164. LEFT HAND VERTICAL STABILIZER UPPER REAR SPAR CAP FORWARD FLANGE OF # 4 BANJO FITTING AT STATION 2164 CRACKED APPROXIMATELY 5/8" TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAIR 5 AND REPAIR CARRIED OUT AS PER SRM 55-30-02-2R FIGURE 202 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT 5400 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2700 FLIGHT CYCLES PER SRM 55-30- 02-2R TABLE 203 REPAIR 5.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 80,099 hrs · 16,447 cycles

MAIN DECK STATION 635 X = 47 SEAT TRACK FOUND CRACKED. THE SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665 X = 47 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RAIL — CORRODED (FUSELAGE) · airframe 78,163 hrs · 15,826 cycles

FUSELAGE MAINFRAME CENTER CARGO DOOR LWR JAMB RAIL AT FWD SPOOL AT STATION 1. COMPLY WITH EA 1-5310-T0338224 REV NR POS P1. REPAIRED STRUCTURAL JAMB RAIL IN AFT CENTER CARGO AT FWD SPOOL.

Part: SKIN — GOUGED (LT WING SLAT) · airframe 78,017 hrs · 15,769 cycles

LEFT WING LEADING EDGE UPPER SKIN BETWEEN XIS 286 - 247, SLAT TRACKS 3 AND 4 HAS SKIN GOUGES. FROM THE NR 2 SLAT T/E RUB STRIP. REPAIRED IAW SRM 57-40-02-2R, WITH 301 1-2HRD032, SHEET.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 76,802 hrs · 15,409 cycles

EMERGENCY LIGHT BATTERY ONE LOW ALERT DURING EMERGENCY LIGHT TEST. PERFORMED EMERGENCY LIGHT TEST IAW FIM 33-51-02-00, FIGURE 104, AND AMM 33-51-01-5. NO FAULTS NOTED AND OPS CHECKED GOOD, NO HISTORY. ACFT OK TO CONTINUE.

Part: LONGERON — CORRODED (BS 1139) · corrosion level 2 · airframe 75,144 hrs · 14,896 cycles

CENTER ACCESSORY COMPARTMENT BILGE AREA LONGERON 51L BS 6-100 CORRODED AND CRACKED. REPAIRED IAW EA 1-5310-T0329467 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 75,144 hrs · 14,896 cycles

ONE CRACK INDICATION APPROXIMATELY 2 INCHES IN LENGTH, FOUND DURING X-RAY INSPECTION BS 5-123, LONGERON SPLICE 3L. THE LONGERONSPLICE WAS REMOVED IAW SRM 51-33- 01-0G. A NEW LONGERON SPLICE WAS FABRICATED IAW DWG A5A7111 REV C AND INSTALLED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 75,144 hrs · 14,896 cycles

ONE CRACK INDICATION APPROXIMATELY 1 INCH IN LENGTH, FOUND DURING X-RAY INSPECTION AT BS 5-123, LONGERON SPLICE 2L FWD CENTRE SECTION. THE LONGERON SPLICE WAS REMOVED IAW SRM 51-33-01-0G. A NEW LONGERON SPLICE WAS FABRICATED IAW DWG A5A7111 REV C AND INSTALLED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 75,144 hrs · 14,896 cycles

TWO CRACK INDICATIONS APPROXIMATELY 1 INCH, EACH LENGTH FOUND DURING X-RAY INSPECTION AT STA 5-123, LONGERON 1L SPLICE AFT AND FWD CTR SECTION. THE LONGERON SPLICE REMOVED IAW SRM 51-33-01-0G. A NEW LONGERON SPLICE WAS FABRICATED IAW DWG #A5A7111 REV C AND INSTALLED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 200) · airframe 75,144 hrs · 14,896 cycles

TWO CRACK INDICATIONS APPROXIMATELY ONE INCH, EACH IN LENGTH. FOUND DURING X-RAY INSPECTION AT BS 5-123 AT LONGERON 6R SPLICE AFT CTR SECTION. REPAIRED IAW DWG A5A7112 REV 'D' AND SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 75,144 hrs · 14,896 cycles

FOUND CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION ON RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 75,144 hrs · 14,896 cycles

FOUND CRACK INDICATION DURING HFEC INSPECTION ON LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6.6. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 75,144 hrs · 14,896 cycles

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

Part: SEAT TRACK — CORRODED (BS 775) · airframe 75,144 hrs · 14,896 cycles

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

Part: SEAT TRACK — CORRODED (BS 1289) · airframe 75,144 hrs · 14,896 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1289, X=-47.5 FOUND CROWN DAMAGED. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,144 hrs · 14,896 cycles

LT WING LEADING EDGE CAVITY AT XOS 621 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,144 hrs · 14,896 cycles

MAIN DECK SEAT TRACK AT BS 1681, LBL 47.5 FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,144 hrs · 14,896 cycles

RT WING FIXED LEADING EDGE CAVITY AT XOS 699 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. CLASSIFIED AS A MAJOR IAW GMM 6-2-100.

Part: DOUBLER — DAMAGED (BS 535) · airframe 75,144 hrs · 14,896 cycles

MAIN DECK LT SIDEWALL FRAME AT BS 535, LONGERON 24L FOUND REPAIR DOUBLER DAMAGED. REPAIRED IAW SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 75,144 hrs · 14,896 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 5-73, X= 8.5 FOUND CORROSION. THE SEAT TRACK WA REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,144 hrs · 14,896 cycles

RT WING FIXED LEADING EDGE CAVITY AT STA XOS 651 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. CLASSIFIED AS A MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 75,144 hrs · 14,896 cycles

RT WING FIXED LEADING EDGE CAVITY AT XOS 778 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,144 hrs · 14,896 cycles

MAIN DECK SEAT TRACK AT BS 1289, LBL 8.5 FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 75,144 hrs · 14,896 cycles

LT WING FIXED LEADING EDGE CAVITY AT XOS 654 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. CLASSIFIED AS A MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 635) · airframe 75,144 hrs · 14,896 cycles

MAIN DECK SEAT TRACK AT BS 635, LBL 8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CONTACT — BURNED (STROBE) · airframe 74,402 hrs · 14,658 cycles

LEFT UPPER STROBE INOPERATIVE. FOUND BURNED INTERNAL CONTACT IAW AMM 33-47-01-2.

Part: GROMMET — WORN (CABIN) · airframe 728 hrs · 14,103 cycles

DURING PREFLIGHT, FOUND LIGHT COVER OFF OF LIGHT PANEL, ABOVE GALLEY, COVER IN COAT CLOSET. INSTALLED NEW GROMMETS PN 250 IAW SMP.

Part: SKIN — DAMAGED (RT WING) · airframe 727 hrs · 14,073 cycles

DURING POST FLIGHT, FOUND DAMAGE, DENT & 4" LONG CRACK, TO RT WING, FIXED LE SKIN. DAMAGE IS ON UNDERSIDE OF WING LE, BEHIND INBD END OF NR 5 SLAT. REPAIRED IAW EA 1-5730-T0320545 P1.

Part: SKIN — CRACKED (ZONE 200) · airframe 70,479 hrs · 13,392 cycles

R3 PLUG DOOR CUT OUT SURROUNDING FOUND ONE CRACK, INSPECTION ACCESS, FWD MOST LOWER ACCESS. REPAIRED IAW SRM 53-40-15, FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CRACKED (LT MLG DOOR) · airframe 70,479 hrs · 13,392 cycles

MAIN LANDING GEAR LT DOOR SIDE, AFT DOOR HINGE FITTING FOUND WITH CRACKED. REMOVED AND REPLACED IAW SRM 51-35-01 REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100

Part: FORMER — CRACKED (ZONE 600) · airframe 70,479 hrs · 13,392 cycles

RIGHT WING FIXED LE SUPPORT FORMER FOUND CRACKED AT XOS 584. FORMER REMOVED AND REPLACED IAW SRM 51-33-01. FORMER FABRICATED IAW DRAWING ARB2931 REVISION H. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1561) · corrosion level 2 · airframe 70,479 hrs · 13,392 cycles

SEAT TRACK BS 1561 X=8 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, REPAIR 1, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 70,479 hrs · 13,392 cycles

RIGHT WING LE RIB DOUBLER FOUND CRACKED AT XOS 667. DOUBLER FABRICATED IAW DRAWING ARB3954 REVISION K. RIB DOUBLER REMOVED AND REPLACED IAW SRM 51-33-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 70,479 hrs · 13,392 cycles

