N592FE

Part: LINE — LEAKING (HYD SYSTEM) · airframe 93,022 hrs · 21,338 cycles

HYD 3 QTY LO HYD 3 ELEV OFF. EMERGENCY DECLARED. A/C MAINTAINED A #3 HYD SYSTEM QTY OF 5.0 GAL OR BETTER FOR MOST OF THE FLIGHT. UNTIL LANDING GEAR LEVER WAS PLACED INTO THE DOWN POSITION THEN HYD QTY DROPPED TO 2.3 GAL. FOUND PERMASWEDGE UNION LEAKING ON LINE IAW EA 1-3230-T0377535 PT 1 PERFORMED TEMPORARY REPAIR TO MPN AYK7550-585 USING RAW STOCK PIPING 304X1-2X035. PERFORMED LEAK CHECK OF REPAIRED AREA. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — LOOSE (N/A) · airframe 90,928 hrs · 20,790 cycles

L-1 DOOR PRESS TO TEST SLIDE PRESSURE INDICATOR INOP. FOUND L-1 DOOR REMOTE PRESSURE INDICATOR LENS CAP NOT SEAT IN SOCKET. SEAT LENS CAP OPS CHECKS GOOD.

Part: BATTERY — FAILED (N/A) · airframe 90,807 hrs · 20,747 cycles

L1 DOOR REMOTE PRESSURE INDICATOR NOT PRESSING TO TEST. REMOVED AND REPLACED BATTERIES PER MD11 AMM 25-61-04-4. OPS CHECK GOOD

Part: SPAR CAP — CORRODED (LT WING) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING REAR SPAR LOWER CAP AFT FLANGE FOUND CORROSION AT XORS 1070. REPAIR CARRIED OUT AS PER EA 1-5710-T0371094 PART 1. TITLE: WINGS - BASIC WING STRUCTURE - REPAIR FOR EXTENSIVE EXFOLIATION CORROSION COMMON TO HORIZONTAL FLANGE OF ARB7414-1 LOWER REAR SPAR CAP BETWEEN XORS 1057 AND XORS 1076. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (RT NR 6 SLAT) · airframe 90,228 hrs · 20,570 cycles

RIGHT HAND WING NUMBER 6 SLAT RIB FOUND CRACKED AT XOS 868.4 DURING INTERNAL BORESCOPE INSPECTION. RIB REMOVED AND FABRICATED PER DOUGLAS DRAWING ARB1828 REVISION B. INSTALLED FABRICATED RIB AT RIGHT HAND WING NUMBER 6 SLAT AT STATION XOS 868.4 AS PER SRM 51-35-0-OG. AND EA: 1-5750-T0371095 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 200) · airframe 90,228 hrs · 20,570 cycles

RADIOGRAPHY INSPECTION CARRIED OUT ON TRANSVERSE SKIN SPLICE AT STATION 6-100 AND FOUND 01 EACH CRACK INDICATION AT FORWARD SIDE OF STRINGER 7 LEFT CENTER SPLICE, PROPAGATE FROM SECOND FASTENER FROM CENTER APPROXIMATELY 0.5 INCHES LENGTH. MAIN DECK CARGO STATION 6-100 STRINGER 7 LEFT CRACKED SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01-OG. SPLICE FITTING FABRICATED BY MACHINING AS PER DOUGLAS DRAWING A6A7112 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (RT NR 6 SLAT) · airframe 90,228 hrs · 20,570 cycles

RIGHT HAND WING NUMBER 6 SLAT RIB FOUND CRACKED AT XOS 858.1 DURING INTERNAL BORESCOPE INSPECTION. RIB REMOVED AND FABRICATED PER DRAWING ARB1827 REVISION C. INSTALLED FABRICATED RIB AT RIGHT HAND WING NUMBER 6 SLAT AT STATION XOS 858.1 AS PER SRM 51-35-0-OG. AND EA: 1-5750-T0371095 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (LT NR 8 SLAT) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING NUMBER 8 SLAT RIB FOUND CRACKED AT XOS 1010.49 DURING S/M WORK. LEFT HAND WING NUMBER 8 SLAT RIB AT STATION XOS 1010.49 CRACKED RIB REMOVED AND REPLACED WITH FABRICATED RIB AS PER SRM 51-35-01-OG. RIB FABRICATED AS PER DOUGLAS DRAWING ARB1924 REVISION B. AND EA# 1-5750-T0371245 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1661 L12R) · airframe 90,228 hrs · 20,570 cycles

MAIN DECK CARGO COMPARTMENT. RIGHT HAND SIDE STATION 1661 LONGERON 12 RIGHT FRAME FLANGE FOUND DENTED. REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (LT NR 8 SLAT) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING NUMBER 8 SLAT RIB FOUND CRACKED AT XOS 1025.54 DURING S/M WORK. LEFT WING NUMBER 8 SLAT RIB AT STATION XOS 1025.54 CRACKED RIB REMOVED AND REPLACED WITH FABRICATED RIB IAW SRM 51-35-01-OG. RIB FABRICATED IAW DRAWING ARB1925 REVISION B. AND EA 1-5750-T0371245 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — MISREPAIRED (LT WING) · airframe 90,228 hrs · 20,570 cycles

EXISTING REPAIR AT LH WING NUMBER 8 SLAT LOWER SKIN STATION XOS 1026. REPAIR AT LEFT HAND WING NUMBER 8 SLAT LOWER SKIN STATION XOS 1025.548 EVALUATED AND FOUND NOT REPAIRED IAW SRM 57-40-01-2R REPAIR 3 FIGURE 201. REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 3 FIG 201 AND EA : 1-5750-T0371245 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1641 L12-13R) · airframe 90,228 hrs · 20,570 cycles

AT THE TIME OF INSPECTION ON EO E1-5100-7-5001 PART 1. MCD RIGHT HAND STATION 1641 BETWWEEN LONGERON 12 TO 13 FOUND A DENT ON THE FUSELAGE FRAME THAT WAS NOT DOCUMENTED FOR EVALUATIONS. MAIN DECK CARGO COMPARTMENT RIGHT HAND STATION 1641 BETWEEN LONGERON 12 TO 13 ON THE FUSELAGE FRAME DENTED AREA REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. INITIAL INSPECTION TO BE CARRY OUT AT 14,500 FLIGHT CIRCLES AND REPETITIVE INSPECTION AT EVERY 9,500 FLIGHT CIRCLES. INSPECTION METHOD HIGH FREQUENCY EDDY CURRENT AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2 TABLE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 90,228 hrs · 20,570 cycles

CENTRE CARGO COMPARTMENT FOUND LONGERON 47 RIGHT BETWEEN STATION 1541 TO STATION 5-113 SUSPECT CRACK. LONGERON SPLICE RMOVED AND REPLACED WITH FABRICATED MACHINING SPLICE AS PER SRM 51-33-01-OG. SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7116 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 90,228 hrs · 20,570 cycles

CENTER CARGO COMPARTMENT FOUND LONGERON 45 LEFT SPLICE BETWEEN STATION 1541 TO STATION 5-113 SUSPECT CRACK. CENTER CARGO COMPARTMENT CRACK SPLICE LONGERON 45 LEFT BETWEEN STATION 1541 TO STATION 5-113 REMOVED AND REPLACED WITH FABRICATED MACHINING SPLICE AS PER SRM 51-33-01-OG. SPLICE FABRICATED BY MACHINED AS PER DOUGLAS DRAWING A5A7116 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 10/11/2022

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 90,228 hrs · 20,570 cycles

CENTRE CARGO COMPARTMENT FOUND LONGERON 49 LEFT SPLICE BETWEEN STATION 1541 TO STATION 5-113 SUSPECT CRACK.

Part: SEAT TRACK — CORRODED (BS 1997) · airframe 90,228 hrs · 20,570 cycles

CABIN SEAT TRACK FLANGE AT STATION 1997 X=-107.25 FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51- 21-01-OG AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101. CORRODED SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1964) · airframe 90,228 hrs · 20,570 cycles

CABIN SEAT TRACK FLANGE AT STATION 1964 X=-107.25 FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51- 21-01-OG AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101. CORRODED SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM NO. N01133 FOR DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIGINAL SUBMISSION DATE: 10/26/2022

Part: LONGERON — CRACKED (ZONE 100) · airframe 90,228 hrs · 20,570 cycles

CENTRE CARGO COMPARTMENT FOUND LONGERON 49 RIGHT BETWEEN STATION 1541 TO STATION 5-113 SUSPECT CRACK.

Part: SKIN — CRACKED (LT NR 2 SLAT) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING NO.2 SLAT LOWER SKIN OUTBOARD AFT CORNER FOUND CRACKED AT STATION XIS 358. REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 3 FIGURE 201 AND EA: 1-5750-T0371210 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 90,228 hrs · 20,570 cycles

CENTER CARGO COMPARTMENT FOUND LONGERON 50 RIGHT SPLICE BETWEEN STATION 1541 TO STATION 5-113 SUSPECT CRACK. CENTER CARGO COMPARTMENT CRACK SPLICE LONGERON 50 RIGHT BETWEEN STATION 1541 TO STATION 5-113 REMOVED AND REPLACED WITH FABRICATED MACHINING SPLICE AS PER SRM 51-33-01-OG. SPLICE FABRICATED BY MACHINED AS PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIGINAL SUBMISSION DATE: 10/11/2022

Part: LONGERON — CRACKED (ZONE 100) · airframe 90,228 hrs · 20,570 cycles

CENTRE CARGO COMPARTMENT FOUND LONGERON 46 RIGHT BETWEEN STATION 1541 TO STATION 5-113 SUSPECT CRACK.

Part: TRUNNION — CRACKED (LT MLG) · airframe 90,228 hrs · 20,570 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION ON NOSE LANDING GEAR LEFT HAND TRUNNION FITTING FORWARD LOWER CORNER STATION Y=585 EXISTING TRIMMED OUT AREA FOUND CRACK APPROXIMATELY 0.2 INCHES. NOSE LANDING GEAR LEFT HAND TRUNNION FITTING FORWARD LOWER CORNER STATION Y=585 CRACKED AREA REPAIRED AS PER EA# 1-5310-T0371187 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 90,228 hrs · 20,570 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT L3 DOOR FORWARD JAMB LOWER WEB LEFT HAND SIDE STATION 1250.75 LONGERON 27 LEFT EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT L3 DOOR FORWARD JAMB LOWER WEB LEFT HAND SIDE STATION 1250.75 LONGERON 27 LEFT EVALUATED AND FOUND REPAIRED IAW SRM 53-40-15-2R REPAIR 3 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 10/5/2022

Part: NONE — NONE (NONE) · airframe 90,228 hrs · 20,570 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT R3 DOOR AFT JAMB LOWER WEB RIGHT HAND SIDE STATION 1305.25 LONGERON 27 RIGHT EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT R3 DOOR AFT JAMB LOWER WEB RIGHT HAND SIDE STATION 1305.25 LONGERON 27 RIGHT EVALUATED AND FOUND REPAIRED IAW SRM 53-40-15-2R REPAIR 3 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 10/5/2022

Part: NONE — NONE (NONE) · airframe 90,228 hrs · 20,570 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 625 TO STATION 665 X = -27.5 RIGHT HAND

Part: NONE — NONE (NONE) · airframe 90,228 hrs · 20,570 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT R3 DOOR FORWARD JAMB LOWER WEB RIGHT HAND SIDE STATION 1250.75 LONGERON 27 RIGHT EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT R3 DOOR FORWARD JAMB LOWER WEB RIGHT HAND SIDE STATION 1250.75 LONGERON 27 RIGHT EVALUATED AND FOUND REPAIRED IAW SRM 53-40-15-2R REPAIR 3 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 10/5/2022

Part: LONGERON SPLICE — CRACKED (CARGO BAY) · airframe 90,228 hrs · 20,570 cycles

CENTRE CARGO COMPARTMENT, FOUND LONGERON 40 LEFT SPLICE BETWEEN STATION 1541 TO STATION 5-113 SUSPECT CRACK.

Part: RIB — CRACKED (LT NR 1 SLAT) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING NUMBER 1 SLAT INBOARD FILLET FAIRING OUTBOARD RIB FOUND CRACKED.

Part: LONGERON SPLICE — CRACKED (CARGO BAY) · airframe 90,228 hrs · 20,570 cycles

CENTRE CARGO COMPARTMENT, FOUND LONGERON 35 RIGHT SPLICE BETWEEN STATION 1541 TO STATION 5-113 SUSPECT CRACK.

Part: FORMER — CHAFED (ZONE 500) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING FIXED LEADING EDGE FORMER XOS 912. FORMER STATION XOS 912 EVALUATED AND FOUND DAMAGED WITH DEEP CHAFF MARK. FORMER REMOVED AND REPLACED WITH FABRICATED FORMER AS PER SRM 51-33-01-0G. FORMER FABRICATED AS PER DRAWING ARB2921 REV A. EO 1-5100-7-5001 B7 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING FIXED LEADING EDGE NUMBER 15 SLAT TRACK CUTOUT SKIN AT XOS 944 FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE XOS 944 NUMBER 15 SLAT TRACK CUTOUT SKIN CARRIED OUT REPAIR AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (LT WING LE) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING FIXED LEADING EDGE RIB ANGLE FOUND CRACKED AT XOS584. LEFT HAND WING FIXED LEADING EDGE XOS 584 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-33-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB2931. REVISION H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING FIXED LEADING EDGE NUMBER 16 SLAT TRACK CUTOUT SKIN AT XOS 1005 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201 AND EA# 1-5730- T0371131 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 90,228 hrs · 20,570 cycles

AGING AIRCRAFT - EXISTING REPAIR AT FUSELAGE SKIN CENTER CARGO DOOR CUTOUT AFT JAMB STATION 1781 RIGHT HAND SIDE BETWEEN LONGERON 40 RIGHT TO LONGERON 41 RIGHT.

