N582FE
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FEDERAL EXPRESS CORPORATION (FDEA) | Operator | on 1999-06-30 | Operator named in NTSB report |
Accident & incident history
Operated by FEDERAL EXPRESS CORPORATION (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
370 reports on file, 1997-06-24 – 2024-05-17.
Part: HYDRAULIC LINE — FAILED (NR 3 HYD SYS) · airframe 98,006 hrs · 23,890 cycles
BOS - HYDRAULIC SYS 3 FAILURE PASSING DURING CLIMB OUT. RESERVOIR LEVEL DEPLETED TO ZERO. FOUND SLAT SYSTEM HYDRAULIC LINE LEAKING FLUID. MADE A CUT APROX 3 FT INBOARD AND 3 FT OTBD FROM CENTER OF PYLON. INSTALLED 6 FT LONG FLEX LINE MADE OF THREE 2 FT LONG FLEX LINES UNIONED TOGETHER AND RINGLOKED TO THE 2 CUT ENDS OF THE RIGID LINE TO THE FLEX LINE. NR 3 HYDRAULIC SYSTEM NEEDS TO BE SERVICED AND SYSTEM NEEDS OPS AND LEAK CHECK. REFERENCE AMM 20-10-01-2.
Part: PIPE — LOOSE (N/A) · airframe 97,941 hrs · 23,862 cycles
HYD 2 OFF LEVEL 1 IN CRUISE. FOLLOWED QRH. HYD SYNOPTIC SHOWED SYSTEM 2 FLUID QUANTITY DECREASING. FLUID LEVEL DECREASED BELOW 2.5 AND THEN RECEIVED LEVEL 2 HYD 2 FAIL. QUANTITY DROPPED TO 0.0. WHILE CONFIGURING TO LAND, RECEIVED LEVEL 2 FLAP DISAG AND FLAPS WOULD NOT EXTEND BEYOND 20 DEGREES. COMPLETED QRH AND LANDED WITHOUT FURTHER INCIDENT. ***EMERGENCY DECLARED*** REMOVED ACCESS PANEL 373CL FROM LH SIDE OF VERTICAL STAB TO FOM. FOUND LOWER B- NUT ON HYDRAULIC PIPE AMK7550-504 LOOSE. TIGHTENED B-NUT PER AMM 20-50-01-2. PERFORMED LEAK CHECK OF HYDRAULIC LINE AMK7550-504 LOWER B-NUT WITH HYRAULICS OPERATING. NO LEAKS FOUND.
Part: FRAME — CORRODED (ZONE 100) · airframe 97,938 hrs · 23,861 cycles
DURING FRAME 410 REMOVAL FOUND CORROSION ON FRAME 421 AT 6 0'CLOCK POSITION BLENDED MINOR CORROSION IN REF. TO MD11 SRM 53-00-00-2R; FIGURE 205.
Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 97,938 hrs · 23,861 cycles
#1 ENG FWD MOUNT FWD RH MOUNT HOLE PITTED, APPEARS TO HAVE CORROSION. COMPLIED WITH EA 1-5450-T0378566 P1 AND P2 TITLE: NACELLES/PYLON- WING PYLON/STRUT - FWD ENGINE MOUNT, FWD IB TRUSS BOLT HOLE CORROSION PERMANENT REPAIR.
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 97,938 hrs · 23,861 cycles
FOUND EXFOLIATING CORROSION ON FRAME MEMBER (HOLE IN FRAME) JUST BEHIND LAVATORY SERVICE PANEL IN THE AVIONICS AREA. MWT COMPLIED WITH E.A. 1-5310-T0378654, PT 1; FUSELAGE-MAINFRAME-FUSE FRAME CORROSION AT FR STA, 410.580 AND 421.507 AT CENTERLINE DUE TO LAV LEAK-FRAME REPAIR. THIS IS A MAJOR REPAIR. REMOVED AND REPLACED FR 410 IN REF. TO MD11 SRM 51-31-01-0G; 51-33-01-0G; 51-35-01-0G; DOUGLAS DRAWING ABA7223 CONF-505. BLENDED MINOR CORROSION IN REF. TO MD11 SRM 53-00-00-2R; FIGURE 205.
Earlier reports · 1997–2022 · 365 reports
2022
Part: SKIN — CRACKED (ZONE 500) · airframe 94,880 hrs · 22,942 cycles
02 EACH FASTERNER HOLES #10 AND #12 FOUND CRACK INDICATION DURING OPEN - HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 02 EACH FASTENER HOLES #10 AND #12 BUSHING REPAIR CARRIED OUT AS PER MD 11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLES AFTER BUSHING REPAIR COMPLETION AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLES AS PER MD 11 SRM 57-20-02-2R REPAIR 5 TABLE 201 FIGURE 202 / REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: BULKHEAD — CRACKED (ZONE 100) · airframe 94,880 hrs · 22,942 cycles
CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LEFT HAND SIDE DOUBLER CUTOUT ( SPOILER MIXER QUADRANT ACCESS LOCATION) FOUND CRACK. CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LEFT HAND SPOILER MIXER QUADRANT ACCESS LOCATION AT STATION 1381 CRACKED DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. DOUBLER FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AEA 0526 REVISION NC. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: LONGERON — CORRODED (BS 1611 L48R) · corrosion level 2 · airframe 94,880 hrs · 22,942 cycles
LOWER CENTER CARGO COMPARTMENT BILGE STATION 1611, LONGERON 48 RIGHT HAND FOUND CORROSION. CORROSION AT LOWER CENTER CARGO COMPARTMENT BILGE STATION 1611, LONGERON 48 RIGHT HAND REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R REPAIR GENERAL FIGURE 205. REPAIR CARRIED OUT AT LOWER CENTER CARGO COMPARTMENT BILGE STATION 1571 TO STATION 1631, LONGERON 48 RIGHT HAND AS PER E.A.#:1-5310-T0370588 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 94,880 hrs · 22,942 cycles
CENTER ACCESSORY COMPARTMENT AT APPROXIMATELY STATION 1159 LONGERON 51 RIGHT FOUND CORROSION. CENTER ACCESSORY COMPARTMENT AT APPROXIMATELY STATION 1159 LONGERON 51 RIGHT WITH EXFOLIATION CORROSION REMOVED AND REPLACED AS PER SRM 51-31-01-0G. LONGERON 51 RIGHT FABRICATED AS PER DOUGLAS DRAWING AAA 7086 REVISION NEW BY MACHINING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/16/2022
Part: DOUBLER — CRACKED (LT WING LE) · airframe 94,880 hrs · 22,942 cycles
LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 669 FOUND CRACK. LEFT WING - FIXED LEADING EDGE AT STATION XOS 669 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022
Part: DOUBLER — CORRODED (ZONE 500) · airframe 94,880 hrs · 22,942 cycles
LEFT WING - FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK. LEFT WING - FIXED LEADING EDGE AT STATION XOS 667 CRACKED RIB DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022
Part: DOUBLER — CRACKED (ZONE 600) · airframe 94,880 hrs · 22,942 cycles
RIGHT WING - FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK. RIGHT WING - FIXED LEADING EDGE AT STATION XOS 667 CRACKED RIB DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022
Part: DOUBLER — CRACKED (ZONE 600) · airframe 94,880 hrs · 22,942 cycles
RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK. RIGHT WING - FIXED LEADING EDGE AT STATION XOS 655 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022
Part: DOUBLER — CRACKED (ZONE 500) · airframe 94,880 hrs · 22,942 cycles
LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 664 FOUND CRACK. LEFT WING - FIXED LEADING EDGE AT STATION XOS 664 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022
Part: DOUBLER — CRACKED (ZONE 500) · airframe 94,880 hrs · 22,942 cycles
LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK. LEFT WING - FIXED LEADING EDGE AT STATION XOS 655 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022
Part: SKIN — CRACKED (ZONE 500) · airframe 94,880 hrs · 22,942 cycles
LEFT WING - DROOPED LEADING EDGE UPPER SKIN FOUND CRACK AT STATION XDLE 319. LEFT WING - DROOPED LEADING EDGE UPPER AT STATION XDLE 319 CRACKED SKIN REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 5 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022
Part: SKIN — CHAFED (LT WING) · airframe 94,880 hrs · 22,942 cycles
LEFT WING - WING ANTI - ICE TELESCOPIC DUCT CUTOUT EXISTING REPAIR DOUBLER FOUND CHAFFED AT STATION XOS 464. LEFT WING - WING ANTI - ICE TELESCOPIC DUCT CUTOUT AT STATION XOS 464 CHAFFED EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01-OG AND PERFORMED REPAIR AS PER SRM 57-40-01-2R REPAIR 10 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022
Part: SKIN — GOUGED (LT WING SLAT) · airframe 94,880 hrs · 22,942 cycles
LEFT WING - NUMBER 2 SLAT INNER SURFACE FOUND GOUGE AT STATION XIS 267. LEFT WING - NUMBER 2 SLAT ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-80-20-4. CONTROL SURFACE ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-80-20-5. REFER SNRM NUMBER N01076 FOR WORK DETAIL. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022
Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 93,969 hrs · 22,704 cycles
HYD 2 OFF AT 2.5 GALLONS AND HYD 2 FAIL AT 1.0 GALLON. QUALITY DROPPED TO 0.0. INSTALLED #2 ENGINE LEFT PUMP(UPPER) UPTO AND INCLUDING PARA 3.F.(3) MD11 AMM 29-11-20-4-1. TO END LEAK AND OP`S CHECK GOOD OK FOR SERVICE. REMOVED, INSPECTED, AND REPLACED CASE DRAIN AND PRESSURE FILTERS #2 ENGINE HYD MANIFOLD UPTO AND INCLUDING PARA 3.G.(3).
Part: PLUG — LEAKING (N/A) · airframe 93,805 hrs · 22,670 cycles
PDIS 582 29-02 2562 14APR22 ANC FACT U RECEIVED A HYD 2 OFF. HYD 2 QUANTITY 2.4. ***EMERGENCY DECLARED*** ENT BY: 316582 RPT BY:316582 FACT 14APR22 09:38 ANC U FOUND CASE RELIEF VALVE PLUG ON HYDRAULIC PUMP LOOSE. RESEALED AND RESECURED PLUG, OPS AND LEAK CHECK GOOD. REF MD-11 AMM 29-11-20-4-1 FOUND CASE RELIEF VALVE PLUG ON HYDRAULIC PUMP LOOSE. RESEALED AND RESECURED PLUG, OPS AND LEAK CHECK GOOD. REF MD-11 AMM 29-11-20-4-1
2021
Part: TUBE — LEAKING (HYD SYSTEM) · airframe 91,222 hrs · 21,930 cycles
HYD 1 QTY LO ON SHORT FINAL. QTY WENT DOWN TO 1.4 FOUND #1 ENGINE UPPER CASE DRAIN TUBE WITH A HOLE CHAFFED THROUGH. REPLACED DRAIN TUBE. SERVICED THE RESERVOIR, RAN ENGINE AND CYCLED FLIGHT CONTROLS FOR LEAK CHECK
Part: FUEL CONTROL — FAILED (NR 3 ENGINE) · airframe 91,144 hrs · 21,902 cycles
RIGHT AFTER TAKEOFF ,HEARD ABOUT 5 COMPRESSOR STALLS FROM THE NO 3 ENGINE ALSO NOTICED FLASHES OUT OF THE RIGHT WINDOW . N1 EGT SHOWED FLUCUATIONS UNTIL POWER WAS REDUCED TO CLIMB POWER TAKEOFF WAS MAX THRUST ENGINE OPERATED NORMAL REMAINDER OF FLIGHT DID NOT SHUT THE ENGINE DOWN NO ENGINE PARAMETERS EXCEEDED. REMOVED AND REPLACED NUMBER 3 ENGINE HMU IAW AMM 73-21-01-4-1. REQUIRES APPLICABLE ADJUSTMENT TEST AND PROCEDURES PER AMM TASK 71-00-00-700-809. PERFORMED GROUND ILDE CHECK, FLIGHT IDLE CHECK AND MAX POWER ASSURANCE CHECK ENG RUN PER MD11 AMM 71-00-00-5-1, ALL PARAMETERS ARE WITHIN LIMITS. A/C OK FOR SERVICE.
Part: DETECTOR — FAILED (BLEED SYSTEM) · airframe 91,099 hrs · 21,886 cycles
APPOXIMATELY 5 HOURS ENROUTE FIRST INDICATION OF BLEED AIR PROBLEM WAS LEVEL ONE ALERT "AIR SYS 2 OFF". FOUND THE ESC HAD LOCKED OUT THE MFC FROM PREVIOUS FAULTS. RESET THE ESC FAILURES AND THEN TESTED THE MFC AND ALL TEST PASSED WITHOUT ANY SENSOR FAILURES OR OTHER FAILURES AFTER THE NEW MFC WAS INSTALLED. PERFORMED THE AIR TEST 3 MORE TIMES AND STILL NO FAILURES. PERFORMED ENG RUN WITH ALL 3 ENGINES AND ISOLATED EACH MANIFOLD AND ALL SYSTEMS OPERATE NORMAL WITH GOOD PRESSURE AND NO FAILURES OR SHUTDOWNS. AFTER SHUTDOWN PERFORMED AIR SYSTEM TEST AGAIN AND STILL NO FAILURES. ALL TEST PERFORMED PER MD11 AMM 21-08-00-0 AND 36-23-01-5 AND MD11 JRH.