RIGHT WING FIXED LE NR 15 SLAT TRACK CUT OUT FOUND CRACKED XOS 944. REPAIRED IAW SRM 57-40- 02 FIGURE 201, REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (ZONE 600) · airframe 70,479 hrs · 13,392 cycles

RIGHT WING LE SUPPORT FORMER FOUND CRACKED AT XOS 559. FORMER FABRICATED IAW DRAWING ARB1162 REVISION S. FORMER REMOVED AND REPLACED IAW SRM 51-33-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 1561) · corrosion level 2 · airframe 70,479 hrs · 13,392 cycles

SEAT TRACK BS 1561 X -8 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, REPAIR 1, FIGURE 201. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 70,479 hrs · 13,392 cycles

LEFT WING FIXED LE PANEL 519CB FWD CORNER CUT OUT FOUND CRACKED XOS 610. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: PANEL — CRACKED (LT WING) · airframe 70,479 hrs · 13,392 cycles

LEFT WING LE PANEL 518FB FWD CORNER CUT OUT FOUND CRACKED XOS 500. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: BOLT — PULLED (AILERON ACTUATOR) · airframe 69,316 hrs · 13,042 cycles

DURING CONTROL CHECK, NO GREEN BOX ON RT AILERON. RETURNED TO GATE. FOUND RT INBD AILERON DROPPED WITH HYD POWER ON, FURTHER INSPECTION FOUND RT INBD ACTUATOR DETACHED FROM WING STRUCTURE, ALL FOUR BOLTS PULLED OUT FROM ACTUATOR. REMOVED AND REPLACED RT INBD AILERON ACTUATOR IAW AMM 27-13-20-4.

Part: LINER — DAMAGED (NR 1 ENGINE) · airframe 68,289 hrs · 12,712 cycles

AFTER ADDING POWER FOR TAKEOFF & ACCELERATING THROUGH 60 KTS, HEARD A LOUD HISSING NOISE & FELT SWERVE TO THE LEFT. ABORTED TAKEOFF & RETURNED TO THE GATE. NO ABNORMAL ENGINE INDICATIONS, BUT AFTER RETURN TO GATE, DISCOVERED HONEYCOMB MATERIAL IN THE FAN BLADES. NR 1 ENGINE SEGMENT FWD OUTER LINERS BROKEN. REPLACED THE BROKEN OGV STATOR SEGMENTS AND BROKEN OGV STATOR VANE AND REINSTALLED ALONG WITH FAN STATOR FAIRING. ALSO REINSTALLED THE FOUR NEW ACCOUSTICAL LINER SEGMENTS.

Part: MECHANISM — DIRTY (MLG) · airframe 66,510 hrs · 12,149 cycles

AFTER TAKEOFF, RECEIVED RED PRIMARY & SECONDARY LIGHTS WITH THE GEAR HANDLE UP. RAN QRH AND RED LIGHT WENT OUT. TRIED TO WIGGLE AND PUSH GEAR HANDLE PRIOR TO CYCLING GEAR. ALL LIGHTS STAYED ON. PUT GEAR HANDLE DOWN, HANDLE WAS STUCK OUT AND NEEDED TO BE PUSHED IN TO INDICATE FOUR GREEN LIGHTS. NEXT RETRACTION WAS NORMAL. CLEANED AND LUBRICATED THE LANDING GEAR CONTROL MECHANISM IN REF TO AMM 32-31-007, CYCLED HANDLE THROUGH SEVERAL TIMES AND SYS OPERATED NORMALLY, ACFT IS OK FOR CONTINUE SERVICE.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 65,707 hrs · 11,896 cycles

SEVEN FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 690 AND XORS= 700. REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 65,707 hrs · 11,896 cycles

TWELVE FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 690 AND STA XORS= 700. REPAIRED AS PER SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: BEAM — CRACKED (ZONE 200) · airframe 65,707 hrs · 11,896 cycles

UPON REMOVAL OF MAIN DECK R3 DOOR FOUND UPPER BEAM AFT END CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — CORRODED (BS 1220-1250) · corrosion level 2 · airframe 65,707 hrs · 11,896 cycles

MAIN DECK COMPARTMENT- FLOOR SEAT TRACK FOUND WITH CORROSION AT BS 1220 TO 1250 X= -75. CARRIED OUT SEAT TRACK SEGMENT REPLACEMENT REPAIR IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 65,707 hrs · 11,896 cycles

CENTER CARGO DOOR ROTARY ACTUATOR BEAM FOUND CRACKED. REPAIRED IAW E.A. 1-5310-165173. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 65,707 hrs · 11,896 cycles

LEFT WING NR 8 SLAT TRACK UPPER DOOR CUT-OUT CRACKED. REPAIRED AS PER E.A. 1-5730-163557. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,707 hrs · 11,896 cycles

MAIN DECK COMPARTMENT- FLOOR SEAT TRACK FOUND WITH CORROSION AT BS 1250 TO 1390 X=-75. CARRIED OUT REPAIR IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,707 hrs · 11,896 cycles

MAIN DECK COMPARTMENT -FLOOR SEAT TRACK FOUND WITH CORROSION AT BS 1390 TO 1530, RBL 75. CARRIED OUT REPAIR IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 600) · airframe 65,707 hrs · 11,896 cycles

RT WING SLAT TRACK NR 12 LOWER OTBD CUT-OUT CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (A/C DOOR) · airframe 65,707 hrs · 11,896 cycles

LEFT AIR CON COMPARTMENT NR 2 DOOR EXTERIOR UPPER SKIN EDGE CRACKED. REPAIRED AS PER SRM 52-40-01 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 65,707 hrs · 11,896 cycles

RT WING T/E PANEL 641JB CUT-OUT WITH CORROSION. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — PUNCTURED (NR 2 SLAT) · airframe 65,707 hrs · 11,896 cycles

RIGHT WING NR 2 SLAT LOWER SURFACE SKIN PUNCTURED. REPAIRED IAW EA 1-5750- 163560. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CORRODED (LT WING TE) · corrosion level 2 · airframe 65,707 hrs · 11,896 cycles

LT WING T/E PANEL 541JB CUT-OUT WITH CORROSION. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: DUCT — CRACKED (ZONE 500) · airframe 65,707 hrs · 11,896 cycles

LT WING TELESCOPIC DUCT UPPER DOOR CUT-OUT CRACKED. REPAIRED IAW SRM 57-40- 01 REPAIR 10 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 61,438 hrs · 10,724 cycles

L1 EMERGENCY EXIT LIGHT COVER DROPPED OFF. R & R EMERG EXIT LIGHT COVER ALIGNMENT PINS, OPS CKS GOOD. OK FOR SERVICE. FINAL CLOSED.

Part: BLADES — DAMAGED (ENGINE) · airframe 60,643 hrs · 10,535 cycles

DURING INITIAL CLIMBOUT, FELT MODERATE VIBRATION (FELT LIKE NOSE GEAR SPINNING). AFTER INITIAL LEVEL OFF AT 9000 FT, VIBRATION LESSENED. DURING CLIMB TO 15000 FT, VIBRATION CONTINUED TO REVERSE WITH HIGH EVM READING. RAN QRH & WITH HIGH EVM & VIBRATION AT HIGH POWER SETTING ELECTED TO RETURN TO DEPARTURE. NO REVERSE USED ON & NR 2 SHUTDOWN ON GROUND AFTER COOLING. FOUND 3 ADJACENT BLADES DAMAGED & 3 MORE BLADES DAMAGED APPX 160 DEG AWAY FROM FIRST 3. 1 OTHER BLADE SLIGHTLY DAMAGED 1 BLADE AWAY FROM SECOND 3. FROM FIRST BLADE REFERENCED NR 1, DAMAGED BLADES ARE GOING CCW FACING BLADES 1, 2, 3, 14, 16, 17, 18. INSPECTED BLADES 14, 16, 17, AND 18, WITHIN LIMITS IAW MM 72-30-00-6. DUE TO RECALCULATED FAN BALANCE, ZEROED SPINNER WITH NO SPINNER WEIGHTS. R & R 7 DAMAGED FAN BLADES INCLUDING 4 WITHIN LIMITS, DUE TO FPI INSP NOT AVALIABLE PDX. RECALCULATED FAN BALANCE & INSTALLED FAN BLADES IAW MM 72-31-02-4. ACCOMPLISHED POWER ASSURANCE CHECK & VIBRATION CHECK IAW JRH & MM 71-00-00-5. ALL PARAMETERS NORMAL. ACFT OK FOR SERVICE.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,598 hrs · 10,518 cycles

MAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= 95.5 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.153 INCH. MATERIAL REMOVED = 0.014 INCH AND FOUND ACCEPTABLE AS PER E.A. 1-5710-143826, . REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,598 hrs · 10,518 cycles

MAIN DECK - OVERWING TANK UPPER SURFACE AT STA 1227, X= 99.5 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.151 INCH. MATERIAL REMOVED = 0.016 INCH AND FOUND ACCEPTABLE AS PER FEDEX E.A. #1-5710-143826, TITLE: WINGS - BASIC WING STRUCTURE - CENTER WING UPPER AUXILLARY FUEL TANK SKIN CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,598 hrs · 10,518 cycles

MAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= 88 TO X= 84 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.150 INCH. MATERIAL REMOVED = 0.017 INCH AND FOUND ACCEPTABLE AS PER E.A. #1-5710-143826. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,598 hrs · 10,518 cycles

MAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= 99.5 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.151 INCH. MATERIAL REMOVED = 0.016 INCH AND FOUND ACCEPTABLE AS PER E.A. 1-5710-143826. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: FUEL CELL — CORRODED (OVERWING) · corrosion level 2 · airframe 60,598 hrs · 10,518 cycles

MAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= -80 TO X= -101 FOUND SEVERAL AREAS OF CORROSION. CORROSION REPAIRED IAW EA NR1-5710-143826, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: FUEL CELL — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,598 hrs · 10,518 cycles

MAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= 60.5 FOUND CORROED. CORROSION REMOVED IAW SRM 51-21-01, REV 45. ORIGINAL MATERIAL THICKNESS = 0.167 INCH, REMAINING THICKNESS = 0.137 INCH. MATERIAL REMOVED = 0.030 INCH AND FOUND. ACCEPTABLE IAW EA NR1-5710-143826, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,598 hrs · 10,518 cycles

MAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= -60 TO X= -8 FOUND SEVERAL AREAS OF CORROSION. CORRODED AREA REPAIRED IAW EA NR1-5710-143826, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 111.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 60,598 hrs · 10,518 cycles

MAIN DECK STA 650, X =75.25, FOUND SEAT TRACK CRACKED. MAIN DECK-CRACKED SEAT TRACK AT STA 650, X =75.25 REPAIRED FROM STA 643 TO STA 685 IAW EA NR1-5310-143827 PART 1, TITLE: FUSELAGE - MAIN FRAME - CURVED SEAT TRACK REPAIR AT X = 75.25 AND STA 643. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: FRAME — DENTED (ZONE 200) · airframe 60,598 hrs · 10,518 cycles

MAIN DECK CABIN, FRAME AT STA 1661, LONGERON 12 RT, FOUND DENTED. CARRIED OUT REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 45. REPETIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 2 REV 45. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: FRAME — DENTED (ZONE 200) · airframe 60,598 hrs · 10,518 cycles

MAIN DECK CABIN, FRAME AT STA 1561, LONGERON 12 RT FOUND DENTED. CARRIED OUT REPAIR IAW SRM 53-00-07, FIGURE 201, REPAIR 2, REV 45. REPETIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 2 REV 45. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,598 hrs · 10,518 cycles

LOWER CTR CARGO COMPARTMENT - BILGE AREA STA 5-123 LONGERON 44R FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-00-05 REPAIR 1 FIGURE 202 REVISION 45 AND E.A. 1-5310-143504, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 60,598 hrs · 10,518 cycles

LWR CTR CARGO COMPARTMENT BILGE AREA STA 5-123, LONGERON 49 LT SPLICE FITTING FOUND CRACKED. SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 45. NEW SPLICE FITTING FABRICATED AS PER DRAWING A5A7114 REVISION F. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: RIB — CRACKED (ZONE 600) · airframe 60,598 hrs · 10,518 cycles

RT WING L/E RIB 16 FOUND CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. NEW RIB FABRICATED AS PER DRAWING ARB2850, REVISION G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 60,598 hrs · 10,518 cycles

RT WING INBD FLAP VANE LOWER SURFACE DELAMINATED. RT WING INBD FLAP VANE ASSY R & R IAW AMM27-50-22-4 REV 69.0. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5 REV 69.0.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 60,598 hrs · 10,518 cycles

LT WING INBD FLAP VANE LOWER SURFACE MID AREA 05 EACH LOCATION DELAMINATED. LT WING INBD FLAP VANE ASSY R & E IAW AMM27-50-22-4 REV 69.0. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5. REV 69.0.

Part: RELAY — INOPERATIVE (BATTERY) · airframe 58,686 hrs · 10,046 cycles

IN LEVEL FLIGHT AT FL330, RECEIVED A LEVEL 1 BAT DISCHARGING ALERT. IT STAYED ON FOR ABOUT 3 MIN, WENT OUT FOR ABOUT 1 MIN, THEN REMAINED ON FOR THE REMAINDER OF THE FLIGHT. R & R R2-17 RELAY IAW SWP 24-31-00, OPS CHECK OF ELECTRICAL BATTERY IAW AMM 24-32-00-05 NO DISCREPANCIES NOTED. PERFORMED EPCU RTS IAW AMM 24-08-01-5 ALL TEST PASSED. ACFT OK TO CONTINUE SERVICE.

Part: CONNECTOR — CORRODED (MLG) · airframe 58,657 hrs · 10,034 cycles

AFTER T/O OAK GEAR SHOWED RED LT MAIN PRIMARY SECONDARY. COMPLED WITH CHECK LIST, RECKED GEAR PRIMARY SECONDARY BOTH SHOW GREEN LANDED MEM WITHOUT INCIDENT. INTERROGATED PSEU AND FOUND NO FAULTS ON SYS. TEST IAW AMM ATA 31-71-01-2. CHECKED D1-81 AND FOUND NO PROBLEMS. ADJUSTMENT WAS CORRECT IAW AMM ATA 32-61-15. LT GEAR DOOR LATCH SENSOR LINK CHECKED GOOD. ALL SECURE. INSPECTED LT DOWN/LOCK PRIMARY AND SECONDARY SENSORS AND FOUND CONNECTOR PLUGS CORRODED ON BOTH SENSORS. R & R THE SAME IAW AMM 32-61-15-5.

Part: PSEU — FAILED (MLG) · airframe 58,653 hrs · 10,033 cycles

AFTER TAKEOFF HAD AN UNSAFE GEAR INDICATION FOR LT MAIN ON BOTH PRIMARY AND SYNOPTIC DISPLAY WHEN GEAR RETRACTED. COMPLETED WITH QRH, RECYCLED GEAR AND GOT A NORMAL UP INDICATION ON BOTH PRIMARY AND SYNOPTIC. LANDED WITHOUT INCIDENT. VISUALLY INSPECTED LT MLG/DOOR-NO DISCREPANCY NOTED. PERFORMED BITE TEST ON PSEU, FOUND FOLLOWING FAULT CODES:19,11,21,13,20,12. PERFORMED ADJ/TEST OF MLG UP AND DOOR PROX SENSOR/TARGET D1-81, FOUND NORMAL AND WITHIN LIMIT. R & R PSEU(U1-1036). FUNCTIONAL TEST SATISFACTORY. ACFT OK FOR SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 58,040 hrs · 9,904 cycles

ENG NR1 OIL TEMP HI ALERT APPEARED, ALL OTHER INDICATIONS NORMAL. OIL TEMP MAXED AT 220 DEGREES C. SHUTDOWN NR1 ENG IAW QRH. OIL TEMP RETURNED TO 80 DEGREE C IMMEDIATLY AFTER SHUTDOWN. VIA SATCOM CONSULTED WITH GOC, MOCC, POWERPLANT DUTY OFFICER AND TECH PILOT. 450 INTO FLT ACCOMPLISHED INFLIGHT RESTART, ALL ENG INDICATIONS NORMAL. BLEED AIR NR 1 OFF ALERT AFTER RESTART. OIL TEMP OVER 175 NR C 10 TO 12 MIN. ACCOMPLISHED FIM 79-00 FIG-108 FOR OIL TEMP FLUCTATING & FIM 79-00- FIG- 103 TO ADDRESS HIGH OIL TEMP NO DEFECTS FOUND. REPLACED DEFECTIVE NR 2 DEU PER AMM 31-61-02-4