Part: STIFFENER — CRACKED (BS 2164) · airframe 90,228 hrs · 20,570 cycles

EMPENNAGE TAILCONE BULKHEAD STATION 2164 MOST LOWER STIFFENER FOUND CRACKS. TAILCONE BULKHEAD STATION 2164 MOST LOWER CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-33-01-OG. STIFFENER REWORKED AS PER DOUGLAS DRAWING AJC7001 REVISION DT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 90,228 hrs · 20,570 cycles

RIGHT HAND WING FIXED LEADING EDGE DOUBLER FOUND CRACKED AT XOS 906. DOUBLER REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER SRM 51-33-01-OG. DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954. REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING FIXED LEADING EDGE RIB DOUBLER FOUND CRACKED AT XOS789. LEFT HAND WING FIXED LEADING EDGE XOS 789 CRACKED RIB DOUBLER REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER SRM 51-33-01-OG. DOUBLER FABRICATED AS PER DRAWING ARB3954. REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SKIN — CRACKED (LT WING LE) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING FIXED LEADING EDGE LOWER SKIN AT XOS 995 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 9 FIGURE 201 AND EA 1-5730-T0371131 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING FIXED LEADING EDGE NUMBER 13 SLAT TRACK CUTOUT SKIN FOUND CRACKED AT XOS835. LEFT HAND WING FIXED LEADING EDGE XOS 835 NUMBER 13 SLAT TRACK CUTOUT SKIN CARRIED OUT REPAIR AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 90,228 hrs · 20,570 cycles

RIGHT HAND WING FIXED LEADING EDGE LOWER DOUBLER FOUND CRACKED AT XOS 547. DOUBLER REMOVED AND REPLACED WITH FABRICATED DOUBLER AS PER SRM 51-33-01-OG. DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB2933. REVISION AJ. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 90,228 hrs · 20,570 cycles

RIGHT HAND WING FIXED LEADING EDGE LOWER DOUBLER FOUND CRACKED AT XOS 471. DOUBLER REMOVED AND REPLACED AS PER SRM 51-33-01-OG. DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB2933. REVISION AJ. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING LE) · airframe 90,228 hrs · 20,570 cycles

HIGH FREQUENCY EDDY CURRENTINSPECTIN ON RIGHT HAND WING FIXED LEADING EDGE SKIN AT STATION XOS 602.65 FUEL ACCESS DOOR FORWARD INBOARD CORNER FOUND 02 EA CRACK APPROXIMATELY 1.0 INCH AND 0.2 INCH. RIGHT HAND WING FIXED LEADING EDGE SKIN AT STATION XOS 602.65 FUEL ACCESS DOOR FORWARD INBOARD CORNER CARRIED OUT REPAIR AS PER SRM 57-40-01-2R REPAIR 18 FIGURE 201. INITIAL INSPECTION CARRY OUT NEXT C CHECK NOT EXCEEDING 24 MONTHS AND REPETITIVE INSPECTION CARRY OUT EVERY C CHECK NOT EXCEEDING 24 MONTHS BY VISUAL METHOD AS PER SRM 57-40-01-2R TABLE 204/REPAIR 18. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 90,228 hrs · 20,570 cycles

LEFT HAND WING FIXED LEADING EDGE LOWER ANGLE REPAIR DOUBLER FOUND WRONGLY INSTALLED AT XOS 912. LEFT HAND WING FIXED LEADING EDGE LOWER XOS 912 CARRIED OUT DOUBLER REPAIR AS PER SRM 57-40-03-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B7 PART 1. TITLE: STRUCTURES - REPAIR CATALOG - MD - 11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR FOR GMM 6-2-100.

Part: FORMER — BROKEN (RT WING LE) · airframe 90,228 hrs · 20,570 cycles

RIGHT HAND WING FIXED LEADING EDGE FORMER FOUND LOWER ATTACH BROKEN AT XOS 906. BROKEN FORMER REMOVED AND REPLACED WITH FABRICATED FORMER AS PER SRM 51-33-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB1164. REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — FAILED (ZONE 200) · airframe 88,745 hrs · 20,155 cycles

L1 DOOR REMOTE PRESSURE INDICATOR PUSH TO TEST LIGHT INOP FOUND SWITCH INSIDE OF REMOTE PRESS SWITCH WAS BAD. REPLACED REMOTE PRESS SWITCH AND WORKS NORMAL.

Part: SERVO VALVE — LEAKING (RT SPOILER) · airframe 88,436 hrs · 20,074 cycles

#1 HYD SYS QTY READING ZERO. ALL INDICATIONS WERE NORMAL UNTIL FLAPS WERE DROPPED, THEN SYS #1 HYD QTY RAPIDLY DROPPED TO ZERO. R/H SPOILER DRIVE SERVO VALVE LEAKING OUT OF COMPONENT. REPLACED SPOILER SERVO DRIVE ACTUATOR. LEAK CHECKS GOOD

Part: PIN — FAILED (DRIVE CHAIN ASSY) · airframe 86,832 hrs · 19,655 cycles

PDIS 592 27-40 6412 13MAY21 KIX OPEN U LOGPAGES:383476 AFTER T/O IN A TURN RECIEVED LEVEL 2 STAB OUT OF TRIM ALERT - DISCONNECTED AP CLEARED WING UP VERY HEAVY ON PITCH CONTROL - NOTICED STAB TRIM STUCK AT 8.0 ( T/O TRIM ) AND DID NOT MOVE YOKE TRIM SW OR SUITCASE HANDLES - DECLEARED TO RTB - DECLEARED EMERGENCY - DAMPED FUEL IN RADER HOLDING PATTERN - STAB REMAINED AT 8.0 THRU LANDED AND BLOCK IN. SHGN 13MAY21 04:01 KIX U CHECKED STAB TRIM FUNCTION PER AMM 27-44-04-5. SEEMS TO BE MECHANICAL FUSE PIN BROKEN IN CHAIN DRIVE UNIT. PART NIS KIX. MPN: AJH7378-1 CPN: 0047594 QTY: 1 REPLACED HORIZONTAL STAB CHAIN DRIVE UNIT FUSE PIN AND REINSTALLED CHAIN DRIVE UNIT PER AMM 27-44-06-4. NEED ADJUST CHAIN TENSION. TENSION METER NOT AVAIL AT THIS TIME. PERFORMED HORIZONTAL STABILIZER DRIVE CHAIN ADJUST AND WITHIN LIMIT. ALSO INSPECTED ACME DRIVE, DRIVE CHAIN, JACK SCREW AND OTHER RELATED COMPONENTS AND NO DEFECT FOUND.

Part: INDICATOR — INOPERATIVE (L1 DOOR SLIDE) · airframe 85,941 hrs · 19,378 cycles

EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATOR LIGHT INOP L1 DOOR. RELEASED FOR SERVICE PER MEL : 25-61-02. L1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY. L1 DOOR SYS PRESS VERIFIED PER MEL25-61-02. A/C OK FOR SERVICE. REMOVED AND REPLACED L1 SLIDE REMOTE PRESSURE INDICATOR BATTERIES REF AMM 25-61-04. OPS CHECKED GOOD.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

CENTER CARGO STATION 5-123 RIGHT X= -33 CHANNEL FOUND CORRODED. CENTER CARGO STATION 5-123. RIGHT X= -33 CHANNEL REPAIR CARRIED OUT, AS PER MD-11 SRM 53-50-53-2R REPAIR 1 FIGURE 201 AND REFER TO FEDEX ENGINEERING REQUEST SYSTEM ER NR 20-04025 FOR DISPOSITION. REPAIR CLASSIFIED AS MINOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 85,422 hrs · 19,230 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY XORS 683, BEHIND SLAT NR 6 INBOARD SECTION, FOUND CRACKED. RIGHT WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY XORS 683, BEHIND SLAT NR 6 INBOARD SECTION, REPAIR CARRIED OUT, AS PER MD-11, SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: ANGLE — CHAFED (ZONE 200) · airframe 85,422 hrs · 19,230 cycles

MAIN DECK AT LEFT STATION 535 LONGERON 24, EXISTING REPAIR OUTER ANGLE FOUND CHAFED, AS MARKED. MAIN DECK AT LEFT ON FRAME STATION 535 LONGERON 24 REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK SEAT TRACK CROWN AT STATION 1541 X=27.5 FOUND CORROSION, AS MARKED. MAIN DECK AT STATION 1541 X=27.5 LEFT SEAT TRACK CROWN CORROSION. REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIR BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1571 TO EXISTING SPLICE STATION 1531 X=27.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK SEAT TRACK CROWN AT STATION 1541 X=47.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT AT STATION 1541 X=47.5 SEAT TRACK CROWN BASE AREA 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 AT STATION 1591 TO EXISTING SPLICE STATION 1531 X=47.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: ANGLE — CHAFED (ZONE 200) · airframe 85,422 hrs · 19,230 cycles

MAIN DECK AT STATION 535 LONGERON 20, EXISTING REPAIR OUTER ANGLE FOUND CHAFED, AS MARKED. MAIN DECK AT LEFT ON FRAME STATION 535 LONGERON 20 REPAIR CARRIED OUT IN ACCORANCE WITH SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1671 X=8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT AT STATION 1671 X=8.5 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 AT EXISTING SPLICES STATION 1651 TO STATION 1691 X=8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 85,422 hrs · 19,230 cycles

LEFT HAND WING, FIXED LEADING EDGE FORMER AT APPROXIMATELY XORS 480-500, BEHIND SLAT NR 4 MID SECTION, FOUND CRACKED. LEFT HAND WING, FIXED LEADING EDGE CRACKED FORMER AT APPROXIMATELY XORS 480-500, BEHIND SLAT NR 4 MID SECTION, REMOVED AND REPLACED WITH FABRICATED FORMER. FORMER FABRICATED, PER DOUGLAS DRAWING: ARB2931 REV H. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1671 X= -8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT AT STATION 1671 X= -8.5 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 AT STATION 1651 TO STATION 1691 X= -8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 85,422 hrs · 19,230 cycles

LEFT WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY BETWEEN XORS 505- 540, INSIDE LEFT REFUEL PANEL CUTOUT, FOUND CRACKS. LEFT WING LEADING EDGE BEADED DOUBLER AT APPROXIMATELY BETWEEN XORS 505-540, INSIDE LEFT REFUEL PANEL CUTOUT. REPAIR CARRIED OUT, AS PER MD-11, SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1199 X= -8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT, STATION 1199 X= -8.5 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 AT STATION 1189 TO STATION 1229 X= -8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1388 X= -8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT STATION 1388 RIGHT X= -8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101. ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIR BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1391 TO EXISTING SPLICE STATION 1311 X= -8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK COMPARTMENT, SEAT TRACK AT STATION 5-63 X=8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT AT STATION 5-63 X=8.5 SEAT TRACK EXFOLIATED 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 AT EXISTING SPLICES STATION 5-43 TO STATION 5-123 X=8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1381 X=27.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT STATION 1381 X=27.5 LEFT 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 AT STATION 1391 TO EXISTING SPLICE STATION 1311 X=27.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1525 X=8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT STATION 1525 X=8.5 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 AT STATION 1471 TO EXISTING SPLICE STATION 1531 X=8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 85,422 hrs · 19,230 cycles

MAIN DECK COMPARTMENT, SEAT TRACK AT STATION 1358 X=8.5 FOUND CORROSION, AS MARKED. MAIN DECK COMPARTMENT STATION 1358 LEFT X=8.5 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 AT STATION 1351 TO STATION 1411 X=8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: WEB — CRACKED (CENTER CARGO) · airframe 85,422 hrs · 19,230 cycles

CENTER CARGO STATION 1841 APPROXIMATELY X= -3 FOUND WEBBING PUNCTURED. CENTER CARGO STATION 1841 APPROXIMATELY X=0 TO X= -23 REPAIR CARRIED OUT, PER MD-11 SRM 53-00-00-2R FIGURE 211. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: GENERATOR — MALFUNCTIONED (NR 1) · airframe 84,078 hrs · 18,903 cycles

GEN 3 ON MEL. AT GEAR DOWN GOT "GEN 1 OFF" A/C WENT ON EMERGENCY POWER LOST ALL ASSOCIATED SYSTEMS. GEN 1 CAME BACK ONLINE EXITING THE RUNWAY.

Part: CONTROL UNIT — MALFUNCTIONED (ELECTRICAL SYS) · airframe 84,078 hrs · 18,903 cycles

GEN 3 ON MEL. AT GEAR DOWN GOT "GEN 1 OFF" A/C WENT ON EMERGENCY POWER LOST ALL ASSOCIATED SYSTEMS. GEN 1 CAME BACK ONLINE EXITING THE RUNWAY. PERFORMED T/S AND REPL EPCU IAW AMM 24-08-01-4 REF WRI: 24-00 4955.

Part: SMOKE DETECTOR — FALSE ACTIVATION (MAIN CARGO) · airframe 82,879 hrs · 18,503 cycles

PDIS 592 26-12 3896 14SEP19 MEM FACT U LOGPAGES:2863413 CABIN SMOKE DETECT @ 9000 FT SHGN 14SEP19 11:38 MEM U PERFORMED GVI OF CARGO SMOKE DETORS, ALL DISPLAYED GREEN. PERFORMED OPERATIONAL TEST OF CARGO SMOKE SYSTEM, REF AMM 26-15-1-5. NO FAULTS NOTED. NEEDS ADDITIONAL TROUBLESHOOTING. UPDT 14SEP19 15:29 MEM U MEM FIRE DEPT REPORTED THE CAPTAIN STATED THE ALERT WAS ON FOR LESS THAN 2 SEC. REF FIM TASK 26-15-01-00 PERFOMED ADJ/TEST OF UPPER DECK SMOKE DETECTORS PER AMM 26-14-01-5. DISCONECTED EACH DETECTOR TO VERIFY TEST WOULD SHOW FAILURE AND INSERTED OBJECT TO MAKE EACH UNIT SHOW SMOKE. NO FAULTS NOTED. NO CURRENT OR LAST LEG FAULTS IN MSC. PERFOMED R-T-S OF MSC REF AMM 31-42-01-5, ALL TEST PASSED. NO HISTORY OF CABIN SMOKE. A/C OK FOR CONT SERVICE. REOPEN ITEM DUE TO MOCC REQUEST TO COMPLY WITH TSI 26-12-3897 AND TSI 24-30-3881. REF TSI 26-12-3897 R/R THE FIRST 4 MAIN CARGO DECK SMOKE DETECTORS REF AMM 26-14-01-4 OPS CHECKS GOOD. REF TSI 26-12-3897 R/R MSC REF AMM 31-42-01-4. REF TSI 24-30-3881 PERFOMED FIM 24-30-03-00 STEP 1. PERFOMED OPS CHECK OF BATTERIES REF AMM 24-34-02-5,ALL TEST GOOD.