2020
Part: SEAT TRACK — CORRODED (BS 430-450) · airframe 89,879 hrs · 21,552 cycles
FORWARD CABIN RT SEAT TRACK STATION 430 TO STATION 450 , X = - 85.5 FOUND WITH CORROSION. CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED WITH NEW SEAT TRACK FROM EXISTING SPLICE STATION 484.784 TO END OF PART STATION 414.784 X= -85.5 AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: SEAT TRACK — CRACKED (BS 1217) · airframe 89,879 hrs · 21,552 cycles
CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CRACKED AT STATION 1217 , X = - 75.25. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO EXISTING SPLICE STATION 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: FRAME — DENTED (BS 1601) · airframe 89,879 hrs · 21,552 cycles
CABIN - MAIN DECK UPON REMOVAL OF UPPER SIDEWALL LINER FOR INSPECTION ACCESS ( WORK CARD T1-5310-71733 A P2I ) FOUND FRAME DENTED AT STATION 1601 , LONGERON 12 LEFT . CABIN - MAIN DECK CARGO COMPARTMENT , DENTED FRAME AT STATION 1601 , LONGERON 12 LEFT REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2 . 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: DOUBLER — CORRODED (RT WING) · corrosion level 2 · airframe 89,879 hrs · 21,552 cycles
RIGHT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XW=227 REAR SPAR AREA FOUND CORROSION. RIGHT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XW=227 REAR SPAR AREA CORROSION REMOVED AND REPAIRED, AS PER EA NR 1-5730-T0355692 PART 1 TITLE: WINGS-PLATES AND SKINS-RT WING-CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN XW 212 AND XW 229.5, 229.5. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: DOUBLER — CORRODED (RT WING) · corrosion level 2 · airframe 89,879 hrs · 21,552 cycles
RIGHT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER INBOARD SIDE APPROXIMATE STATION XW 212.2972 AREA FOUND CORROSION. RIGHT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER INBOARD SIDE APPROXIMATE STATION XW 212.2972 AREA CORROSION, REMOVED. FOUND EXCEED LIMIT AS 0.100 INCHES MAXIMUM MATERIAL REMOVAL FOR GENERAL CORROSION. REMOVAL PER SRM 57-20-01-1A FIGURE 101 ALLOWABLE DAMAGE 1. REPAIRED, AS PER EA NR 1-5730-T0355692 PART 1 TITLE: WINGS-PLATES AND SKINS-RT WING-CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN XW 212 AND XW 229.5. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: DOUBLER — CORRODED (RT WING) · airframe 89,879 hrs · 21,552 cycles
RIGHT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XORS 282 AREA FOUND CORROSION.
Part: DOUBLER — CORRODED (RT WING) · airframe 89,879 hrs · 21,552 cycles
RIGHT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER INBOARD SIDE APPROXIMATE STATION XORS 254 AREA FOUND CORROSION.
Part: DOUBLER — CORRODED (RT WING) · corrosion level 2 · airframe 89,879 hrs · 21,552 cycles
AGING AIRCRAFT, EXISTING REPAIR AT RIGHT HAND WING, UPPER SURFACE MAIN LANDING GEAR SUPPORT DOUBLER (DIAMOND DOUBLER) STATION XW 212.2972. EXISTING REPAIR AT RIGHT HAND WING UPPER SURFACE MAIN LANDING GEAR SUPPORT DOUBLER STATION XW 212.2972. EVALUATED FOUND VISIBLE CORROSION DAMAGE AT REPAIR AREA. CORROSION REMOVED AND REPAIRED PER EA NR 1-5730-T0355692 PART 1 TITLE: WINGS-PLATES AND SKINS-RT WING-CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN XW 212 AND XW 229.5, REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM N00077 FOR WORK DETAILS ACCOMPLISHMENT. EO 1-5100-7-5001 B6 PART1 TITLE: STRUCTURES-REPAIR CATALOG-MD-11-REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: DOUBLER — CORRODED (RT WING) · corrosion level 2 · airframe 89,879 hrs · 21,552 cycles
RIGHT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XW 229.5 AREA FOUND CORROSION. RIGHT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XW 229.5 AREA CORROSION REMOVED. FOUND EXCEED LIMIT AS 0.100 INCHES MAXIMUM MATERIAL REMOVAL FOR GENERAL CORROSION. REMOVAL PER SRM 57-20-01-1A FIGURE 101 ALLOWABLE DAMAGE 1 AND REPAIRED, AS PER EA NR 1-5730-T0355692 PART 1 TITLE: WINGS-PLATES AND SKINS-RT WING-CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN XW 212 AND XW 229.5. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: DOUBLER — CORRODED (RT WING) · airframe 89,879 hrs · 21,552 cycles
RIGHT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XORS 275 AREA FOUND CORROSION.
Part: DOUBLER — CORRODED (LT WING MLG) · airframe 89,879 hrs · 21,552 cycles
LEFT WING, UPPER SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER, OUTBOARD SIDE APPROXIMATELY XORS 279 AREA FOUND CORRODED. LEFT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XW=229.5 BELOW STRINGER 1, 4 INCHES AREA CORROSION. REMOVED AND REPAIRED, AS PER EA NR 1-5730-T0355659 PART 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: DOUBLER — CORRODED (LT MLG SUPPORT) · airframe 89,879 hrs · 21,552 cycles
LEFT WING, UPPER SURFACE, MAIN LANDING GEAR SUPPORT UPPER DOUBLER, OUTBOARD SIDE, APPROXIMATELY XORS 274 AREA FOUND CORRODED. LEFT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XW=221.5 BELOW STRINGER 1 AREA CORROSION. REMOVED AND REPAIRED, AS PER EA 1-5730-T0355659 PART 1 TITLE: WINGS-PLATES AND SKINS-LT WING-CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN XW 212 AND XW 229.5. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: DOUBLER — CORRODED (LT WING MLG) · airframe 89,879 hrs · 21,552 cycles
LEFT WING UPPER SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER, OUTBOARD AFT SIDE, APPROXIMATELY XORS 277 AREA FOUND CORRODED. LEFT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD AFT SIDE APPROXIMATE STATION XW=221.5 REAR SPAR AREA CORROSION. REMOVED AND REPAIRED, AS PER EA NR 1-5730-T0355659 PART 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: DOUBLER — CORRODED (LT WING MLG) · airframe 89,879 hrs · 21,552 cycles
LEFT WING UPPER SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER, OUTBOARD SIDE, APPROXIMATELY XORS 284 AREA FOUND CORRODED. LEFT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XW 229.5 AREA CORROSION REMOVED FOUND EXCEED LIMIT AS 0.100" MAXIMUM MATERIAL REMOVAL FOR GENERAL CORROSION REMOVAL, PER SRM 57-20-01-1A FIGURE 101 ALLOWABLE DAMAGE 1 AND REPAIRED AS PER EA NR 1-5730-T0355659 PART 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: DOUBLER — CORRODED (LT WING MLG) · airframe 89,879 hrs · 21,552 cycles
LEFT WING, UPPER SURFACE OF MAIN LANDING GEAR SUPPORT UPPER DOUBLER, OUTBOARD SIDE APPROXIMATELY XORS 277 AREA FOUND CORRODED. LEFT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER OUTBOARD SIDE APPROXIMATE STATION XW=229.5 BELOW STRINGER 1, 2 INCHES AREA CORROSION REMOVED AND REPAIRED, AS PER EA 1-5730-T0355659 PART 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: LONGERON — CORRODED (BS 1661-1681) · airframe 89,879 hrs · 21,552 cycles
CENTER CARGO COMPARTMENT - STATION 1661 TO STATION 1681 , LONGERON 52 FOUND CORRODED. CORRODED AREA AT CENTER CARGO COMPARTMENT STATION 1661 TO STATION 1681 LONGERON 52 FOUND OUT OF LIMITS, PER SRM 53-00-05-2R FIGURE 203. REPAIR 1 AND REPAIRED, PER EA 1-5310-T0356267. REPAIR CLASSIFIED MAJOR, PER GMM 6-2-100.
Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 89,879 hrs · 21,552 cycles
CABIN, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NUMBER 231HF TOP SURFACE DELAMINATED AT LEFT HAND STATION 595 TO STATION 675. DELAMINATED FLOOR PANEL 231HF AT CABIN LEFT HAND STATION 595 TO STATION 675 REMOVED, AS PER AMM 53-21-04. FLOOR PANEL 231HF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL 231HF INSTALLED, AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 89,879 hrs · 21,552 cycles
CABIN FLOOR PANEL 231HF TOP SURFACE DAMAGED AT BS 595 TO 675.
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 89,879 hrs · 21,552 cycles
CABIN FLOOR PANEL 262BF FOUND DAMAGED AT RH STA 1159-STA 1239
Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 89,879 hrs · 21,552 cycles
CABIN, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NUMBER 262BF FOUND DELAMINATED AT RIGHT HAND STATION 1159 TO STATION 1239. DELAMINATED FLOOR PANEL 262BF AT CABIN RIGHT HAND STATION 1159 TO STATION 1239 REMOVED, AS PER AMM 53-21-04. FLOOR PANEL 262BF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL 262BF INSTALLED, AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR, AS PER GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (BS 755) · airframe 89,879 hrs · 21,552 cycles
MAIN DECK SEAT TRACK CROWN DAMAGED AT BS 755 , X = 8.5 .
Part: DOUBLER — CRACKED (RT WING) · airframe 89,879 hrs · 21,552 cycles
RIGHT WING, LEADING EDGE CAVITY AT XOS 757, BEADED DOUBLER CRACKED. DOUBLER REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED (LT WING LE) · airframe 89,879 hrs · 21,552 cycles
DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE LEFT FIXED LEADING EDGE SKIN, AT CORNER NUMBER 13, SLAT TRACK NR 10 CUT OUT AFT INBOARD CORNER FOUND CRACKED APPROXIMATELY 0.4 INCHES IN LENGTH AT XOS 657. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FINGER DOUBLER — DETACHED (RT WING TE) · airframe 89,879 hrs · 21,552 cycles
RIGHT WING TRAILING EDGE FINGER DOUBLER AT 641KB FOUND DELAMINATED. RT WING, TRAILING EDGE FINGER DOUBLER AT 641KB STATION XW 375.34 REPAIR CARRIED OUT, AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 89,879 hrs · 21,552 cycles
LEFT WING, LEADING EDGE CAVITY AT XOS 500 BEADED DOUBLER FOUND CRACKED. DOUBLER REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 89,879 hrs · 21,552 cycles
RIGHT WING - LEADING EDGE CAVITY AT XOS 751 BEADED DOUBLER FOUND CRACKED. RT WING, LEADING EDGE CAVITY AT STATION XOS=751 DOUBLER REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FRAME — DENTED (BS 1621) · airframe 89,879 hrs · 21,552 cycles
CABIN, MAIN DECK CARGO COMPARTMENT FRAME DENTED AT STATION 1621, LONGERON 12 RT. CABIN, MAIN DECK CARGO COMPARTMENT AT STATION 1621, LONGERON 12 RT, DENTED FRAME, REPAIRED AS PER SRM 53-00-07 -2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED-INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: FRAME — DENTED (BS 1621) · airframe 89,879 hrs · 21,552 cycles
CABIN - MAIN DECK CARGO COMPARTMENT FRAME DENTED AT STATION 1621 , LONGERON 12 RIGHT
Part: FAN — FAILED (CABIN AIR) · airframe 89,704 hrs · 21,505 cycles
ON DESCENT INTO KOAK PASSING THROUGH APPROX FL280 STARTED SMELLING AN ACRID SMELL ACCOMPANIED BY A RUMBLING SOUND. THE FO SAID HE FELT VIBRATIONS UNDER HIS FEET. THE SMELL INCREASED, SO WE DECLARED AN EMERGENCY. AS WE GOT BELOW 10,000FT AND THE PLANE DEPRESSURIZED, THE SMELL DISSIPATED. FOUND ELECTRICAL SMELL COMING FROM NR 3 AVIONICS RACK FAN, DEFERRED NR 3 FAN SEE WRI 21-26/0461. PERFORMED PACK BURN OUT, PER AMM 21-53-00-7. FOUND WHENEVER APU AIR WAS SELECTED A SMELL OF BURNT OIL COULD BE DETECTED. DEFFERED APU SEE WRI 49-90/0464. REPLACED 1 AND 2 PACK COALESCER BAGS, PER AMM 21-53-00-7. WITH ALL THREE ENGINES RUNNING AND APU AIR NOT SELECTED NO BRUNT OIL OR ELECTRICAL SMELLS ARE DETECTED.
2019
Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 86,874 hrs · 20,647 cycles
EMERGENCY LIGHT BAT 1 LO ALERT DURING PRE-FLIGHT. T/S PER MD11 FIM 33-52-00-01. ALL TESTS PASS. NO HISTORY FOR OVER 30 DAYS. PERFORMED ADJ/TEST PER MD11 AMM 33-50-00-5. OPS CK GOOD.