Part: SUPPORT — CRACKED (ZONE 700) · airframe 55,243 hrs · 9,241 cycles

LEFT MAIN LANDING GEAR WHEEL WELL, CUT-OUT ON GEAR DOOR CYLINDER SUPPORT CRACKED AT STA 1441. LEFT MAIN LANDING GEAR WHEEL WELL, CUT-OUT ON GEAR DOOR CYLINDER SUPPORT AT STA 1441 REPAIRED AS PER FEDEX EA NR 1-5310-127493 TITLE: FUSELAGE, MAIN FRAME, LEFT MAIN LANDING GEAR DOOR SUPPORT AEA0218-501 LIGHTENING HOLE DAMAGED REPAIR. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100 REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 55,243 hrs · 9,241 cycles

RIGHT INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) PIVOT LUG OUTBOARD BORE FOUND CORROSION. REPAIRED AS PER E.A. 1-5750-127487, NEW BUSHING INSTALLED AS PER EA 1-5750-127487. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: HINGE — CORRODED (ZONE 600) · airframe 55,243 hrs · 9,241 cycles

RIGHT INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) PIVOT LUG INBOARD BORE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127487, BUSHING FABRICATED AS PER MD 11 CMM 57-52-03 REVISION 63 AND NEW BUSHING INSTALLED AS PER E.A. NO. 1-5750-127487. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 55,243 hrs · 9,241 cycles

CRACK INDICATION APPROXIMATELY 1.5 INCH FOUND ON RIGHT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGES OF UPPER REAR SPAR CAPS AREA. REPAIRED AS PER SRM 55-20-00 FIGURE 3 VOLUME I REVISION 40. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100 REVISION 107. REPETITIVE INSPECTION REQUIRED, INITIAL AT 5400 CYCLES AND REPETITIVE INSPECTION AT 2700 CYCLES AS PER SRM 55-20-00 FIGURE 3 VOLUME I REVISION 40.

Part: FRAME — DEFORMED (ZONE 200) · airframe 55,243 hrs · 9,241 cycles

MAIN DECK, AT STA 1701 LONGERON 12 LEFT, FRAME FOUND DEFORMED. REPAIRED AS PER SRM 53-30-00 FIGURE 1, VOLUME I REVISION 40. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1, VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 55,243 hrs · 9,241 cycles

MAIN DECK, AT STATION 1006, X = 8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 989 TO STA 1029, X = 8.5, AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,243 hrs · 9,241 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES NR A, NR B AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 55,243 hrs · 9,241 cycles

LEFT INBOARD FLAP UPPER SURFACE FOUND CHAFED THROUGH ON SKIN AT 9 INCHES OUTBOARD OF INBOARD END. TRIMMED OFF AS PER SRM 57-10-00 FIGURE 39 VOLUME I REVISION 40. REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIGURE 39 VOLUME I REVISION 40.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,243 hrs · 9,241 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME I I REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SKIN — CRACKED (ZONE 600) · airframe 55,243 hrs · 9,241 cycles

RIGHT WING LEADING EDGE SLAT TRACK NR 14 CUTOUT FOUND CRACKED AT CORNER EDGE. OUT CRACKED CORNER EDGE, TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,243 hrs · 9,241 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,243 hrs · 9,241 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,243 hrs · 9,241 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SKIN — CRACKED (ZONE 500) · airframe 55,243 hrs · 9,241 cycles

LEFT WING LEADING EDGE SLAT TRACK NR 14 CUTOUT FOUND CRACKED AT CORNER EDGE. OUT CRACKED CORNER EDGE, TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,243 hrs · 9,241 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES NR B, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,243 hrs · 9,241 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: UPLOCK SENSOR — MALFUNCTIONED (RT MLG) · airframe 53,317 hrs · 8,828 cycles

RT MAIN LDG GEAR WOULD NOT RETRACT ON FIRST ATTEMPT. SLOWED TO <230KIAS AND RECYCLED GEAR. 2ND RETRACT ATTEMPT WAS SUCCESSFUL. AS CREW BRIEF, DID NOT SEE SECONDARY MAIN LANDING GEAR INDICATION WHEN HAD NOT RETRACT. ALSO THEY COULD NOT FEEL ACTUAL DRAG. PERFORMED EXTERNAL VISUAL CK, FOUND NO DAMAGE AND NEED MORE T/S. FOUND CLEARANCE ON RT LANDING GEAR UP AND LOCK SENSOR OF 3.577MM (OUT OF LIMIT). REMOVED AND REPLACED RT LANDING GEAR UP AND LOCK SENSOR PER MM 32-61-15-4 AND ADJUSTED CLEARANCE PER MM 32-61-15-5. RT LANDING GEAR UP AND LOCK SENSOR R-T-S PASSED. A/C OK FOR SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (NR 2 SLAT) · airframe 53,211 hrs · 8,803 cycles

DURING APPROACH TO LFPG EXPERIENCED A LEVEL NR 2 "SLAT DISAGREE" ALERT DURING SLAT EXTENSION. COMPLIED WITH QRH AND CONDUCTED A FLAP/RETRACT LANDING TO RUNWAY 26R AT LFPG. LANDING WEIGHT WAS REDUCED AS MUCH AS POSSIBLE AND NO FURTHER PROBLEMS WERE ENCOUNTERED. CREW DECLARED A EMERGENCY. T/S AS PER FIM:31-71-07-00. SELF TEST ON PSEU SHOWED NO FAULT, LEG-1 WAS SHOWING A FAULT CODE 12. FOLLOWED T/S TREE, REMOVED AND REPLACED PSEU AS PER AMM:31-71-01-2. CARRIED OUT ADJ/TEST AS PER AMM:31-71-01-2 AND PERFORMED SLAT ELECTRICAL CONTROL ADJ/TEST AS PER AMM:27-86-00-5. ALL TESTS PASSED. A/C OK FOR SERVICE. RETURNED TO SERVICE.

Part: SKIN — DENTED (ZONE 500) · airframe 50,330 hrs · 8,145 cycles

LT WING INBOARD FLAP LOWER SEGMENT FOUND WITH SEVERAL DENTS. 10-05-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — DENTED (ZONE 600) · airframe 50,330 hrs · 8,145 cycles

RT WING INBOARD FLAP LOWER SEGMENT FOUND WITH SEVERAL DENTS. 10-05-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 200) · airframe 50,330 hrs · 8,145 cycles

RT WING TO FUSELAGE BODY FAIRING ENCLOSED AREA FOUND LONGERON 28 AT STA 1289 WITH CORROSION. 10-04-07 CORROSION REMOVED AS PER SRM 51-31-012 VOLUME II. HOLES PICKED UP ON NEW LONGERON AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPIAR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 50,330 hrs · 8,145 cycles

MAIN DECK CARGO COMPARTMENT, MAINFRAME STA 1681 AT LONGERON 12L FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 50,330 hrs · 8,145 cycles

MAIN DECK CABIN SEAT TRACK AT STA 635, X = 27.5 LT FOUND WITH CRACK. FOUND AFTER REMOVAL OF LOWER FWD CARGO CEILING PANEL. 10-04-07 REPAIRED BY SECTION A SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 50,330 hrs · 8,145 cycles

MAIN DECK CARGO COMPARTMENT: MAINFRAME STA 1681 AT LONGERON 12R FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYLCES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 50,330 hrs · 8,145 cycles

MAIN DECK CARGO COMPARTMENT: MAINFRAME STA 1701 AT LONGERON 12L FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYLCES TO BE CARRIE OUT AS PER SRM 53-30-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 50,330 hrs · 8,145 cycles

MAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1741 AT LONGERON 12L FOUND WITH DENT. 10-04-07 REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG I VOL I. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYLCES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,330 hrs · 8,145 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK STA 770, X = 75.25 FOUND EDGE CHIPPED. 10-04-07 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ATTACH FITTING — CRACKED (LT MLG WW) · airframe 50,330 hrs · 8,145 cycles

LEFT MAIN LANDING GEAR WHEEL WELL, FOUND STRUT ATTACHMENT FLIPPER DOOR CRACKED. 10-04-07 CARRIED OUT REPAIR AS PER SRM 52-10-00 FIGURE 18 VOLUME I. OPS CHECK CARRIED OUT AS PER AMM 32-31-00-700-803 FOUND 'SAT'. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 50,330 hrs · 8,145 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK STA 755, X = 47.5 FOUND EDGE CHIPPED. 10-04-07 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 50,330 hrs · 8,145 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK STA 755, X= 8.5 FOUND EDGE CHIPPED. 10-04-07 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STOP FITTING — CRACKED (LT WING TE FLAP) · airframe 50,330 hrs · 8,145 cycles

