N619FE

Part: NONE — FAILED (ZONE 200) · airframe 79,279 hrs · 19,383 cycles

DURING PREFLIGHT EMERGENCY LIGHT TEST RECEIVED LEVEL 1 EMER LT BAT 1 LO REMOVED AND REPLACED EMERGENCY LIGHTINGPOWER SUPPLY. OPS CHECK GOOD.

Part: NONE — NONE (N/A) · airframe 78,974 hrs · 19,287 cycles

FOUND DAMAGE AT FUSELAGE AFT OF CENTER CARGO DOOR APROX 7 INCH BY 3 INCH SHGN 26JAN22 03:45 CGN U C/W THE REMOTION OF THE INTERNAL AFT CGO SIDEWALL PLASTIC LINERS INCLUDING THE METALIC HOLDER, FOR EASY ACCESS, AS PER SRM-51-35-01-0G. INSTALLED ALL REPAIR PARTS, CLASS II REPAIR COMPLETED IAW SRM 53-00-01-2R FIG 201.

Part: SKIN — DAMAGED (N/A) · airframe 78,488 hrs · 19,152 cycles

FWD CARGO DOOR LEADING EDGE DAMAGED ABOVE FWD LOWER CORNER REPAIRED DAMAGED LEADING EDGE PER MD-11 SRM 53-00-15-2R REPAIR 8 FIG. 202 AND E.A. 1- 5330-T0365533

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL #262FF AT STATION 1256 - 1305 FOR UNDERFLOOR INSPECTION ACCESS FOUND FLOOR PANEL DELAMINATED. DELAMINATED FLOOR PANEL #262FF REMOVED AT CABIN STATION 1256 - STATION 1305 AS PER PER AMM 53-21-04-4. FLOOR PANEL #262FF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #262FF INSTALLED AS PER AMM 53-21-04-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 76,705 hrs · 18,702 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AND FOUND CRACK INDICATION ON LONGERON 49 RIGHT LOWER CHORD AT NOSE LANDING GEAR RIGHT HAND TRUNNION AT STATION 583. NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING AT STATION 546 Ï¿½ STATION 595 LONGERON 49 RIGHT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FABRICATED LONGERON AS PER DOUGLAS DRAWING ACA 3796 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: TRUNNION — CRACKED (NLG) · airframe 76,705 hrs · 18,702 cycles

FUSELAGE: NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING SUSPECTED CRACK AT STATION 584. NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING STATION 584 AREA REPAIR CARRIED OUT AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 6-2-100. REQUIRES INITIAL INSPECTION AT 1,500 FLIGHT CYCLE AND REPETITIVE INSPECTION AT AT EVERY 1,500 FLIGHT CYCLE BY HIGH FREQUENCY EDDY CURRENT OR LIQUID PENETRANT METHOD PER SRM 53-10-14-2R REPAIR 2 FIGURE 202 TABLE 201.

Part: FRAME — DENTED (ZONE 200) · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - RIGHT HAND SIDEWALL STATION 1701 LONGERON 12 RIGHT FOUND FRAME FRAME DENT. MAIN DECK CARGO - RIGHT HAND SIDEWALL AT STATION 1701 LONGERON 12 RIGHT , DENTED FRAME REPAIRED AS PER SRM 53-00-07-2R REPAIR 2 FIGURE 201. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - SEAT TRACK AT STATION 1721 X = - 75.25 FOUND CORROSION. MAIN DECK CARGO , AT SEAT TRACK STATION 1721 , X = - 75.25 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1751 TO STATION 1711 , X = - 75.25 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - SEAT TRACK AT STATION 1841 TO STATION 1851 X = 27.5 FOUND CORRODED. MAIN DECK CARGO - AT SEAT TRACK STATION 1841 TO STATION 1851 , X = 27.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1751 TO END OF PART STATION 1887 X = 27.5 AS PER SRM 53-00- 52-2R REPAIR 1 FIGURE 201. REFER TO SNRM N01023 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - SEAT TRACK AT STATION 1841 X = - 75.25 CORRODED. MAIN DECK CARGO - AT SEAT TRACK STATION 1841 X = - 75.25 CORROSION EVALUATED , FOUND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED AS PER E.A. # : 1-5310-T0360421 P1. TITLE : FUSELAGE - MAINFRAME - CORROSION FOUND ON CURVE SEAT TRACK BETWEEN STA 1781 AND STA 1887, AT X = - 75.25 - SRM SPLICE REPAIR - ALTERNATE MATERIAL FOR SEAT TRACK REPLACEMENT REPLACEMENT SECTION. REFER TO SNRM N01022 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - SEAT TRACK AT STATION 1781 TO STATION 1801 X = 27.5 FOUND CORRODED. MAIN DECK CARGO - AT SEAT TRACK STATION 1781 TO STATION 1801 , X = 27.5 , CORROSION EVALUATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1751 TO END OF PART STATION 1887 X = 27.5 , AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - SEAT TRACK AT STATION 1868 X = 8.5 CORRODED. MAIN DECK CARGO AT SEAT TRACK STATION 1868 , X = 8.5 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1831 TO END OF PART STATION 1887 , X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - SEAT TRACK AT STATION 1868 , X = 27.5 FOUND CORRODED. MAIN DECK CARGO - AT SEAT TRACK STATION 1868 X = 27.5 , CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1751 TO END OF PART STATION 1887 , X = 27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REFER TO SNRM N01023 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - SEAT TRACK AT STATION 1781 TO STATION 1821 X = - 75.25 CORRODED. MAIN DECK CARGO - AT SEAT TRACK STATION 1781 TO STATION 1821 , X = - 75.25 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED AS PER E.A.#: 1-5310-T0360421 P1. P1.TITLE : FUSELAGE - MAINFRAME - CORROSION FOUND ON CURVE SEAT TRACK BETWEEN STA STA 1781 AND STA 1887 , AT X = - 75.25 - SRM SPLICE REPAIR - ALTERNATE MATERIAL FOR SEAT SEAT TRACK REPLACEMENT SECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 76,705 hrs · 18,702 cycles

DURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA AND FOUND 02 EACH CRACKS WITH LENGTH APPROXIMATELY 0.250" STATION 583 LEFT HAND NOSE LANDING GEAR TRUNNION FITTING STATION 583 REPAIR CARRIED OUT AS PER EA 1-5310-T0312182 A PART 3. TITLE: FUSELAGE - MAIN FRAME - LH NLG TRUNION FITTING CRACK INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 76,705 hrs · 18,702 cycles

03 EACH FASTENER HOLES (# 13, # 14, # 32) FOUND CRACK INDICATION DURING OPEN Ï¿½ HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.65. LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.65 03 EACH CRACK INDICATION FASTENER HOLES (# 13, # 14, # 32) BUSHING REPAIR CARRIED OUT AS PER MD-11SRM57-20-02-2R FIGURE 201 REPAIR 5. INITIAL INSPECTION TO BE CARRY OUT AT 2000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRY OUT AT EVERY 2000 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT INSPECTION AND ULTRASONIC INSPECTION PER MD-11 SRM 57-20-02-2R FIGURE 202 REPAIR 5 TABLE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,705 hrs · 18,702 cycles

MAIN DECK CARGO - SEAT TRACK STATION 1239 , X = - 75.25 FOUND WITH CORROSION. MAIN DECK CARGO - AT SEAT TRACK STATION 1239 , X = - 75.25 CORROSION FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO STATION 1269 X = - 75.25 , AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 76,705 hrs · 18,702 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 695. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT INTERNAL BEADED DOUBLER AT STATION XOS 695. 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: SKIN — CRACKED (LT WING LE) · airframe 76,705 hrs · 18,702 cycles

LEFT HAND WING FIXED LEADING EDGE #12 SLAT TRACK CUTOUT OUTBOARD CORNER FOUND CRACK AT STATION XOS 778. REPAIR CARRED OUT AT LEFT HAND WING FIXED LEADING EDGE #12 SLAT TRACK CUTOUT OUTBOARD CORNER STATION XOS 778 AS PER MD-11 SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LIGHT — NO TEST (L1 RAFT) · airframe 76,207 hrs · 18,572 cycles

PDIS 619 25-60 8081. 17DEC20 AFW OPEN U LOGPAGES:3366007. L1 RAFT LIGHT ON DOOR WILL NOT TEST. CANCEL, N/A SDR ENTERED IN ERROR.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 75,889 hrs · 18,472 cycles

50 MIN INTO FLT, GOT A LEVEL 1 HYD-2L OFF ALERT. COMPLIED W/QRH. HYD-2R IN GREEN, QTY 8.3. A FEW MINUTES LATER LEVEL 1 HYD-2R OFF ALERT. COMPLIED W/QRH. QUANTITY CONTINUED TO DECREASE AND CONFERRED WITH MX AND GOCC. OVER COURSE OF NEXT HOUR QUANTITY DECREASED TO 4.5. MX ADVISED TO RUN QRH FOR HYD-2 QTY LO, COMPLIED W/QRH, QUANTITY DECREASED TO 0.2 GAL W/NR 2 PUMPS OFF AND 2-3 RMP OFF. RESERVOIR TEMP AT 2 DEGREES C. PRIOR TO RUNNING QRH, NR 2 PRESSURE PERIODICALLY WENT FROM 60 PSI TO 700 PSI. REMOVED AND REPLACED NUMBER 2 ENGINE UPPER HYD PUMP ONLY, AS PER MD-11 M/M REF: 29-11-20-4-1. HYDRAULIC SYSTEM NR 2 OPERATIONS CHECK NORMAL.

Part: SEAL — LOOSE (L1 DOOR) · airframe 75,678 hrs · 18,419 cycles

PDIS 619 52-10 7779 08OCT20 MEM FACT U. L1 DOOR WOULD NOT ARM ONCE CLOSED. FACT 08OCT20 21:34 MEM U. RESEATED DOOR SEAL, REF MD11 AMM 25-23-03-4.