2018
Part: DOUBLER — CORRODED (LT WING) · corrosion level 2 · airframe 85,231 hrs · 20,127 cycles
LT WING FOUND UNDERWING LOWER FRONT SPAR DOUBLER AT STA XOS 1198.587 JUST AFT OF NR 8 SLAT CAVITY, WITH CORROSION AS MARKED. LT WING LOWER FRONT SPAR DOUBLER AT STA XOS 1198.587 AFT OF NR 8 SLAT CAVITY CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 12. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. CORROSION AT STA XOS 1198.587, LT WING LOWER FRONT SPAR DOUBLER FOUND EXCEEDED LIMIT AS PER SRM 57-00-00 REPAIR GENERAL.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,231 hrs · 20,127 cycles
CABIN, RT STA 1541 - 1562, X=-8.5 SEAT TRACK CROWN FOUND DAMAGED. DAMAGED SEAT TRACK CROWN REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1531 TO STA 1591, X= -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED (LT WING) · airframe 85,231 hrs · 20,127 cycles
1 EA FASTENER HOLE NR 36 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 36 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B'.
Part: SKIN — CRACKED (LT WING) · airframe 85,231 hrs · 20,127 cycles
1 EA FASTENER HOLE NR 6 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 6 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B'.
Part: SKIN — CRACKED (LT WING) · airframe 85,231 hrs · 20,127 cycles
1 EA FASTENER HOLE NR 32 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 32 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B'.
Part: SKIN — CRACKED (RT WING) · airframe 85,231 hrs · 20,127 cycles
1 EA FASTENER HOLE NR 7 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 7 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B'.
Part: SKIN — CRACKED (LT WING) · airframe 85,231 hrs · 20,127 cycles
1 EA FASTENER HOLE NR 9 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 9 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B'.
Part: SKIN — CRACKED (LT WING) · airframe 85,231 hrs · 20,127 cycles
1 EA FASTENER HOLE NR 15 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 15 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B'.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,231 hrs · 20,127 cycles
CABIN LT STA 1521, X=8.5 SEAT TRACK CROWN FOUND DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-83 TO STA 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: SKIN — CRACKED (RT WING) · airframe 85,231 hrs · 20,127 cycles
1 EA FASTENER HOLE NR 27 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 27 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY 'B'.
Part: SKIN — CRACKED (RT WING) · airframe 85,231 hrs · 20,127 cycles
RT WING FOUND SLAT TRACK NR 12 CUTOUT CORNER CRACKED, STA XOS 774 RT WING SLAT TRACK NR 12 CUTOUT CORNER, STA XOS 774 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED (LT WING) · airframe 85,231 hrs · 20,127 cycles
LT WING FOUND SLAT TRACK NR 14 CUTOUT CORNER CRACKED, STA XOS 881 LT WING SLAT TRACK NR 14 CUTOUT CORNER, STA XOS 881 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CRACKED (RT WING) · airframe 85,231 hrs · 20,127 cycles
RT WING FOUND SLAT TRACK NR 14 CUTOUT CORNER CRACKED, STA XOS 889 RT WING SLAT TRACK NR 14 CUTOUT CORNER, STA XOS 889 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 85,231 hrs · 20,127 cycles
AFT ACCESSORY COMPARTMENT RT FUSELAGE SKIN AT STA 2163.685 LONGERON 33R-35R, FOUND CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. RT FUSELAGE SKIN AT STA 2163.685 LONGERON 33R - LONGERON 35R CORROSION REMOVED AS PER 51-21-01-0G AND FOUND OUT OF LIMIT AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. MATERIAL THICKNESS: 0.095", MATERIAL REMOVED: 0.034" AND REMAINING THICKNESS: 0.061"
Part: DOUBLER — CRACKED (LT WING) · airframe 85,231 hrs · 20,127 cycles
LT WING FOUND LEADING EDGE CAVITY BEADED DOUBLER CRACKED AT STA XOS 585. LT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 585 CARRIED OUT REPAIR 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 85,231 hrs · 20,127 cycles
LT WING FOUND LEADING EDGE CAVITY WITH BEADED DOUBLER CRACKED AS MARKED AT STA XOS 695. LT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 695 CARRIED OUT REPAIR 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 85,231 hrs · 20,127 cycles
LT WING FOUND LEADING EDGE CAVITY WITH BEADED DOUBLER CRACKED AS MARKED AT STA XOS 626. LT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 626 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,231 hrs · 20,127 cycles
CABIN LT STA 1121, X=8.5 SEAT TRACK FOUND CORROSION. CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1089 TO STA 6-0, X=8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
2017
Part: CABLE — BROKEN (L1 DOOR) · airframe 83,225 hrs · 19,529 cycles
L1 DOOR MAIN AFT DRIVE CABLE BROKEN. REF IPC 52-11-05-01, ITEM 312 IS UPPER CABLE THAT IS BROKEN. REMOVED AND REPLACED AFT UPPER L1 DOOR DRIVE CABLE REF AMM 52-11-03-4 UP TO AND INCLUDING STEP E(7).
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 82,577 hrs · 19,373 cycles
EMERGENCY LIGHT TEST DID NOT PASS. CARRIED OUT ADJUSTMENT TEST ON EMERGENCY LIGHTS IAW AMM 33-50-00-5. CHECKED GOOD.
Part: WARNING LIGHT — FALSE ACTIVATION (BATTERY PACK) · airframe 82,390 hrs · 19,305 cycles
DURING A PREFLIGHT, RECEIVED AN ALERT FOR THE EMERGENCY LIGHT BATTERY 1 LOW. COMPLIED WITH FIM 33-51-02-00 EMERGENCY LIGHTS BATTERY POWER SUPPLY TEST. NO FAULTS NOTED, ACFT OK FOR SERVICE. NO HISTORY IN PAST 90 DAYS.
Part: GIRT BAR — UNSECURE (L1 DOOR SLIDE) · airframe 82,376 hrs · 19,301 cycles
L1 DOOR GIRT BAR IS LOOSE AND HANGING DOWN. REINSTALLED THE GIRT BAR IAW AMM 25-61-01-4.
Part: HINGE — WORN (CARGO DOOR) · airframe 82,331 hrs · 19,279 cycles
MDC DOOR FWD HINGE HAS PLAY. HINGE SECTION REPLACED.
2016
Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 81,303 hrs · 18,945 cycles
DOOR DISARMED ANNUNCIATOR AT L1 DOOR INOP RELAMPED, OPS CHECKS GOOD.
Part: FEEDER CABLE — DAMAGED (NR 2 GENERATOR) · airframe 81,230 hrs · 18,920 cycles
NR 2 ENGINE GENERATOR FEEDER CABLE BY THE ENGINE ANTI-ICE VALVES ARE DAMAGED.
Part: FEEDER CABLE — DAMAGED (NR 2 ENGINE) · airframe 80,312 hrs · 18,636 cycles
AFT FUSELAGE COMPARTMENT AT BS 2033, DURING DEFECT RECTIFICATION, FOUND ONE FEEDER CABLE FOR ENGINE NR 2 WITH DEEP CUT AND ON EWIRING CLAMP WITH SIGN OF ARCING.
Part: SPAR — CRACKED (ZONE 300) · airframe 80,312 hrs · 18,636 cycles
AFTER PANEL 364RR, EMPENNAGE, INSIDE PANEL 364RR AFT SPAR WEB FOUND CRACK AT STA Y = 2164.
Part: HINGE — CORRODED (LT WING) · airframe 80,312 hrs · 18,636 cycles
LEFT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA, 0.390", FINAL HOLE DIA: 0.407" AND MAXIMUM ALLOWABLE HOLE DIA: 0.391". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326550, PT 1, STEP 1C TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, LT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR GMM 6-2-100. REFER TO WRI #57504780 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD BORE SURFACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.387", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.379", MINIMUM ALLOWABLE THICKNESS: 0.408". REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-T0309816 A PART 2, STEP 1. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.221", FINAL HOLE DIA: 1.225", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326620, PART 1, STEP 1A TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002, RT WING, OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504782 FOR WORK DETAILS.
Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.290", FINAL HOLE DIA: 1.328" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-69360B, PT 5, STEP 1A & 1D. TITLE: WINGS-T/E & T/E DEVICES, RT INBD FLAP HINGE BRACKET ASSY REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57504794 FOR WORK DETAILS.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, PIVOT BORE FOUND, CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.316" AND MAXIMUM ALLOWABLE HOLE DIA: 2.3135". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326550, PT 1, STEP 1B, TITLE : WINGS, FLIGHT SURFACES, EO 1-5750-7-5002-LT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57504780 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT, INBD BORE SURFACE AREA CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.715", MATERIAL REMOVED: 0.003", REMAINING THICK: 0.712". MINIMUM ALLOWABLE THICKNESS: 0.720". REPAIR CARRIED OUT IAW EA 1-5750-T0309816A, PART 2, STEP 1. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (TE FLAP) · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.289", FINAL HOLE DIA: 1.328" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-69360B, PT 5, STEP 1A & STEP 1D, TITLE: WINGS - T/E & T/E DEVICES, RT INBD FLAP HINGE BRACKET ASSY, REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100. REFER TO WRI 57504794 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.221", FINAL HOLE DIA: 1.225", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326620, PART 1, STA 1A TITLE: WINGS-FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO WRI: 57504782 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT CMM 57-44-09. EXISTING HOLE: DIA 0.880". FINAL HOLE: DIA 0.953". MAXIMUM ALLOWABLE HOLE: DIA 0.944", REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-T0309816A, PART 2, STEP 1A. TITLE: WINGS-FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LEFT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.188", FINAL HOLE DIA: 1.235" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-T0323098A, PT 4, STEP 1A & STEP 1D TITLE: WINGS, FLIGHT SURFACES, LT INBD FLAP OTBD HINGE BRACKET BORE INSPECTIONS. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100, REFER TO WRI 57504793. FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RT WING, OTBD FLAP, OTBD FWD HINGE LOWER MOUNT INBD CORRODED. REWORKED AND FOUND, EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.521", FINAL HOLE: DIA 0.613", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-T0309816, PART 2, STEP 1B AND STEP 1: TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP-OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, INBD FLAP OTBD FWD HINGE, WING SIDE, PIVOT BORE FOUND, CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-07. EXISTING HOLE DIA: 2.531", FINAL HOLE DIA: 2.536" AND MAXIMUM ALLOWABLE HOLE DIA: 2.531". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326697A, PT 1, STEP 4 & STEP 6. TITLE: WINGS, FLIGHT SURFACES, RT WING, INBD FLAP, OTBD FORWARD HINGE BRACKET ASSEMBLY. CORROSION REPAIR & PSE 57.55.01.1 INSPECTION ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57504767 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.880", FINAL HOLE: DIA 0.953", MAXIMUM ALLOWABLE HOLE: DIA 0.944". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0309816A, PART 2, STEP 1A. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.391", FINAL HOLE DIA: 0.407" AND MAXIMUM ALLOWABLE HOLE DIA: 0.391". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-T0326550, PT 1, STEP 1C, TITLE : WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-LT WING-OTBD FLAP, OUTBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57504780 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD BORE SURFACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.709", MATERIAL REMOVED: 0.003", REMAINING THICKNESS: 0.706". MINIMUM ALLOWABLE THICKNESS: 0.720". REPAIR CARRIED OUT IAW EA NR 1-5750-T0309816 A PART 2, STEP 1. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.380", FINAL HOLE DIA: 0.407", MAXIMUM ALLOWABLE HOLE DIA: 0.391". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0309816, A PART 2, STEP 1C. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RT WING, OTBD FLAP, OTBD HINGE, WING SIDE, OTBD ACTUATOR ATTACH BORE, CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0309816 A, PART 2, STEP 1D. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.662", FINAL HOLE DIA: 0.699", MAXIMUM ALLOWABLE HOLE DIA: 0.667". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1-5750-T0309816, PART 2, STEP 1E. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.188", FINAL HOLE DIA: 1.235" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0323098A, PT 4, STEP 1A, STEP 1D TITLE: WINGS, FLIGHT SURFACES, LT INBD FLAP, OTBD HINGE BRACKET BORE INSPECTIONS. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100. REFER TO WRI 57504793 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, OTBD FLAP, OTBD HINGE, WING SIDE, INBD ACTUATOR ATTACH BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0309816, A PART 2, STEP 1D. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI:57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.674", FINAL HOLE DIA: 0.691" AND MAXIMUM ALLOWABLE HOLE DIA: 0.667". NEW REPAIR BUSHING, FABRICATED AND INSTALLED IAW EA NR 1-5750-T0326550, PT 1, STEP 1E, TITLE: WINGS - FLIGHT SURFACES, EO NR 1-5750-7-5002, LT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57504780 FOR WORK DETAILS.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 1.247", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326550, PT 1 STEP 1D TITLE WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, LT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57504780 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RT WING, OTBD FLAP, OTBD FORWARD HINGE LOWER MOUNT INBD BORE SURFACE AREA CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.414", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.406", MINIMUM ALLOWABLE, THICKNESS: 0.408", REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-T0309816A, PART 2, STEP 1. TITLE: WINGS, FLIGHT SURFACES, EA 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LEFT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08 EXISTING HOLE DIA: 1.225", FINAL HOLE DIA: 1.231", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326615, PART 1, STEP 1A TITLE: WINGS-FLIGHT SURFACES A, EO 1-5750-7-5002, LEFT WING, OTBD FLAP, INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504781 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.581", FINAL HOLE: DIA 0.613", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0309816A, PART 2, STEP 1B AND STEP 1. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LEFT WING, OTBD FLAP, INBD FORWARD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.218", FINAL HOLE DIA: 1.224", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326615, PART 1, STEP 1A TITLE: WINGS-FLIGHT SURFACES, EO 1-5750-7-5002, LT WING, OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504781 FOR WORK DETAILS.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE FOUND CORROSION. CORROSION AT RT WING, OTBD FLAP, OTBD FORWARD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE, NR 7 HOLE, REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.424", FINAL HOLE DIA: 0.456". MAXIMUM ALLOWABLE HOLE DIA: 0.391", REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0309816, A PART 2, STEP 1C. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-RT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57506779 FOR WORK DETAILS.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LEFT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 1.238", FINAL HOLE DIA: 1.244" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326550, PT 1, STEP 1D, TITLE: WINGS, FLIGHT SURFACE, EO 1-5750-7-5002, LT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57504780 FOR WORK DETAILS.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
LEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.618", FINAL HOLE DIA: 0.645" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326550, PT 1, STEP 1 & STEP 1A TITLE: WINGS, FLIGHT SURFACES, EO1-5750-7-5002. LEFT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57504780 FOR WORK DETAILS.
Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 80,312 hrs · 18,636 cycles
DURING HFEC INSPECTION CARRIED OUT ON REAR SPAR CAP RT FORWARD FLANGE UPPER SECTION CRACKED. APPROXIMATE 0.50 INCH IN LENGTH AS MARKED AT STA Y=2164. CRACKED AREA REPAIRED PER EA NR 1-5530-T0326616 PT 1 TITLE: AD 98-25-15 - STABILIZERS - VERTICAL STABILIZER. REAR SPAR P/N: AJC7515-501. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 80,312 hrs · 18,636 cycles
DURING HFEC INSPECTION, CARRIED OUT ON REAR SPAR CAP LT FORWARD FLANGE UPPER SECTION FOUND CRACKED. CRACK APPROXIMATE 2.0 INCHES IN LENGTH AS MARKED AT STA Y =2164. CRACKED AREA REPAIRED PER EA NR 1-5530-T0326617 PT 1 TITLE: AD 98-25-15 - STABILIZERS - VERTICAL STABILIZER. REAR SPAR P/N: AJC7515-501 FORWARD FLANGE RADIUS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK, AFT CABIN LT FLOOR SUPPORT AT STA 1887-2007, X=57 FOUND CORROSION AS MARKED.
Part: STRINGER — CRACKED (LT WING) · airframe 80,312 hrs · 18,636 cycles
LEFT WING, LT FIXED L/E AT STA XOS 669, STR FOUND CRACKED AS MARKED.
Part: SKIN — GOUGED (RT WING) · airframe 80,312 hrs · 18,636 cycles
TO COMPLY WITH EA 1-5730-T0320378, PART 4. WINGS, PLATES AND SKIN GOUGED AT STA XIS 250-XIS 256 APPROXIMATELY 8" FWD OF AFT EDGE L/E SKIN, RT WING.
Part: DOUBLER — CRACKED (RT WING) · airframe 80,312 hrs · 18,636 cycles
RT WING, RT L/E AT STA XOS 626 BEADED DOUBLER FOUND CRACKED AS MARKED.
Part: DOUBLER — CRACKED (RT WING) · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, RT L/E AT STA XOS 788.5 RIB DOUBLER FOUND CRACKED AS MARKED.
Part: STRINGER — CRACKED (RT WING) · airframe 80,312 hrs · 18,636 cycles
RIGHT WING, RT L/E AT STA XOS 669, STRINGER FOUND CRACKED AS MARKED.
Part: DOUBLER — CRACKED (RT WING) · airframe 80,312 hrs · 18,636 cycles
RT WING, RT L/E AT STA XOS 639 BEADED DOUBLER FOUND CRACKED AS MARKED.
Part: FRAME — DENTED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
CABIN - LT STA 1761, LONGERON L-11L FRAME FOUND DENT.
Part: FRAME — DENTED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
CABIN - RT STA 1741, LONGERON L-11R FRAME FOUND DENT.
Part: DOUBLER — CRACKED (LT WING) · airframe 80,312 hrs · 18,636 cycles
LT WING L/E AT STA XOS 645 BEADED DOUBLER FOUND CRACKED AS MARKED. CRACKED DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 80,312 hrs · 18,636 cycles
LEFT WING L/E AT STA XOS 731 BEADED DOUBLER FOUND CRACKED AS MARKED. CRACKED DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
CENTER CARGO COMPARTMENT, BILGE AREA FOUND LONGERON 52, STA 5-85, CORRODED AS MARKED.
Part: FRAME — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
CABIN -RT STA 1761, LONGERON L-11R FRAME FOUND CRACKED.
Part: DOUBLER — CRACKED (LT WING) · airframe 80,312 hrs · 18,636 cycles
LEFT WING L/E AT STA XOS 669 BEADED DOUBLER FOUND CRACKED AS MARKED. CRACKED DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK RT FLOOR SEAT TRACK AT STA 1285, X=-8.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1264 TO STA 1311 X= -8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK RT FLOOR SEAT TRACK AT STA 1425, X=-47.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1390 TO STA 1431 X = -47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK LT FLOOR SEAT TRACK AT STA 755, X= 8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 745-STA 785 X= 8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,312 hrs · 18,636 cycles
MAIN DECK, AFT CABIN RT FLOOR SUPPORT AT STA 1887 - STA 2007, X=-25, FOUND CORROSION AS MARKED. R & R WITH NEW FABRICATED FLOOR SUPPORT IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7087, REV P. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: BEAM — CRACKED (L3 DOOR) · airframe 80,312 hrs · 18,636 cycles
CABIN-L3 DOOR PLUG NR 7 FWD STOP FITTING BEAM FOUND CRACKED. R & R WITH NEW STOP FITTING BEAM IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK LT FLOOR SEAT TRACK AT STA 755, X=47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR NR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK LT FLOOR SEAT TRACK AT STA 635, X= 8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 645 X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK LT FLOOR SEAT TRACK AT STA 635, X= 47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665X=47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: WEB — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25 TO 1315.42, LONGERON L26L TO L27L FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201 REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK RT FLOOR SEAT TRACK AT STA 635, X=-8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625-STA 645 X= -8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK RT FLOOR SEAT TRACK AT STA 5-5, X= -27.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63 X= -27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: WEB — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX AT STA 1250.75 TO 1256.75, LONGERON L26R-L27R, FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201. REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK LT FLOOR SEAT TRACK AT STA 5-5, X= 27.5, FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63 X=27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK LT FLOOR SEAT TRACK AT STA 1643, X= 8.5, FOUND CORROSION AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1570 TO STA 1651 X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: WEB — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX AT STA 1250.75 TO 1256.75, LONGERON L26L TO L27L, FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201. REPAIR NR 3 AND EA 1-5310-T0326798A, PT 1 TITLE: FUSELAGE MAIN FRAME, CENTER FUSELAGE, OVERWING PASSENGER DOOR. REPAIR ON FORWARD JAMB LOWER WEB BOX BETWEEN STA 1250.75 AND STA 1256.75. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53104791 FOR WORK DETAILS.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK LT FLOOR SEAT TRACK AT STA 770, X= 74.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 765-STA 783 X=74.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK RT FLOOR SEAT TRACK AT STA 778, X=-74.5 FOUND CORROSION AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 765-STA 818 X= -74.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. COMPLIED WITH EA 1-5320-T0326733 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,312 hrs · 18,636 cycles
MAIN DECK RT FLOOR SEAT TRACK AT STA 635, X=-47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625-STA 645X= -47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,074 hrs · 18,565 cycles
SEAT TRACK DAMAGED AT POSITION 10L & 9L MCD & LOCK POSITION S1539. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-00-52.
Part: LAMP — INOPERATIVE (BOTTLE PRESSURE) · airframe 79,256 hrs · 18,317 cycles
LEFT CABIN DOOR, FWD PRESS TO TEST SLIDE BOTTLE LIGHT INOPERATIVE. REPLACED THE LAMP IN THE L1 EVAC SLIDE REMOTE PRESSURE INDICATOR. OPS CHECKED NORMAL IAW 25-61-04-5.
2015
Part: SWITCH — INOPERATIVE (O2 MASK) · airframe 79,182 hrs · 18,294 cycles
DON O2 MASK COURIER COMPARTMENT FAIL TO ILLUMINATE, DURING PREFLIGHT CHECK. R & R COURIER DON OXYGEN SWITCH PN JMS2109-42-20A IAW SWPM 20-00. OPERATIONS TESTED SATISFACTORY IAW AMM 35-21-07-5. ITEM OK FOR SERVICE.
Part: WIRE HARNESS — CHAFED (CARGO BAY) · airframe 776 hrs · 17,851 cycles
DURING OFF LOAD RAMP, REPORTED CTR CARGO LOADING SYS IS INOPERATIVE. CHECKED & FOUND CTR CARGO LOADING SYS CB LATERAL ROLLERS & LOADING CONTROL, 2 EACH POPPED OUT. TROUBLESHOOTING FOUND WIRE HARNESS AGS 9122-J504 CHAFING WITH PANEL STRINGER, CAUSED BURNED WIRES 11 EACH. CTR COMPARTMENT CARGO HANDLING SYS INOPERATIVE. COMPLIED WITH EA 1-2497-T0317943 PART 1 FOR WIRING. TEMPORARY REPAIR & COMPLIED WITH EA 1-5320-T0317946 PART 1 FOR CLOSURE PANEL AT STATION 1701 HARNESS CHAFING DAMAGE.
Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 768 hrs · 17,636 cycles
AFTER SWITCHING EMER POWER TO ARM DURING PREFLIGHT, WE RECEIVED A LEVEL ONE, EMER PWR TST FAIL, ALERT. CYCLED BATTERY CHARGER CB'S & PERFORMED RTS OF EPCU IAW AMM 24-08-01-5. ALL CHECKED NORMAL AT THIS TIME. PERFORMED EMER POWER TEST IAW AMM 24-24-00-5. OPERATIONS CHECKED NORMAL AT THIS TIME. ACFT OK FOR CONTINUED SERVICE.
2014
Part: LAMP — INOPERATIVE (PRESS TO TEST) · airframe 76,484 hrs · 17,520 cycles
R1 DOOR EVACUATION SLIDE PRESS TO TEST SWITCH IS INOPERATIVE. R & R LAMP.
Part: COVER — DISLODGED (R1 DOOR) · airframe 75,408 hrs · 17,179 cycles
R1 DOOR SLIDE COVER IS DISLODGED FROM DOOR. REINSTALLED EVACUATION SLIDE RAFT & CONTAINER. ALL TESTS SATISFACTORY.
Part: SKIN — DAMAGED (LT WING) · airframe 75,251 hrs · 17,126 cycles
AGING ACFT LT WING LE UPPER SURFACE FOUND EXISTING REPAIR AT APPROXIMATELY STATION XIS 247. EVALUATED AND FOUND DAMAGED LEFT WING LEADING EDGE UPPER SURFACE AT STA XIS 247. CARRIED OUT REPAIR AS PER SRM 57-40-02 FIGURE 201 REPAIR 8 REV 55 EO 1-5100-7-5001 B4 PART 1.
Part: SKIN — DELAMINATED (FLAP VANE) · airframe 75,251 hrs · 17,126 cycles
RIGHT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM STATION XIFH 127.800 TO XIFH 216.300. RT WING INBOARD FLAP VANE ASSEMBLY R&R AS PER AMM 27-50-22-4 REVISION 79 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-830-801 REVISION 79. FOUND SATISFACTORY REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 122.
Part: DOUBLER — CRACKED (LT WING) · airframe 75,251 hrs · 17,126 cycles
LEFT WING LEADING EDGE LOWER ACCESS CUTOUT FOUND DOUBLER CRACKED AT APPROXIMATE STATION XOS 602. CRACKED DOUBLER R&R IAW DRAWING ARB2933 REV T AND SRM 51-31-01 REV 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.
Part: FRAME — DENTED (FUSELAGE) · airframe 75,251 hrs · 17,126 cycles
CABIN MAIN CARGO COMPARTMENT LT STATION 1741, LONGERON 12LH SIDEWALL FRAME DENTED. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.
Part: FRAME — DENTED (FUSELAGE) · airframe 75,251 hrs · 17,126 cycles
CABIN MAIN CARGO COMPARTMENT RT STATION 1641 LONGERON 12RT SIDEWALL FRAME DENTED. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.
Part: DOUBLER — CRACKED (RT WING) · airframe 75,251 hrs · 17,126 cycles
RIGHT WING LE CAVITY BEADED DOUBLER FOUND CRACKED AT APPROXIMATE STATION XOS 910. CARRIED OUT REPAIR AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 55 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.
Part: DOUBLER — CRACKED (RT WING) · airframe 75,251 hrs · 17,126 cycles
RIGHT WING LE CAVITY BEADED DOUBLER FOUND CRACKED AT APPROXIMATE STATION XOS 669. CARRIED OUT REPAIR AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.