LEFT WING OUTBOARD FLAP SECONDARY UPSTOP FITTING FOUND CRACKED. 10-04-07 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUT — CRACKED (FUSELAGE) · airframe 50,330 hrs · 8,145 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL FOUND STRUT ATTACHING FLIPPER DOOR CRACKED. 10-04-07 CARRIED OUT REPAIR AS PER SRM 52-10-00 FIGURE 18 VOLUME I. OPERATIONS CHECK OF RIGHT HAND MAIN LANDING GEAR FLIPPER DOOR CARRIED OUT AS PER AMM 32-31-00-700-803 FOUND 'SATIS'. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 50,330 hrs · 8,145 cycles

RIGHT WING LEADING EDGE CAVITY STRINGER AT XOS 667 FOUND CRACKED. 10-04-07 STRINGER REPAIRED AS PER FEDEX E.A. 1-5710-113193. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 50,330 hrs · 8,145 cycles

RIGHT WING NR 3 SLAT TELESCOPIC DUCT CUTOUT FOUND CRACKED. 10-04-07 REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 50,160 hrs · 8,114 cycles

PASSING 9000FT AFTER T/O CAPT NOTICED FAINT BURNT PAPER ODOR. NO OTHER INDICATIONS, F/O WENT TO COURIER AREA NO FUMES BUT NOTICED EMERGENCY LIGHT ON. CAPT MADE DECISION TO RETURN TO HKG. DECLARED EMERGENCY, UNEVENTFUL LANDING. PANELED SHUTDOWN ENGS TO REMOVE PWR FROM A/C. REPLACED NR 2B TRANSFORMER RECTIFIER. REMOVED ALL DU, AFS PANELS AND FLIGHT CONTROL PANELS, NO FAULTS. OVERHEAD CB PANEL INSP'D AND CKD OK. REMOVED AND REPLACED EPCU. REPLACED ALL 3 COALESCER BAGS INSP THE COCKPIT WINDSHIELD HEAT ELECTRICAL WIRE, THE AV COMPT AND LWR FWD CARGO TEMP CONTROL VALVE RT SIDE. EMERG LIGHTS CKD OK.

Part: BRACKET — CORRODED (ZONE 600) · airframe 45,688 hrs · 7,125 cycles

RIGHT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-97759, WINGS RT OUTBOARD TRAILING EDGE FLAP, INBD BRACKET OUTBD FORWARD AND INBD AFT ATTACHMENT BORE CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · airframe 45,688 hrs · 7,125 cycles

RIGHT WING OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING OUTBOARD FORWARD HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-97759 WINGS RT OUTBOARD TRAILING EDGE FLAP. INBD BRACKET OUTBD FORWARD AND INBD AFT ATTACHMENT BORE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: STRUT — CORRODED (ZONE 600) · airframe 45,688 hrs · 7,125 cycles

RIGHT WING OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING FORWARD HOLE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP INBOARD FLAP HINGE AFT FITTING FORWARD HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-97760, TITLE, WINGS OUTBOARD TRAILING EDGE FLAP. RIGHT INBOARD SUPPORT STRUT, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUT — CORRODED (ZONE 600) · airframe 45,688 hrs · 7,125 cycles

RIGHT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-97760, WINGS OUTBOARD TRAILING EDGE FLAP RT INBD SUPPORT STRUT CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING OUTBOARD AFT HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FLAP HINGE FORWARD FITTING OUTBOARD AFT HOLE CORROSION REPAIRED AS PER FEDEX E.A. NR 1-5750-99639, TITLE: WINGS LEFT OUTBOARD TRAILING EDGE FLAP, INBOARD BRACKET ATTACHMENT BORES CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-99639, WINGS LH OUTBOARD TRAILING EDGE FLAP INBD BRACKET ATTACHMENT BORE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 45,688 hrs · 7,125 cycles

FORWARD CARGO DOOR CUTOUT, FUSELAGE SKIN ON FORWARD DOOR JAMB FOUND WITH SCRATCHES AT LONGERON 40R. SCRATCH MARK AT FORWARD CARGO DOOR CUT-OUT FUSELAGE SKIN ON FORWARD DOOR JAMB TRIMMED OUT AND CARRIED OUT. REPAIR AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 600) · airframe 45,688 hrs · 7,125 cycles

RT WING - OUTBOARD FLAP, INBOARD HINGE FITTING, INBOARD AFT BORE HOLE FOUND CORRODED. RIGHT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMENT TEST CARRIED OUT AS PER MM 27-50-00-710-801.

Part: STRUT — CORRODED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING AFT HOLE FOUND CORRODED. LEFT HAND WING OUTBOARD FLAP INBOARD FLAP HINGE AFT FITTING AFT HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-99638, TITLE: WINGS OUTBOARD TRAILING EDGE FLAP, LEFT INBOARD SUPPORT STRUT, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING OUTBOARD FORWARD HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-99639, WINGS LT OUTBOARD TRAILING EDGE FLAP INBD BRACKET ATTACHMENT BORES CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

FOUND LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD FORWARD HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD FORWARD HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-99639, TITLE: WINGS LEFT OUTBOARD TRAILING EDGE FLAP INBOARD BRACKET ATTACHMENT BORES, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER 6-2-100.

Part: STRUT — CORRODED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

FOUND LEFT WING OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING FORWARD HOLE FOUND CORRODED. LEFT WING OUTBOARD FLAP INBOARD FLAP HINGE AFT FITTING FORWARD HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-99638. WINGS OUTBOARD TRAILING EDGE FLAP, LEFT HAND INBOARD SUPPORT STRUT CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 600) · airframe 45,688 hrs · 7,125 cycles

FOUND RIGHT WING, OUTBOARD FLAP, INBOARD HINGE FITTING INBOARD MID BORE HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMENT TEST CARRIED OUT AS PER MM 27-50-00-710-801.

Part: FITTING — CORRODED (ZONE 600) · airframe 45,688 hrs · 7,125 cycles

RIGHT WING, OUTBOARD FLAP, INBOARD HINGE FITTING OUTBOARD MID BORE HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMENT TEST CARRIED OUT AS PER MM 27-50-00-710-801.

Part: SPAR CAP — CORRODED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

FOUND LEFT WING, REAR SPAR UPPER CHORD AT APPROX STA XORS 1040. FOUND CORRODED. CORROSION AT LEFT WING REAR SPAR UPPER CHORD AT APPROX STA XORS 1040. REPAIRED AS PER FEDEX EA NR 1-5710-97758, TITLE: WINGS, LEFT REAR SPAR UPPER CAP AFT TANG CORROSION CENTERED AT STATION XORS = 1040, REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 200) · airframe 45,688 hrs · 7,125 cycles

MAIN DECK COMPARTMENT FOUND LONGERON 17R CRACKED BETWEEN STA 1239 TO 1247. FOUND LONGERON 17R BETWEEN STA 1239 TO 1247 AT MAIN DECK COMPARTMENT. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CORRODED (ZONE 600) · airframe 45,688 hrs · 7,125 cycles

RIGHT WING - OUTBOARD FLAP, INBOARD HINGE FITTING OUTBOARD LOWER BORE HOLE FOUND CORRODED. RIGHT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMENT TEST CARRIED OUT AS PER MM 27-50-00-710-801.

Part: FRAME — DENTED (ZONE 200) · airframe 45,688 hrs · 7,125 cycles

MAIN DECK COMPARTMENT FRAME FOUND WITH DENT AT RT BS 1701, LONGERON 12R. DENTED AREA REPAIR CARRIED OUT AS PER SRM 53-30-00.