Part: BRACKET — FAILED (LT MLG) · airframe 82,603 hrs · 18,424 cycles

PDIS 592 32-12 3641 25JUL19 MEM OPEN U LOGPAGES:3095639 AFTER T/O GEAR SHOWED LEFT MAIN PRIMARY/SECONDARY INDICATION UNSAFE. CYCLED GEAR AND GOT GOOD DOWN INDICATION. AFTER FOLLOWING QRH, CYCLED GEAR AND PROBLEM REMAINED. ALL INDICATIONS FOR GEAR DOWN WERE GOOD. LANDING SAFELY. SHGN 25JUL19 09:01 MEM U DEBRIEF FROM CREW: GEAR WOULD NOT RETRACT. LEFT MAIN GEAR DID NOT LOCK IN THE UP POSITION. CREW PERFORMED AN AIR RETURN. UPON ARRIVAL, FOUND #6 MLG BRAKE WET FROM HYDRAULIC FLUID LEAKING. SHGN 26JUL19 03:36 MEM REMOVED AND REPLACED LT MLG HOSE ALIGNMENT BRACKET REF SMP. BLED AND LEAK CHECKED FLEX LINE REF AMM 32-37-01-4, CHECKS GOOD. PROTECTION SHIELD STILL NEEDS TO BE INSTALLED. INSTALLED NEW BRACKET ASSEMBLY AND PROTECTION SHIELD, REINSTALLED HYDRAULIC HOSES AND ELECTRICAL HARNESS TO PROTECTION SHIELD, AND RECONNECTED MAIN LANDING GEAR TORQUE LINKS ON LEFT HAND MAIN LANDING GEAR REFERENCE AMM 32-11-12-4.

Part: SHUTOFF VALVE — FAILED (ELEVATOR) · airframe 82,154 hrs · 18,273 cycles

PDIS 592 29-02 3353 03MAY19 IND FACT U LOGPAGES:3094152 DURING CLIMB OUT TO FL 390 WE RECIVED A LVL 1 HYD 3 ELEV OFF ALERT NO.3 QUANTITY WAS 4.5.W/3-2 NRMP INOP. DURING CRUISE QTY LEVEL WENT TO 4.1. DESCENT INTO IND WE CONFIGURED W/FLAPS 15 AND GEAR DOWN QTY WENT TO 2.3 ON NR 3 CONFIGURED A/C W/ FLAPS 35 AND GEAR DOWN QTY ON NR 3 REMAINED AT 2.3 LANDED A/C UNEVENTFULLY AND TAXIED CLEAR OF RWN 23R FLUID WAS LEAKING NEAR THE ELEVATOR, WE STOPPED A/C AND WAS TOWED INTO GATE. FACT 03MAY19 05:56 IND U REMOVED AND REPLACED NON-REVERSIBLE MOTOR PUMP SHUT-OFF VALVE IAW AMM CH 27-26-40-4-0. LEAK CHECK GOOD.

Part: WASHER — WORN (RT MLG TRUNNION) · airframe 81,487 hrs · 18,089 cycles

CENTER LANDING GEAR RT TRUNNION PIN NUT HAS GAP BETWEEN WASHER AND NUT. REMOVED AND REPLACED CENTER LANDING GEAR RT TRUNNION PIN WASHER AND NUT IAW DAC DWG NYG 6210 VIEW G-G.

Part: ROD — SHEARED (NR 1 ENGINE) · airframe 81,196 hrs · 17,991 cycles

COMPRESSOR STALL CLIMBING OUT OF 12,000 FT NR 1 ENG FL330 2ND COMPRESSOR STALL. WHILE ON DESCENT FOR LANDING OBSERVED THE FOLLOWING AT 6000 NR 1 EGT 512 EGT, 85% N1, NR 2 38 EGT, 77 %, NR 3 351 EGT 77%. CREW DEBRIEF, NR 2 ENG EGT WAS 358 NOT 38. NR 1 ENG THROTTLE NEEDED TO BE RETARDED MORE THAN 1 KNOB DUE TO NR 1 ENG N2 WAS HIGHER THAN ENG'S NR 2 & NR 3 AND NR 1 ENG N1 WAS LOWER THAN ENG'S NR 2 & NR 3 N1. NR 1 ENG EGT WAS HIGHER THAN ENG'S 2 & 3, NO ENG VIBRATION FELT. DURING VSV GVI INSPECTION FOUND ON THE RT SIDE ON THE VSV LEVER ASSY AFT MOST BEARING ROD SHEARED REF CF6-80C2 IPC 72-0-02 FIG 25 ITEM 110 DETAIL "E".

Part: TRANSMITTER — FALSE ACTIVATION (TIRE PRESSURE) · airframe 81,132 hrs · 17,968 cycles

TIRE FAIL AFTER GEAR RETRACTION. REMOVED AND REPLACE TIRE PRESSURE TRANSMITTER. OK FOR SERIVCE

Part: SWITCH — STUCK (ZONE 200) · airframe 81,101 hrs · 17,960 cycles

DURING FLIGHT, LEFT SIDE CREW ENTRANCE DOOR SLIDE/RAFT INSIDE LIGHT CAME ON FOR REMAINING OF FLIGHT. FOUND LIGHT SWITCH STUCK IN. REMOVED SWITCH AND READJUSTED SWITCH, OPS CHECKS GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= -2 FOUND CORROSION ON FLANGE AT STA 1950 AS MARKED MAIN DECK AFT FLOOR SUPPORT AT STA 1887 TO STA 2007, X= -2 CORROSION ON FLOOR SUPPORT FLANGE AT STA 1950, X= -2 REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1950, X= -2 REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 5 AND EA 1-5310-T0342644 PART 1 TITLE: FUSELAGE- MAINFRAME- CORROSION, FLANGES ON AFT CENTER LAVATORY RIGHT INBOARD FLOOR SUPPORT BETWEEN STA1942 AND STA2007. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N00839 AND WRI 53-10/2676 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= -2 FOUND CORROSION ON FLANGE AT STA 1988 AS MARKED MAIN DECK AFT FLOOR SUPPORT AT STA 1887 TO STA 2007, X= -2 CORROSION ON FLOOR SUPPORT FLANGE AT STA 1988, X= -2 REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53- 00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1988, X= -2 REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 5 AND EA 1-5310-T0342644 PART 1 TITLE: FUSELAGE- MAINFRAME- CORROSION, FLANGES ON AFT CENTER LAVATORY RIGHT INBOARD FLOOR SUPPORT BETWEEN STA1942 AND STA2007. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. REFER TO SNRM N00839 AND WRI 53-10/2676 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= -2 FOUND CORROSION ON FLANGE AT STA 1970 AS MARKED MAIN DECK AFT FLOOR SUPPORT AT STA 1887 TO STA 2007, X= -2 CORROSION ON FLOOR SUPPORT FLANGE AT STA 1970, X= -2 REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1970, X= -2 REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 5 AND EA 1-5310-T0342644 PART 1 TITLE: FUSELAGE- MAINFRAME- CORROSION, FLANGES ON AFT CENTER LAVATORY RIGHT INBOARD FLOOR SUPPORT BETWEEN STA1942 AND STA2007. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N00839 AND WRI 53-10/2676 FOR WORK DETAILS.

Part: BUSHING — CORRODED (LT WING) · airframe 81,031 hrs · 17,948 cycles

LEFT WING INBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD HOLE BORE FOUND CORROSION. CORROSION REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332062 A PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BUSHING — CORRODED (RT WING) · airframe 81,031 hrs · 17,948 cycles

RIGHT WING INBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. CORROSION REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332063 B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= 2 FOUND CORROSION ON FLANGE AT STA 1895 AS MARKED. MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= 2, CORROSION ON FLOOR SUPPORT FLANGE AT STA 1895 REMOVED AND FOUND TO EXCEED LIMIT PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1895, X= 2 REPAIRED AS PER SRM 53-00-52- 2R FIG 201 REPAIR 5. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: BUSHING — CORRODED (LT WING) · airframe 81,031 hrs · 17,948 cycles

LEFT WING INBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332062 A PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= 2 FOUND CORROSION ON FLANGE AT STA 1929 AS MARKED. MAIN DECK AFT FLOOR SUPPORT AT STA 1887-2007 X= 2, CORROSION ON FLOOR SUPPORT FLANGE AT STA 1929 REMOVED AND FOUND TO EXCEED LIMIT PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1929, X= 2 REPAIRED AS PER SRM 53-00-52-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: BUSHING — CORRODED (RT WING) · airframe 81,031 hrs · 17,948 cycles

RIGHT WING INBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. CORROSION REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332063 B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION REWORKED AND FOUND BEYOND REWORK LIMIT AS PER CMM57-44-09. NEW REPAIR SHIM FABRICATED AND INSTALLED PER CMM57-44-09 AND EA NR 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SUPPORT FRAME — CORRODED (RT MLG) · airframe 81,031 hrs · 17,948 cycles

AFTER REMOVED RT MLG RETRACT SUPPORT FRAME FOR REPAIR, FOUND UPPER AFT BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1)(A)(1) REPAIR 1. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5740-T0342673 PT 1 STEP 7D & 7D(3). REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SUPPORT FRAME — CORRODED (RT MLG) · airframe 81,031 hrs · 17,948 cycles

DURING REPLACEMENT OF RT MLG RETRACT SUPPORT FRAME LOWER AFT MOUNT BOLT PLI WASHER, FOUND BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1) (A)(1) REPAIR 1. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5740-T0342673 PT 1 STEP 7D & 7D(3). REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SUPPORT FRAME — CORRODED (LT MLG) · airframe 81,031 hrs · 17,948 cycles

DURING REPLACEMENT OF LT MLG RETRACT SUPPORT FRAME LOWER FWD MOUNT BOLT PLI WASHER, FOUND BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1) (A)(1) REPAIR 1. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5740-T0342582 PT 1 STEP 6D & 6D(3). REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SUPPORT FRAME — CORRODED (RT MLG) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

DURING REPLACEMENT OF RT MLG RETRACT SUPPORT FRAME LOWER TWO MOUNT BOLT PLI WASHER FOUND BOLT HOLE OF SUPPORT FRAME CORROSION. CORROSION REWORKED, FOUND EXCEEDED LIMIT PER SRM 57-20-14-2R PARA 4C STEP (1)(A)(1) REPAIR 1. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5740-T0342673 PT 1 STEP 7D AND 7D(3). REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) FWD MOUNT INBD HOLE BORE FOUND CORROSION. HOLE NR 6 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 AND EA 1-5750-73333C PT 3 STEP 1. EO 1-5750-7-5002 RT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-73333C PT 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE FOUND CORROSION. NR 7 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2C. EO 1-5750-7-5002 LT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-T0342336 PT 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORROSION. HOLE BORE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW SHOULDER BUSHING FABRICATED PER EA 1-5750-T0342336 PT 1 STEP 2A AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEP 2. EO 1-5750-7-5002 LT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-T0342336 PT 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE BORE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2B. EO 1-5750-7-5002 LT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-73333C PT 3 STEP 1. EO 1-5750-7-5002 RT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) LOWER MOUNT INBD HOLE BORE FOUND CORROSION LH WING O/B FLAP I/B HINGE ( WING SIDE) LOWER MOUNT I/B HOLE BORE (#7 HOLE) CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED PER MD11 CMM57-44-08 AND FEDEX EA #1-5750-T0342352 PT 1 STEPS 2 & 2A 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 FEDEX EA #1-5750-T0342352 PT 1 & SNRM #N00312 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACH INBD LUG HOLE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2D. EO 1-5750-7-5002 LT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-T0342336 PT 1 FOR WORK DETAILS.

Part: SKIN — PUNCTURED (TE FLAP VANE) · airframe 81,031 hrs · 17,948 cycles

RIGHT WING INBD FLAP VANE LOWER SURFACE FOUND PUNCTURED AT XIFH 193.875. SKIN REPAIR CARRIED OUT METAL BONDED WITH FILLER AND DOUBLER AS PER SRM 51-71-00 PARAGRAPH 20 AN EA 1-5750-T0342536 PART 1. REPAIR ON RT INBD FLAP VANE ARC2557-54 LOWER SKIN. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP INBD (WING SIDE) CLEVIS FITTING HOLE BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-16. OVERSIZED BUSHING AND REPAIR WASHER FABRICATED AND INSTALLED PER CMM57-44-16 AND EA 1-5740-130969A PT 2 STEPS 2, 2A & 2B. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 AND EA 1-5750-73333C PT 3 STEP 1. EO 1-5750-7-5002 RT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-73333C PT 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. HOLE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. LH WING O/B FLAP I/B HINGE ( WING SIDE) LOWER MOUNT O/B HOLE BORE( #7 HOLE) CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED PER MD11 CMM57-44-08 AND FEDEX EA #1-5750-T0342352 PT 1 STEPS 2 & 2A 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 GMM6-2-100. REFER TO FEDEX EA #1-5750-T0342352 PT 1 & SNRM #N00312 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED FOUND EXCEEDED LIMIT PER CMM57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) FWD MOUNT OUTBD HOLE BORE FOUND CORROSION. NR 6 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW REPAIR BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-73333C PT 3 STEP 1. EO 1-5750-7-5002 RT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-73333C PT 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORROSION. HOLE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. LUG HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-T0342352 PT 1 STEPS 2 & 2C. EO 1-5750-7-5002 LT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-T0342352 PT 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE SURFACE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. REPAIR EVALUATED FOUND ACTUATOR ATTACHED I/B LUG SURFACE REMAINING THICKNESS 0.317" ACCEPTED PER EA 1-5750-73333C PT 3 STEP 1 FIG 2. EO 1-5750-7-5002 RT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-73333C PT 3 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. HOLE BORE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW SHOULDER BUSHING FABRICATED PER EA 1-5750-T0342336 PT 1 STEP 2A AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEP 2. EO 1-5750-7-5002 LT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-T0342336 PT 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) BARREL NUT HOLE SURFACE FOUND CORROSION LH WING O/B FLAP I/B HINGE ( WING SIDE) BARREL NUT HOLE SURFACE CORROSION REWORKED AS PER MD1 CMM57-44-08. NEW REPAIR SHIM FABRICATED AND INSTALLED PER MD11 CMM57-44-08 AND FEDEX EA #1-5750-T0342352 PT 1 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 GMM6-2-100. REFER TO FEDEX EA #1- 5750-T0342352 PT 1 & SNRM #N00312 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. LUG HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-T0342352 PT 1 STEPS 2 & 2C. EO 1-5750-7-5002 LT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-T0342352 PT 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR ATTACH OUTBD LUG HOLE FOUND CORROSION. NR 8 HOLE CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2D. EO 1-5750-7-5002 LT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-T0342336 PT 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE FOUND CORROSION. BOLT HOLE NR 7 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2C. EO 1-5750-7-5002 LT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO EA 1-5750-T0342336 PT 1 FOR WORK DETAILS.