Part: PROXIMITY SENSOR — OBSTRUCTED (MLG) · airframe 75,577 hrs · 18,388 cycles

AFTER GEAR RETRACTION WITH GEAR HANDLE UP, NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. FOLLOWED QRH. SECONDARY INDICATION ON CONFIG PAGE INDICATED SAFE, ON GEAR EXTENSION WITH GEAR HANDLE DOWN BOTH PRIMARY AND THE SECONDARY INDICATIONS WERE RED UNSAFE. FOLLOWED QRH, TRIED ALTERNATE GEAR EXTENSION AND WITH CENTER GEAR UP, LANDED WITH CENTER GEAR UP, SECONDARY LIGHT INDICATED GREEN SAFE AFTER LANDING. FOUND OVERHEAD INSULATION BLANKET TORN, FALLEN DOWN AND OBSTRUCTED NOSE LANDING GEAR LOCKED SENSORS. REMOVED TORN BLANKET BETWEEN NOSE LANDING GEAR LOCKED PROXIMITY SENSORS AND TARGETS, PER AMM 32-61-17-4. PRIMARY AND SECONDARY LANDING GEAR INDICATORS SHOWN ALL GREEN. INSPECTED NOSE LANDING GEAR DOWN AND LOCKED SENSORS AND TARGETS, NO DEFECTS NOTED. COMPLIED WITH EA NR 1-2500-T356992 A PT1 AND PERFORMED NOSE LANDING GEAR LOCKED PROXIMITY SENSOR RETURN TO SERVICE TEST, PER AMM 32-61-17-5, NO DEFECTS NOTED.

Part: STRUT — FAILED (NLG) · airframe 73,965 hrs · 18,008 cycles

RIGHT NOSE TIRE SEPERATED FROM AIRCRAFT *************************************************** TFOA CATEGORY: 1 INSTALLED NOSE LANDING GEAR AND DRAG BRACE ASSY REF W/C 32T1001 REMOVED AND REPLACED LEFT WHEEL AND TIRE ASSEMBLY, NOSE LANDING GEAR REF AMM 32-42-01-4. REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEEL TRANSMISSION UNITS REF MD11 AMM 32-46-09-4. OPS CHECK GOOD. REMOVED AND REPLACED RIGHT NOSE WHEEL AIR PRESSURE TRANSDUCER REF MD11 AMM 32-46-03-4. OPS CHECK GOOD. C/W NOSE LANDING GEAR CHANGE PER W/C 32T1001. ALL STEPS COMPLETED

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE(NR 4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA #: 1-5750-T0330688A PART 1 STEP 1F(1) AND STEP 1F(3). TITLE : WINGS-FLIGHT SURFACES- RT WING-INBD FLAP -OUTBD FWD HINGE(WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57505939 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE(NR 4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA #: 1-5750-T0330688A PART 1 STEP 1F(1) AND STEP 1F(3). TITLE : WINGS-FLIGHT SURFACES- RT WING-INBD FLAP -OUTBD FWD HINGE(WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57505939 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE (HOLE NR 4) 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-T0346606 P1 STEP 1F(1) AND STEP 1F(3). TITLE : WINGS- FLIGHT SURFACES- LT WING- INBD FLAP -OUTBD FWD HINGE(WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO EA #: 1- 5750-T0346606 P1 AND SNRM NR N00609 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE (HOLE NR 4)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-T0346606 P1 STEP 1F(1) AND STEP 1F(3). TITLE : WINGS- FLIGHT SURFACES- LT WING- INBD FLAP -OUTBD FWD HINGE(WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO EA #: 1-5750-T0346606 P1 AND SNRM NR N00609 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLES SURFACE CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-09 AND FOUND LOWER BARREL NUT FACE EXCEED LIMIT BASE THE DIFFERENCE BETWEEN DRAWING ARC0503 AND MD-11 CMM 57-44-09. SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. #: 1-5750-T0346580 P1 STEP 1.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002-RH WING-OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD FWD HINGE (WING SIDE) BARREL NUTS HOLE SURFACE CORROSION CORROSION AT LEFT HAND WING - OUTBOARD FLAP INBOARD FORWARD HINGE ( WING SIDE) BARREL NUT HOLE SURFACE REWORKED AND FOUND LOWER BARREL NUT FACE EXCEED LIMIT BASE THE DIFFERENCE BETWEEN DRAWING ARC0502 AND MD-11 CMM 57-44-08. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. #: 1-5750-T0346419 P1 STEP 1.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002-LH WING-OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING LEADING EDGE CAVITY AT XOS 789 DOUBLER CRACKED. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATE DOUBLER AS PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT LEFT HAND WING LEADING EDGE CAVITY AT XOS 789 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING LEADING EDGE CAVITY AT XOS 584 FORMER CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB2931 REVISION H. INSTALLED FABRICATED FORMER AT LEFT HAND WING LEADING EDGE CAVITY AT XOS 584 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 457) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

FORWARD CABIN - UPON REMOVAL OF FLOOR PANEL FOUND SEAT TRACK FLANGE CORROSION AT STATION 457 , X = 0. FORWARD CABIN - AT SEAT TRACK STATION 457 X = 0 , CORROSSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-31-01-0G . SEAT TRACK FABRICATED BY MACHINING AS PER DOUGLAS DRAWING SP11530031 REVISION D . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING "E" ECCENTRIC HOLE BORE CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING "E" ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201(SHEET 1). OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A. #: 1-5750-T0346581A P1 STEP 1B.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP VANE ASSY- MISSING ID PLATE AND TRACK SUPPORT CORROSION REPAIR. AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. #: 1-5750-T0346581A P1 AND SNRM NO. N00644 FOR WORK DETAILS.

Part: FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING "B" ECCENTRIC HOLE BORE CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING "B" ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201(SHEET 1). OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A. #: 1-5750-T0346581A P1 STEP 1A.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP VANE ASSY- MISSING ID PLATE AND TRACK SUPPORT CORROSION REPAIR. AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1801) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

MAIN DECK COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORROSION AT STATION 1801 X = - 27. MAIN DECK COMPARTMENT FLOOR AT SEAT TRACK STATION 1801 X = - 27 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1771 TO STATION 1811 X = - 27 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE(#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44- 07.OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.#: 1-5750-T0330688A PART 1 STEP 1F(1) AND STEP 1F(3). TITLE : WINGS- FLIGHT SURFACES- RH WING-INBD FLAP -OUTBD FWD HINGE(WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57505939 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44- 07.REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A.#: 1-5750-T0346606 P1 STEP 1F(1) AND STEP 1F(3). TITLE : WINGS-FLIGHT SURFACES- LH WING- INBD FLAP -OUTBD FWD HINGE(WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1621) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

MAIN DECK COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORROSION AT STATION 1621 X = - 75. MAIN DECK COMPARTMENT FLOOR AT SEAT TRACK STATION 1621 X = - 75 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1611 TO STATION 1711 X = - 75 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 1681) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STATION 1681 X = - 75. MAIN DECK COMPARTMENT FLOOR SEAT TRACK AT STATION 1681 X = - 75 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1611 TO STATION 1711 X = - 75 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00863 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1661) · airframe 71,810 hrs · 17,373 cycles

MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR DENTED AT RIGHT HAND STATION 1661, LONGERON 12 RIGHT CABIN - MAIN DECK CARGO COMPARTMENT AT RIGHT HAND FRAME STATION 1661 LONGERON 12 RIGHT , EXISTING DENTED REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2 , REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO CARRIED OUT AS PER SRM 53-00-07 TABLE 201 REPAIR 2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: DOUBLER — CRACKED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 862 - 868 FOUND WITH CRACK. REPAIR CARRIED OUT AT LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 862 - 868 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 542 - XOS 547 FOUND WITH CRACK. REAPIR CARRIED OUT AT LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 542 - XOS 547 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 616 - 620 FOUND WITH CRACK. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 616 - 620 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 625 - 629 FOUND WITH CRACK. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 625 - 629 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 637 - 643 FOUND WITH CRACK. REPAIR CARRIED OUT AT LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 637 - 643 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 667 - 672 FOUND WITH CRACK. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 667 - 672 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 625 - 629 AS FOUND WITH CRACK. REPAIR CARRIED OUT AT LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 625 - 629 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 610 - 616 FOUND WITH CRACK. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 610 - 616 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 691 - 697 FOUND WITH CRACK. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 691 - 697 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 729 - 735 FOUND WITH CRACK. REPAIR CARRIED OUT AT LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 729 - 735 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 759 - 764 FOUND WITH CRACK. REPAIR CARRIED OUT AT LEFT HAND WING LEADIND EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 759 - 764 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 652 - 657 FOUND WITH CRACK. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 652 - 657 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING - INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT INBOARD HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND EA #: 1-5750-132236C P5 STEP 2A AND STEP 2B. TITLE: WINGS- FLIGHT SURFACES- LT WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57506228 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 71,810 hrs · 17,373 cycles

MAIN DECK COMPARTMENT AFT FLOOR PANEL SUPPORT FOUND CRACKED AT STATION 1921 X = 25 MAIN DECK COMPARTMENT AT STATION 1921 X = 25 CRACKED AFT FLOOR PANEL SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = 25 AS PER SRM 51-31-01-0G. AFT FLOOR PANEL SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA 7087 REVISION M . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING - OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA #: 1-5750-T0346541 P1 STEP 2A.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING-OUTBD FLAP, INBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING - INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT OUTBOARD HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND EA #: 1-5750-132237D P5 STEP 2A AND STEP 2B. TITLE: WINGS- FLIGHT SURFACES- RT WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.REFER TO WRI : 57506229 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING - INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT OUTBOARD HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND EA #: 1-5750-132236C P5 STEP 2A AND STEP 2B. TITLE: WINGS- FLIGHT SURFACES- LT WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57506228 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING - OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE CORROSION CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA #: 1-5750-T0346541 P1 STEP 2B. TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002-RT WING-OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750-T0346541 P1 AND SNRM NR N00271 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 71,810 hrs · 17,373 cycles