Part: SKIN — CRACKED (LE SLAT) · airframe 75,251 hrs · 17,126 cycles
RIGHT WING DROOP LE UPPER SURFACE FOUND CRACKED APPROXIMATELY 1.5 INCH IN LENGTH AT FASTENER HOLE AT STATION XDLE 329.774. CRACKED ON UPPER SURFACE AT RT WING DROOP LE AT STATION XDLE 329.774. CARRIED OUT REPAIR IAW SRM 57-40-01 FIGURE 201 REPAIR 5 REVISION 55 REPAIR. CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.
Part: SKIN — CRACKED (RT WING) · airframe 74,963 hrs · 17,032 cycles
DURING WALK AROUND FOUND SUSPECTED CRACK IN RT WING AROUND SLAT DRIVE MECHANISM ACCESS DOOR. HFEC INSPECTED CRACK INDICATED IAW SOPM 20-30-00. REMOVED DAMAGE IAW SRM 57-40-02 REPAIR 7. PERFORMED HFEC OF CUT OUT AREA ON RT WING TO ENSURE CRACK REMOVAL IAW NTM PT6. FABRICATED REPAIR PARTS IAW SRM 57-40-02 FIG 202. REPAIRED RT WING SLAT DRIVE ACCESS DOOR IAW SRM 57-40-02 REPAIR 7.
Part: GUIDE — BROKEN (LT MLG) · airframe 74,805 hrs · 16,974 cycles
DURING CLIMB OUT 250 KIAS, RECEIVED RED WARNING LIGHTS ON NOSE GEAR & LT MAIN PRIMARY LIGHTS. SLOWED TO 230KIAS RECEIVED LIGHTS PRIMARY & SECONDARY. ACCOMPLISHED CHECKLIST, CYCLED GEAR, ALL LIGHTS EXTINGUISHED. ON POST FLIGHT INSPECTION FOUND BRAKE HOSE GUIDE BROKEN & HANGING FROM HOSES ON LT MAIN GEAR. SWUNG GEAR AS PRECAUTIONARY IAW AMM 32-31-00-700-802, OPS CHECKED GOOD.
2013
Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 73,093 hrs · 16,391 cycles
R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST, HAS NO INDICATION.
Part: BUTTON — INOPERATIVE (R1 DOOR SLIDE) · airframe 73,093 hrs · 16,391 cycles
R1 ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST, NO INDICATION. R & R AND OPS CHECKED OK IAW MM 25-61-04-4.
Part: COOLING FAN — BURNED (AVIONICS) · airframe 72,762 hrs · 16,295 cycles
HEARD A LOUD FAN SOUND UNDER COCKPIT FLOOR (AVIONICS). SOUND SUDDENLY STOPPED AND A SLIGHT BURNING ODOR IN COCKPIT. NO OTHER INDICATIONS. R & R NR 3 AVIONIC COOLING FAN ASSY IAW AMM 21-26-02-2-1.
Part: ANTI-ICE VALVE — FAILED (WING) · airframe 72,082 hrs · 16,084 cycles
ON DEPARTURE GOT LEVEL 2 WING A/I DISAGREE. COMPLIED WITH QRH FIM 30-11-02 AND FOUND BAD RT WING DE-ICE VALVE. REMOVED INOP VALVE AND INSTALLED A SERVICEABLE VALVE IAW THE AMM 30-11-01-4. PERFORMED OPERATION CHECKS IAW 30-11-00-5 AND NOTED OPS GOOD. NO LEAKS NOTED OK TO CONTINUE.
Part: DOWNLOCK — CRACKED (MLG) · airframe 71,873 hrs · 16,019 cycles
RECEIVED HYD 3 ELEV ALERT AT 1 14 ENROUTE (FL 350). HYD QTY WAS 4.8 QTY CONTINUED DECREASING UNTIL RECEIVING HYD 3 OFF ALERT. (QTY 2.8) QRH REFERENCED AND CONTACTED MOCC. LOST 3 HYD WHEN EXTENDING GEAR. LANDED AND CLEARED RWY. TOWED TO PARKING. FOUND THREADS ON UNLOCK CYLINDER RESTRICTOR CRACKED. R & R UNLOCK ACTUATOR REF AMM 32-33-02-4, SERVICED NR 3 HYD SYS REF AMM 12-13-02-3. PREMATURE REMOVAL/INSTALLATION.
2012
Part: COALESCER BAG — ODOR · airframe 71,033 hrs · 15,809 cycles
DURING PREFLIGHT WITH EXTERNAL AIR CONNECTED, THERE APPEARED AN OILY SMOKE ODOR ENTERED THE COCKPIT. NR 1 PACK TEMP CLIMBED TO 182 FACT. R & R NR 1 PACK COALESCER BAG REF AMM 21-54-05-2. OPERATED NR 1 PACK AND NO OIL ODOR FOUND REF AMM 21-53-20-5. LEAK/OPS CHECKED GOOD.
Part: SKIN — WORN (AILERON) · airframe 70,919 hrs · 15,766 cycles
LEFT WING INBD AILERON ASSY LOWER FORWARD RUB STRIP WORN. SKIN FABRICATED AS PER DRAWING ARC1250 REVISION D. RUBSTRIP (SKIN) REMOVED AND REPLACED AS PER E.A. 1-5750-162367. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
Part: SEAT TRACK — WORN (BS 1531) · airframe 70,919 hrs · 15,766 cycles
MAIN DECK SEAT TRACK WORN AT BS 1531 X=-8. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
Part: PANEL — CORRODED (RT WING) · airframe 70,919 hrs · 15,766 cycles
RT WING T/E PANEL NR 641JB CUT OUT LOWER SURFACE FOUND CORRODED. R & R IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.
Part: SEAT TRACK — CRACKED (BS 1501-1511) · airframe 70,919 hrs · 15,766 cycles
MAIN DECK CARGO SEAT TRACK AT BS 1501 TO 1511 X=-75.25, FOUND CRACKED. REPAIR CARRIED OUT AND INSTALLED AS PER AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
Part: LONGERON — CRACKED (BS 1790 L47R) · airframe 70,919 hrs · 15,766 cycles
CENTER CARGO BS 1790, LONGERON 47R FOUND CRACKED. REPAIRED IAW SRM 53-00-05, REPAIR 1, FIG 202, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.
Part: PANEL — CORRODED (LT WING) · airframe 70,919 hrs · 15,766 cycles
LT WING T/E PANEL 541JB CUTOUT FOUND CORRODED. R & R IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.
2011
Part: ACCESS PANEL — MISSING (NR 1 NACELLE) · airframe 69,229 hrs · 15,287 cycles
ON POST FLIGHT INSPECTION, NOTED ACCESS PANEL MISSING FROM NR1 ENGINE PYLON OTBD SIDE, ACCESS PANEL IS DIRECTLY ABOVE AFT ENGINE MOUNT BOLTS. INSTALLED MISSING ACCESS PANEL AND NUTPLATES AND FASTENERS AS REQUIRED REF SRM 51-31-01.
Part: FIRE LOOP — MALFUNCTIONED (NR 2 NACELLE) · airframe 67,543 hrs · 14,855 cycles
LEVELING AT FL 250 RECEIVED LEVEL 3, ENG NR 2, FIRE INDICATION. COMPLETED PHASE 1 PROCEDURES, DUMPED FUEL AND RETURN TO DEPARTURE. R & R LWR TURB LOOP A RESPONDER IAW MM 26-11-03-4. FINAL CLOSED.
2010
Part: DOUBLER — CORRODED (ZONE 500) · airframe 65,589 hrs · 14,398 cycles
LT WING UPPER WING SURFACE MLG SUPPORT UPPER DOUBLER AT XORS 290 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER EA 1-5710-143434. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.
Part: DOUBLER — CORRODED (LT WING) · airframe 65,589 hrs · 14,398 cycles
LT WING UPPER WING SURFACE MLG SUPPORT UPPER DOUBLER AT XORS 288 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER EA 1-5710-143434. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.
Part: SKIN — CRACKED (ZONE 500) · airframe 65,589 hrs · 14,398 cycles
LEFT WING LEADING EDGE LOWER ACCESS PANEL 519CB CUT OUT, INBOARD CORNER SKIN FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57-40-02 FIGURE 201, REPAIR 7, REVISION 44. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.
Part: SKIN — CRACKED (ZONE 500) · airframe 65,589 hrs · 14,398 cycles
LEFT WING LOWER SKIN PANEL, OUTER WING ACCESS DOOR CUT OUT AT APPROXIMATELY BETWEEN XORS 683.400 AND XORS 713.600, 03 EACH FASTENER HOLE FOUND WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSPECTION. 03 EACH FASTENER HOLE AT LEFT HAND WING LOWER SKIN FUEL TANK ACCESS PANEL 536AB CUT OUT AT APPROXIMATELY XORS 683.400 TO XORS 713.600 CARRIED OUT REPAIR BY INSTALLATION OF BUSHING IN REWORK FASTENER HOLE AS PER DRAWING SG11570004, REVISION A. BUSHING FABRICATED AS PER DRAWING SG11570004, REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.
Part: SKIN — CRACKED (ZONE 600) · airframe 65,589 hrs · 14,398 cycles
RIGHT WING LOWER SKIN PANEL OUTER WING ACCESS DOOR CUT OUT AT APPROXIMATELY BETWEEN XORS 683.400 AND XORS 713.600, 01 EACH FASTENER HOLE FOUND WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSPECTION. CARRIED OUT REPAIR BY INSTALLATION OF BUSHING IN REWORK FASTENER HOLE AS PER DRAWING SG11570004, REVISION A. BUSHING FABRICATED AS PER DRAWING SG11570004, REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.
Part: FLOORBEAM — CRACKED (BS 392) · airframe 65,589 hrs · 14,398 cycles
FORWARD AVIONICS COMPARTMENT FLOORBEAM AREA FROM CABIN CENTER LOWER CHORD AT STA 392, RBL 15 FOUND CRACKED. HFEC INSPECTION CARRIED OUT AS PER NDT SPM REVISION 13 PART 06-10-01.001, RESULT NO CRACK EVIDENT.
Part: SKIN — CORRODED (RT WING) · airframe 65,589 hrs · 14,398 cycles
RIGHT WING UPPER SURFACE, MAIN LANDING GEAR SUPPORT UPPER DOUBLER AT XORS 277 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER E.A. 1-5730-143750. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.
Part: RIB — CRACKED (RT WING) · airframe 65,589 hrs · 14,398 cycles
RIGHT WING NR 1 LEADING EDGE SLAT INBOARD PERFORMANCE FILLET OUTBOARD EDGE RIB FOUND CRACKED AROUND AFT FASTENER HOLE. CARRIED OUT REPAIR AS PER SRM 57-40-71 FIGURE 201, REPAIR 1, REVISION 44. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.
Part: FRAME — CRACKED (ZONE 300) · airframe 65,589 hrs · 14,398 cycles
UPPER AFT FUSELAGE FRAME CLIP AT CANT STA Y = 2069 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01, REVISION 44. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.
2009
Part: PILOT VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 62,396 hrs · 13,664 cycles
ON TAKE OFF BLEED AIR 2 OFF ALERT. TRIED MANUAL AND 2ND AUTO CHANNEL COULD NOT RESTORE (BLEED AIR 3 PREVIOUSLY DEFERRED) AIR TURNBACK PHNL 90,000 LBS FUEL DUMPED. REPLACED NR 2 PRESSURE REGULATOR PILOT VALVE IAW AMM 36-12-20-4. RAN NR 2 ENG IAW JRH. NR 2 PNEU OP CHKS OK. ACFT OK FOR SVC.
Part: PRESSURE SWITCH — FAILED (OIL FILTER) · airframe 62,005 hrs · 13,577 cycles
ON TAKEOFF RUN APPROX 50KTS HAD A NR 3 ENG LEVEL 2 "ENG OIL FILTER". REJECTED TAKEOFF AND COMPLIED WITH QRH. REMOVED AND REPLACED THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH.
Part: SKIN — CORRODED (WING BOX) · airframe 60,558 hrs · 13,206 cycles
CABIN - R/H STA 1229, X= -70 CENTER WING UPPER PANEL FOUND CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-127463: WINGS, CENTER WING UPPER AUXILIARY FUEL TANK SKIN CORROSION, REPAIR.
Part: SKIN — CORRODED (WING BOX) · airframe 60,558 hrs · 13,206 cycles
CABIN, RT STA 1229 X= -43 TO X= -53, CENTER WING UPPER PANEL FOUND CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-127463: WINGS, CENTER WING UPPER AUXILLIARY FUEL TANK SKIN CORROSION, REPAIR.