Part: HINGE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) PIVOT HOLE BORE FOUND CORROSION. LH WING ( WING SIDE ) O/B FLAP I/B HINGE PIVOT HOLE BORE #4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM 57-44-08. NEW OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED PER MD11 CMM57-44-08 AND FEDEX EA #1-5750-T0342352 PT 1 STEP 2 AND 2A 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: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

FWD CABIN, UPON LAVATORY MODULE REMOVED FOR FLOORBEAM ATTACH ANGLE REPAIR ACCESS, FOUND RT FLOOR SUPPORT AT STA 413, X= -25 CORROSION. FLOOR SUPPORT CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING WSP0668 REVISION 'B'. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 81,031 hrs · 17,948 cycles

RIGHT WING LEADING EDGE COMPT LOWER SURFACE PANEL CUTOUT FWD EDGE DOUBLER AT STA XOS 604 FOUND CRACK. CRACKED DOUBLER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW DOUBLER AS PER DRAWING ARB2933 REVISION AJ. INSTALLED NEW DOUBLER AT RIGHT WING LEADING EDGE COMPT LOWER SURFACE PANEL CUTOUT AT STA XOS 604 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT ATTACHED OUTBD LUG HOLE FOUND CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0326166 B PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 81,031 hrs · 17,948 cycles

VERTICAL STAB REAR CENTER SPAR TO REAR SPAR INTERCOSTAL STA 2164, RIGHT SIDE AFT END FOUND CRACKED. INTERCOSTAL REPAIR CARRIED OUT AS PER SRM 55-30-02-2R FIGURE 204 REPAIR 7 AND EA 1-5530-T0342479 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT OUTBD LUG HOLE FOUND CORROSION. HOLE A AND B REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-73337 D PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

RIGHT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT ATTACHED INBD LUG HOLE FOUND CORROSION. CORROSION (HOLE F AND G) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0326166 B PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

LEFT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT INBD LUG HOLE FOUND CORROSION. CORROSION (HOLE F AND G) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-73337 D PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 81,031 hrs · 17,948 cycles

UPPER AUX FUEL TANK STRINGER NR 47 FROM XCW=50 TO XCW=57 FOUND CRACK. UPPER AUX FUEL TANK STRINGER REPAIRED AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 81,031 hrs · 17,948 cycles

UPPER AUX FUEL TANK STRINGER 52 FROM XCW=50 TO XCW=56 FOUND CRACK. UPPER AUX FUEL TANK STRINGER 52 FROM XCW=35.5 TO XCW=59.5 AREA REPAIRED AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPLICE — NOT REPORTED (LT WING) · airframe 81,031 hrs · 17,948 cycles

LT WING, DURING ACCOMPLISHMENT OF EA 1-5710-T0329978 PART 2 FOUND UNABLE TO COMPLY WITH STEP 3 WORK INSTRUCTIONS AS P/N ARB3143-1 NOT AVAILABLE FOR REPLACEMENT EXISTING SPLICE REMOVED AS PER SRM 51-31-01-0G. NEW SPLICE FABRICATED AS PER DRAWING ARB3143 REVISION B AND INSTALLED NEW SPLICE AT LT WING AT STA XORS 685.40 STRINGER 11 AS PER SRM 51-33-01-0G AND DRAWING ARB3218 REVISION AH. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 81,031 hrs · 17,948 cycles

HFEC INSPECTION CARRIED OUT ON RT REAR SPAR CAP FORWARD FLANGE LOCATED AT THE UPPER SECTION OF NR 4 BANJO FITTING OF LOWER VERTICAL STABILIZER, STA 2164 AND FOUND CRACK APPROX 0.2" LENGTH. SPAR CAP FORWARD FLANGE TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAIR 5. REPAIR CARRIED OUT AT RT NR 4 BANJO FITTING AS PER SRM 55-30-02-2R FIGURE 202 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT LT CURVE SEAT TRACK AT STA 1940 TO STA 2007, X= 107 FOUND CORROSION. SEAT TRACK CORROSION REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED LT CURVED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1831 TO STA 2007, X= 107 AS PER SRM 53-00-00-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X= 25 FOUND CORROSION. FLOOR SUPPORT CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7087 REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 81,031 hrs · 17,948 cycles

DURING ACCOMPLISHMENT OF HFEC INSPECTION AT LT WING LEADING EDGE SKIN ADJACENT TO CUTOUTS AND ACCESS DOORS, FOUND 1EA CRACK INDICATION AT CORNER NR 13, APPROXIMATE 0.2" IN LENGTH. REPAIR CARRIED OUT AT LT WING FIXED LEADING EDGE AT CORNER NR 13, AT STA XOS 657 AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT 1887- STA 2007, X= 2 FOUND CORROSION ON FLANGE AT STA 1910 AS MARKED. CORROSION REMOVED AND FOUND TO EXCEED LIMIT PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1910, X= 2 REPAIRED AS PER SRM 53-00-52-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 81,031 hrs · 17,948 cycles

RT WING LEADING EDGE CAVITY AT STA XOS 587 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY AT STA XOS 587 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X= 56 FOUND CRACKED. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 81,031 hrs · 17,948 cycles

LT WING LEADING EDGE CAVITY AT STA XOS 744 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT AT LT WING LEADING EDGE CAVITY AT STA XOS 744 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X=-25 FOUND CRACKED. MAIN DECK AFT FLOOR SUPPORT 1887- STA 2007, X=-25 CRACKED FLANGE LOBE REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT AT STA 1887- STA 2007, X=-56 FOUND CRACKED. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 81,031 hrs · 17,948 cycles

HFEC INSPECTION CARRIED OUT ON LT REAR SPAR CAP FORWARD FLANGE LOCATED AT THE UPPER SECTION OF NR 4 BANJO FITTING OF LOWER VERTICAL STABILIZER , STA Y=2164 AND FOUND CRACK APPROX. 1.5 " LENGTH. SPAR CAP FORWARD FLANGE TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAIR 5. REPAIR CARRIED OUT AT LT NR 4 BANJO FITTING AS PER SRM 55-30-02-2R FIGURE 202 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (LE SLAT) · airframe 81,031 hrs · 17,948 cycles

RT WING DROOP LEADING EDGE FOUND CHAFED, STA XDLE 309. REPAIR CARRIED OUT AT RT WING DROOP ASSEMBLY LEADING EDGE AT INBOARD STA XDLE 309 AS PER SRM 57-40--01-2R FIGURE 202 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

MAIN DECK AFT FLOOR SUPPORT 1887- STA 2007, X=-2 FOUND CORROSION ON FLANGE AT STA 1962 AS MARKED. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT FLANGE AT STA 1962, X= -2 REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 5 AND EA 1-5310-T0342644 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

FLIGHT COMPARTMENT RT OBSERVER SEAT BASE CUTOUT WEB FOUND CRACK, AT STA 360, X=- 8. CRACKED WEB REPAIRED AS PER SRM 53-10-51-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPLICE — NOT REPORTED (RT WING) · airframe 81,031 hrs · 17,948 cycles

RT WING, DURING ACCOMPLISHMENT OF EA 1-5710-T0329981 PART 2 FOUND UNABLE TO COMPLY WITH STEP 3 WORK INSTRUCTIONS AS P/N ARB3143-2 NOT AVAILABLE FOR REPLACEMENT EXISTING SPLICE REMOVED AS PER SRM 51-31-01-0G. NEW SPLICE FABRICATED AS PER DRAWING ARB3143 REVISION B AND INSTALLED NEW SPLICE AT RT WING AT STA XORS 685.40 STRINGER 11 AS PER SRM 51-33-01-0G AND DRAWING ARB3218 REVISION AH. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (LT WING) · airframe 81,031 hrs · 17,948 cycles

LEFT HAND WING LEADING EDGE FORMER/STIFFENER AT STA XOS 549 FOUND CRACKED. CRACKED FORMER(STIFFENER) REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2918 REVISION G. INSTALLED NEW FORMER (STIFFENER) AT LEFT HAND WING LEADING EDGE AT STA XOS 549 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK LT FRAME AT STA 535 LONGERON 19L EXISTING REPAIR ANGLE DAMAGED MAIN DECK. REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,031 hrs · 17,948 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1229, X=-75.25 FOUND CORROSION MAIN DECK FLOOR. 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 REPLACEMENT FROM STA 1169 TO EXISTING SPLICE AT STA 1269, X= -75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK LT FRAME AT STA 535 LONGERON 24L FOUND EXISTING REPAIR ANGLE DAMAGED. REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

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

Part: FRAME — DAMAGED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

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

Part: FORMER — CRACKED (LT WING) · airframe 81,031 hrs · 17,948 cycles

LEFT HAND WING LEADING EDGE FORMER AT STA XOS 1025 FOUND CRACKED. CRACKED FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2920 REVISION BB. INSTALLED NEW FORMER AT LEFT HAND WING LEADING EDGE CAVITY AT STA XOS 1025 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 81,031 hrs · 17,948 cycles

RIGHT HAND WING LEADING EDGE CAVITY FORMER AT STA XOS 1025 FOUND CRACKED. CRACKED FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2920 REVISION BB. INSTALLED NEW FORMER AT RIGHT HAND WING LEADING EDGE CAVITY AT STA XOS 1025 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 775 X = 8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLEND OUT AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES STA 745 TO STA 801, X=8.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1541 X = 8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLEND OUT AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICE STA 5-123/1531 TO STA 1671, X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK LT FRAME AT STA 1661 LONGERON 12L FOUND EXISTING REPAIR ANGLE DAMAGED. DAMAGED REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 5-11 X = 8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED EDGE BLEND OUT AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-43 TO EXSITING SPLICE STA 5-0, X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SKIN PANEL — CRACKED (VERTICAL STAB) · airframe 81,031 hrs · 17,948 cycles

EMPENNAGE LT SIDE LOWER VERTICAL STABILIZER IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN PANEL CRACKED. SKIN PANEL REPAIR CARRIED OUT AS PER EA 1-5530-T0342403 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 5-11 X = 27.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLEND OUT AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-63 TO EXISTING SPLICE AT STA 5-0, X= 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1541 X =-47.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLENDOUT AND EXCEEDED LIMIT AS PER SRM-53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1571 TO EXISTING SPLICE STA 5-123/1531, X= - 47.5 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,031 hrs · 17,948 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1541 X =-8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGED CROWN EDGE BLEND OUT AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1571 TO EXISTING SPLICE AT STA 5-123/ 1531, X= -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RELAY — INOPERATIVE (L1 DOOR) · airframe 80,957 hrs · 17,933 cycles

L1 DOOR CONTROL SWITCH WAS STICKING IN THE OPEN POSITION. THE DOOR CONTINUES TO OPEN EVEN IF SWITCH IS NOT HELD IN POSITION. REMOVED AND REPLACED THE RELAY R1-177 IAW SWPM 20-20-03. DOOR OPERATED THROUGH FULL TRAVEL OPEN AND CLOSED IAW AMM 52-11-02-2. OK FOR SERVICE.

Part: ACTUATOR — FAILED (L1 DOOR) · airframe 80,810 hrs · 17,878 cycles

L1 DOOR VERY SLOW TO ENGAGE AND START MOVING WITH THE ELECTRIC SWITCH. WHEN USING EXTERIOR SWITCH, MOTOR AND OR RELAY WAS CHATTERING. REMOVED AND REPLACED THE L1 DOOR ACTUATOR IAW AMM 52-11-01-4. OPS CHECKED GOOD.

Part: ACTUATOR — INTERMITTENT (L1 DOOR) · airframe 79,939 hrs · 17,612 cycles

L1 DOOR WILL NOT OPEN ELETRICALLY. ON ARRIVAL, OPS CHECK OF THE L1 DOOR, FOUND NORMAL, NO FAULTS NOTED IAW AMM 52-10-01-2. RESET THE CLUTCH RELEASE ON THE ELECTRICAL ACTUATOR TO LET THE DOOR OPERATE AGAIN. SUSPPECT CLUTCH STUCK INTERMITTENTLY, R & R THE DOOR ELECTRICAL ACTUATOR IAW AMM 52-11-01-4. PERFORMED AN OPS CHECK OF THE L1 DOOR IAW AMM 52-10-01-2. CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: CONNECTOR — DIRTY (FIRE DETECTION) · airframe 76,914 hrs · 16,749 cycles

AT 80-90 KNOTS, RECEIVED A NR 1 ENGINE FIRE ALERT, AFTER STOPPING AIRCRAFT COMPLIED WITH QRH PROCEDURE, INCLUDING DISCHARGING SINGLE FIRE BOTTLE. FOUND HIGH RESISTANCE TO GROUND 2 MEGA OHMS ON B LOOP CAUSED BY WATER AND CARBON. CLEANED ON ALL CONNECTORS CHECKED FOR DUCT LEAKS, NONE FOUND. TROUBLESHOT THE FIRE DETECTION SYSTEM IAW FIM 26-11-4, NO ADDITIONAL FAULTS FOUND. OK FOR SERVICE. COMPLETED ALL ACTIONS. ACFT OK FOR SERVICE.