MAIN DECK COMPARTMENT AFT FLOOR PANEL SUPPORT FOUND CRACKED AT STATION 1887 X = 56 MAIN DECK COMPARTMENT CRACKED AFT FLOOR PANEL SUPPORT AT STATION 1887 X = 56 REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = 56 AS PER SRM 51-31-01-0G. AFT FLOOR PANEL SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA 7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CRACKED (RT WING) · airframe 71,810 hrs · 17,373 cycles

RH WING TE REAR SPAR LOWER CAP SILL AT APPROX STA XORS 415 FOUND CRACK CRACKED SILL REMOVED AS PER SRM 51-31-01-0G AND REPLACED SILL AT RIGHT HAND WING TRAILING EDGE REAR SPAR LOWER CAP AT APPROXIMATE XORS 415 AS PER SRM 51-34-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

RIGHT HAND WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUTS HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE BORE (NR 10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA #: 1-5750-T0346580 P1 STEP 2B.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002-RT WING-OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750-T0346580 P1 AND SNRM NR N00202 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 1981) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

MAIN DECK COMPARTMENT AFT FLOOR PANEL SUPPORT FOUND WITH CORROSION AT STATION 1981 X = - 02 . MAIN DECK COMPARTMENT AFT FLOOR PANEL SUPPORT AT STATION 1981 X = - 02 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 . CORRODED FLOOR PANEL SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = - 02 AS PER SRM 51-31-01-0G . FLOOR PANEL SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7080 REVISION S. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: FRAME — CHAFED (BS 535) · airframe 71,810 hrs · 17,373 cycles

MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR AT STATION 535 LONGERON 24 LEFT FOUND OUTER REPAIR ANGLE CHAFFED. CABIN - MAIN DECK CARGO COMPARTMENT FRAME AT STATION 535 LONGERON 24 LEFT CHAFFED MARK AT EXISTING OUTER REPAIR ANGLE REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205, CHAFFED EXISTING OUTER REPAIR ANGLE REMOVED AS PER SRM 51-31-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100,

Part: FLOOR SUPPORT — CORRODED (BS 1961) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

MAIN DECK COMPARTMENT AFT FLOOR PANEL SUPPORT FOUND WITH CORROSION AT STATION 1961 X = - 56 MAIN DECK COMPARTMENT AFT FLOOR PANEL SUPPORT AT STATION 1961 X = - 56 CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 . CORRODED FLOOR PANEL SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = - 56 AS PER SRM 51-31-01-0G. FLOOR PANEL SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7551 REVISION G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — CRACKED (BS 495) · airframe 71,810 hrs · 17,373 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA FOUND CRACKED AT STATION 495 X = - 8.5 CABIN - MAIN DECK CARGO COMPARTMENT CRACKED SEAT TRACK AT STATION 495 X = - 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 494 TO EXISTING SPLICE STATION 525 X = - 8.5 AS PER SRM 53 -00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1991) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

MAIN DECK COMPARTMENT AFT FLOOR PANEL SUPPORT FOUND WITH CORROSION AT STATION 1991 X = - 25 MAIN DECK COMPARTMENT AT AFT FLOOR PANEL SUPPORT STATION 1991 X = -25 CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 CORRODED FLOOR PANEL SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = - 25 AS PER SRM 51-31-01-0G . FLOOR PANEL SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7087 REVISION M . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD FORWARD HINGE ( WING SIDE) PIVOT HOLE BORE CORROSION CORROSION AT LEFT HAND WING - OUTBOARD FLAP INBOARD FORWARD HINGE ( WING SIDE) PIVOT HOLE BORE(#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44- 08 AND E.A. #: 1-5750-T0346419 P1 STEP 1A.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- LH WING-OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD FORWARD HINGE ( WING SIDE) LOWER MOUNT INBOARD HOLE SURFACE CORROSION CORROSION AT LEFT HAND WING - OUTBOARD FLAP INBOARD FORWARD HINGE ( WING SIDE) LOWER MOUNT INBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER E.A. #: 1-5750-T0346419 P1 STEP 1B AND STEP 1.REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. #: 1-5750-T0346419 P1 STEP 1.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002-LH WING-OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. #: 1-5750-T0346419 P1 AND SNRM NO. N00240 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE ( WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE ( WING SIDE) PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44- 09 AND E.A. #: 1-5750-T0346454 P1 STEP 1A.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- LH WING-OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1981) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

MAIN DECK COMPARTMENT AFT FLOOR PANEL SUPPORT FOUND WITH CORROSIONAT AT STATION 1981 X = 02. MAIN DECK COMPARTMENT AFT FLOOR PANEL SUPPORT AT STATION 1981 X = 02 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 . CORRODED FLOOR PANEL SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = 02 AS PER SRM 51-31-01-0G . FLOOR PANEL SUPPORT FABRICATED AS PER DRAWING AGA 7081 REVISION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,810 hrs · 17,373 cycles

LEFT HAND WING - OUTBOARD FLAP INBOARD FORWARD HINGE ( WING SIDE) LOWER MOUNT OUTBOARD HOLE SURFACE CORROSION CORROSION AT LEFT HAND WING - OUTBOARD FLAP INBOARD FORWARD HINGE ( WING SIDE) LOWER MOUNT OUTOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER E.A. #: 1-5750-T0346419 P1 STEP 1B AND STEP 1 AND MD-11 CMM 57-44-08.REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. #: 1-5750-T0346419 P1 STEP 1.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002-LH WING-OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO E.A. #: 1- 5750-T0346419 P1 AND SNRM NO. N00240 FOR WORK DETAILS.

Part: SKIN — CHAFED (LT WING) · airframe 71,810 hrs · 17,373 cycles

LEFT WING DROOP LEADING EDGE UPPER SKIN OUTBOARD EDGE FOUND CHAFING MARK AT STATION XDLE 329.774 REPAIR CARRY OUT AT LEFT HAND WING DROOP LEADING EDGE UPPER SKIN OUTBOARD EDGE AT XDLE 329.774 AS PER SRM 57-40-01-2R FIGURE 202 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CONTAINER — FIRE (CARGO BAY) · airframe 70,454 hrs · 16,992 cycles

MDIS 619 05-50 5502 04OCT18 MEM OPEN U DURING ONLOAD OF CENTER CARGO, A FIRE WAS DISCOVERED EMANATING FROM A LD-3 CONTAINER, FIRE SERVICES WERE SUMMONED. IN AN ATTEMPT TO SUPPRESS THE FIRE. WATER WAS APPLIED TO THE CONTAINER, THUS CONTAMINATING THE COMPLETE CENTER CARGO. WATER NOW FLOWING OUT OF CAVITY DRAINS FROM CENTER GEAR AFT. CARGO CONTAINER FIRE SUPPRESSED. SHGN 05OCT18 01:52 MEM BEGAN REMOVING BELLY INSULATION BLANKETS FROM CENTER CARGO BAY DUE TO CONTAINER FIRE ALSO STARTED A SYPHON HOSE TO DRAIN WATER FROM 4 BAYS DIRECTLY INBD OF CENTER DOOR BLANKETS REMOVED FROM STA 1641-1701 BELLY AREA ONLY APPROXIMATLY STR 15-50 FACT 05OCT18 18:04 MEM REMOVED AND REPLACED ALL CENTER CARGO FLOOR INSULATION REF AMM 25-85-01-4. SYPHON HOSE REMOVED. CENTER CARGO COMPARTMENT BACK TO NORMAL CONFIGURATION.

Part: HINGE — WORN (CARGO DOOR) · airframe 70,172 hrs · 16,901 cycles

CENTER CARGO DOOR, FWD HIINGE SECTION, FUSELAGE SIDE WAS WORN. CARGO DOOR HAD 6 LOBES WORN. THE LOBES WERE REPAIRED IAW CMM 52-32-17. ORIGINAL HINGE REINSTALLED.

Part: HINGE — WORN (CARGO DOOR) · airframe 70,172 hrs · 16,901 cycles

CENTER CARGO DOOR AFT HINGE SECTION, FUSELAGE SIDE WAS WORN. THE DOOR SIDE AFT LOBE WAS FOUND WORN, LOBE WAS REPAIRED IAW CMM 52-32-17. FOUND 3 LOBES WORN ON THE FUSELAGE SIDE AFT HINGE, REPAIRED IAW CMM 52-32-17. ORIGINAL HINGE INSTALLED.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 69,805 hrs · 16,811 cycles

L1 SLIDE REMOTE PRESS INDICATOR SWITCH INOP. RELAMPED AND PERFORMED ADJ TEST REF MM'S 25-61-04-4, 25-61-04-5. ALL TESTS NORMAL A/C RELEASED FOR SERVICE.

Part: TIRE — FAILED (MLG) · airframe 69,257 hrs · 16,663 cycles

DURING TAKEOFF, AT 125 KTS, RECIEVED A TIRE FAILURE. TIRE FAILURE CONTINUED UNTIL THE REJECT SPEED WAS BELOW 80 KNOTS. TIRE TEMP ON TIRE 3 REACHED 485F, TIRE 4 TEMP REACHED 455F. NONE OF THE TIRES DEFLATED ON THE CONFIG SYNOPTIC. OAT 8 DEGRESS C, INSPECTED ALL TIRES AND BRAKES,NO DEFECTS NOTED, ALL TIRES AND BRAKES ARE WITHIN SERVICE CHECK LIMITS.

Part: ELBOW — CRACKED (ENGINE FUEL) · airframe 69,024 hrs · 16,592 cycles

NOTICED EXCESSIVE FUEL BURN ON 3 CONSECUTIVE WAYPOINTS, SHORTLY AFTER, RECEIVED A LEVEL 2 FUEL QTY USED CHECK, POSSIBLE FUEL LEAK, RAN QRH PROCEDURE AND NR 2 TANK OR ENGINE ISOLATED AS SOURCE OF LEAK. FURTHER TROUBLESHOOTING DETERMINED IT WAS NR 2 ENG AS SOURCE, SHUTDOWN THE NR 2 ENGINE IAW QRH. FOUND A CRACKED FUEL ELBOW. REMOVED AND REPLACED IAW AMM 28-00-00-4.