Part: SUPPORT — DAMAGED (ZONE 600) · airframe 60,558 hrs · 13,206 cycles
RT WING REAR SPAR NR 4 SPOILER HINGE SUPPORT HOLE FOUND ELONGATED. RT WING REAR SPAR NR 4 SPOILER HINGE SUPPORT HOLE REPAIR CARRIED OUT AS PER E.A. 1-5750-127474. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: ATTACH FITTING — CORRODED (ZONE 500) · airframe 60,558 hrs · 13,206 cycles
LT WING OTBD FLAP VANE NR 2 TRACK FITTING ATTACH BORES FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127466. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 60,558 hrs · 13,206 cycles
RT WING OTBD FLAP VANE NR 2 FROM INBD TRACK FITTING ATTACH BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127473. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: SUPPORT — CORRODED (RT MLG) · airframe 60,558 hrs · 13,206 cycles
AFTER REMOVAL OF FRAME SUPPORT MOUNTING BOLTS PER SNRM N01267 FROM RT MAIN LANDING GEAR RETRACT CYLINDER ASSY FOUND MOUNTING HOLES WITH CORROSION. REPAIRED AS PER EA 1-5740-127479. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SUPPORT FRAME — CORRODED (MLG) · airframe 60,558 hrs · 13,206 cycles
AFTER REMOVAL OF LT MAIN LANDING GEAR RETRACT CYLINDER SUPPORT FRAME MOUNTING BOLTS PER SNRM N01194 FOUND MOUNTING BORE HOLES WITH CORROSION. REPAIRED AS PER EA 1-5740-127470. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SHEAR TIE — CRACKED (BS 1841 L51L) · airframe 60,558 hrs · 13,206 cycles
CENTER CARGO, UPON REMOVED EXISTING REPAIR DOUBLER BILGE AREA FRAME SHEAR CLIP CRACKED AT STA 1841, LONGERON- 51L. REMOVED AND REPLACED WITH NEW SHEAR TIE AS PER SRM 51-33-01 VOL. II.
Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 60,558 hrs · 13,206 cycles
LT WING, INBD FLAP INBD SEGMENT OTBD AFT UPPER SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT OTBD AFT UPPER SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IN ACCORDANCE WITH SRM 57-10-00 FIG 38 VOL I. EXISTING REPAIR DOUBLER REMOVED AND REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 38 VOL I. FEDEX EO 1-51-7-5001 A4 PART 1, TITLE: STRUCTURES, REPAIR CATALOG, MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: SKIN — MISREPAIRED (ZONE 500) · airframe 60,558 hrs · 13,206 cycles
EXISTING REPAIR, LT WING, INBD FLAP INBD SEGMENT, INBD UPPER LEADING EDGE SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT, INBD UPPER LEADING EDGE SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IAW ANY SRM REPAIR SCHEME. LT WING INBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-02.
Part: SKIN — MISREPAIRED (ZONE 500) · airframe 60,558 hrs · 13,206 cycles
EXISTING REPAIR, LT WING NR 7 LEADING EDGE EXTERIOR OTBD SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING NR 7 LEADING EDGE SLAT EXTERIOR OTBD SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IAW ANY SRM REPAIR SCHEME. REPAIR CARRIED OUT PER FEDEX EA 1-5750-127465: WINGS, FLIGHT SURFACES, LT WING NR 7 SLAT EXISTING EXTERNAL REPAIR DOUBLER. REPAIR CLASSIFIED AS PER MINOR AS PER FEDEX GMM 6- 2-100.
Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 60,558 hrs · 13,206 cycles
LT WING, INBD FLAP INBD SEGMENT, MIDDLE AFT UPPER SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT MIDDLE AFT UPPER AFT UPPER SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IAW SRM 57-10-00 FIG 38 VOL I. EXISTING REPAIR DOUBLER REMOVED AND REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 38 VOL I FEDEX EO 1- 51-7-5001 A4 PART 1, TITLE: STRUCTURES, REPAIR CATALOG MD-11. REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: SKIN — MISREPAIRED (ZONE 100) · airframe 60,558 hrs · 13,206 cycles
FUSELAGE, EXISTING REPAIR DOUBLER AT SKIN STATION 1841, AROUND LONGERON-52L. EXISTING REPAIR DOUBLER AT FUSELAGE SKIN AT STA 1841, AROUND LONGERON 52L EVALUATED AND FOUND NOT ACCOMPLISHED IAW SRM 53-20-00 FIG 2 VOL I. EXISTING REPAIR DOUBLER REMOVED AND NEW REPAIR CARRIED OUT AS PER SRM 53-20-00 FIG 2 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 60,558 hrs · 13,206 cycles
RT WING, INBD FLAP INBD SEGMENT UPPER MIDDLE AFT SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING INBD FLAP INBD SEGMENT UPPER MIDDLE AFT SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IAW SRM 57-10-00 FIG 38 VOL I. EXISTING REPAIR DOUBLER REMOVED AND REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 38 VOL I. FEDEX EO 1-51-7-5001 A4 PART 1, TITLE: STRUCTURES, REPAIR CATALOG, MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 60,558 hrs · 13,206 cycles
RT WING, OTBD FLAP OTBD HINGE BRACKET SIDE LOAD LOWER HOLE SURFACE CORROSION. COMPLIED WITH EA 1-5750-128580. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FRAME — DENTED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CABIN, RT STATION 1721, LONGERON 11 TO LONGERON 13 FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FRAME — DENTED (BS 1641) · airframe 60,558 hrs · 13,206 cycles
CABIN, LT STATION 1641, LONGERON 11 TO LONGERON 13 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL I. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SKIN — CORRODED (ZONE 600) · airframe 60,558 hrs · 13,206 cycles
RT WING, UPPER SKIN CORROSION AT APPROX XORS= 260, STRINGER 31. REPAIRED AS PER SRM 51-00-01 FIG 6 VOL. I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CABIN, LT STATION 415 TO 475, X=107 SEAT TRACK FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS PER MAJOR AS PER GMM 6-2-100.
Part: LONGERON — CRACKED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
MAIN DECK, BELOW NR 3R DOOR SILL AREA AT STA 1293, LONGERON 27R FOUND 01 SUSPECT CRACK AT THE RADIUS. REMOVED AND REPLACED AS PER SRM 51-31-00 VOL. II. REPAIR CLASSIFIED AS PER MAJOR AS PER GMM 6- 2-100.
Part: SEAT TRACK — CORRODED (BS 1880) · airframe 60,558 hrs · 13,206 cycles
MAIN DECK, SEAT TRACK AT STA 1880, X= -8.5, FOUND 01 CORROSION IN THE CHANNEL. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL. I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
MAIN DECK, SEAT TRACK AT STA 1326, X= -8.5, UNDER FLOOR PANEL NR 263LF FOUND 02 CORROSION NEAR FASTENER HOLES. REPAIRED FROM STA. 1310 TO STA 1370, X= -8.5 AS PER SRM 53-70-00 FIG.I VOL. I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FRAME — DENTED (BS 1681) · airframe 60,558 hrs · 13,206 cycles
CABIN, RT STATION 1681, LONGERON 11 TO LONGERON 13 FRAME FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL I. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FRAME — DENTED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CABIN, RT STATION 1701, LONGERON 11 TO LONGERON 13 FOUND DENT. REPAIRED AS PER SRM 53-30-00 FIG. I VOL. I. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. I VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: STOP FITTING — CRACKED (LT WING TE FLAP) · airframe 60,558 hrs · 13,206 cycles
LT WING OTBD FLAP SECONDARY UP STOP CRACKED. CRACKED FITTING REMOVED AND REPLACED NEW FITTING AT LT WING OUTBD FLAP AS PER SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: SUPPORT FITTING — DAMAGED (DOOR FRAME) · airframe 60,558 hrs · 13,206 cycles
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-00 VOL. II. NEW SUPPORT FITTING FABRICATED AS PER DRAWING AFA7132 AND COMPLIED WITH EA 1-2580-128579. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. REMOVED AND REPLACED REFER TO EA 1-5310-127432. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 4 LOWER JAMB AT HOLE D. COMPLIED WITH EA 1-5310-127432. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 60,558 hrs · 13,206 cycles
CRACK INDICATION FOUND DURING HFEC OPEN HOLE ISPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 60,558 hrs · 13,206 cycles
LT WING, OTBD FLAP INBD FWD HINGE BRACKET ACTUATOR ATTACH INBD BORE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127460. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 60,558 hrs · 13,206 cycles
RT WING, OTBD FLAP OTBD FORWARD HINGE BRACKET LOWER ATTACH BORE FORWARD FACE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-128580. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 60,558 hrs · 13,206 cycles
LT WING, OTBD FLAP OUTBD FWD HINGE BRACKET LOWER ATTACH OTBD BORE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127462. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: VANE — DELAMINATED (LT WING) · airframe 60,558 hrs · 13,206 cycles
LEFT WING INBOARD FLAP VANE FOUND DELAMINATION ON LOWER SURFACE. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-22-5.
Part: SKIN — DAMAGED (NR 3 SLAT) · airframe 60,558 hrs · 13,206 cycles
LEFT WING LEADING EDGE SKIN AT NR 3 SLAT FOUND WITH CUT MARK. REPAIR CARRIED AT LT WING LEADING EDGE SKIN AT NR 3 SLAT TRACK AS PER SRM 57-10-00 FIG 24 VOL I. REPAIR CLASSIFIED AS PER GMM 6-2-100.
Part: GCU — FAILED (NR 3) · airframe 60,452 hrs · 13,181 cycles
EPGS FAULT FOLLOWED BY NR 3 GEN OFF PASSING 5000 FT ON DEP. RAN NR 3 ENG PER MD-11 JRH SEVERAL TIMES. COULDN'T DUPLICATE B FAULT. COMPARED WITH NR 1 ENG, ALL INDICATION NML. OPERATED EPCU IN MANUAL MODE, TURN "GEN RELAY" AND BUS TIE RELAY" OFF THEN ON. ALL FUNCTION NML IN SERIES, PARALLEL MODE. ADVANCED PWR, NOTHING HAPPENED. PER MTSI24-20/4706 AND HISTORY, REMOVED AND REPLACED NR 3 GCU PER MM 24-21-03-4. CLOSE AND SECURED NR 3 ENG COWLING PER MM 71-10-00-2. RAN NR 3 ENG PER JRH, OPS CHECK NORMAL AND EPCU R-T-S PASSED PER MM 24-21-03-5, 24-08-01-5. ACFT OK FOR SVC.
2007
Part: BRACKET — DAMAGED (ZONE 600) · airframe 55,529 hrs · 12,134 cycles
RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FORWARD SUPPORT INBOARD AFT BORE EXISTING DIAMETER = 0.5INCH. COMPLIED WITH FEDEX EA 1-5750-115159.
Part: STRUT — CORRODED (ZONE 600) · airframe 55,529 hrs · 12,134 cycles
RIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING STRUT 1 FASTENER HOLE FOUND CORROSION. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5750-115157, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: STRUT — CORRODED (ZONE 600) · airframe 55,529 hrs · 12,134 cycles
RIGHT WING, OUTBOARD FLAP OUTBOARD HINGE AFT FAIRING STRUT 1 FASTENER HOLE FOUND CORROSION. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5750-115158, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 55,529 hrs · 12,134 cycles
FORWARD CARGO COMPARTMENT, MAIN DECK CARGO SEAT TRACK LBL 47.5 FOUND CRACK. 09-04-07 MAIN DECK CARGO SEAT TRACK FROM STA 625 TO STA 665 LBL 47.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: HINGE — CORRODED (ZONE 600) · airframe 55,529 hrs · 12,134 cycles
RIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT 1 FASTENER HOLE FOUND CORROSION. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5750-115156, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: PANEL — CRACKED (ZONE 600) · airframe 55,529 hrs · 12,134 cycles
RIGHT WING REFUELING PANEL CUT OUT INBOARD CORNER FOUND WITH CRACK. 09-04-07 RT WING REFUELLING PANEL CUT OUT INBOARD CORNER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 21 VOL. I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.
Part: SKIN — CRACKED (ZONE 500) · airframe 55,529 hrs · 12,134 cycles
CRACK INDICATIONS REVEALED IN FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN LHW LOWER SKIN ACCESS DOOR, BETWEEN STA XORS=683.400 TO STA XORS=713.600. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5710-115154, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: SKIN — CRACKED (ZONE 600) · airframe 55,529 hrs · 12,134 cycles
CRACK INDICATIONS REVEALED IN FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN RT WING LOWER SKIN ACCESS DOOR, BETWEEN STA XORS=683.400 TO STA XORS=713.600. 09-04-07 COMPLIED WITH FEDEX EA 1-5710-115155, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: SUPPORT FITTING — CRACKED (ZONE 600) · airframe 55,529 hrs · 12,134 cycles
CRACK FOUND ON OUTBOARD FASTENER HOLE OF LOWER ROW FASTENERS OF ARC4009 RIGHT OUTBOARD FLAP HINGE SUPPORT FITTING. 09-04-07 RT OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-830-805, FOUND SATISFACTORY.
Part: STRUCTURE — CRACKED (ZONE 600) · airframe 55,529 hrs · 12,134 cycles
RIGHT WING, ANTI-ICE TELESCOPING DUCT DOOR CUTOUT CORNER FOUND CRACK. 09-04-07 COMPLIED WITH FEDEX EA 1-5710-115161, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: SUPPORT FITTING — BROKEN (ZONE 500) · airframe 55,529 hrs · 12,134 cycles
LEFT WING, NR 3 LEADING EDGE SLAT OUTBOARD SUPPORT FITTING BROKEN. 09-04-07 REMOVED & REPLACED AS PER AMM 27-80-30. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-30, FOUND SATISFACTORY.
Part: STRUCTURE — CRACKED (ZONE 500) · airframe 55,529 hrs · 12,134 cycles
LEFT WING, LEADING EDGE SLAT DROOP LOWER SURFACE FOUND CRACK. 09-04-07 LT WING LEADING EDGE SLAT DROOP ASSY REMOVED AND REPLACED AS PER AMM 27-80-10. ADJUSTMENT CARRIED OUT AS PER AMM 27-80-10, FOUND SATISFACTORY.