Part: STRUCTURE — CORRODED (BS 470) · corrosion level 2 · airframe 76,583 hrs · 16,640 cycles

FORWARD AVIONICS COMPARTMENT BILGE AREA BS 470 FOUND WITH CORRODED. REPAIRED IAW EA 1-5310-T0330006 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 76,583 hrs · 16,640 cycles

DURING HFEC INSPECTION ON RT WING FIXED LEADING EDGE SLAT TRACK NR 10 CUTOUT, AFT INBD CORNER NR 13, FOUND ONE CRACK APPROXIMATELY 0.25IN LONG. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,583 hrs · 16,640 cycles

LEFT WING FIXED LEADING EDGE CAVITY AT XOS 767 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,583 hrs · 16,640 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 664 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 76,583 hrs · 16,640 cycles

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

Part: SEAT TRACK — CRACKED (BS 635) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 635, LBL 27.5 FOUND CRACKED. SEAT TRACK REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (BS 1621) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK LEFT FRAME AT BS 1621 FOUND DAMAGED. REPAIRED THE FRAME IAW SRM 53-00-07-2R FIG 201 REPAIR 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-00.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 635, LBL 47.5 FOUND CRACKED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (BS 1741) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK LEFT FRAME AT BS 1741 FOUND DAMAGED. FRAME REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 635) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 635, RBL 27.5 FOUND CRACKED. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 755) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 755, LBL 47.5 FOUND CRACKED. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (BS 1661) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK RIGHT FRAME AT BS 1661 FOUND DAMAGED. FRAME REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 76,583 hrs · 16,640 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 738 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 5-5 TO 5-15, RBL 47.5 FOUND THE CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIRED CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 76,583 hrs · 16,640 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 553 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 76,583 hrs · 16,640 cycles

RH WING FIXED LEADING EDGE CAVITY AT STA XOS 638 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 5-5 TO 5-10, RBL 8.5 FOUND THE CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 76,583 hrs · 16,640 cycles

LEFT WING FIXED LEADING EDGE CAVITY AT XOS 620 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 76,583 hrs · 16,640 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 613 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 753-763) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 753 TO 763, RBL 47.5 FOUND DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 76,583 hrs · 16,640 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 683 BEADED DOUBLER CRACKED. REPAIRED SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 76,583 hrs · 16,640 cycles

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

Part: DOUBLER — CRACKED (RT WING LE) · airframe 76,583 hrs · 16,640 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 563 BEADED DOUBLER CRACKED. REPAIR IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 76,583 hrs · 16,640 cycles

LEFT WING FIXED LEADING EDGE CAVITY AT XOS 544 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 76,583 hrs · 16,640 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 669 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 5-5, LBL 47.5 FOUND THE CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1287) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1287, RBL 8.5 FOUND CROWN DAMAGE. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 5-5 TO 5-15, X=-27 FOUND THE CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1287) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 1287, LBL 27 FOUND DAMAGED. SEAT TRACK REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1287) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 1287, RBL 47.5 FOUND DAMAGED. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1279-1287) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 1279 TO 1287 LBL 47.5 FOUND DAMAGED. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 773) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 773, LBL 75.25 SEAT TRACK DAMAGED. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 6-40, X=-47.5 FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1139) · airframe 76,583 hrs · 16,640 cycles

MAIN DECK SEAT TRACK AT BS 1139, RBL 47.5 FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DEU — FAULTY (COCKPIT) · airframe 75,750 hrs · 16,394 cycles

ON CLIMBOUT, PASSING 8,000 FT, WE HAD THE FOLLOWING ALERTS: LVL 2, GEN LOAD HI, LVL 1, BUS AC 1 OFF, BUS AC 2 OFF, BUS AC 3 OFF, SEL LSAS ROB OFF, GALLEY BUS OFF, SEL FUEL SYS MANUAL. THE SD SHOWED THE ASSOCIATED BUSSES OFF WITH ADG, EMERGENCY BUSSES AND DC BUSSES GREEN. THE OVERHEAD PANEL HAD NO ABNORMAL INDICATIONS. QRH COMPLIED WITH FOR EACH ALERT. SYSTEM COMPONENTS ASSOCIATED WITH THE AC BUSSES APPEARED TO WORK. REPLACED NR 3 DEU, REF AMM 31-61-02-4, CONFIRMED CONFIG CODE, REF AMM 31-61-00-2, AND SOFTWARE MATCHED DEU 1 AND DEU 2, REF AMM 31-61-02-3. PERFORMED REQUIRED RVSM TEST REF AMM 34-10-00-2, TABLE 1. ALL TESTS PASSED.

Part: STATOR — DISINTEGRATED (NR 3 BRAKE) · airframe 733 hrs · 15,598 cycles

NR 3 MAIN BRAKE CTR STATOR DISINTEGRATED, ALL OTHERS COMING APART. WILL R & R BRAKE. R&R NR 3 BRAKE ASSY IAW MM 32-43-20-4. OK FOR SERV.

Part: ADG — DEPLOYED · airframe 720 hrs · 15,201 cycles

PERFORMED AIR TURN BACK DUE TO ADG DEPLOYED IN FLIGHT UNCOMMANDED, REPEAT.

Part: LATCH — WORN (ADG) · airframe 720 hrs · 15,198 cycles

ADG DEPLOYED DURING CLIMB OUT. FLIGHT CONTINUED TO DESTINATION. VERIFIED DOOR LINK AND ADG DOWN POSITION ARE CORRECTLY ADJUSTED IAW AMM 24-25-01-5. OPS TEST FOR ADG SNUBBER CARRIED OUT AND TESTED NORMALLY IAW AMM 24-25-04-2.

Part: ADG — UNWANTED DEPLOY (N/A) · airframe 720 hrs · 15,201 cycles

APPROXIMATELY 10 MIN AFTER TAKEOFF, ADG AUTOMATICALLY DEPLOYED ON ITS OWN. FOLLOWED MTSI 24-25 7243 DISCONNECTED RELEASE CABLE & ADG DOOR LINKAGE, THEN INSPECTED RELEASE CABLE FOR ROUTING & BINDING, NO DEFECT NOTED. INSPECTED ADG & LATCH MECHANISM FOR WEAR OR OTHER DAMAGE, NO DEFECT NOTED. CHECKED RIGGING OF RELEASE CABLE & ADG DOOR LINKAGE, FOUND OUT OF RIG. PERFORMED ADG RELEASE CABLE RIGGING, ADG DOWN POSITION ADJUSTMENT, ALSO PERFORMED ADG DOOR LINKAGE ADJUSTMENT IAW AMM24-25-01-5. SHAKE DOWN RELEASE CABLE & ADG AT STOWED POSITION, ADG STAYED IN STOW POSITION. ACFT OK FOR SERVICE.

Part: FORMER — CRACKED (RT WING) · airframe 72,007 hrs · 15,190 cycles

RIGHT WING LE PANEL CUT OUT FORMER AT XOS 559 FOUND CRACKED. FORMER REMOVED IAW SRM 51-31-01. NEW FORMER FABRICATED IAW DWG ARB1162 REV S AND INSTALLED IAW SRM 51-31-01. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 72,007 hrs · 15,190 cycles

CENTER CARGO LONGERON SPLICE FITTING FOUND CRACK AT STATION 5 - 123 LONGERON 45R. LONGERON REMOVED AS PER SRM 51-33-01 NEW LONGERON SPLICE FITTING FABRICATED BY MACHINING PER DRAWING A5A7116 REVISION D AND INSTALLED AS PER SRM 51-33-01 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: REPAIR — BULGED (FUSELAGE) · airframe 72,007 hrs · 15,190 cycles

LOWER FUSELAGE SKIN AT STATION 735 - 755 LONGERON 38R - 39R ON EXISTING REPAIR FOUND SKIN BULGING. REPAIR REMOVED AS PER SRM 51-31-01 NEW REPAIR CARRIED OUT AS PER SRM 53- 00-01 FIGURE 201 (SHEET 2) REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 72,007 hrs · 15,190 cycles

CENTER CARGO LONGERON SPLICE FITTING FOUND CRACK AT STATION 5 - 123 LONGERON 44R. LONGERON REMOVED AS PER SRM 51-33-01 NEW LONGERON SPLICE FITTING FABRICATED BY MACHINING PER DRAWING A5A7114 REVISION J AND INSTALLED AS PER SRM 51-33-01 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: FRAME — DENTED (BS 1721) · airframe 72,007 hrs · 15,190 cycles

REPAIR ON FRAME FOUND DENTED, BS 1721 BETWEEN LONGERONS 12 & 13L. REPAIRED IAW SRM 51-33-01 AND SRM 53-00-07 FIGURE 201 REPAIR 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1681) · airframe 72,007 hrs · 15,190 cycles

REPAIR ON FRAME FOUND DENTED, BS 1681 BETWEEN LONGERONS 12 & 13L. REPAIRED IAW SRM 51-33-01 AND SRM 53-00-07 FIGURE 201 REPAIR 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1701) · airframe 72,007 hrs · 15,190 cycles

RT SIDE REPAIR ON FRAME FOUND DENTED BS 1701 BETWEEN LONGERONS 12 & 13R. REPAIRED IAW SRM 51-33-01 AND SRM 53-00-07 FIGURE 201 REPAIR 2. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 72,007 hrs · 15,190 cycles

DURING AN INSPECTION, LEFT WING NR 8 SLAT LOWER SURFACE FOUND CRACKED ABOUT THREE INCHES AT XOS 1086. REPAIRED IAW EA1-5750-T0314714 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: RIB — DAMAGED (NR 8 SLAT) · airframe 72,007 hrs · 15,190 cycles

DURING NR 8 SLAT ASSEMBLY REMOVAL, FOUND LEFT WING NR 8 SLAT INBD TRACK RIB HAS AN ELONGATED HOLE. REPAIRED IAW EA 1-5750-T0314714 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: RIB — DAMAGED (NR 8 SLAT) · airframe 72,007 hrs · 15,190 cycles

DURING SLAT REMOVAL, FOUND LEFT WING NR 8 SLAT INBD TRACK RIB HAS AN ELONGATED HOLE. REPAIRED IAW EA 1-5750-T0314714 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (NR 8 SLAT) · airframe 71,986 hrs · 15,187 cycles

FOUND A HOLE & CRACKS IN LE SKIN OF NR 8 SLAT.

Part: PRESSURE SWITCH — MALFUNCTIONED (NR 2 ENGINE OIL) · airframe 71,584 hrs · 15,049 cycles

APPROXIMATELY 1 HOUR INTO FLIGHT, RECEIVED A NR 2 ENGINE OIL FILTER ALERT. RETARDED THROTTLE TO IDLE IAW CHECKLIST. ALERT STILL REMAINED. SHUTDOWN THE ENGINE. ALL OTHER INDICATIONS WERE NORMAL. TROUBLESHOT IAW FIM 79-00-03. REPLACED OIL SCAVENGE FILTER ELEMENT IAW MM 79-22-05-4-1. NO CONTAMINATION FOUND IN OLD FILTER. R & R OIL FILTER DIFFERENTAL PRESSURE SWITCH IAW MM 79-35-01-4-1. RAN ENGINE IAW JRH, NO LEAKS NOTED & NO ENGINE FILTER ALERTS. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,270 hrs · 14,937 cycles

DURING EMERGENCY LIGHT TEST, RECEIVED AN EMERGENCY LIGHT BATTERY 1 LOW. TROUBLESHOOTING IS REQUIRED PRIOR TO INSTALLING PARTS. R & R EMERGENCY BATTERY IAW AMM 33-51-01-4 & FUNCTIONED IAW AMM 33-51-01-5. ALL TESTS PASSED. R & R EMERGENCY LIGHTS BATTERY IAW AMM 33-51-01-4 AND TESTED SATISFACTORY IAW AMM 33-51-01-5.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,246 hrs · 14,931 cycles

ON EMER LIGHT TEST GOT EMER LT BAT 1 LO MEL 33-50-04, EMER LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PER AMM CHP33-51-01-4 AND FUNCTIONED PER AMM CHP33-51-01-5. ALL TESTS PASSED.

Part: SKIN — CRACKED (LT WING) · airframe 70,532 hrs · 14,684 cycles

FOUND POSSIBLE CRACK ON LT WING AT INBD SIDE OF PRESS REFUEL DOOR, NDT NOTIFIED. LT WING LE LWR CRACK AREA, HFEC INSPECTION OF SUSPECT CRACK AREA, COMPLIED WITH & CONFIRMED CRACK IAW NTM 06-00-06. CUT OUT CRACK IAW 57-40-02. PERFORMED HFEC OF CUT OUT AREA IAW NTM PT6, NO CRACKS NOTED. FABRICATED DOUBLER FROM .063 TITANIUM & OK TO INSTALL ALL. REPAIRED IAW EA 1-5730-T0308436 P 1. AWAITING FINAL EA.

Part: LATCH — OUT OF ADJUST (ADG) · airframe 69,852 hrs · 14,457 cycles

ADG DEPLOYED IN FLIGHT. INSPECTED ADG & FOUND NO DEFECTS. ATTEMPTED TO STOW ADG IAW MD 1124-25-01-2. FOUND UP LATCH NOT FULLY ENGAGED. ADJUSTED UP LATCH & PUSH PULL CABLE IAW MM 24-25-01-5. DEPLOYED ADG & RESTOWED ADG IAW MM 24-25-01-2, OPERATIONS CHECKED NORMAL.

Part: INDICATOR — INOPERATIVE (R1 DOOR SLIDE) · airframe 69,570 hrs · 14,376 cycles

R1 DOOR SLIDE WILL NOT TEST. R & R REMOTE PRESSURE INDICATOR LIGHT ASSEMBLY IAW AMM 25-61-04-4.

Part: ENGINE — FAILED · airframe 68,808 hrs · 14,110 cycles

IMMEDIATELY AFTER TAKEOFF, HEARD A DULL VIBRATION. CHECKED ENGINES AND FOUND EVM COMP =5.0 AMBER WITH A AMBER BOX. N1 WAS BETWEEN 80-85 PERCENT, N2 WAS NEAR 110 PERCENT. REMOVED AND REPLACED ENGINE.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 67,617 hrs · 13,739 cycles

RT WING NR 6 L/E SLAT INBD TRACK CUTOUT INBD LOWER CORNER FOUND CRACKED DURING OTBD SLAT CONTROL CABLES INSPECTION. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 51. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: SLIDE — FAILED (R1 DOOR) · airframe 67,026 hrs · 13,574 cycles

PRE-FLIGHT CHECKED FOUND R1 DOOR EVACUATION REMOTE PTT INDICATOR LIGHT REMAIN ON. PERFORMED TROUBLESHOOTING FOUND ESCAPE SLIDE BOTTLE PRESSURE SWITCH SHORTED, BOTTLE PRESSURE REMAIN 2200PSI IN GREEN BAND. R & R R1 DOOR SLIDE ASSY AS PER MM 25-61-15-4, AND PRESSURE SWITCH OPS CHECKED GOOD AS PER MM 25-61-15-5. A/C OK FOR SERVICE.

Part: PANEL — MISSING (NR 1 NACELLE) · airframe 64,060 hrs · 12,742 cycles

DURING EXTERIOR PREFLIGHT INPECTION WALKAROUND, FOUND A PANEL MISSING ON THE NR 1 ENGINE UPPER PYLON, LT SIDE. REPLACED MISSING ANCHOR NUT AND INSTALLED NR 1 ENGINE PYLON PANEL 438EL. CHECKED GOOD IAW AMM 54-51-01-6-0.