Part: ELBOW — CRACKED (FUEL LINE) · airframe 69,024 hrs · 16,592 cycles

NOTICED EXCESSIVE FUEL BURN ON THREE CONSECUTIVE WAYPOINTS, SHORTLY THEREAFTER RECIEVED A LEVEL 2 FUEL QTY USED CHECK, POSSIBLE FUEL LEAK. RAN QRH PRCEDURE AND THE NR 2 TANK OR ENGINE ISOLATED AS SOURCE OF LEAK. FURTHER TROUBLESHOOTING DETERMINED IT WAS THE NR 2 ENGINE. SHUTDOWN THE NR 2 ENGINE IAW QRH. VISUALLY INSPECTED THE FUEL LINE & FOUND THE ELBOW CRACKED. THE ELBOW WAS REMOVED AND REPLACED IAW AMM 28-21-01-4. TESTED OK, ACFT OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,960 hrs · 16,572 cycles

DURING PREFIGHT, EMERGENCY LIGHT TEST, A LOW BATTERY ALERT. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY, IAW AMM 33-51-01-4. OPS CHECKED NORMAL.

Part: SENSOR — FAILED (ANTI ICE SYSTEM) · airframe 68,659 hrs · 16,479 cycles

ENROUTE WHILE DESCENDING, SELECTED ENGINE ANTI-ICE ON. RECEIVED A LEVEL 1 NR 2 ENGINE. ANTI ICE DUCT FAILED MESSAGE. RETURNED TO DEPARTURE. COMPLIED WITH FIM, INSPECTED ANTI-ICE DUCT AND FOUND NO EVIDENCE OF LEAK. CHECKED ANTI-ICE SENSOR RESISTANCE AND FOUND VALUE BELOW LIMITS.

Part: LIMIT SWITCH — FAILED (L1 DOOR) · airframe 68,598 hrs · 16,463 cycles

FOUND THE L1 DOOR WILL NOT OPEN ELECTRICALLY. R & R LT FWD DOOR UP LIMIT SWITCH S1-592. PERFORMED A LT FWD DOOR OPS TEST, TESTED OK IAW AMM 52-11-02-5. OK FOR SERVICE.

Part: DOUBLER — CRACKED (RT WING) · airframe 67,184 hrs · 16,065 cycles

REWORK REQUIRED - RT WING LEADING EDGE INTERIOR BEADED DOUBLER AT APPROX STA XOS 550 UNDER REFUEL PANEL FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE INTERIOR BEADED DOUBLER AT APPROX XOS 550 PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 67,184 hrs · 16,065 cycles

MAIN DECK CARGO TRACK AT BS 635, LBL 8.5 FOUND CRACKED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 635) · airframe 67,184 hrs · 16,065 cycles

MAIN DECK CARGO TRACK AT BS 635, LBL 27.5 FOUND CRACKED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 812) · airframe 67,184 hrs · 16,065 cycles

MAIN DECK CARGO TRACK AT BS 812, LBL 27.5 FOUND CRACKED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 67,184 hrs · 16,065 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 789 DOUBLER FOUND CRACKED. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DRAWING ARB3954, REV K, AND SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — WORN (BS 1239-1247) · airframe 67,184 hrs · 16,065 cycles

MAIN DECK CARGO TRACK LBL 47.5, BS 1239 TO 1247 FOUND WORN. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ANGLE — CHAFED (BS 535) · airframe 67,184 hrs · 16,065 cycles

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

Part: DOUBLER — CRACKED (LT WING) · airframe 67,184 hrs · 16,065 cycles

LEFT WING FIXED LEADING EDGE CAVITY DOUBLER AT NR 4 SLAT MID TRACK XOS 600 FOUND CRACKED. CRACKED DOUBLER REMOVED AND REPLACED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 67,184 hrs · 16,065 cycles

LEFT WING FIXED LEADING EDGE CAVITY FOUND DOUBLER AT NR 4 SLAT INBD TRACK XOS 550 FOUND CRACKED. THE DOUBLER WAS REMOVED AND REPLACED IAW DRAWING ARB2933, REV AJ, AND SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 67,184 hrs · 16,065 cycles

RIGHT WING FIXED LEADING EDGE CAVITY FOUND DOUBLER NEAR NR 3 SLAT OTBD TRACK XOS 550 FOUND CRACKED. THE DOUBLER WAS REMOVED AND REPLACED IAW DRAWING ARB2933, REV AJ, AND SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 67,184 hrs · 16,065 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 667 NEAR THE NR 5 SLAT INBD TRACK FOUND A DOUBLER CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED IAW DRAWING ARB3954, REV K, AND INSTALLED IAW SRM 51-33-01-0G. REPAIR CLASSFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 67,184 hrs · 16,065 cycles

LT WING- FIXED LEADING EDGE CAVITY AT APPROX, XOS 667 NEAR NR 5 SLAT I/B TRACK FOUND STRINGER CRACKED AS MARKED. REPAIR CARRIED OUT AT LT WING FIXED LEADING EDGE CAVITY AT APPROX XOS 667 PER SRM 57-40-03-2R FIG 202 REPAIR 2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 67,184 hrs · 16,065 cycles

RIGHT WING FIXED LEADING EDGE CAVITY AT XOS 667 NEAR THE NR 5 SLAT INBD TRACK FOUND THE STRINGER CRACKED. THE STRINGER WAS REPAIRED IAW SRM 57-40-03-2R FIG 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CONTROL PANEL — ODOR (AUTOPILOT SYS) · airframe 64,625 hrs · 15,355 cycles

ON FLIGHT CONTROL CHECK. PREMATURE REMOVAL, INSTALLATION OFF MPN: 4059032-901, POS: ON SRL: 94110395, TAG NR: 2676C8 ON MPN: 4059032-901, CPN: 2210019, SRL: 99010475, TAG NR: D61528, REASON CODE: PREMATURE REMOVAL, INSTALLATION OFF MPN: 4059001-908, POS: 1, SRL: 91120431, TAG NR: 44E355, ON MPN: 4059001-908, CPN: 2211063, SRL: 91120422, TAG NR: 3E0909. FOUND AUTO FLIGHT SYSTEM CONTROL PANEL HAD A BURNED ELECTRICAL ODOR COMING FROM IT. REPLACED AFSC PANEL IAW AMM 22-01-02-4. WHILE TESTING PANEL FOUND NR 1 FCC WOULD NOT PASS RTS, REPLACED NR 1 FCC IAW AMM 22-01-03-4. TESTED BOTH NR 1 FCC AND NR 2 FCC IAW AMM 22-00-00-5, NOW BOTH SYS TESTS NORMALLY.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 619 hrs · 14,538 cycles

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

Part: SKIN — DENTED (TE FLAP) · airframe 619 hrs · 14,538 cycles

RIGHT WING, FOUND A DENT ON RT INBD FLAP LOWER SKIN ON INBD END. REPAIRED IAW EA 1-5750-T0318573 PART 1. MAJOR IAW GMM 6-2-100.

Part: REPAIR — GOUGED (CARGO DOOR) · airframe 619 hrs · 14,538 cycles

AGEING ACFT, EXISTING REPAIR ON CTR CARGO DOOR FWD LOWER EDGE. EXISTING REPAIR EVALUATED & FOUND DEEP GOUGE MARK. EXISTING REPAIR R & R CARRIED OUT IAW EA 1-5230-T0318606 P 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. REFER TO WRI 52300851 FOR WORK DETAILS. .

Part: SEAT TRACK — CORRODED (BS 1200-1219) · airframe 619 hrs · 14,538 cycles

MAIN DECK SEAT TRACK FLANGE AT BS 1200 - 1219, X -107 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 619 hrs · 14,538 cycles

CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STATION 5-0, LONGERON 7R. STRINGER SPLICE CRACK LENGTH APPROX 1 INCH. R & R IAW SRM 51-33-01-0G. NEW LONGERON SPLICE FABRICATED BY MACHINING IAW DWG AEA7633 REVISION B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SUPPORT FRAME — CRACKED (LT WING) · airframe 619 hrs · 14,538 cycles

LEFT WING, FIXED LE LOWER SUPPORT FORMER AT XOS 1026, FOUND CRACKED. FORMER REMOVED IAW SRM 51-31-01-0G. FABRICATED NEW FORMER IAW DWG ARB2920 REVISION BB. INSTALLED NEW FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 619 hrs · 14,538 cycles

LEFT WING, FIXED LE BEADED DOUBLER AT XOS 654.5, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SUPPORT FRAME — CRACKED (RT WING) · airframe 619 hrs · 14,538 cycles

RIGHT WING, FIXED LE LOWER SUPPORT FORMER AT STATION XOS 1026, FOUND CRACK DURING OTBD SLAT CONTROL CABLE INSPECTION. FORMER REMOVED IAW SRM 51-31-01-0G. FABRICATED A NEW FORMER IAW DWG ARB2920 REVISION BB. INSTALLED NEW FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: REPAIR — DAMAGED (FUSELAGE) · airframe 619 hrs · 14,538 cycles

AGEING ACFT, EXISTING REPAIR ON LT FRAME AT MAIN DECK CARGO COMPARTMENT AT STATION 1681, LONGERON 12L. EXISTING REPAIR EVALUATED & FOUND DAMAGED. CARRIED OUT REPAIR IAW SRM 53-00-07-2R FIGURE 201 REPAIR 2 EO 1-5100-7-5001 B5 PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100. INITIAL INSPECTION AT 14,500 FLIGHT CYCLES, REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07-2R TABLE 201 REPAIR 2.