Part: FRAME — DENTED (ZONE 200) · airframe 45,688 hrs · 7,125 cycles

MAIN DECK COMPARTMENT FRAME FOUND WITH DENT AT LT BS 1681, LONGERON 12L. DENTED AREA REPAIR CARRIED OUT AS PER SRM 53-30-00.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

CRACK FOUND DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 13 (UPPER STRINGER) AT APPROX. XORS 577. CRACK AT LT WING TANK END OF STRINGER 13 AT APPROX. XORS 577 REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 45,688 hrs · 7,125 cycles

SNRM N00178: MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CHAFFED MARK AT STA 1801 LBL 27. CORRECTIVE ACTION: SNRM N00178: MAIN DECK COMPARTMENT SEAT TRACK AT STA 1801 LBL 27 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 45,688 hrs · 7,125 cycles

SNRM N00177: MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CHAFFED MARK AT STA 1801 LBL 8. CORRECTIVE ACTION: SNRM N00177: MAIN DECK COMPARTMENT SEAT TRACK AT STA 1801 LBL 8 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

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

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 45,688 hrs · 7,125 cycles

SNRM N00179: MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CHAFFED MARK AT STA 1801 LBL 47. CORRECTIVE ACTION: SNRM N00179: MAIN DECK COMPARTMENT SEAT TRACK AT STA 1801 LBL 47 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

CRACK FOUND DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 44 (LOWER STRINGER) AT APPROX. XORS 523. CRACK AT LT WING TANK END OF STRINGER 44 AT APPROX. XORS 523 REPAIRED AS 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 45,688 hrs · 7,125 cycles

CRACK FOUND DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 43 (LOWER STRINGER) AT APPROX. XORS 565. CRACK AT LT WING TANK END OF STRINGER 43 AT APPROX. XORS 565 REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 45,688 hrs · 7,125 cycles

CRACK FOUND AFTER HFEC INSPECTION ON RT WING AT END OF STR 42, XORS 629 STARTING FROM THE FIRST OUTBOARD FASTENER TO THE INBOARD FASTENER. RT WING STRINGER 42 END CRACKED AREA REPAIRED AS PER FEDEX EA 1-5720-97551, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 45,688 hrs · 7,125 cycles

CRACK FOUND DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 41 (LOWER STRINGER). CRACK AT LT WING TANK END OF STRINGER 41 REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: A/C PACK — ODOR (NR 1) · airframe 43,190 hrs · 6,527 cycles

AFTER T/O AT TOP OF CLIMB, NOTICED STRONG ACRID ODOR & SMOKE IN COCKPIT. RETURNED TO ANC. ISOLATED TO NR 1 PACK. PERFORMED AC PACK & DISTRIBUTION DUCT CLEANING. ODOR REMAINS NO SMOKE NOTED. PERFORMED NR 1 AC PACK FUNCTIONAL CHECK. ODOR IS DISSIPATING. UNABLE TO REPRODUCE SMOKE AS DURING INITIAL TS. PACKS WERE OPERATED USING BOTH APU & NR 1 ENGINE PNEUMATIC SUPPLY. REPLACED NR 1 PACK ALESCER BAG, NR 1 ENG PRV. INSPECTED PNEUMATIC DUCT FOR EVIDENCE OF OIL. NONE FOUND. RAN NR 1 ENG PER MD-11 JRH. COULD NOT INDUCE SMOKE COCKPIT. AC RELEASED FOR SERVICE PER MEL/CDL: 36-10-02-A.

Part: PITOT LINE — OBSTRUCTED (FIRST OFFICERS) · airframe 41,432 hrs · 6,137 cycles

FL 340 CLR AIR, A/P DISCON, NEITHER A/P AVBL, IAS COMPARATOR F/O A/S INDICATED UPPER FOOT, RAN QRH AIRSPEED LOST, SUSPECT, ERRATIC CHECKLIST, DETERMINED F/O'S A/S ERRONEOUS BY 25 KIAS. F/O SELECTED ALT STATIC SOURCE IAS COMPARATOR DISAPPEARED AND A/S MATCHED. DUMPED 10,000 LBS OF FUEL. DIVERTED TO OAK. INSPECTED FIRST OFFICERS PITOT TUBE AND FOUND PITOT DRAIN HOLE BLOCKED. REMOVED BLOCKAGE AND APPLIED DRY NITROGEN CLEANING OUT LINE MM 34-11-00-2. PERFORMED PITOT STATIC SYS TEST ON F/O AND STBY AIRSPEED INDICATOR. ALL INDICATIONS WITHIN LIMITS. PERFORMED RTS OF MSC AIR DATA HEATERS TEST PASSED. A/C OK TO CONTINUE.

Part: FMC — FAILED (NR 1) · airframe 41,203 hrs · 6,083 cycles

CLIMBING THROUGH FL380 EXPERIENCED POWER INTERUPTION WITH NO APPARENT CAUSE. LOST BOTH A/P'S AND ATS WITH MAP FAIL ALERT ON BOTH SIDES AND IRS/NAV X'D OUT ON CAPT'S PFD. CAPT'S MCDU DISPLAY REVERTED TO ACARS - APPLICATION MENU. F/O SELECTED STBY OPERATION. INITIALLY F/O MCDU WOULD NOT TUNE A VOR FREQUENCY. LATER IN DESCENT F/O NAV/RAD TUNED OK. AP1 AND AP2 RETURNED TO NORMAL BUT ATS REMAINED INOP IN 1 AND 2 POSITIONS. INTERROGATED DEU'S 1, 2, & 3. FAULT HISTORY SHOWED FMC 1 FAILURE. REMOVED AND REPLACED FMC 1. AUTOTHROTTLES, FCC'S ALL OPS CHECK NORM PER M/M. RETURNED TO SERVICE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,990 hrs · 6,033 cycles

CENTER CARGO, INTERCOSTAL AT STA Y= 1710 FOUND CRACKED.

Part: FRAME — DAMAGED (ZONE 200) · airframe 40,990 hrs · 6,033 cycles

MAIN DECK, LT TRANSVERSE FRAME AT STA 535 FOUND DAMAGED IN TWO PLACES. MAIN DECK, LT TRANSVERSE FRAME AT STA 535 DAMAGE REPAIRED AS PER SRZ-53-503.

Part: FRAME — CRACKED (TAIL CONE) · airframe 40,990 hrs · 6,033 cycles

FWD TAIL CONE AFT MOST FRAME CRACKED AT 2 PLACES ABOVE & BELOW THE RIGHT TOP LATCH KEEPER ASSY CUTOUT AREA. REPAIRED AS PER SRM 53-00-01 FIG 9 VOL 2.

Part: CLIP — CRACKED (FUSELAGE) · airframe 40,990 hrs · 6,033 cycles

AFT FUSELAGE COMPARTMENT - DOG HOUSE CANT STA Y=2092.88 FRAME CLIP P/N AJC7028-11, CRACKED. REPLACED AS PER SRM 51-35-01 VOL2.

Part: CLIP — CRACKED (FUSELAGE) · airframe 40,990 hrs · 6,033 cycles

AFT FUSELAGE COMPARTMENT - DOG HOUSE CANT STA Y=2046 FRAME CLIP P/N AJC7021-11, CRACKED.

Part: TRACK — CRACKED (NR 2 T/R) · airframe 40,990 hrs · 6,033 cycles

ENGINE NR 2 RIGHT HAND THRUST REVERSER UPPER SLIDER TRACK AFT EDGE FOUND CRACKED AND WORN. THRUST REVERSER REPLACED AS PER WORK CARD NR 78T3902-R.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 40,990 hrs · 6,033 cycles

ENGINE NR 2 LEFT HAND THRUST REVERSER UPPER SLIDER TRACK AFT EDGE FOUND WITH SUSPECT CRACK. CRACK REPAIRED REF FAA FORM 8130-3.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 40,990 hrs · 6,033 cycles

CENTER CARGO - BILGE AREA AT STA Y=1711 - 49L LONGERON AT SPLICE AREA FOUND CRACKED. CRACKED LONGERON SPLICED AND REMOVED PER 53-10-00 VOLUME I, FIGURE 1. NEW LONGERON FABRICATED SRM 51-33-01 VOLUME II AND INSTALLED PER SRM 53-10-00 VOLUME I, FIGURE 1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 40,990 hrs · 6,033 cycles

CTR CARGO - STA Y1806 STR34L LONGERON CRACKED. CRACKED LONGERON CUT AND REMOVED BETWEEN STA Y= 1791 TO Y= 1810 PER SRM 53-10-00 VOLUME I, FIGURE 1. LONGERON SPLICE FABRICATED PER DWG AFA7736. SPLICE FITTING AND NEW LONGERON INSTALLED PER SRM 53-10-00 VOLUME I, FIGURE 1.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 40,990 hrs · 6,033 cycles

CTR CARGO - STA Y1541 STR36L LONGERON SPLICE CRACKED. SPLICE REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED PER DWG A5A7114 AND PART MARKED PER GMM 7-0-1001. NEW LONGERON SPLICE INSTALLED PER SRM 51-33-01 VOLUME II.