Part: SKIN — MISREPAIRED (ZONE 400) · airframe 62,177 hrs · 12,285 cycles

NR 2 ENGINE PYLON FOUND AN EXISTING REPAIR ON RT SIDE OF PYLON SKIN, Y= 2075. FOUND NOT CARRIED OUT IN ACCORDANCE WITH APPROVED DATA. REPAIR REMOVED AND NEW REPAIR INSTALLED AS PER E.A. 1-5410-143549. E.O. 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SKIN — MISREPAIRED (ZONE 400) · airframe 62,177 hrs · 12,285 cycles

NR 2 ENGINE PYLON FOUND AN REPAIR ON RT SIDE OF PYLON SKIN, Y= 2300. FOUND NOT CARRIED OUT IN ACCORDANCE WITH APPROVED DATA. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED AS PER FEDEX E.A. 1-5410-143549. E.O. 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 62,177 hrs · 12,285 cycles

REPAIR FOUND ON CTR CARGO DOOR SKIN FWD LOWER CORNER. REPAIR NOT CARRIED OUT IN ACCORDANCE WITH APPROVED DATA. CENTER CARGO DOOR CARRIED OUT REPAIR AS PER SRM 52-30-16 FIGURE 201 REPAIR 3 REVISION 46. E.O. 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112. FOR INSPECTION REFER E.A. 1-5230-143555.

Part: SKIN — CRACKED (ZONE 500) · airframe 62,177 hrs · 12,285 cycles

LT WING - 24 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 TO STA XORS 713.6. REPAIR CARRIED OUT AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS 683.4 TO STATION XORS 713.6 AS PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 112.

Part: WEB — MISREPAIRED (ZONE 100) · airframe 62,177 hrs · 12,285 cycles

REPAIR FOUND ON FRAME STATION 1841 WEB BL-0 TO LBL-20 IN CENTER CARGO COMPARTMENT BILGE AREA. REPAIR EVALUATED AND FOUND NOT IN ACCORDANCE WITH APPROVED DATA. REPAIR AND WEB REMOVED AS PER SRM 51-31-01 REVISION 46. NEW WEB FABRICATED AS PER DRAWING AGA7170 REVISION T AND NEW WEB INSTALLED AS PER SRM 51-31-01 REVISION 46. E.O. 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SKIN — CRACKED (ZONE 600) · airframe 62,177 hrs · 12,285 cycles

RT WING - 22 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 TO STA XORS 713.6. REPAIR CARRIED OUT AT R/H WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS 683.4 TO STATION XORS 713.6 AS PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 112.

Part: FRAME — MISREPAIRED (BS 535 S22-25L) · airframe 62,177 hrs · 12,285 cycles

FRAME REPAIR AT STA 535, LONGERON 22 LT TO LONGERON 25 LT. EVALUATED AND FOUND NOT REPAIRED IAW APPROVED DATA. CARRIED OUT REPAIR IAW DWG SG10530002, REV 0. EO 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: FRAME — MISREPAIRED (BS 535 L18-21L) · airframe 62,177 hrs · 12,285 cycles

FRAME REPAIR AT STA 535 LT, L-18, -L21. EVALUATED AND FOUND NOT REPAIRED IAW APPROVED DATA. CARRIED OUT REPAIR IAW DWG SG10530002, REV 0. EO 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (ZONE 600) · airframe 62,177 hrs · 12,285 cycles

RT WING INBD OF RIB NR 16 WING L/E LOWER SKIN AT STA XORS 885 FOUND CRACKED. TRIMMED OUT AND INSTALLED WITH FABRICATED REPAIR FILLER AND DOUBLER IAW SRM 57-40-02, FIG 201 REVISION 46. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.

Part: RIB — CRACKED (ZONE 600) · airframe 62,177 hrs · 12,285 cycles

RT WING FWD OF RIB NR 16 WING L/E LOWER CHORD AT STATION XORS 900 FOUND CRACKED. COMPLIED WITH EA 1-5730-143986. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 62,177 hrs · 12,285 cycles

REPAIR DOUBLER AT LT WING INBD SIDE OF NR 19 SLAT TRACK SLAT LOWER SURFACE. FOUND NOT CARRIED OUT IAW APPROVED DATA. REMOVED AND NEW REPAIR INSTALLED IAW SRM 57-40-01, FIG 201. REPAIR 3, REV 46. EO 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 112.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 62,177 hrs · 12,285 cycles

REPAIR AT FUSELAGE STA 735 TO STA 765 BETWEEN LONGERONS 39L TO 41L. REPAIR FOUND NOT CARRIED OUT IAW APPROVED DATA. CARRIED OUT REPAIR IAW SRM 53-00-01, FIG 201, REV 46. EO 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: LONGERON — MISREPAIRED (ZONE 100) · airframe 62,177 hrs · 12,285 cycles

REPAIR FOUND ON LT SIDEWALL LONGERON 40L AT FWD CARGO COMPARTMENT. REPAIR FOUND NOT IAW APPROVED DATA. FWD CARGO COMPARTMENT 40L LT SIDEWALL CARRIED OUT SPLICE REPAIR IAW SRM 53-00-05, FIG 202 FIG 1 REV 46. EO 1-5100-7-5001, A5, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 62,177 hrs · 12,285 cycles

REPAIR DOUBLER AT LT WING INBD SIDE OF NR 4 SLAT TRACK SLAT INNER SURFACE FOUND NOT CARRIED OUT IAW APPROVED DATA. REMOVED AND NEW REPAIR INSTALLED IAW SRM 57-40-01, FIG 201, REPAIR 3, REV 46. EO 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 62,177 hrs · 12,285 cycles

REPAIR AT CENTER CARGO DOOR CUT-OUT FORWARD JAMB SKIN L-40R TO L- 41R. EVALUATED AND FOUND PREVIOUSLY NOT CARRIED OUT AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 46. REPAIR CARRIED OUT REPAIR AS PER SRM SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 46. EO 1-5100-7-5001 A5 PART 1.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 61,173 hrs · 12,035 cycles

DURING MAINT"A"CHECK, EMERGENCY LIGHT TEST FAILED WITH "EMER LT BAT LO" ALERT ON DISPLAY. MX R & R EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51-01-4 TEST PASSED AMM 33-51-01-5.

Part: DOOR — MISSING (FUSELAGE) · airframe 57,933 hrs · 11,277 cycles

DURING WALK AROUND FOUND NR 2 ENGINE PATIO ACCESS DOOR ON BOTTOM OF FUSELAGE IS MISSING. NOTED DAMAGE TO SKIN AREA AFT OF DOOR CUT AND ALSO HINGE ATTACH POINT IS DAMAGE. INSTALLED NEW TAILCONE IAW AMM 53-52-01-4.

Part: SKIN — CRACKED (LT WING) · airframe 56,738 hrs · 11,004 cycles

LT WING NR 14 SLAT TRACK CUT-OUT OTBD EDGE SURFACE FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG21 VOL1 REV40.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 56,738 hrs · 11,004 cycles

RT WING OTBD FLAP INBD FWD HINGE CLEVIS FITTING BORE CORRODED. REPAIRED IAW EA 1-5740-130969.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 56,738 hrs · 11,004 cycles

CABIN - LEFT STA 1521-1541 LONGERON -6 SPLICE FITTING FOUND CRACKED. SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL2 REV40. (MAJOR CAT A REPAIR)

Part: MOUNT — CORRODED (ZONE 500) · airframe 56,738 hrs · 11,004 cycles

LT WING OTBD FLAP OTBD FWD HINGE LWR MOUNT OTBD BORE CORROSION. REPAIRED IAW EA 1-5740-130970.

Part: RIB — CRACKED (ZONE 600) · airframe 56,738 hrs · 11,004 cycles

RT WING L/E RIB NR 16 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL2 REV 40.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 56,738 hrs · 11,004 cycles

LT WING OTBD FLAP OTBD FWD HINGE PIVOT BORE CORROSION. REPAIRED IAW EA 1-5740-130970.

Part: SKIN — CHAFED (BS 1701 L12L) · airframe 56,738 hrs · 11,004 cycles

CABIN - LT STA 1701 LONGERON -12 REPAIR DOUBLER FOUND CHAFED AT FRAME. CHAFED REPAIR REMOVED IAW SRM 51-31-00 VOL II REV40 AND REPAIRED IAW SRM 53- 30-00 FIG1 VOLI REV 40. REPETITIVE INSP REQUIRED, INITIAL INSP AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-30-00, FIG 1 VOL 1, REV40. (MAJOR CAT B REPAIR)

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 56,738 hrs · 11,004 cycles

RT WING OTBD FLAP OTBD FWD HINGE FWD MOUNT INBD BORE CORROSION. REPAIRED IAW EA 1-5740-130971.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 56,738 hrs · 11,004 cycles

LT WING OTBD FLAP INBD FWD HINGE ACTUATOR OTBD BORE CORRODED. REPAIRED IAW EA 1-5740-130970.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 56,738 hrs · 11,004 cycles

RT WING OTBD FLAP OTBD FWD HINGE ACTUATOR OTBD BORE CORROSION. REPAIRED IAW EA 1-5740-130971.

Part: MOUNT — CORRODED (LT WING TE FLAP) · airframe 56,738 hrs · 11,004 cycles

LT WING OTBD FLAP OTBD FWD HINGE LWR MOUNT INBD BORE CORROSION. REPAIRED IAW EA1-5740-130970.

Part: DISPLAY — FAILED (COCKPIT) · airframe 52,913 hrs · 10,157 cycles

ENGINE FAIL LIGHT CAME ON AT APPROX 85KT. REJECT TAKEOFF. NO OTHER INDICATIONS. LIGHT WENT OUT WHEN POWERED BACK. ON TAXI OUT DID NOTICE X ON NR 2 ENG OIL TEMP FOR A FEW SECONDS. WENT OUT-BACK TO NORMAL. FLIGHT CREW ALSO REPORTED THAT THERE WAS NOT ANY SIGNIFICANT SPLIT IN ANY OF THE ENGINE INDICATION, AND CHECKING THE DEU'S FCC'S ECU'S ON ALL THREE ENGINES SHOWED NO FAULTS. REMOVED AND REPLACED NR 1 AND NR 2 DEU. NR 1 FAILED TO BOOTUP, CAPT'S DISPLAYS ARE X'D OUT. INSTALLED ORIGINAL NR 1 DEU. SWAPPED NR 1 AND NR 3 DEU. PERFORMED RTS ON ALL THREE DEUS. PERFORMED PWR ASSUR RUNS, NO DEFECTS NOTED, ALL OIL PRESS INDICATIONS NORMAL W/NO ENG FAIL LIGHTS. OK FOR SERV.

Part: FRAME — CRACKED (MLG DOOR) · airframe 52,106 hrs · 9,977 cycles

LEFT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA FOUND CRACKED. CRACK AT LEFT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA. REPAIRED AS PER FEDEX EA NR 1-3210-116534, TITLE: LANDING GEAR MAIN GEAR DOOR LEFT MAIN LANDING GEAR DOOR FRAME, REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CRACKED (MLG DOOR) · airframe 52,106 hrs · 9,977 cycles

RIGHT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA, FOUND CRACKED. CRACK AT RIGHT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA REPAIRED AS PER FEDEX EA NR 1-3210-116535, TITLE: LANDING GEAR, MAIN GEAR DOOR, RIGHT MAIN LANDING GEAR DOOR FRAME REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (T/E FLAP) · airframe 52,106 hrs · 9,977 cycles

RIGHT WING, INBOARD FLAP LOWER SURFACE FOUND DENT AT XIFH 147. DENT AREA MEASURED AND DEPTH 0.038" FOUND ACCEPTABLE PER SRM 57-10-00- FIGURE 17 VOLUME I. HFEC INSPECTION CARRIED OUT AS PER DAC NDT SPM REVISION 13 PART 6 06-10-01.001 ON DENT AREA FOUND NO CRACK EVIDENT. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — DENTED (T/E FLAP) · airframe 52,106 hrs · 9,977 cycles

RIGHT WING, INBOARD FLAP UPPER SURFACE FOUND DENT AT XIFH 184.5. DENT AREA MEASURED DEPTH = 0.050" FOUND WITHIN LIMIT PER SRM 51-80-01 VOLUME II. HFEC INSPECTION CARRIED OUT AS PER DAC NDT SPM REVISION 13 06-10-01.001 AND FOUND NO CRACK EVIDENT AT DENT REWORK AREA. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 600) · airframe 52,106 hrs · 9,977 cycles

RIGHT WING - INBOARD FLAP UPPER SURFACE FOUND DENT AT XIFH 193. REPAIR CARRIED OUT AT RIGHT HAND WING INBOARD FLAP UPPER SURFACE AT XIFH 193 AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (RT WING TE FLAP) · airframe 52,106 hrs · 9,977 cycles

RT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT OUTBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-116536. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (RT WING TE FLAP) · airframe 52,106 hrs · 9,977 cycles

RIGHT WING, OUTBOARD FLAP OUTBOARD HINGE AFT FAIRING SUPPORT OUTBOARD AFT FASTENER HOLE FOUND CORRODED. CORROSION REPAIRED AS PER FEDEX E.A. 1-5750-117237, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 52,106 hrs · 9,977 cycles

RIGHT WING, LEADING EDGE STRINGER FOUND CRACK AT XOS 1015. REPAIRED AS PER FEDEX E.A. 1- 5720-117239, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 52,106 hrs · 9,977 cycles

NOSE LANDING GEAR LEFT TRUNNION FITTING FORWARD LOWER CORNER FOUND CRACKED. REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERVALS.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 52,106 hrs · 9,977 cycles

RIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT FITTING HOLE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-30-4. OUTBOARD FLAP ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (LT WING TE FLAP) · airframe 52,106 hrs · 9,977 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER AMM 27-50-30-4. OUTBOARD FLAP ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (RT WING TE FLAP) · airframe 52,106 hrs · 9,977 cycles

RT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT OUTBOARD AFT HOLE FOUND CORROSION. REPAIRED AS PER FEDEX E.A. 1-5750-116536. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 700) · airframe 52,106 hrs · 9,977 cycles

01 EACH FASTENER HOLE FOUND CRACK AT 9 O'CLOCK POSITION APPROXIMATELY 0.350" IN LENGTH, AT LEFT SIDE TRUNNION FITTING LOWER LONGERON DURING TRUNNION FITTING CRACK AREA TRIMMED OUT INSPECTION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAL — TORN (E/E DOOR) · airframe 50,582 hrs · 9,652 cycles

PDIS AT FL210 AND CLIMBING HEARD LOUD BANG FOLLOWED BY SOUND OF RUSHING AIR. CABIN ALTITUDE BEGAN CLIMB. STOPPED CLIMB AT 230 AND CABIN CONTINUED TO CLIMB. SUSPECT LOSS OF AVIONICS DOOR SEAL AND RTB. FOUND E/E DOOR SEAL TORN, MPN ABA7800-1. REMOVED AND REPLACED AVIONICS DOOR SEAL ASSY AS PER SMP. PERFORMED ADJ/TEST OF AVIONICS DOOR ASSY AS PER MD-11 AMM 52-41-01-5. OPS TEST FOUND OKAY, ALSO PERFORMED FUSELAGE PRESSURE DECAY ADJ/TEST AS PER MD 11 AMM 21-00-00-5, OPS TEST FOUND "SATIS ".