Part: REPAIR — DAMAGED (FUSELAGE) · airframe 619 hrs · 14,538 cycles

AGEING ACFT, EXISTING REPAIR ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 665 & 765, X=47.5. EXISTING REPAIR EVALUATED & FOUND DAMAGED. DAMAGED SEAT TRACK R & R CARRIED OUT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1 EO 1-5100-7-5001 B5 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRAP — CRACKED (TE FLAP) · airframe 619 hrs · 14,538 cycles

LEFT WING OTBD FLAP INBD FWD HINGE TENSION STRAP FOUND CRACKED XW486. TENSION STRAP REMOVED IAW SRM 51-33-01-0G & REPLACED WITH NEW SUPPORT TENSION STRAP IAW SRM 51-33-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: BULKHEAD — CRACKED (BS 1841) · airframe 619 hrs · 14,538 cycles

CENTER CARGO BAY BS 1841 BULKHEAD FOUND CRACKED AT RBL 1.5 - 3.0. REPAIRED IAW SRM 53-00-00-2R FIGURE 211. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LE DROOP) · airframe 619 hrs · 14,538 cycles

LEFT WING LE DROOP UPPER SKIN FOUND CRACK FROM XDLE 328.5 TO 330. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: REPAIR — DAMAGED (FUSELAGE) · airframe 619 hrs · 14,538 cycles

AGEING ACFT, EXISTING REPAIR ON BULKHEAD SKIN AT CTR CARGO COMPARTMENT STATION 1841, LBL 3.0 TO 9.0. EXISTING REPAIR ON BULKHEAD SKIN EVALUATED & FOUND DAMAGED. EXISTING REPAIR R & R CARRIED OUT IAW SRM 53-00-00-2R FIGURE 211 EO 1-5100-7-5001 B5 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: BATTERY — FAILED (L2 DOOR SLIDE) · airframe 57,379 hrs · 13,105 cycles

L2 DOOR SLIDE REMOTE PRESSURE INDICATIOR PTT SWITCH FAILED TO TEST. REPLACED BATTERIES. REMOTE PRESSURE INDICATOR EVAC SLIDE TESTED NORMAL IAW MM 21-61-04-5. OK FOR SERVICE.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 57,069 hrs · 13,009 cycles

RT WING INBD FLAP T/E WEDGE LOWER SURFACE FOUND CRACKED AT XIFH 130 TO 134. REPAIRED IAW SRM 57-50-02, REPAIR 3, FIGURE 201, REV 53 AND EA 1- 5750-T0301707, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: FLOOR SUPPORT — CORRODED (BS 421) · corrosion level 2 · airframe 57,069 hrs · 13,009 cycles

FORWARD LAVATORY FLOOR SUPPORT FOUND CORRODED AT BS 421. R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 57,069 hrs · 13,009 cycles

LEFT WING INBD FLAP LOWER SURFACE, FOUND PUNCTURED ABOUT ONE INCH IN DIAMETER AT XIFH 242. REPAIRED IAW EA 1-5750-T0301706, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 57,069 hrs · 13,009 cycles

LEFT WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XOS 701. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIGURE 203, REV 53 TYPE "A". REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 57,069 hrs · 13,009 cycles

MAIN CARGO FLOOR PANEL 282AF FOUND DELAMINATED. FLOOR PANEL REMOVED IAW AMM 53-21-04, REV 76.1. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J AND SRM 51-90-01, REV 53, AND INSTALLED IAW AMM 53-21-04, REV 76.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — CRACKED (ZONE 600) · airframe 57,069 hrs · 13,009 cycles

RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6, TEN FASTENER HOLES FOUND CRACKED INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. CARRIED OUT BUSHING REPAIR IAW SRM 57-20-02, REPAIR 5, FIG 201 REV 53 AND EA 1-5710-T0301691 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 57,069 hrs · 13,009 cycles

RIGHT WING INBD FLAP LOWER SURFACE FOUND DENTED AT XIFH 250 AND ONE INCH FROM T/E. REPAIRED IAW SRM 57-50-01, REPAIR 1, FIGURE 201, REV 53 AND EA 1-5750-T0301707, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — CRACKED (ZONE 500) · airframe 57,069 hrs · 13,009 cycles

LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6, SEVEN FASTENER HOLES FOUND CRACKED INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. CARRIED OUT BUSHING REPAIR IAW SRM 57-20-02, REPAIR 5, FIGURE 201, REV 53 AND EA 1-5710-T0301690, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — CRACKED (ZONE 500) · airframe 57,069 hrs · 13,009 cycles

LEFT WING L/E LOWER ACCESS PANEL 519CB CUTOUT SKIN INBD FWD CORNER FOUND CRACKED AT XOS 612. REPAIRED IAW SRM 57-40-02, FIG 202 REPAIR 7, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,069 hrs · 13,009 cycles

BS 1250.75 - 1256.75 L/E DOOR FORWARD FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6 -2-100, REV 116.

Part: DOOR FRAME — CRACKED (R3 DOORWAY) · airframe 57,069 hrs · 13,009 cycles

BS 1250.75 - 1256.75, R3 DOOR FWD FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53 -40-15, FIG 201, REPAIR 3, REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: DOOR FRAME — CRACKED (R3 DOORWAY) · airframe 57,069 hrs · 13,009 cycles

BS 1305.25 - 1315.42, R3 DOOR AFT FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201 REPAIR 3 REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: DOOR FRAME — CRACKED (L3 DOORWAY) · airframe 57,069 hrs · 13,009 cycles

BS 1305.25 - 1315.42 L3 DOOR AFT FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6 -2-100, REV 116.

Part: FLOOR SUPPORT — CRACKED (BS 400-430) · airframe 57,069 hrs · 13,009 cycles

FORWARD CABIN FLOOR SUPPORT AT BS 400-430, LBL 32 FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 57,069 hrs · 13,009 cycles

LOWER FUSELAGE RT A/C PACK NR 3 DOOR FRAME AFT UPPER CORNER AREA FOUND CRACKED. TRIMMED OUT AND REPAIRED IAW SRM 53-20-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SEAT TRACK — CORRODED (BS 610) · corrosion level 2 · airframe 57,069 hrs · 13,009 cycles

FORWARD CABIN BS 610, X=-47.5 SEAT TRACK FOUND WITH SURFACE CORROSION. REPAIRED BY SECTION SEAT TRACK REPLACEMENT FROM STATION 605 TO STATION 645 X = -47.5 IAW SRM 53-00-52, FIG 201. REPAIRED BY SECTION SEAT TRACK REPLACEMENT FROM BS 605 - 645 IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — CRACKED (ZONE 600) · airframe 57,069 hrs · 13,009 cycles

DURING SPOILER UPPER SURFACE INSPECTION, RT WING L/E DROOP UPPER SURFACE FOUND CRACKED ABOUT 2 INCHES LONG AT XDLE 324. REPAIRED IAW SRM 57-40-01, REPAIR 5, FIGURE 201, REVISION 53. REPAIR DOUBLER INSTALLED IAW SRM 57-40-01, REPAIR 5, FIGURE 201, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 57,069 hrs · 13,009 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON NR 4 BANJO FITTING OF VERTICAL STABILIZER STA 2164, A CRACK FOUND ON RADIUS OF THE RT SIDE OF REAR SPAR CAP FWD FLANGE LOCATED AT THE UPPER SECTION APPROX. 0.75" LENGTH. REPAIRED IAW EA 1-5530-T0301678, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: WIRE HARNESS — DAMAGED · airframe 55,786 hrs · 12,645 cycles

FORTY MINUTES INTO FLIGHT RECEIVED A LEVEL ONE "FIRE DET 1 FAULT" ALERT IT WAS FOLLOWED BY INTERMITTENT LEVEL THREE NR 1 FIRE ALERT AND "FIRE DET 1 FAIL" ALERTS. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. CFDS SHOWS NOT CURRENT FAULTS FOR FDCU 1. LEG 1 FAULTS SHOWS "UP RIGHT FIRE DET ASSY B", UP RIGHT ASSY A". LEG 2 FAULT SHOWS "LOWER FIRE DET ASSY A". REPLACED NR 1 ENG UPPER RT LOOP ASSY AND LOWER TURBINE RAIL ASSY IAW AMM 26-11-03-4-1. REPLACED LT HARNESS ASSY IAW 71-50-04-4-1. REPLACED SEMI RIGID CABLES IAW AMM 71-50-04-2-1. FDCU 1 SHOWS NO CURRENT FAULTS. RTS PASS. AWAITING HIGH POWER ENG RUN. PERFORMED HIGH POWER ENGINE RUN IAW JRH. NO FIRE DETECTION FAULT OR ALERT. NO CURRENT FAULT AFTER ENGINE SHUTDOWN. ACFT OK FOR CONTINUE SERVICE.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 52,106 hrs · 11,655 cycles

LOWER PART OF VERTICAL STABILIZER, RT REAR CENTER SPAR TO REAR SPAR LOWER WEB FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 1-5530-154227. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SKIN — CRACKED (RT WING) · airframe 52,106 hrs · 11,655 cycles

04 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA.XORS=683.4 AND STA=713.6. REPAIR CARRIED OUT AS PER DRAWING SG11570004 REV A. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.

Part: LONGERON — CRACKED (200) · airframe 52,106 hrs · 11,655 cycles

CRACK INDICATION APPROX 1" IN LENGTH FOUND DURING X-RAY INSP AT STA 6-100 , LONGERON -7R AFT SECTION EDGE. CARRIED OUT REPAIR AS PER SRM 53-00-05 FIG 202 REV 47 & DRAWING AEA7478 REV A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SKIN — CORRODED (BS 2150) · corrosion level 2 · airframe 52,106 hrs · 11,655 cycles

BS 2150 SKIN FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-01 REPAIR 3 FIG. 201 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SKIN — CRACKED (LT WING) · airframe 52,106 hrs · 11,655 cycles

03 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA.XORS=683.4 AND STA XORS=713.6

Part: SKIN — CRACKED (EMPENNAGE) · airframe 52,106 hrs · 11,655 cycles

EMP - AFC RT DOGHOUSE ENTRANCE CUTOUT FOUND CRACKED AT INBD FWD CORNER. REPAIR DOUBLER FABRICATED AS PER SRM 53-70-02 FIG.201 REV 47 REPAIR DOUBLER INSTALLED AS PER SRM 51-33-01 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 52,106 hrs · 11,655 cycles

CABIN - RT STA 5-0 -STA 5-3, X=-8.75 SEAT TRACK FOUND CHAFED. DAMAGED SEAT TRACK TRIMMED AND REPAIR CARRIED OUT AS PER SRM 53-00-52 FIG. 201 REPAIR 1 REV 47 . REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.