Part: STRUCTURE — CRACKED (ZONE 500) · airframe 55,529 hrs · 12,134 cycles
LEFT WING, LEADING EDGE TELESCOPING DUCT CUTOUT OUTBOARD CORNER FOUND CRACK. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5710-115160, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: WIRE — DAMAGED · airframe 55,526 hrs · 12,133 cycles
PASSING FL 270 ON CLIMB A/P TRIPPED OFF FOLLOWED BY MULTIPLE OTHER ALERTS. ENGINE NR 3 FLAMED OUT WITH "0" FUEL FLOW. FOLLOWED CHECKLIST FOR RESTART WITH NO SUCCESS. TANK NR 3 PUMPS WERE UNPOWERED. ENG NR 3 WAS SUCTION FEEDING. ATTEMPTED RESTART WITH FUEL SYSTEM IN MANUAL AND CROSSFEEDING TO NR 3 WITH NO SUCCESS, BATTERY BUSS T/R2A AND GS BUSSES WERE UNPOWERED. LATERAL FUEL IMBALANCE OCCURRED. ACCOMPLISHED EA 1-2400-114788 PART-1 AS FOLLOW INSTRUCTIONS, REPAIRED DAMAGED WIRES. REMOVED AND REPLACED ASSOCIATED COMPONENTS AND R-T-S RELATED SYSTEMS. A/C OK FOR CONTINUE SERVICE.
Part: VALVE — FAILED (ZONE 600) · airframe 53,699 hrs · 11,719 cycles
ON DEPARTURE WHEN WING ANTI-ICE SELECTED ON GOT WING ANTI-ICE DISAGREE AND MOMENTARILY MANIFOLD FAIL. PERFORMED QRH PROCEDURE, REMAINED CLEAR OF ICING CONDITION. WING DISAGREE INDICATION REMAINED. TROUBLE SHOT CARRIED OUT PRECAUTIONARY MEASURE DELTA P SENSOR REMOVED AND REPLACED PER MD11 MM CHP30-11-02-4 AND RT WING ANTI-ICE SHUTOFF VALVE REMOVED AND REPLACED PER MD11 MM CHP30-11-01-4. ENGINE RUN CARRIED OUT PER MD11 JRH CHP5A ALL INDICATIONS NORMAL AND ANTI-ICE TEST CARRIED OUT PER MD11 MM CHP 30-11-00-5. ALL TESTS PASSED.
2006
Part: SKIN — DENTED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
FUSELAGE - EXTERIOR SKIN WHILE CARRYING OUT REPETITIVE INSPECTION ON DENTED MARK AT STA 640 STRINGER 38L TO 39L FOUND REQUIRE REPAIR. FORWARD CARGO STA 640 STRINGER 38L TO 39L DENTED MARK CARRIED OUT REPAIR AS PER SRM 53-20-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVE INSPECTION REQUIRED AS PER FEDEX EA 1-5320-95833, TITLE: FUSELAGE - SRM SKIN REPAIR AT STATION Y=640 AT LONGERON 38 AND 39 LEFT HAND - TRACKING.
Part: SKIN — DENTED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
FUSELAGE - EXTERIOR SKIN WHILE CARRYING OUT REPETITIVE INSPECTION ON DENTED MARK 3 FEET AFT OF CENTER CARGO DOOR FOUND REQUIRE REPAIR. THREE FEET AFT OF CENTER CARGO DOOR DENTED SKIN CARRIED OUT REPAIR AS PER SRM 53-20-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVE INSPECTION REQUIRED AS PER FEDEX EA 1-5320-95832, TITLE: FUSELAGE - SRM SKIN REPAIR AT STATION Y=1823 AT LONGERON 33 AND 34 RIGHT HAND - TRACKING.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,296 hrs · 11,154 cycles
SNRM N01239: MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1795 RBL 27. SNRM N01239: MAIN DECK COMPARTMENT SEAT TRACK AT STA 1795 RBL 27 CARRIED OUT. REPAIR IAW SRM 53-70-00 FIG1, VOL 1. REPAIR CLASSIFIED AS MAJOR IAW MFG GMM 6-2-100.
Part: TRUNNION — CORRODED (ZONE 700) · airframe 51,296 hrs · 11,154 cycles
DURING THE CORROSION REMOVAL OF CENTER LANDING GEAR LEFT TRUNNION SUPPORT FITTING FOUND FORWARD BOLT HOLE TOP SPOTFACE AREA WITH CRACK. REPAIRED AS PER FEDEX EA NR 1-5340-95821.
Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,296 hrs · 11,154 cycles
R3 DOOR JAMB AREA FOUND WITH CORROSION. R3 DOOR JAMB AREA CARRIED OUT REPAIR AS PER SRM 53-50-00 FIG 17 VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: SKIN — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION, STRINGER 19 LBL 104. MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE CORROSION AT STRINGER 19 LBL 104 REMOVED AS PER SRM 51-21-01 VOL II ORIG THICKNESS: 0.150"; THICKNESS REMAINING: 0.138"; MAT'L REMOVED: 0.012"; FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG 12 VOL I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.
Part: SKIN — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND CORROSION BETWEEN STRINGER 14 AND STRINGER 15 LBL 66. MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE CORROSION BETWEEN STRINGER 14 AND STRINGER 15 LBL 66. REMOVED AS PER SRM 51-21-01 VOL II ORIG THICKNESS: 0.184"; THICKNESS REMAINING: 0.166"; MAT'L REMOVED: 0.018"; FOUND WITHIN LIMIT AS PER DWG APB7447. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.
Part: LONGERON — CRACKED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
LONGERON 48L FOUND CRACKED AFTER SPLICE REMOVAL FOR REPAIR, FORWARD OF STA 5 -113, CENTER CARGO COMPARTMENT. REMOVED AND REPLACED WITH NEW LONGERON IAW SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR IAW FEDEX GMM 6-2-100.
Part: LONGERON — CRACKED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
LONGERON 52 STA 979 FOUND CRACKED AFTER FASTENERS REMOVED FOR CORROSION CLEAN UP ON CAP ANGLE FORWARD CARGO. COMPLIED WITH FEDEX EA 1-5330-95835.
Part: FUEL TANK — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
FOUND MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION BETWEEN STRINGER 14 AND STRINGER 15 RBL 81. COMPLIED WITH FEDEX EA 1-5710-95814.
Part: FUEL TANK — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION AT STRINGER 16 RBL 79. REMOVED AS PER SRM 51-21-01 VOLUME II. REWORKED AREA MEASURED: MATERIAL THICKNESS = 0.194", THICKNESS REMAINED = 0.158", MATERIAL REMOVED = 0.036". FOUND WITHIN LIMIT AS PER DRAWING NR APB7441 AND SRM 57-20-00 VOLUME I FIGURE 12. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: FUEL TANK — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION AT STRINGER 15 RBL 75 TO RBL 104. REMOVED AS PER SRM 51-21-01 VOLUME II. REWORKED AREA MEASURED: MATERIAL THICKNESS = 0.164", THICKNESS REMAINED = 0.147", THICKNESS REMOVED = 0.017" FOUND WITHIN LIMIT AS PER DRAWING NR APB7441 AND SRM 57-20-00 FIGURE 12 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: FUEL TANK — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
FOUND MAIN DECK COMPARTMENT CENTER WING TANK TOP SURFACE FOUND WITH CORROSION BETWEEN STRINGER 14 AND STRINGER 15 RBL 46.
Part: TRUNNION — CRACKED (ZONE 700) · airframe 51,296 hrs · 11,154 cycles
UPON REMOVAL OF NOSE LANDING GEAR ASSEMBLY FOUND RIGHT TRUNNION FITTING LOWER AREA WITH CRACK. REPAIRED IAW SRM 53-40-00.
Part: FITTING — CRACKED (ZONE 700) · airframe 51,296 hrs · 11,154 cycles
UPON REMOVAL OF NOSE LANDING GEAR ASSEMBLY FOUND LEFT TRUNNION FITTING LOWER AREA WITH CRACK. REPAIRED IAW SRM 53-40-00.
Part: FASTENER — MISINSTALLED (ZONE 400) · airframe 51,296 hrs · 11,154 cycles
ENGINE NR 1 PYLON AT RIGHT SIDE MATING TO THRUST REVERSER COWL FOUND CHAFING DUE WRONG FASTENER INSTALLED ON REVERSER. COMPLIED WITH FEDEX EA 1-5450-95813.
Part: SPAR — CORRODED (ZONE 500) · airframe 51,296 hrs · 11,154 cycles
FOUND LEFT WING, REAR SPAR AT ABOUT XORS 1042 CORRODED. CORRODED AREA AT LEFT HAND WING - REAR SPAR LOWER CHORD AT ABOUT XORS 1042 REPAIRED AS PER FEDEX E.A. #1-5710-95809, TITLE: WINGS - LEFT HAND REAR SPAR LOWER CAP AFT TANG UPPER SURFACE CORROSION CENTERED AT STATION XORS = 1045 - REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: SPAR CAP — CORRODED (ZONE 600) · airframe 51,296 hrs · 11,154 cycles
RIGHT HAND WING - REAR SPAR UPPER SPAR CAP AT STA XORS 1027 TO STA XORS 1045 FOUND CORROSION. REPAIR CARRIED OUT ON RIGHT HAND WING REAR SPAR UPPER SPAR CAP AT STA XORS 1027 TO XORS 1045 AS PER FEDEX EA 1-5710-95811, TITLE: WINGS - RIGHT HAND REAR SPAR CAP UPPER AFT TANG CORROSION AT STATIONS XORS = 1027 THROUGH XORS = 1045 - REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: DOUBLER — CHAFED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
FORWARD CARGO DOOR CUTOUT AFT DOUBLER APPROX FLOOR LEVEL EDGE CHAFED. FORWARD CARGO DOOR CUTOUT AFT DOUBLER CHAFING MARK REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG 1A VOL.I.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1795-1805 RBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 1795-1805 RBL 8 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: SPAR CAP — CORRODED (ZONE 500) · airframe 51,296 hrs · 11,154 cycles
LEFT HAND WING - REAR SPAR UPPER SPAR CAP AT STA XORS 1025 TO STA XORS 1045 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND EXCEEDED LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I. ORIGINAL THICKNESS = 0.145" MATERIAL REMOVED = 0.054", REMAINING THICKNESS = 0.091". REWORK AREA REPAIRED AS PER FEDEX EA 1-5710-95812, TITLE: WINGS - LEFT HAND REAR SPAR UPPER CAP AFT TANG CORROSION CENTERED AT STATION XORS = 1042 - REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SPAR CAP — CORRODED (ZONE 600) · airframe 51,296 hrs · 11,154 cycles
RIGHT HAND WING - REAR SPAR UPPER SPAR CAP AT STA XORS 1062 FOUND CORROSION. CORROSION ON RIGHT HAND WING, REAR SPAR UPPER SPAR CAP AT STA XORS 1062 REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I. ORIGINAL MEASURED THICKNESS = 0.150" AND MINIMUM ORIGINAL BLUEPRINT THICKNESS = 0.122", THICKNESS REMOVED = 0.033" AND THICKNESS REMAINING = 0.117". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (ZONE 500) · airframe 51,296 hrs · 11,154 cycles
LEFT HAND WING - FIXED LEADING EDGE COMPARTMENT CANTED AREA FOUND FORMER DOUBLER AT STA XIS 562 WITH CRACKED. LEFT HAND WING - FIXED LEADING EDGE COMPARTMENT CANTED AREA AT STA XIS 562 CRACKED DOUBLER. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PER DRAWING ARB3954. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: SPLICE — CORRODED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
CENTER CARGO LONGERON 48L BETWEEN STA 5-113 TO 1541 SPLICE CORRODED. CENTER CARGO LONGERON 48L BETWEEN STA 5-113 TO 1541 CORRODED SPLICE REMOVED AS PER SRM 51-33-01 VOL II. NEW SPLICE FABRICATED AS PER DWG NR A5A7125-501. NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL.II.
Part: LONGERON — CORRODED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
CENTER CARGO RIGHT LONGERON 48R BETWEEN STA 1561 TO 1581 CORRODED. CENTER CARGO RIGHT SIDE STA 1561 TO STA 1581 LONGERON 48R SPLICE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS = 0.200", MATERIAL REMOVED = 0.010", REMAINING THICKNESS = 0.190".
Part: DOUBLER — CHAFED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
FORWARD CARGO DOOR CUTOUT FORWARD DOUBLER APPROX FLOOR LEVEL EDGE CHAFED. FWD CARGO DOOR CUTOUT FWD DAMAGED DOUBLERS REMOVED AS PER SRM 51-33-01 VOL II. NEW DOUBLERS FABRICATED AS PER SRM 53-50-00 FIG 16 VOL I. NEW DOUBLERS PROTECTED AS PER SRM 51-21-01 VOL.II. DOUBLERS AND FILLERS INSTALLED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1551 RBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 1551 RBL 8 CARRIED OUT. REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
CENTER CARGO - LEFT HAND LONGERON 41 SPLICE AT STA 5-113 TO 1541 CRACKED. CRACKED SPLICE ON CENTER CARGO LEFT HAND LONGERON 41 AT STA 5-113 TO 1541 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FRAME — CRACKED (ZONE 600) · airframe 51,296 hrs · 11,154 cycles
RIGHT WING LEADING EDGE CANTED AREA FORMER AT STA XORS 480, SUSPECTED CRACKED. CRACK FORMER ON RT WING LEADING EDGE CANTED AREA AT STA XORS 480. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. NEW FORMER FABRICATED AS PER DWG ARB2931. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1581 RBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 1581 RBL 8 REPAIR CARRIED OUT AS PER SRM 53-70-00 VOL I FIG 1.