Part: WIRE — BURNED (BS 1136) · airframe 49,558 hrs · 9,422 cycles

FOUND SEVERAL WIRES AND MOD BLOCKS BURNED AT S3-438 IN CENTER ACCESSORY LT SIDE JUST AFT OF EPC BAY NR 1 AT STA 1136 JUST BELOW FLOOR PANEL. INSPECTED AND REPAIRED DAMAGED WIRES AND MOD BLOCKS PER EA 1-2821-109931 "FUEL SYSTEM REPAIR/INSPECT DAMAGED WIRES". PERFORMED OPS CHECKS ON AFFECTED CIRCUITS PER W/D 23-41-03, 26- 23-01, 28-22-05, 32-44-01, 32-48-02, AND 36-15-01. ALL CHECKS NORMAL.

Part: SKIN — DENTED (ZONE 300) · airframe 47,275 hrs · 8,897 cycles

LT HORIZONTAL STAB LEADING EDGE SKIN DENTED, MEASURES 2" BY 1" BY 0.210" DEEP. NO SRM REPAIR ON DENT POSITION AREA. DENT MARK ON LT HORIZONTAL STAB LEADING EDGE SKIN TRIMMED OUT AND REPAIR CARRIED OUT PER FEDEX EA NR 1-5510-103523, STABILIZERS, HORIZONTAL STABILIZER, REPAIR LEADING EDGE DENT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 47,275 hrs · 8,897 cycles

AFT CARGO - STA 1896 1964 TO STA 1896 BL = 0 AT WASTE TANK COMPARTMENT CUTOUT FOUND WITH CORRODED FRAME. AGA7137-17. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME I. FRAME AT STA 1975, LONGERON 39L TO 40L TRIMMED OUT FOR ACCESS AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I, FIGURE 9. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — UNKNOWN (LT WING) · airframe 47,275 hrs · 8,897 cycles

LEFT HAND WING - STRINGER 11 SPLICE FOUND WITH EXISTING REPAIR. SPLICE REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR — CRACKED (LT MLG) · airframe 47,275 hrs · 8,897 cycles

LEFT HAND MAIN LANDING GEAR. FLIPPER DOOR FOUND CRACKED ARC2827-1. CRACK STOP DRILLED AND REPAIR DOUBLER INSTALLED PER SRM 52-10-00 VOLUME I, FIGURE 18. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — UNKNOWN (RT WING) · airframe 47,275 hrs · 8,897 cycles

RIGHT HAND WING - STRINGER 11 SPLICE FOUND WITH EXISTING REPAIR. STRINGER 11 SPLICE REMOVED AND REPLACED PER SRM 51-33-01 VOULUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

MAIN DECK CARGO COMPT - SEAT TRACK AT STA 1701 X = 27.5 FOUND DAMAGED AFA7795-509. REPAIR CARRIED OUT PER SRM 53-70-00, VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

FOUND MAIN DECK CARGO COMPT, SEAT TRACK AT STA 755 X = 8.5 DAMAGED. REMOVED AND REPLACED FROM EXISTING SPLICE AT STA 746 TO STA 801, X = 8.5 PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-3-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

MAIN DECK CARGO COMPT - SEAT TRACK AT STA 1066 X = 47 FOUND DAMAGED. SEAT TRACK AT STA 1651 TO STA 1691 X = 47 TRIMMED OUT AND REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,275 hrs · 8,897 cycles

RIGHT HAND WING LEADING EDGE FIXED PANEL BEADED DOUBLER AT STA XOS 780 FOUND CRACKED ARB2894-2. REPAIRED AS PER SRM 57-10- VOLUME I, FIGURE 25. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

MAIN DECK CARGO COMPT - SEAT TRACK AT STA 1661 X = 27.5 FOUND DAMAGED AFA7795-509. DAMAGED SEAT TRACK AT STA 1631 TO STA 1711, X = 27.5 TRIMMED OUT AND REPAIR CARRIED OUT PER SRM 53-70-00, VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

MAIN DECK CARGO COMPT - SEAT TRACK AT STA 1089 X = -47 FOUND DAMAGED. REMOVED AND REPLACED FROM STA 1069 TO EXISTING SPLICE AT STA 1129, X = -47 PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

CENTER CARGO: STA 5-113 TO STA 1541, LONGERON 49R FOUND WITH CRACKED SPLICE FITTING A5A7114-511. CRACKED LONGERON 49R SPLICE FITTING REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

MAIN DECK CARGO COMPT - SEAT TRACK AT STA 1661 X = 8.5 FOUND DAMAGED AFA7795-507. DAMAGED SEAT TRACK AT STA 1651 TO STA 1691, X = 8.5 TRIMMED OUT AND REPAIR CARRIED OUT PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MJOR PER GMMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 200) · airframe 47,275 hrs · 8,897 cycles

CENTER CARGO: STA 5-113 TO STA 1541, LONGERON 51R FOUND WITH CRACKED SPLICE FITTING A5A7114-523. CRACKED LONGERON 51R SPLICE FITTING REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,275 hrs · 8,897 cycles

LEFT HAND WING LEADING EDGE CAVITY AT ABOUT STA XOS 628 BEADED DOUBLER FOUND CRACKED ARB2983-1. REPAIRED PER FEDEX E.A. 1-5730-103529, WINGS LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.

Part: SKIN — DENTED (HORIZ STAB) · airframe 47,275 hrs · 8,897 cycles

LEFT HAND HORIZONTAL STABILIZER LEADING EDGE SKIN DENT MEASURES APPROXIMATELY 2 X 1 X 0.210 DEEP. NO SRM REPAIR ON DENT AREA ALC8400-5. REPAIR CARRIED OUT PER FEDEX E.A. 1-5510-103523, STABILIZERS - HORIZONTAL STABILIZER - REPAIR LEADING EDGE DENT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,275 hrs · 8,897 cycles

RIGHT HAND WING LEADING EDGE FIXED PANEL BEADED DOUBLER AT STA XOS 666 FOUND CRACKED ARB2984-502. REPAIRED AS PER EA 1-5730-103526, WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

AFT CARGO - RIGHT HAND STA 1871 - STA 1887 LONGERON SPLICE 40R FOUND CRACKED AGA7048. CRACKED LONGERON 40R SPLICE TRIMMED OUT FROM STA 1862 TO STA 1895 AND REPAIR CARRIED OUT PER SRM 53-10- 00 VOLUME I, FIGURE 2. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,275 hrs · 8,897 cycles

LEFT HAND WING LEADING EDGE CAVITY AT ABOUT STA XOS 647 BEADED DOUBLER FOUND CRACKED ARB2983-1. REPAIRED PER FEDEX E.A. 1-5730-103529, WINGS LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,275 hrs · 8,897 cycles

LEFT HAND WING LEADING EDGE CAVITY AT ABOUT STA XOS 643 BEADED DOUBLER FOUND CRACKED ARB2984-501. REPAIRED PER FEDEX E.A. 1-5730-103528.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,275 hrs · 8,897 cycles

RIGHT HAND WING LEADING EDGE FIXED PANEL BEADED DOUBLER AT STA XOS 643 FOUND CRACKED ARB2983-2. CRACKED BEADED DOUBLER AT STA XOS 643 REPAIRED PER FEDEX E.A. 1-5730-103527, WINGS LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100

Part: DOUBLER — CRACKED (RT WING) · airframe 47,275 hrs · 8,897 cycles

RIGHT HAND WING LEADING EDGE FIXED PANEL BEADED DOUBLER AT STA XOS 692 FOUND CRACKED. REPAIRED AS PER E.A. 1-5730-103526, WINGS - LEADING EDGE BEADED DOUBLER - PERMANENT REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: REPAIR — DETECTED (LT WING) · airframe 47,275 hrs · 8,897 cycles

LEFT HAND WING - EXISTING REPAIR FOUND AT XORS 704, STRINGER 11. REMOVED PER SRM 51-33-01 VOLUME II. NEW REPAIR CARRIED OUT PER SRM 57-20-00 VOLUME 1, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

CENTER CARGO: STA 5-113 TO STA 1541, LONGERON 52 FOUND WITH CRACKED SPLICE FITTING A5A7114-515. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

CENTER CARGO: COMPT TUNNEL RT SIDE AT APPROXIMATELY STA 5-113 TO STA 1541, LONGERON 39R FOUND WITH CRACKED SPLICE FITTING A5A7114-521. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

CENTER CARGO: COMPT TUNNEL LT SIDE AT APPROXIMATELY STA 5-113 TO STA 1541, LONGERON 35L FOUND WITH CRACKED SPLICE FITTING A5A7114-525. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

MAIN DECK CARGO - MAIN FRAME AT STA 1721 LONGERON 12L FOUND WITH DENT AFA0019-3. CARRIED OUT REPAIR PER SRM 53-70-00 FIGURE 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

CENTER CARGO: COMPT TUNNEL RT SIDE AT APPROXIMATELY STA 5-113 TO STA 1541, LONGERON 37R FOUND WITH CRACKED SPLICE FITTING A5A7114-519. CRACKED LONGERON 37R SPLICE REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

CENTER CARGO: STA 5-113 TO STA 1541, LONGERON 50L FOUND WITH CRACKED SPLICE FITTING A5A7114-515. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

CENTER CARGO: STA 5-113 TO STA 1541, LONGERON 51R FOUND WITH CRACKED SPLICE FITTING. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (RT WING) · airframe 47,275 hrs · 8,897 cycles

RIGHT HAND WING REAR SPAR UPPER SURFACE TRAILING EDGE FIXED PANEL SUPPORT STRUCTURE STA XORS 1042 FOUND WITH CORROSION. FOUND EXCEEDED LIMITS PER SRM 57-20-00 VOLUME I FIGURE 16. COMPLIED WITH FEDEX EA 1-5720-95656 PART 1, WINGS - OUTER WING / REAR SPAR TRAILING EDGE - RT REAR SPAR UPPER CAP REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: REPAIR — DETECTED (RT WING) · airframe 47,275 hrs · 8,897 cycles

RIGHT HAND WING - EXISTING REPAIR FOUND AT XORS 704, STRINGER 11 ARB7511-2. REMOVED PER SRM 51-33-01 VOLUME II AND NEW REPAIR CARRIED OUT PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 47,275 hrs · 8,897 cycles

CENTER CARGO: STA 5-113 TO STA 1541, LONGERON 38R FOUND WITH CRACKED SPLICE FITTING A5A7114-517. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 47,275 hrs · 8,897 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT HAND WING TANK AT THE END OF STRINGER 44 AT WING STA XORS 523. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 47,275 hrs · 8,897 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 12 (UPPER STRINGER) AT APPROX WING STA XORS 642. CARRIED OUT REPAIR PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 47,275 hrs · 8,897 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 13 (UPPER STRINGER) AT APPROX WING STA XORS 577. TRIMMED OUT AND REPAIR CARRIED OUT PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (LT WING) · airframe 47,275 hrs · 8,897 cycles

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

Part: STRUCTURE — CRACKED (LT WING) · airframe 47,275 hrs · 8,897 cycles

CRACK FOUND DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF STRINGER 12 (UPPER STRINGER) AT APPROX WING STA XORS 642. CARRIED OUT REPAIR PER SRM 57-20-00 VOLUME I, FIGURE 12. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 47,275 hrs · 8,897 cycles

RIGHT HAND WING, LEADING EDGE UPPER SURFACE TELESCOPIC DUCT CUTOUT FOUND CRACKED. COMPLIED WITH FEDEX E.A 1-5730-103251, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 47,275 hrs · 8,897 cycles

LEFT HAND WING, ANTI-ICE DUCT LEADING EDGE CUTOUT INBOARD CORNER FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-103522. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — GOUGED (LT WING) · airframe 47,275 hrs · 8,897 cycles

LT WING FIXED LEADING EDGE UPPER SURFACE AT STA XORS 164 FOUND WITH DEEP GOUGE. REPAIRED PER SRM 57-10-00 VOLUME, FIGURE 24. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: CHARGER — MALFUNCTIONED (E/E BAY) · airframe 45,965 hrs · 8,592 cycles

LVL 1 ALERT "BATTERY CHARGING" LIGHT ILLUMINATED 20 MIN AFTER T/O REMAINED ON ABOUT 1 MIN. RETURN TO MEM. LIGHT DID NOT RE-ILLUMINATE. REMOVED AND REPLACED BATTERY CHARGER PER MM 24-34-03-4. DRAINED BATTERIES TO 22V, BATTERIES CHARGED IN APPROX 4 MIN, AND BATTERY CHARGING ALERT NEVER RETURNED. A/C OK FOR SERVICE. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 100-0212-01, POS ONL SRL 1204 TAG 78A130 ON MFG 100-0212-01 SRL 1144 TAG 45A975.

Part: FUSE — UNKNOWN (MLG) · airframe 45,530 hrs · 8,483 cycles

AFTER T/O GEAR HANDLE WOULD NOT MOVE, FOLLOWED RED TABS, DUMPED 4500 LBS. RETURNED TO SFS. LANDED UNEVENTUALLY. REMOVED AND REPLACED TRUCK BEAM TRIM CYLINDER FUSE. BLEED SYSTEM ADJ/TEST SATISFIED. PERFORMED A/C JACKING & PERFORMED LANDING GEAR RETRACTION/EXTENSION OK. RII COMPIED WITH.