Part: SUPPORT — DAMAGED (MLG) · corrosion level 3 · airframe 40,514 hrs · 5,927 cycles

DURING AIRPLANE'S CONVERSION P-F/ACF RT WING INTERNAL T/E STRUCTURE STA XORS 264 LWR SIDE MAIN LANDING GEAR SUPPORT BOLT DRAIN OBSTRUCTED AND NUTS ON TL WITH RUST. REMOVE TRUNNION SUPPORT FITTING AND HEAVILY CORRODED ARB0621:BLEND OUT, NDI , PROTECT AREA, INSTALL NEW FASTENERS.

Part: RIB — CRACKED (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

RT OUTBOARD FLAP NOSE RIB SUPPORT ISLAND FOUND 01 CRACK AT OUTBOARD SIDE APPROX .1875 INCH LONG. RT OUTBD FLAP NOSE RIB DAMAGED SUPPORT ISLAND CARRIED OUT REPAIR IAW FEDEX EA 1-5750-63119, TITLE- WINGS- TRAILING EDGE FLAPS- OUTBOARD TRAILING EDGE FLAP- SECONDARY UP STOP- REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING O/B T/E FLAP O/B AFT HINGE ASSY FOUND PIVOT BEARING MOUNT HOLE I/B BORE SURFACE CORRODED. ( FLAP SIDE ). LT WING O/B T/E FLAP O/B AFT HINGE ASSY (FLAP SIDE) PIVOT BEARING MOUNT HOLE I/B BORE SURFACE REPAIRED AS PER FEDEX EA 1-5750-63180.

Part: BUSHING — LOOSE (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

LEFT WING I/B TRAILING EDGE FLAP ASSY HAS LEADING EDGE SIDE GUIDE ROLLER BRACKET ASSY WITH BOLT MOUNT HOLE; LOWER BUSHING LOOSE. LT WING I/B T/E FLAP ASSY HAS L/E SIDE GUIDE ROLLER BRACKET ASSY WITH BOLT MOUNT HOLE; LOWER BUSHING LOOSE REPAIRED AS PER FEDEX EA 1-5750-63188, TITLE- WINGS- LT INBOARD FLAP- REPAIR UP STOP BRACKET.

Part: RIB — CHAFED (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

LEFT WING I/B TRAILING EDGE FLAP VANE TRACK NR 1 & 3 STRUCTURE RIB SURFACE FOUND CHAFED MARKS. CHAFED MARK ON LT WING I/B T/E FLAP VANE TRACK NR 1 & 3 STRUCTURE RIB SURFACE AREA SMOOTHEN OUT AND FOUND WITH IN LIMIT AS PER SRM 57-00-01 FIG. 1A VOL. 1.

Part: HINGE — CHAFED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING O/B T/E, I/B FLAP HINGE BRACKET ASSY FOUND FWD O/B UNDERWING FITTING WITH LOWER SURFACE CHAFFED. ( LOCATED APPROX. 5 INCH FROM FITTING L/E ) BLENDED CARRIED OUT & FOUND WITH IN LIMIT AS PER FEDEX EA 1-5720-68430 WINGS - OUTER WING - O/B FLAP I/B FLAP HINGE BRACKET SUPPORT.

Part: HINGE — CORRODED (LT WING) · airframe 36,079 hrs · 4,906 cycles

SNRM N0740 3A L2 FH WING 2FB FLAP 2FB HINGE 28 2FC SIDE 29 CORROSION FOUND ON LOWER ATTACHMENT HOLE12 FB BORE. LT WING O/B FLAP O/B HINGE ( A/C SIDE ) LOWER ATTACHMENT HOLE I/B BORE REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

SNRM N 741 3A L2 FH WING 2FB FLAP I2 FB HINGE 28 2FC SIDE 29 CORROSION FOUND ON FWD ATTACHMENT HOLE 2FB BORE.

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT WING O/B FLAP O/B HINGE ( A/C SIDE ) CORROSION FOUND ON UPPER ATTACHMENT HOLE I/B BORE. RT WING O/B FLAP O/B HINGE ( A/C SIDE ) UPPER ATTACHMENT I/B HOLE BORE REPAIERD AS PER CMM 57-44-09.

Part: HINGE — CORRODED (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

SNRM N0739 3A L2 FH WING 2FB FLAP 2FB HINGE 28 2FC SIDE 29 CORROSION FOUND ON FORWARD ATTACHMENT HOLE I2 FB BORE. ** S/D ** COMING

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING I/B T/E FLAP, O/B FWD HINGE FITTING ASSY HAS PIVOT BEARING MOUNT LUG SPOT FACES RUSTY. LT WING I/B T/E FLAP, O/B FWD HINGE FITTING ASSY HAS PIVOT BEARING MOUNT LUG SPOT FACES REPAIRED AS PER FEDEX EA 1-5750-63187, TITLE: WINGS- TRAILING EDGE FLAPS- LH I/B FLAP, O/B HINGE LUG SURFACE REWORK.

Part: HINGE FITTING — DAMAGED (TE FLAP) · airframe 36,079 hrs · 4,906 cycles

LT WING, IB FLAP, OB FORWARD HINGE FITTING HAS HYD ACTUATOR'S UPPER OB MOUNT LUG HOLE WITH TOOL MARK. LT WING IB FLAP OB HINGE (WING SIDE) HYD ACTUATOR ATTACHMENT OB HOLE REPAIRED IAW CMM 57-44-07.

Part: HINGE — CORRODED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING - O/B T/E FLAP, I/B FWD HINGE FITTING FOUND HYD ACTUATOR'S INBOARD MOUNT HOLE SPOT FACES WITH SURFACE CORROSION. LT WING O/B FLAP, I/B FWD HINGE FITTING HYD ACTUATOR INBOARD MOUNT HOLE SPOT FACES SURFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT OUTBD FLAP VANE NR 2 ( FROM INBD) TEE FITTING ATTACH HOLE CORRODED. CORROSION AT THE FITTING ATTACH HOLE RT OUTBD FLAP VANE NR 2 REMOVED AS PER FEDEX EA 1-5750-63189, WINGS: RT OUTBOARD VANE-TEE FITTING REWORK.

Part: HINGE — CORRODED (TE FLAPS) · airframe 36,079 hrs · 4,906 cycles

LT WING - O/B T/E FLAP, O/B FWD FLAP HINGE FITTING FOUND HYD ACTUATOR'S INBOARD MOUNT HOLE SPOT FACES WITH CORROSION. LT WING O/B FLAP, O/B FWD HINGE FITTING HYD ACTUATOR INBOARD MOUNT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING - O/B FLAP, I/B FWD HINGE FITTING HAS SURFACE CORROSION ON SPOT FACES OF THE PIVOT BEARING MOUNT HOLE. LT WING O/B FLAP, I/B FWD HINGE FITTING PIVOT BEARING MOUNT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING O/B FLAP I/B HINGE FITTING (WING SIDE) ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES FOUND CORROSION. LT WING O/B FLAP I/B HINGE FITTING (WING SIDE) ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES REPAIRED AS PER FEDEX EA 1-5740-63185.

Part: FITTING — CORRODED (TE FLAP HINGE) · airframe 36,079 hrs · 4,906 cycles

LT WING 2FB FLAP 2FB HINGE FITTING 28 WING SIDE 29 LOWER PIVOT ATTACHMENT BORE HOLE FOUND CORROSION. LT WING O/B FLAP O/B HINGE FITTING ( WING SIDE ) LOWER PIVOT ATTACHMENT HOLE BORE REPAIRED AS PER CMM 57-44-09.

Part: HINGE FITTING — CORRODED (TE FLAP) · airframe 36,079 hrs · 4,906 cycles

RT WING FLAP HINGE FITTING 28 WING SIDE 29 REAR SPAR LOWER MOUNT BOLT HOLE FOUND CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING - O/B FLAP I/B HINGE FITTING ( WING SIDE ) LOWER PIVOT ATTACHMENT BORE HOLE FOUND CORROSION. LT WING O/B FLAP I/B HINGE FITTING (WING SIDE) LOWER PIVOT ATTACHMENT HOLE BORE REPAIRED AS PER CMM 57-44-08.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

LT WING - INBOARD FLAP OUTBOARD HINGE FITTING (FLAP SIDE) LOWER PIVOT ATTCHMENT INBOARD & OUTBOARD BORE HOLES FOUND CORROSION. LT WING - INBOARD FLAP OUTBOARD HINGE FITTING (FLAP SIDE) LOWER PIVOT ATTACHMENT INBOARD & OUTBOARD HOLE BORES REPAIRED AS PER FEDEX EA 1-5750-63117, TITLE WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- LT INBOARD FLAP OUTBOARD HINGE BORE REPAIRS

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING O/B FLAP I/B HINGE FITTING (FLAP SIDE) LOWER PIVOT ATTACHMENT I/B & O/B BORE HOLES FOUND CORROSION. LT WING O/B FLAP I/B HINGE FITTING (FLAP SIDE) LOWER PIVOT ATTACHMENT I/B & O/B HOLES BORE REPAIRED AS PER FEDEX EA 1-5750-63120,

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING O/B FLAP O/B HINGE FITTING (WING SIDE) ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES FOUND CORROSION. LT WING O/B FLAP O/B HINGE FITTING (WING SIDE) ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES REPAIRED AS PER FEDEX EA 1-5740-63182.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

SNRM N0568 3A L2 LT WING - I2 FB FLAP 2 FB HINGE FITTING 28 FLAP SIDE 29 ACTUATOR ATTACHMENT I2 FB 26 2 FB BOLT HOLE FOUND CORROSION. LT WING - I/B FLAP ( FLAP SIDE ) O/B HINGE ACTUATOR ATTACHMENT I/B & O/B BOLT HOLES REPAIRED AS PER CMM 57-52-03.