Part: FRAME — DENTED (BS 166 L11R) · airframe 52,106 hrs · 11,655 cycles

FRAME BS 1661 L11R, FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REPAIR 1 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 52,106 hrs · 11,655 cycles

LEFT WING INBD FLAP VANE LOWER SURFACE FOUND WITH DELAMINATION. VANE ASSY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REV. 70. ADJUSTED AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REV 70.0. CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.

Part: DUCT — RUPTURED (NR 3 ENGINE) · airframe 50,373 hrs · 11,212 cycles

AFTER TAKEOFF ICE DET SINGLE ALERT FOLLOWED BY MOMENTARY MANIFOLD FAIL LIGHT. THEN AIR 3 OFF. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX FOUND PNEU DUCT RUPTURED INBD OF NR3 ENGINE. REPLACED DUCT IAW AMM 36-14-02-4.

Part: PROXIMITY SENSOR — DIRTY (MLG) · airframe 46,893 hrs · 10,433 cycles

ON GEAR EXTENSION HAD NOSE GEAR UNSAFE INDICATION ON CONFIG PAGE (SECONDARY DISPLAY) RECYCLED AND RECEIVED PROPER DISPLAY. PERFORMED INSP OF NOSE GEAR EXTENSION SYS FOUND PROXIMITY SENSORS DIRTY WITH GREASE CLEANED AND PERFORMED TARGETS AND PROXIMITY IAW AMM 32-61-00-0. ALL FOUND GOOD. ACFT OK FOR SERVICE.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 46,180 hrs · 10,280 cycles

CABIN RT BELOW FLOOR AT STA 1229 'X' = -66.5 CTR WING TANK UPPER SURFACE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5710-132234, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 108.

Part: SKIN — CORRODED (ZONE 600) · airframe 46,180 hrs · 10,280 cycles

RT WING UPPER SURFACE FOUND CORROSION AT XORS 97 AFT OF FWD EDGE 6 INCHES. REPAIRED AS PER E.A. NR 1-5710-132239, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 108.

Part: LONGERON — CRACKED (LT MLG) · airframe 46,180 hrs · 10,280 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSP ON NLG LT SIDE TRUNNION FITTING TRIM OUT AREA FOUND LONGERON CRACK APPROX 0.3 INCH. TRIMMED OUT AREA CRACKED LONGERON REMOVED AND REPLACED AS PER SRM 51-31-01, REVISION 41. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 108.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 46,180 hrs · 10,280 cycles

RT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG OTBD BORE FOUND WITH CORROSION. REPAIRED AS PER E.A. NR 1-5750-132237. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 108.

Part: HINGE — GOUGED (LT WING TE FLAP) · airframe 46,180 hrs · 10,280 cycles

LT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG INBD FOUND WITH TOOL MARKS. REPAIR CARRIED OUT AS PER E.A. 1-5750-132236, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 108.

Part: HINGE — GOUGED (LT WING TE FLAP) · airframe 46,180 hrs · 10,280 cycles

LT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG OTBD FOUND WITH TOOL MARKS. REPAIR CARRIED OUT AS PER E.A. 1-5750-132236, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 108.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 46,180 hrs · 10,280 cycles

LT WING OTBD FLAP INBD FWD HINGE FITTING LWR INBD ATTACH HOLE FWD AND AFT SURFACE FOUND CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5750-132235, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 108.

Part: DOUBLER — CRACKED (MLG WW) · airframe 46,180 hrs · 10,280 cycles

CTR LANDING GEAR WHEEL WELL LT WEB DOUBLER CRACKED AT STA 1392, X = 31.5. REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-31-01 REVISION 41. DOUBLER FABRICATED AS PER DRAWING NR AEA0526 REVISION NC. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 108.

Part: SKIN — DENTED (BS 1921-1941) · airframe 46,180 hrs · 10,280 cycles

FUSELAGE SKIN AT STA 1921 TO 1941, LONGERON 46 RT TO 50 RT INSPECTED BUT NO DENT FOUND. HOWEVER DENT FOUND ON STA 1921 TO 1941 LONGERON 46 LT TO 50 LT. REPAIR CARRIED OUT PER E.A. 1-5310-130882 REVISION A PART 2,

Part: RIB — CRACKED (SLAT TRACK) · airframe 46,180 hrs · 10,280 cycles

RT WING SLAT TRACK NR 16 INBD SUPPORT RIB CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, REVISION 41. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100, REVISION 108.

Part: RIB — CRACKED (SLAT TRACK) · airframe 46,180 hrs · 10,280 cycles

LT WING SLAT TRACK NR 16 INBD SUPPORT RIB CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01, REVISION 41. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100, REVISION 108.

Part: TRUNNION — CRACKED (NLG WW) · airframe 46,180 hrs · 10,280 cycles

NLG WW, LT NLG TRUNNION FITTING FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2, REVISION 41. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 108. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 CYCLE AND REPETITIVE INSPECTION TO CARRY OUT AT 1500 CYCLE AS PER SRM 53-10-14 REPAIR 2 TABLE 201, REVISION 41.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 41,098 hrs · 9,189 cycles

UPPER CARGO DOOR CUT OUT, NR 5 LOWER JAMB SUPPORT FITTING CRACKED. FITTING REMOVED & REPLACED PER SRM 51-33-01 VOL II. MOUNTING HOLES ON NR 5 JAMB BEAM REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 41,098 hrs · 9,189 cycles

UPPER CARGO DOOR CUT OUT, NR 4 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED PER SRM 51-33-01 VOL II. MOUNTING HOLES ON NR 4 JAMB BEAM REPAIR CARRIED OUT PER EA 1-5310-112624, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 41,098 hrs · 9,189 cycles

UPPER CARGO DOOR CUT OUT, NR 2 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED PER SRM 51-33-01 VOL.II. MOUNTING HOLES ON NR 2 JAMB BEAM REPAIR CARRIED OUT PER SRM 53-50-00 FIG. 10 VOL I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 41,098 hrs · 9,189 cycles

UPPER CARGO DOOR CUT OUT, NR 7 LOWER JAMB SUPPORT FITTING MOUNTING HOLE CRACKED. MOUNTING HOLES REAMED PER SRM 53-50-00 FIG. 10 VOL.I. AND BUSHING REPAIR CARRIED OUT PER SRM 53-50-00 FIG. 10. VOL.I. BUSHING FABRICATED PER SRM 53-50-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 41,098 hrs · 9,189 cycles

UPPER CARGO DOOR CUT OUT, NR 6 LOWER JAMB SUPPORT FITTING MOUNTING HOLE CRACKED. MOUNTING HOLES REAMED PER SRM 53-50-00 FIG. 10 VOL.I. AND BUSHING REPAIR CARRIED OUT PER SRM 53-50-00 FIG. 10. VOL.I. BUSHING FABRICATED PER SRM 53-50-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 41,098 hrs · 9,189 cycles

UPPER CARGO DOOR CUT OUT, NR 3 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED PER SRM 51-33-01 VOL.II. MOUNTING HOLES ON NR 3 JAMB BEAM REPAIR CARRIED OUT PER SRM 53-50-00 FIG 10 VOL.I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 41,098 hrs · 9,189 cycles

UPPER CARGO DOOR CUT OUT, NR 1 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED AS PER SRM 51-33-01 VOL.II. MOUNTING HOLES ON NR 1 JAMB BEAM REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL.I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 41,098 hrs · 9,189 cycles

LT WING, ANTI-ICE TELESCOPE TUBE CUT-OUT AT L/E FIXED COMPARTMENT FOUND OUTBD CORNER CRACKED. TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 43 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, MAIN FUSELAGE FRAME AT STA 5-93 LONGERON 12R , FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION REQUIRED AT 9,500 CYCLES. OIL CONTROL NR 296870.

Part: PANEL — CORRODED (ZONE 200) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, CENTER WING UPPER PANEL AT STA 1219 X = -60 FOUND WITH CORROSION. REWORKED AS PER FEDEX E.A.1-5710-105547, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (LT WING) · airframe 35,999 hrs · 8,093 cycles

LEFT WING TOP SKIN SURFACE AFT AT FORWARD OF INBOARD AILERON FOUND WITH CORROSION. LT WING TOP SKIN SURFACE AFT AT FORWARD OF INBOARD AILERON CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.430", MATERIAL REMOVED = 0.041", REMAINED THICKNESS = 0.389" AND FOUND EXCEEDED LIMIT AS PER SRM 57-10-00 FIGURE 32 VOLUME I. REWORKED AREA REPAIRED AS PER FEDEX E.A. 1-5710-105549, TITLE: WINGS - LEFT HAND UPPER WING SKIN - CORROSION REPAIRS AT XORS = 391.50 COMMON TO STRINGERS 1L AND 2L - BLENDED OUT REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (LT WING) · airframe 35,999 hrs · 8,093 cycles

LEFT WING TOP SKIN SURFACE AFT AT XORS 779 FOUND WITH CORROSION. LT WING TOP SKIN SURFACE AFT AT XORS 792 CORROSION REMOVED AS PER SRM 51- 21-01 VOLUME II. ORIGINAL THICKNESS = 0.175", MATERIAL REMOVED = 0.046", REMAINED THICKNESS = 0.129" AND FOUND EXCEEDED LIMIT AS PER SRM 57-10-00 FIGURE 32 VOLUME I. REWORKED AREA REPAIRED AS PER FEDEX EA 1-5710-105548, TITLE: WINGS - LEFT HAND UPPER WING SKIN - CORROSION REPAIRS AT XORS = 792.86 COMMON TO REAR SPAR AT THE EOP - BLENDED OUT REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 5-53 TO STA 5-63, X = 8 FOUND SCRATCHED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPIAR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, MAIN FUSELAGE FRAME AT STA 1741 ABOUT LONGERON 12R AREA FOUND DENTED. DENT REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION REQUIRED AT 9,500 CYCLES. OIL CONTROL NR 296869.

Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 475, X = 8 CROWN AREA FOUND BROKEN. REPAIR CARRIED OUT BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 495 TO STA 525, X = 8 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DUCT — CRACKED (RT WING) · airframe 35,999 hrs · 8,093 cycles

RIGHT WING, TELESCOPIC DUCT CUTOUT CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-105539. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 35,999 hrs · 8,093 cycles

CRACK FOUND (APPROX 8" LONG) DURING HFEC INSPECTION ON LT WING TANK AT THE END OF UPPER STRINGER 9 XORS 819. CRACK ON LT WING TANK AT THE END OF UPPER STRINGER 9 XORS 819 SLOTTED OUT AND ANGLE REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 879 TO STA 884, X = -8 FOUND WITH NICK MARK. MAIN DECK CARGO COMPARTMENT, NICKED SEAT TRACK AT STA 879 TO STA 884, X = -8 REPAIR CARRIED OUT BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 869 TO STA 909, X = -8 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 955, X= 8 FOUND SCRATCHED. MAIN DECK CARGO COMPARTMENT SCRATCHED SEAT TRACK AT STA 955, X= 8, REPAIR CARRIED OUT BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 869 TO 969, X= 8 AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. REFER TO SNRM N00287 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 35,999 hrs · 8,093 cycles

RIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 728 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT HAND WING FIXED LEADING EDGE AT XOS 728 REPAIRED AS PER FEDEX EA 1-5730-105538, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 35,999 hrs · 8,093 cycles

RIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 698 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT WING FIXED LEADING EDGE AT XOS 698. REPAIRED AS PER FEDEX EA NR 1-5730-105537, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 965, X = -47.5 FOUND WITH NICK MARK. MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 965, X = -47.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 901 TO STA 989, X = -47.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 879-884) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 879 TO STA 884, X = 8 FOUND WITH NICK MARK. MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 879 TO STA 884, X = 8 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 869 TO STA 969, X = 8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 35,999 hrs · 8,093 cycles

CRACK FOUND (APPROX 6" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 13 XORS 577. CRACKED UPPER STRINGER 13 ON RIGHT HAND WING TANK AT XORS 577 TRIMMED OUT 2 BAYS AND REPAIRED WITH SPLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 35,999 hrs · 8,093 cycles

RIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 643 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT WING FIXED LEADING EDGE AT XOS 643. REPAIRED AS PER FEDEX EA NR 1-5730-104824, PERMANENT REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 35,999 hrs · 8,093 cycles

CRACK FOUND (APPROX. 1.5 INCHES LONG) DURING HFEC INSPECTION ON RT WING TANK AT THE END OF LOWER STRINGER 41 XORS 685. CRACK ON RIGHT HAND WING TANK AT THE END OF LOWER STRINGER 41 XORS 685 SLOTTED OUT AND RESIZING ARROWHEAD REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 35,999 hrs · 8,093 cycles

CRACK FOUND (APPROX 12" LONG) DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF UPPER STRINGER 13 XORS 577. CRACKED UPPER STRINGER 13 ON LT WING TANK AT XORS 577 TRIMMED OUT 2 BAYS AND REPAIRED WITH SPLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 35,999 hrs · 8,093 cycles

CRACK FOUND (APPROX 9" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 14 XORS 521. CRACK ON RIGHT WING TANK AT THE END OF STRINGER 14 XORS 521 TRIMMED OUT AND REPAIRED WITH SPLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1000-1015) · airframe 35,999 hrs · 8,093 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1000 TO STA 1015, X = -47.5 FOUND WITH NICK MARK, MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 1000 TO STA 1015, X = -47.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 989 TO STA 1069, X = -47.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

REFERENCE EO 1-5510-7-5000 D1 PART 1, LT NR 36L BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83027.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

REFERENCE EO 1-5510-7-5000 D1 PART 1, RT NR 34R BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83026.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

REFERENCE EO 1-5510-7-5000 D1 PART 1, RT NR 1R BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83029.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

REFERENCE TO EO 1-5510-7-5000 D1 PART 1, LT HAND NR 3L BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83028.

Part: BULKHEAD — DAMAGED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

EMPENNAGE, TO TRIM RIGHT HAND OPERATING BULKHEAD FOR NR 35R BARREL NUT BORE REWORK ACCESS. RT OPERATING BULKHEAD TRIMMED OUT AS PER SRM 51-31-01 VOL II AND FOUND EXCEEDED LIMIT AS PER FEDEX EO NR 1-5510-7-5000. REPAIR CARRIED OUT ON TRIMMED AREA AT RT OPERATING BULKHEAD AS PER FEDEX EA NR 1-5510-87552. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

DURING AFT EXTENDED TAILCONE REMOVAL, FOUND INTERIOR SKIN DETACHED AT SEVERAL LOCATIONS. EXTENDED TAILCONE REPLACED AS PER AMM 53-52-01-4. (CLOSED)

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

LT NR 4L BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83028.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

LT BARREL NUT HOLE NR 28L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83022.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

LT BARREL NUT HOLE NR 16L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83025.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

LT BARREL NUT HOLE NR 22L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83025.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

RT BARREL NUT HOLE NR 31R FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83026.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

RT BARREL NUT HOLE NR 17R. FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83024.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

LT BARREL NUT HOLE NR 30L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83022.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

RT BARREL NUT HOLE NR 29R FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83026.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

WITH REFERENCE TO EO1-5510-7-5000 PART 1, RT NR 5R BORE CORROSION FOUND EXCEEDED LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83023.

Part: FITTING — CORRODED (ZONE 300) · airframe 31,221 hrs · 7,092 cycles

LT NR 26L FITTING BARREL NUT BORE FOUND CORROSION EXCEEDED TO LIMIT. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. (CLOSED)

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 33L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83022

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

WITH REFERENCE TO WORK CARD E1-5510-7-5000, RT BARREL NUT HOLE NR 36R FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83021

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 27L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83022.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

WITH REFERENCE TO WORK CARD E1-5510-7-5000 D1 PART 1, NR 14L FITTING BARREL NUT BORE FOUND BADLY CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 29L, FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83022.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

WITH REFERENCE TO WORK CARD E1-5510-7-5000, REQUIRE TO TRIM LT OPERATING BULKHEAD FOR NR 35L BARREL NUT REWORK ACCESS. TRIMMED OUT AS PER SRM 51-31-01 VOL. II AND FOUND EXCEEDED LIMIT AS PER FEDEX EO 1-5510-7-5000. REPAIR CARRIED OUT ON TRIMMED AREA AT LT OPERATING BULKHEAD AS PER FEDEX EA 1-5510-87552

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 1L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT ON LT HORIZONTAL STABILIZER, LT BARREL NUT HOLE NR 1 AS PER FEDEX EA 1-5510-83020.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 35L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83022

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

EMPENNAGE WITH REFERENCE TO EO 1-5510-7-5000-01 PART 1, FOUND NR 14R FITTING BORE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 31,221 hrs · 7,092 cycles

NR 2 ENGINE, LT THRUST REVERSER UPPER SLIDER TRACK CRACKED. REMOVED AND INSTALLED NEW REVERSER AS PER WORK CARD 78T3002-L AND WORK CARD 78T3902-L. ADJUSTMENT AND OPERATION CHECK CARRIED OUT AS PER WORK CARD 78T3902-L, GE NR 2 LEFT THRUST REVERSER DOOR - INSTALL.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 31,221 hrs · 7,092 cycles

NR 2 ENGINE, RT THRUST REVERSER UPPER SLIDE TRACK CRACKED. REMOVED AND REPLACED AS PER WORK CARD 78T3002-R AND WORK CARD 78T3902-R. ADJUSTMENT AND OPERATIONAL CHECK CARRIED OUT AS PER WORK CARD 78T3902-R, GE NR 2 RIGHT THRUST REVERSER DOOR - INSTALL.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 31,221 hrs · 7,092 cycles

NR 2 ENGINE, NOSE INLET LIP FOUND CRACKED AT 8 O'CLOCK POSITION AND EXISTING REPAIR DOUBLER HAS LOOSE FASTENERS. REMOVED AND REPLACED AS PER AMM 54-22-01-4 AND APPLIED SEALANT AS PER AMM 54-22-01-4.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 31,221 hrs · 7,092 cycles

EMPENNAGE WITH REFERENCE TO EO 1-5510-7-5000-01 PART 1, FOUND NR 26R FITTING BORE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.

Part: TORQUE RING — CRACKED (THRUST REVERSER) · airframe 31,221 hrs · 7,092 cycles

NR 1 ENGINE, RT THRUST REVERSER FORWARD FRAME, UPPER TORQUE RING CRACKED APPROXIMATELY 1.5 IN LENGTH. THRUST REVERSER REMOVED AND INSTALLED NEW REVERSER AS PER WORK CARD 78T3001-R AND WORK CARD 78T3901-R, GE NR 1 RIGHT REVERSER DOOR - INSTALL. REVERSER ADJUSTMENT AND OPERATION CHECK CARRIED OUT AS PER WORK CARD 78T3901-R, GE NR 1 RT REVERSER DOOR - INSTALL.

Part: TORQUE RING — CRACKED (ZONE 400) · airframe 31,221 hrs · 7,092 cycles

NR 3 ENG, RIGHT FORWARD FRAME UPPER TORQUE RING CRACKED APPROXIMATELY 5 INCHES IN LENGTH. THRUST REVERSER REMOVED AND INSTALLED AS PER WORK CARD 78T3003-R AND WORK CARD 78T3903-R FOR WORK DETAILS. THRUST REVERSER ADJUSTMENT AND OPERATION CHECK CARRIED OUT AS PER WORK CARD 78T3903-R, GE NR 3 RT THRUST REVERSER DOOR - INSTALL FOR WORK DETAIL.

Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 31,221 hrs · 7,092 cycles

MAIN DECK CARGO COMPARTMENT FLOOR CARGO TRACK AT STA 1119, LBL 8.5, FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 31,221 hrs · 7,092 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT LBL 27, STATION 635 FOUND CRACKED APPROXIMATELY 2 INCHES LONG. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE I.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 31,221 hrs · 7,092 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT LBL 47, STATION 635 FOUND CRACKED APPROXIMATELY 2 INCHES LONG. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 31,221 hrs · 7,092 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1230 - 1239, LBL 47 FOUND CROWN ELONGATED. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1.

Part: SUPPORT — CRACKED (ZONE 600) · airframe 27,076 hrs · 6,166 cycles

RT O/B TRAILING EDGE FLAP STOP BOLT SUPPORT ISLAND IS CRACKED (2 PLACES) REFER FIGURE 1 (SHEET 10 OF 11 ) FIGURE AV OF 1-5750-7-5002 B. REMOVED & REPLACED SUPPORT FITTINGS PER SRM51-31-01 & DAC DWG. ARC4100. COMPLIED BY AMT 357288.

Part: FITTING — CRACKED (ZONE 600) · airframe 27,076 hrs · 6,166 cycles

RT WING I/B FLAP I/B SIDE LOAD ROLLER FITTING ATTACHMENT IS CRACKED AT BASE RADIUS. REMOVED AND REPLACED R/H WING SIDELOAD ROLLER FITTING IAW M/M 20-50-02-2.

Part: FITTING — CRACKED (ZONE 500) · airframe 27,076 hrs · 6,166 cycles

LT WING I/B FLAP I/B SIDE LOAD ROLLER FITTING ATTACHMENT IS CRACKED AT BASE UPPER RADIUS. CRACK VERIFIED BY NDT. ORDERED NEW FITTING. INSTALLED NEW BEARINGS PER W/C E-1-5750-7-5003BL, SEQ 459 STEPS 33-34. INSTALLED NEW FITTING, TORQUED BOLTS PER SMP M/M 20-50-02-2.

Part: FITTING — CORRODED (TE FLAP) · airframe 27,076 hrs · 6,166 cycles

LT WING INBOARD FLAP OUTBOARD HINGE SUPPORT FITTING AT PIVOT BEARING, FUSE PIN IS HEAVILY CORRODED. REMOVED & REPLACED HINGE PIN, BUSHING, WASHER, NUT & COTTER PIN AND INSTALLED IAW M/M 27-50-20-4.

Part: PSEU — MALFUNCTIONED (L/E SLAT) · airframe 24,416 hrs · 5,560 cycles

ON CLIMBOUT OF FRA, RECEIVED A SLAT DISAGREE ALERT WHEN SLATS RETRACTED WITH A STRONG ROLL TO RIGHT. RED TABS COMPLIED WITH AND SLATS EXTENDED A/S 270 KIAS. SLATS EXTENDED FINE WITH NO CONTROL PROBLEMS. DUMPED FUEL AND DIVERTED TO PARIS. T/S AS PER FIM 31-71-07-00. REMOVED AND REPLACED PROX SENSOR DI-14 AS PER AMM 27-84-03-4. REMOVED AND REPLACED PSEU AS PER AMM 31-71-01-2. PERFORMED OPS/TEST 27-84-00. ALL TESTS ARE OK.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 24,392 hrs · 5,555 cycles

HYD PUMP 1R OFF DISPLAYED DURING CRUISE AT FL280. PUMP 1R FAULT LIGHT ON HYD OVERHEADD ILLUMINATED. HYD SYS 1 TEMP INDICATED 94 DEG C. SUBSEQUENTLY HYD 1 OFF ALERT AND NR 2 AUTOPILOT DISCONNECT. RETURNED TO RPLB. TEMP DECREASED TO 79 DEG C, WHEN ON APPROACH. SLATS EXTENDED, BOTH PUMPS ON, NORMAL FLAP AND GEAR EXTENSION. NO A/P WITH LOWER YAW DAMP INOP. FACT: REMOVED AND REPLACED 1L AND 1R EDP AND CASE DRAIN FILTERS. FLUSHED HYD SYSTEM. OP/LEAK CHECKS GOOD ON ENGINE RUN.

Part: SENSING ELEMENT — DAMAGED (NR 2 ENGINE) · airframe 23,358 hrs · 5,318 cycles

AFTER DEPARTURE AT TPE TURNED ON ANTI ICE (ENGINE NR 2 A-ICE), WE WERE IN ICING CONDITION, DESCENDED LOWERED AND RETURNED TO TPE. FACT 23MAR03 22:52 TPE R RECEIVED A/C PARTS AT 2110Z, REPLACED SENSING ELEMENTS D1-90 IAW MM 30-22-11-4, AND PERFORMED ANTI-ICE MANIFOLD ADJUSTMENT/TEST IAW MM 30-22-11-5, ALL SYSTEM FUNCTION CHECKED NORMAL. NR 2 ENGINE COWLING CLOSED AND PLATFORM SECURED AND LATCHED. OK FOR SERVICE.

Part: RCCB — FAULTY (ELECTRICAL SYS) · airframe 21,936 hrs · 5,018 cycles

JUST PRIOR TO TOP OF CLIMB, RIGHT EMERGENCY AC BUS OFF. CONSULTED WITH MOCC, RETURNED TO AIRPORT. EPCU FAULT LOGGED AND FOUND B1-138 RCCB IN CAC SHOWED OPEN INDICATOR BUT B1-139 CONT CB WAS CLOSED. REMOVED AND REPLACED B1-138 RCCB IAW AMM, ALSO PRECAUTION REMOVED AND REPLACED B1-139 CB. EPCU RTS TEST PASSED IAW AMM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 21,817 hrs · 4,986 cycles

INBD AFT TOILET MOUNTING ATTACHMENT CORRODED AT BS 421. R&R SUPPORT PER SRM 51-33-01, VOL II.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,817 hrs · 4,986 cycles

FWD CABIN LT SEAT TRACK AT BS 470 FOUND CORRODED. R&R SEAT TRACK PER SRM 53-70-00.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 18,379 hrs · 4,230 cycles

FLT 5081 WRI, AFTER T/O NOSE GEAR WOULD NOT RETRACT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,352 hrs · 4,224 cycles

NOSE GEAR UNSAFE IND AFTER GEAR RETRACTION, CYCLED GEAR.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 18,352 hrs · 4,224 cycles

NOSE GEAR LIGHT STAYED AFTER GEAR RETRACTION. CHECKED PHYSICAL CONDITION SENSORS AND TARGETS. NO DEFECTS NOTED. OK FOR SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,775 hrs · 4,102 cycles

FUSELAGE TRANSVERSE FRAME DENTED AT STA 1701 RIGHT ALONG LONGERON 12R. R&R FRAME PER SRM53-30-00 FIG 1 VOL 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,775 hrs · 4,102 cycles

FUSELAGE TRANSVERSE FRAME CRACKED AT STA Y=1601 LEFT 3.0 INCH LENGTH, ALONG LONGERON 12L. REMOVED AND REPLACED FRAME PER SRM 53-30-00 FIG 1 VOL 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,775 hrs · 4,102 cycles

FUSELAGE TRANSVERSE FRAME DENTED AT STA 1661 RIGHT ALONG LONGERON 12R. R&R FRAME PER SRM 53-30-00 FIG 1 VOL 1.

Part: FRAME — CRACKED (MAIN DECK) · airframe 17,775 hrs · 4,102 cycles

N 527 FUSELAGE TRANSVERSE FRAME CRACKED AT STA Y=1571 LEFT ALONG LONGERON 12L. ** S/D ** COMING

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,775 hrs · 4,102 cycles

FUSELAGE TRANSVERSE FRAME DENTED AT STA 1701 LEFT ALONG LONGERON 12L. R&R FRAME PER SRM 53-30-00 FIG 1 VOL 1.

Part: HARNESS — FAULTY (FIRE DETECTION) · airframe 16,063 hrs · 3,733 cycles

IN CRUISE GEAR UP RECD INTERMITTENT FIRE DET 3 FAIL ALERT. CLEARANCE AND PERM TO DUMP FUEL ON RADAR VECTORS. FOUND TERMINAL LUG LOOSE AT DH22C FOR LOOP-B TIGHTENED. FOUND OPEN WIRE BETWEEN DH23C & DH4C OF LOOP-A. REMOVED AND REPLACED WIRE HARNESS PER MM. NO PNEU LEAKS FOUND. RAN RTS PASSED. PERF A HIGH PWR ENG RUN, OPS CK GOOD. AC OK FOR SERVICE.

Part: FIRE DETECTOR — INOPERATIVE (NR 1 ENGINE) · airframe 14,389 hrs · 3,373 cycles

NR 1 ENG FIRE DETECT FAIL ALERT 30 MIN AFT T/O FIRE TEST CAUSED NR 1 FIRE ALERT. REMOVED AND REPLACED NR 1 ENG LWR TURBINE DETECTOR LOOP PER MM 26-11-03-4. OPS CK GOOD.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 13,591 hrs · 3,196 cycles

UPPER CARGO COMP BALLMAT AREA, FLOOR TRACK AT BS 635 X=8.5L CRACKED. UPPER CARGO COMP BALLMAT AREA, FLOOR TRACK AT BS 635 X=8.5R CRACKED. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 VOL 1.

Part: HOSE — INOPERATIVE (NR 7 BRAKE)

RT MLG DID NOT RETRACT. CYCLED GEAR, NO HELP. REMOVED AND REPLACED NR 7 BRAKE HOSE AND SUPPORT IN RT MLG LOWER TORQUE LINK PER 32-40-00 AND 32-45-00-5, 32-31-00-5. AC OK FOR RELEASE.

Part: SEAT TRACK — CRACKED (BS 905)

CRACK APPROX 10 INCHES LONG FOUND ON SEAT TRACK AT STA 905, X= 27.5 (RT) ON UPPER CARGO AREA.