Part: PSEU — MALFUNCTIONED (COCKPIT) · airframe 44,315 hrs · 8,243 cycles

ALL FOUR LANDING GEAR INDICATED UNSAFE UP UPON GEAR RETRACTION AFTER TAKE OFF BOTH PRIMARY AND SECONDARY INDICATORS. COMPLIED WITH JRH AND CYCLED LANDING GEAR. BOTH PRIMARY AND SECONDARY INDICATORS SHOWED AND LOCKED. CONTINUED TO DESTINATION. R & R PSEU PER MM 31-71-01-2.OPS CHECK NORMAL. AS PER MOCC AND FIM, PSEU INOP. TESTED PSEU, TEST PASSED. PSEU LOGGED MANY FAULTS FROM THE PREVIOUS LEG (FAULTS LOGGED 21, 20, 19, 13, 11, 12) PSEU NOT IN STOCK AT HNL, PARTS ON ORDER FROM LAX.

Part: CLAMP — BROKEN (HEAT EXCHANGER) · airframe 43,664 hrs · 8,104 cycles

APPROX 10 MINUTES AFTER T/O, EXPERIENCED MANIF FAIL LIGHT NR 2 ON AIR PNEU WITH ASSOCIATED AUTOMATIC SHUTDOWN OF PACK 2 AND ISOLATION OF MANIFOLD. NEVER GOT ANY LEVEL 1 OR 2 ALERT OR WARNING. RETURNED TO KIX. INSPECTED PACK, COMPARTMENT AREA AND FOUND ONE HOSE FOR HEAT EXCHANGER BROKEN. ALSO, CLAMP BROKEN. REPLACED HOSE AND CLAMP PER SMP. RAN PACK, ABOUT ONE HOUR, FOUND NORMAL AND DECAY CHECKED WITH APU AIR GOOD. RETURNED TO SERVICE.

Part: DOOR — DAMAGED (ZONE 100) · airframe 42,587 hrs · 7,873 cycles

FUSELAGE CAC DOOR UNABLE TO OPEN AFTER CABIN PRESSURIZATION TEST. CAC DOOR REPLACED AS PER AMM 52-43-01-4. ADJUSTMENT, TEST ON CAC DOOR CARRIED OUT AS PER AMM 52-43-01-5.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,587 hrs · 7,873 cycles

MAIN DECK CARGO - SEAT TRACK CORRODED AT STA 1351 RT 76 INCHES. SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOL 1 FIG 1, AT STA 1269 TO 1391.

Part: MOUNT — CORRODED (ZONE 400) · airframe 42,587 hrs · 7,873 cycles

NR 3 PYLON FWD ENGINE MOUNT LT AFT HOLE CORRODED. REPAIRED AS PER FEDEX EA 1-5450-81617.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,587 hrs · 7,873 cycles

MAIN DECK CARGO, SEAT TRACK CORRODED AT STA 461-470 LBL 90. REPLACED IAW SRM 51-33-01 VOL 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,587 hrs · 7,873 cycles

RT FUSELAGE EXTERIOR SKIN BETWEEN STA 1139-1119 LT 25 CRACKED. CRACKED AREA BLENDED AS PER SRM 51-21-01 VOL2 WITH NO FURTHER CRACK AND FOUND WITHIN LIMIT AS PER SRM 53-20-00 FIG 6 VOL 1.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,587 hrs · 7,873 cycles

MAIN DECK CARGO, SEAT TRACK FOUND CRACKED AT STA 820 TO 829, RBL 27. REPAIRED AS PER SRM 53-70-00 FIG 1, VOL 1.

Part: FRAME — DENTED (ZONE 200) · airframe 42,587 hrs · 7,873 cycles

MAIN DECK CARGO, FUSELAGE FRAME FOUND WITH DENT AT STA Y= 1681, LONGERON 12R. REPAIR CARRIED OUT IAW SRM 53-30-00 FIG. 1 VOL. I. COMPLIED WITH FEDEX EA 1-5330-81619.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,587 hrs · 7,873 cycles

MAIN DECK CARGO, SEAT TRACK FOUND WORN AT STA Y= 893 TO Y= 900, X=47. REPAIRED AS PER SRM 53-70-00 FIG1 VOL1.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,587 hrs · 7,873 cycles

MAIN DECK CARGO, SEAT TRACK FOUND CRACKED AT STA 890 TO 900, LBL 27. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG1 VOL1.

Part: STRAP — CORRODED (ZONE 500) · airframe 37,744 hrs · 6,773 cycles

LT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD STRAP NEAR PIVOT BORE FOUND CORROSION. LEFT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD STRAP REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. STRAP WAS FABRICATED AS PER DRAWING ARC2517.

Part: FITTING — CORRODED (ZONE 600) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD LUG OUTBOARD SURFACE FOUND CORRODED. CORROSION AT RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT POINT OUTBOARD LUG SURFACE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73338. WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - INBOARD FLAP OUTBOARD HINGE STRAP FABRICATION DIFFERENCES.

Part: FITTING — CORRODED (ZONE 500) · airframe 37,744 hrs · 6,773 cycles

LT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBD STRAP NEAR PIVOT BORE FOUND CORROSION. CORROSION AT LT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD STRAP NEAR PIVOT BORE (FLAP SIDE) REPAIR CARRIED OUT AS PER EA 1-5750-73338, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - INBOARD FLAP OUTBOARD HINGE STRAP FABRICATION DIFFERENCES.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR LUG INBOARD HOLE HFEC INSPECTION FOUND CORROSION.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP FWD INBOARD HINGE INBOARD ACTUATOR LUG BORE FOUND CORROSION.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD PIVOT LUG BORE FOUND CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP INBOARD AFT HINGE INBOARD ACTUATOR LUG BORE FOUND CORROSION.

Part: FITTING — CRACKED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING INBOARD FLAP TRACK SIDE LOAD FITTING FOUND CRACKED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP INBOARD AFT HINGE PIVOT LUG BORE INBOARD SURFACE FOUND CORROSION.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG BORE FOUND CORROSION.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP INBOARD AFT HINGE INBOARD PIVOT LUG BORE OUTBOARD SURFACE FOUND CORROSION.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD ACTUATOR LUG BORE FOUND CORROSION.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP FWD INBOARD HINGE OUTBOARD ACTUATOR ATTACH LUG BORE FOUND CORROSION.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE FITTING (WING SIDE), ACTUATOR ATTACHMENT LUG OUTBOARD BORE FOUND CORRODED.

Part: STOP FITTING — CRACKED (LT WING) · airframe 37,744 hrs · 6,773 cycles

LEFT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED.

Part: FITTING — CRACKED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING - INBOARD FLAP SIDELOAD FITTING FOUND CRACKED. INBOARD FLAP SIDELOAD FITTING REMOVED AND REPLACED AS PER MM 20-50-02 AND OPERATION CHECK REFER WORK CARD NO : E 1-5750-7-5003A,PT 2, INSPECT AND REFURBISH INBOARD TRAILING EDGE FLAP & VANE ASSEMBLY.

Part: STOP FITTING — CRACKED (RT WING) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT OUTBOARD. FLAP SECONDARY UP STOP REPAIR.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE FITTING (WING SIDE), ACTUATOR ATTACHMENT LUG INBOARD BORE FOUND CORRODED.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 37,744 hrs · 6,773 cycles

FWD CARGO COMPARTMENT - TRANSVERSE LONGITUDINAL SPLICE 46L AT STA 1119 HAS 1 EACH CRACK APPROXIMATELY 1 INCH IN LENGTH. CRACKED SPLICE AT FORWARD CARGO COMPARTMENT STA 1119, LONGERON 46L REMOVED AS PER SRM 51-33-01, VOL II AND REPLACED WITH NEW FABRICATED SPLICE AS PER DRAWING ADA 8424 AND SRM 51-33-01 VOL II.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LT WING INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT BORE FOUND CORROSION. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER EA 1-5750-73337,

Part: HINGE — CORRODED (RT WING) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACH LUG, INBOARD HOLE FOUND CORRODED.

Part: HINGE — CORRODED (RT WING) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACH LUG, OUTBOARD HOLE FOUND CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FWD HINGE INBOARD ACTUATOR LUG BORE FOUND CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), HINGE LUG INBOARD HOLE FOUND CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORE FOUND CORROSION. REMOVED AND REPAIR CARRIED OUT AS PER EA 1-5750-73337.

Part: RIB — CRACKED (ZONE 500) · airframe 37,744 hrs · 6,773 cycles

LT WING SLAT TRACK NR 16 INBOARD SUPPORT RIB CRACKED. LT WING SLAT TRACK NR 16 INBOARD SUPPORT CRACKED RIB REMOVED AND REPLACED AS PER SRM 51-31-01, VOL. II.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

RIGHT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), HINGE LUG OUTBOARD HOLE FOUND CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,744 hrs · 6,773 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FWD HINGE OUTBOARD ACTUATOR LUG BORE FOUND CORRODED.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 37,744 hrs · 6,773 cycles

FLOOR TRACK AT STA 635 LT X = 8.5 CRACKED. FLOOR TRACK AT STA 635 LT X = 8.5 CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-70-00, VOL. I, FIGURE 1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 37,744 hrs · 6,773 cycles

FLOOR SUPPORT AT STA 635 LT =47.5 CRACKED.

Part: PUSHROD — DEFECTIVE (AILERON) · airframe 33,317 hrs · 5,741 cycles

LEVEL 2 -AILERON DEFLECT DISAGREE- DURING FLAP RETRACTION AT 3300 FT. PERFORMED QRH PROCEDURES. THE LEFT AILERON REMAINED DEFLECTED AFTER FLAP RETRACTION. A/C ROLLS RIGHT. RELEASED FOR SERVICE PER MEL/CDL. INSTALLED FIXED PUSH-ROD IN LEFT OUTBOARD DEFLECT AILERON.

Part: BRACKET — CRACKED (T/E FLAP) · airframe 33,196 hrs · 5,714 cycles

RIGHT WING INBOARD FLAP, INBOARD FLAP TRACK BRACKET ASSY TRACK & DRIVE SUPPORT FOUND CRACKED. REMOVED AND REPLACED FLAP ASSY PER MM 27-50-20.

Part: HINGE — CORRODED (T/E FLAP) · airframe 33,196 hrs · 5,714 cycles

LEFT WING O/B FLAP O/B HINGE REAR SPAR BEAM LOWER O/B HOLE FOUND CORRODED. REMOVED AND REPLACED HINGE PER CMM 57-44-09 FIG 401.

Part: HINGE — CORRODED (T/E FLAP) · airframe 33,196 hrs · 5,714 cycles

RIGHT WING O/B FLAP I/B HINGE LOWER REAR SPAR BEAM LUG FACES FOUND CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 33,196 hrs · 5,714 cycles

LEFT WING O/B FLAP O/B HINGE REAR SPAR BEAM LOWER I/B HOLE FOUND CORRODED. REMOVED AND REPLACED HINGE PER CMM 57-44-09 FIG 401, 20-11-01.

Part: ATTACH BOLT — CORRODED (T/E FLAP) · airframe 33,196 hrs · 5,714 cycles

LEFT WING I/B FLAP O/B HINGE LOWER ATTACHMENT BOLT O/B SIDE FOUND CORRODED. REMOVED AND REPLACED HINGE BOLT PER AMM 57-51-01.

Part: ATTACH BOLT — CORRODED (T/E FLAP) · airframe 33,196 hrs · 5,714 cycles

LEFT WING INBOARD FLAP O/B HINGE LOWER ATTACHMENT BOLT INBOARD SIDE FOUND CORRODED. REMOVED AND REPLACED BOLT PER MM 57-51-01.

Part: ATTACH BOLT — CORRODED (T/E FLAP) · airframe 33,196 hrs · 5,714 cycles

RIGHT WING INBOARD FLAP OUTBOARD HINGE LWR ATTACHMENT BOLT O/B SIDE FOUND CORROSION. REMOVED AND REPLACED BOLT PER MM 57-51-01, REF EA 1-5710-64290.

Part: SEAT TRACK — DAMAGED (MAIN DECK) · airframe 29,685 hrs · 4,902 cycles

MAIN DECK FLOOR TRACK DAMAGED AT BS Y=800 X= 47. *S/D* REMOVED AND REPLACED SEAT TRACK PER SRM 51-70-00 FIG 1 VOL 1.

Part: ENGINE — VIBRATION (NR 1)

CLIMBING 11,000 FT FELT VIB NOTICED NR 1 ENG N1 DECREASING, NR 1 ENG VIB MONITORS AMBER. NO FIRE WARNING. SECURED ENG IAW CHECK LIST.

Part: DRAIN LINE — LEAKING (NR 2 ENGINE)

DURING CRUISE GOT HYD SYS 2 FAIL LEVEL 2 ALERT. REPLACED ENGINE HYD CASE DRAIN FILTERS, LT AND RT EDPS AND SERVICED HYDRAULICS. NO LEAKS NOTED.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 28,958 hrs · 4,734 cycles

RED NOSE GEAR WARN LIGHT ILLUM. RECYCLED GEAR LIGHT GREEN ON 2ND ATTEMPT. INSP DOWN PROX AND LOCK PROX SENSOR FOUND NORMAL. PROX SWITCH ELECTRONICS UNIT. TEST PASSED NO SIGNS OF LEAKAGE OR DAMAGE ON UNLOCK CYLINDER AND CK VALVE PER FIM 32-30-06-02. AC OK FOR SERVICE.

Part: TARGET — UNSERVICEABLE (NLG)

ON APPROACH NOSE GEAR UNSAFE ON EXT. Removed and replaced TARGET Per MM 32-61-17-4. RESECURED RIVETS PER SMP. CLEAN ALL TARGETS and SENSORS PRECAUTIONARY. AC OK FOR SERVICE.

Part: DUCT — DAMAGED (NR 2 ENGINE)

00-203 AFT T/O NR 2 ENG ANTI ICE DEFERRED OPEN, GOT DUCT ALERT. REDUCED NR 2 THROTTLE TO IDLE, ALERT WENT OUT. SHUT DOWN ENG PER CKLIST. *S/D* REMOVED AND REPLACED DUCT (P/N 14260-531) PER MM 30-22-09. PERFORMED LEAK TEST PER MM 30-22-09-700-801. CHECK NORMAL. AC OK FOR SERVICE.