Part: HINGE — CORRODED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING - O/B FLAP O/B HINGE FITTING ( WING SIDE ) FWD ATTACHMENT O/B HOLE SPOT FACE FOUND CORROSION. LT WING O/B FLAP, O/B HINGE FITTING ( WING SIDE ) FWD ATTACHMENT O/B HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

3A L2 LT WING -2 FB FLAP I2 FB HINGE FITTING 28 WING SIDE 29 FWD ATTACHMENT I2 FB BOLT HOLE FOUND CORROSION. LT WING - O/B FLAP I/B HINGE FITTING ( WING SIDE ) FWD ATTACHMENT I/B HOLE REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT OUTBD FLAP OUTBD HINGE ( A/C SIDE ) PIVOT HOLE CORRODED AT BORE AND SPOT FACES. RT WING OUTBD FLAP OUTBD HINGE ( A/C SIDE ) PIVOT HOLE BORE AND SPOT FACES ( FWD & AFT FACE ) REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT OUTBOARD FLAP OUTBD HINGE (FLAP SIDE) ACTUATOR ATTACH LUGS CORRODED AT INBD AND OUTBD BORES. RT WING OUTBOARD FLAP OUTBD HINGE (FLAP SIDE) ACTUATOR ATTACH LUGS INBOARD AND OUTBOARD BORES REPAIRED AS PER FEDEX EA 1-5740-63186,

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT OUTBD FLAP INBD HINGE ( A/C SIDE ) MOST FWD ATTACH HOLES FOUND CORROSION AT INBD AND OUTBD BORES. RT WING OUTBD FLAP ( A/C SIDE ) I/B HINGE FWD ATTACHMENT I/B AND O/B HOLES REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT OUTBOARD FLAP INBOARD HINGE 28 2FC SIDE 29 LOWER OUTBOARD ATTACH HOLE CORRODED AT BORE AND FORWARD 2FAFT FACES. RH OUTBD FLAP INBD HINGE (A/C SIDE) LOWER OUTBD ATTACH HOLE CORRODED AT BORE AND FWD / AFT FACES. RT OUTBD FLAP INBD HINGE ( A/C SIDE ) LOWER OUTBD ATTACH HOLE BORE AND FWD / AFT FACES ( SURFACE ) REPAIRED AS PER CMM 57-44-08 AND DWG ARC0502.

Part: HINGE — WORN (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

RIGHT OUTBOARD FLAP OUTBOARD HINGE 28 2FC SIDE 29 OUTBOARD UPPER ATTACH HOLE WORN AT FWD SIDE OF BORE. RT WING OUTBOARD FLAP, OUTBD HINGE ( A/C SIDE ) OUTBD UPPER ATTACH HOLE BORE REPAIRED AS PER CMM 57-44-09.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

SNRM N0478: RT INBOARD FLAP HINGE (FLAP SIDE), PIVOT HOLES CORRODED AT INBOARD AND OUTBOARD BORES.

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT OUTBD FLAP OUTBOARD HINGE ( A/C SIDE ) LOWER INBOARD ATTACH HOLE CORRODED AT BORE AND FWD / AFT FACES. RT WING OUTBOARD FLAP OUTBOARD HINGE ( A/C SIDE ) LOWER INBOARD ATTACHMENT HOLE BORE AND FWD / AFT FACES REPAIRED AS PER CMM 57-44-09.

Part: SUPPORT — CRACKED (T/E FLAP) · airframe 36,079 hrs · 4,906 cycles

LEFT OUTBOARD FLAP NOSE RIB SUPPORT ISLAND FOUND 01 CRACK AT OUTBOARD SIDE, APPROX .1875 INCH LONG. LT OUTBD FLAP NOSE RIB DAMAGED SUPPORT ISLAND CARRIED OUT REPAIR IAW FEDEX EA 1-5750-63119, TITLE- WINGS- TRAILING EDGE FLAPS- OUTBOARD TRAILING EDGE FLAP- SECONDARY UP STOP- REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR ATTACH LUGS CORRODED AT INBOARD AND OUTBOARD BORES AND SPOT FACES. RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR ATTACHMENT LUGS CORRODED AT INBOARD AND OUTBOARD BORES AND SPOT FACES REPAIRED AS PER FEDEX EA 1- 5740-63184.

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

SNRM N0456 3A RT OB FLAP IB HINGE 28 2FC SIDE 29 BOTH IB AND OB UPPER ATTACH HOLES CORRODED AT BORES. RT WING OUTBOARD FLAP INBD HINGE ( A/C SIDE ) BOTH INBOARD AND OUTBOARD UPPER ATTACHED HOLES BORES REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (RT WING) · airframe 36,079 hrs · 4,906 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) LOWER INBOARD ATTACH HOLE CORRODED AT BORE AND FWD / AFT FACE. RIGHT OUTBOARD FLAP INBOARDD HINGE (A/C SIDE) LOWER INBOARD ATTACH HOLE BORE AND FWD & AFT FACE (SURFACE) REPAIRED AS PER CMM 57-44-08 & DWG ARC0502.

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT OUTBD FLAP OUTBD HINGE ( A/C SIDE ) FWD MOST ATTACH HOLES CORRODED AT BORES. RT WING OUTBD FLAP ( A/C SIDE ) OUTBOARD HINGE FWD ATTACHMENT INBOARD AND OUTBOARD HOLES REPAIRED AS PER CMM 57-44-09.

Part: HINGE — CORRODED (ZONE 600) · airframe 36,079 hrs · 4,906 cycles

RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) INBOARD AND OUTBOARD PIVOT HOLES CORRODED AT BORES AND SPOT FACES. RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) INBOARD AND OUTBOARD PIVOT HOLES CORRODED AT BORES AND SPOT FACES REPAIRED AS PER FEDEX EA 1-5750-63181.

Part: HINGE — CORRODED (RT WING) · airframe 36,079 hrs · 4,906 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) FOUND CORROSION ON UPPER OUTBOARD ATTACH HOLE FWD FACE. RIGHT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) UPPER OUTBOARD ATTACH HOLE FWD FACE REMOVED AND REPAIRED AS PER CMM 57-44-08.

Part: HINGE — CORRODED (RT WING) · airframe 36,079 hrs · 4,906 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (A/C SIDE) FOUND CORROSION ON PIVOT HOLE AT BORE AND SPOT FACES. RIGHT WING OUTBOARD FLAP INBOARD HINGE (A/C SIDE) PIVOT HOLE BORE AND SPOT FACES (FWD & AFT FACES) REPAIR AS PER CMM 57-44-08.

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 36,079 hrs · 4,906 cycles

LT WING, FOUND NR 16 SLAT TRACK INBOARD MOST FITTING WITH CRACK. CRACKED RIB ON LH WING, NR 16 SLAT TRACK INBOARD MOST FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,079 hrs · 4,906 cycles

FUSELAGE SKIN DENT (2 PLACES) RIGHT SIDE BETWEEN STA Y 475.0 TO 495.0 LONGERONS 45R TO 46R (A = APPROX 1.5 INCH D; B = APPROX 0.50 INCH D). FUSELAGE SKIN DENT ( 2 PLACES ) RT SIDE BETWEEN STA Y = 475.0 TO 495.0 LONGERONS 45 RT TO 46 RT ( A = APPROX. 1.5 INCH D; B = APPROX. 0.50 INCH D ) REPAIRED CARRID OUT AS PER SRM 53-20-00 VOL.1.