Part: LONGERON — CRACKED (ZONE 300) · airframe 51,296 hrs · 11,154 cycles
EMPENNAGE AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45L TO 46L, CAP SUSPECTED CRACKED. EMPENNAGE AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45L TO 46L END CAP REPAIRED AS PER FEDEX EA NR 1-5310-95818, TITLE: FUSELAGE LONGERON 45L CRACKED BETWEEN STATIONS Y=2007 AND Y=2003 - SR REPAIR AND END CAP FABRICATION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SUPPORT — CORRODED (ZONE 700) · airframe 51,296 hrs · 11,154 cycles
CENTER LANDING GEAR REPLACEMENT LEFT PILLOW BLOCK ATTACHMENT BOTTOM MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5340-95821 FUSELAGE CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING CORROSION REMOVAL AND REPAIR.
Part: LONGERON — CRACKED (ZONE 300) · airframe 51,296 hrs · 11,154 cycles
EMPENNAGE AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45R TO 46R, CAP SUSPECTED CRACKED. EMPENNAGE, AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45R TO 46R END CAP REPAIRED AS PER FEDEX EA NR 1-5310-95817, TITLE: FUSELAGE LONGERON 45R CRACKED BETWEEN STATIONS Y=2007 AND Y=2033 - SR REPAIR AND END CAP FABRICATION.
Part: BLOCK — CORRODED (ZONE 700) · airframe 51,296 hrs · 11,154 cycles
CENTER LANDING GEAR REPLACEMENT, RIGHT PILLOW BLOCK ATTACHMENT BOTTOM MATING SURFACE FOUND CORRODED. RT PILLOW BLOCK ATTACHMENT BOTTOM MATING SURFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER SRM 53-40-00 FIG 15 VOL I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1341-1361 RBL 75. MAIN DECK COMPARTMENT SEAT TRACK AT STA 1341-1361 RBL 75 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: BLOCK — CORRODED (ZONE 700) · airframe 51,296 hrs · 11,154 cycles
CENTER LANDING GEAR REPLACEMENT RIGHT PILLOW BLOCK 3 OFF ATTACHMENT HOLES BORE SURFACE FOUND CORRODED. CENTER LANDING GEAR RIGHT PILLOW BLOCK ATTACHMENT HOLES CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIG 15 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.
Part: BLOCK — CORRODED (ZONE 700) · airframe 51,296 hrs · 11,154 cycles
CENTER LANDING GEAR REPLACEMENT, LEFT PILLOW BLOCK 3 OFF ATTACHMENT HOLES BORE SURFACE FOUND CORRODED. CENTER LANDING GEAR LEFT PILLOW BLOCK CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG 15 VOL I.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
FOUND MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 1805 LBL 8. CARRIED OUT REPAIR IAW SRM 53-70-00
Part: SEAT TRACK — CRACKED (BS 5-20) · airframe 51,296 hrs · 11,154 cycles
FOUND MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 5-20 RBL 27. CARRIED OUT REPAIR IAW SRM 53-70-00.
Part: FRAME — DENTED (BS 1721 S12L) · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT FOUND FRAME WITH DENT AT STA 1721 LONGERON 12L. DENT ON FRAME OF M/D COMPARTMENT STA 1721 LONGERON 12L REPAIRED AS PER SRM 53-30-00 FIG.1 VOL.I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. REPETITIVE INSPECTION REQUIRED AS PER FEDEX EA 1-5330-95834 TITLE: FUSELAGE - SRM FRAME REPAIR AT STATION Y = 1721 AT LONGERON 12 LEFT HAND - TRACKING.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 6-10 TO 6-30 LBL 8. MAIN DECK COMPARTMENT SEAT TRACK CORROSION AT STA 6-10 TO 6-30 LBL 8. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. REFER TO SNRM N00349 FOR WORK DETAILS.
Part: FUEL CAP — CRACKED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
FOUND RIGHT LOWER WING ROOT STA Y1288 TO 1298 LOWER AUX TANK UPPER CAP. FOUND WITH 1 HAIR LINE CRACK MEASURED APPROX 6" IN LENGTH. COMPLIED WITH FEDEX EA 1-5310-95676, TITLE: FUSELAGE CAP ANGLE RIGHT UNDER WING BARREL STRUCTURE AT STATION Y=1298.6, XCW 46, CRACK ANGLE. FABRICATION AND SPLICE INSTALLATION. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: FUEL CAP — CRACKED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
LEFT LOWER WING ROOT STA Y1298 LOWER AUX TANK UPPER CAP FOUND WITH HAIR LINE CRACK MEASURED APPROX 4" IN LENGTH. COMPLIED WITH FEDEX EA 1-5310-95675, TITLE: FUSELAGE, CAP ANGLE LEFT UNDER WING BARREL STRUCTURE AT STATION Y=1298.6, XCW 46, CRACK ANGLE. FABRICATION AND SPLICE INSTALLATION.
Part: STRINGER — CRACKED (ZONE 600) · airframe 51,296 hrs · 11,154 cycles
HFEC INSPECTION CARRIED OUT, FOUND CRACK ON RIGHT WING STRINGER 13 END WITH CRACK LENGTH OF APPROX 12". FOUND CRACK ON RT WING STRINGER 13 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: STRINGER — CRACKED (ZONE 500) · airframe 51,296 hrs · 11,154 cycles
HFEC INSPECTION CARRIED OUT, FOUND CRACK ON LEFT WING STRINGER 14 END (CRACK LENGTH APPROX. 13"). CRACK ON LT WING STRINGER 14 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 51,296 hrs · 11,154 cycles
LT NR 1 AIR CONDITIONING COMPARTMENT APPROX. AT STA 575 INTERNAL FRAME INTERCOSTAL FOUND WITH SURFACE CORROSION. SURFACE CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOLUME I FIGURE 1A. ORIGINAL THICKNESS = 0.050", MATERIAL REMOVED = 0.002", REMAINING THICKNESS = 0.048". REPAIR CLASSIFIED AS MINOR PER GMM 6- 2- 100.
Part: STRINGER — CRACKED (ZONE 500) · airframe 51,296 hrs · 11,154 cycles
HFEC INSPECTION CARRIED OUT ON LEFT WING STRINGER 40 END FOUND CRACK, CRACK LENGTH APPROX 1". CRACK ON LT WING STRINGER 40 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: SEAT TRACK — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 6-88 TO 6-100 LBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 6-88 TO 6-100 LBL 8 CARRIED OUT. REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: STRINGER — CRACKED (ZONE 600) · airframe 51,296 hrs · 11,154 cycles
HFEC INSPECTION CARRIED OUT ON RIGHT WING STRINGER 41 END FOUND CRACK (LENGTH APPROX. 1"). CRACK ON RT WING STRINGER 41 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: STRINGER — CRACKED (ZONE 600) · airframe 51,296 hrs · 11,154 cycles
HFEC INSPECTION CARRIED OUT ON RIGHT WING STRINGER 40 FOUND CRACK (CRACK LENGTH APPROX. 1"). CRACK ON RT WING STRINGER 40 END REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,296 hrs · 11,154 cycles
MAIN DECK COMPARTMENT SEAT TRACK FOUND WITH CORROSION AT STA 6-100 RBL 8. MAIN DECK COMPARTMENT SEAT TRACK AT STA 6-100 RBL 8 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
2005
Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 48,949 hrs · 10,612 cycles
6 HOURS INTO FLIGHT GOT "FUEL MANF DRAIN" AND"TANK 2 FUEL QTY LO" LEVEL. FUEL READ 700 IN 1, 0IN 2, 700 IN 3, 500 AUX, 14000 IN TAIL. AFTER ACCOMPLISHING QRH PROCEDURE. MCDU INDICATED NR 19,000 FUEL REMAINING. RJAA 90 MILES AWAY. DECLARED EMERGENCY AND PROCEEDED TO LAND AT NRT. ON DESCENT AT APP X 14,000 ON DESCENTFUL QTY IND RETURNED 11000 IN 1, 19000 IN 2, 11000 IN 3,500 AUX, 4000 TAIL. RELEASED FOR SERVICE PER MEL/CDL: 28-01-01-02 .
Part: SPAR CAP — CRACKED (NR 2 PYLON) · airframe 47,889 hrs · 10,368 cycles
NACELLES/PYLONS - PYLON STRUCTURE - CRACK ON NR 2 ENGINE PYLON UPPER SPAR CAP COMPLY WITH EA 1-5450-76453. COMPLIED NR 2 ENG UPPER SPAR REPAIR PER EA 1-5450-81683.
Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 47,889 hrs · 10,368 cycles
STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL, COMPLY WITH EA 1-5510-71839. COMPLIED WITH EA 1-5510-71839.
Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 47,889 hrs · 10,368 cycles
STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL COMPLY WITH EA 1-5510-71838. COMPLIED WITH EA 1-5510-71838.
Part: FLAP — DAMAGED (ZONE 500) · airframe 47,889 hrs · 10,368 cycles
LEFTHAND OUTBOARD FLAP; INBOARD HINGE ATTACH FITTING HAS 2.25 INCH CRACK ADJACENT TO ATTACH POINT. ACCESSED THRU PANEL 557GT. REMOVED & INSTALLED NEW FLAP P/N NRC6753-503,S/N LS0205 IAW MM 27-50-30-4. CHECKED & ADJUSTED O/B FLAP & VANE INW MM 27-50-32/27-50-30. REFER N/R N00150.
2004
Part: PLATE — MISSING (ZONE 100) · airframe 47,169 hrs · 10,191 cycles
BOTH LT AND RT PRIMARY STATIC PORTS ARE MISSING THEIR RUB PLATES. REF: MD11 IPC CHAPTER 34-11-60-01, ITEM 322. DISCREPANCY FOUND DURING "C" CHECK MAINTENANCE. (OPEN)
2003
Part: LINE — LEAKING (BRAKE) · airframe 43,219 hrs · 9,259 cycles
AT BLOCK IN NUMBER 5 BRAKE LINE BROKE AND HYD FLUID SPRAYED ONTO HOT BRAKE CAUSING A FLAME WHICH QUICKLY WENT OUT. MEL 31AUG03 19:05 LCK R ACN RELEASED FOR SERVICE PER MEL/CDL: 32-43-02 CATEGORY: C EXPIRATION: 10SEP03 "MEL 32-43-02: NR 5 BRAKE HYD LINE INOP. INSPECTED BRAKE AND TIRE, NO DAMAGE FOUND. A/C OK FOR SERVICE. FACT 01SEP03 01:01 JFK R REPLACED LINE AS PER SMP. LEAK CHECKED OK, BLEED NR 5 BRAKE AS PER MM 32-40-00-6.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 42,860 hrs · 9,165 cycles
RT HORIZONTAL STABILIZER NR 34 BORE CORROSION EXCEEDED CONDITION "3". CORROSION ON RT HORIZONTAL STABILIZER NR 34 BORE REMOVED AND REPAIR CARRIED OUT IAW EA 1-5510-71839 (STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL - BORE 34 RIGHT.
Part: BARREL NUT — CORRODED (HORIZONTAL STAB) · airframe 42,860 hrs · 9,165 cycles
LT HORIZONTAL STAB NR 3 BORE CORROSION EXCEEDED LIMIT. LT HORIZONTAL STAB NR 3 BORE CORROSION REPAIR CARRIED OUT IAW EA 1-5510-71837, STABILIZERS- HORIZONTAL STAB BARREL NUT BORES- CORROSION REMOVAL- BORE 3 LEFT.
Part: STRUCTURE — CORRODED (ZONE 300) · airframe 42,860 hrs · 9,165 cycles
RT HORIZONTAL STABILIZER NR 36 BORE CORROSION EXCEEDED CONDITION "3". CORROSION ON RT HORIZONTAL STABILIZER NR 36 BORE REMOVED AND REPAIR CARRIED-OUT IAW EA 1-5510-71838 (STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL BORE 36 RIGHT).
Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 42,860 hrs · 9,165 cycles
RT HORIZONTAL STABILIZER NR 2 BORE CORROSION EXCEEDED CONDITION 3. CORROSION ON RT HORIZONTAL STABILIZER NR 2 BORE REMOVED AND REPAIR CARRIED OUT IAW EA NR 1-5510-71832.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 42,860 hrs · 9,165 cycles
RIGHT HORIZONTAL STABILIZER NR 13 BORE CORROSION EXCEEDED CONDITION 3. CORROSION ON RIGHT HORIZONTAL STABILIZER NR 13 BORE REMOVED AND REPAIR CARRIED OUT AS PER EA 1-5510-71831
Part: FITTING — CORRODED (HORIZ STAB) · airframe 42,860 hrs · 9,165 cycles
LEFT HORIZONTAL STABILIZER NR 26 BORE CORROSION EXCEEDED LIMIT. LEFT HORIZONTAL STABILIZER NR 26 FITTING FABRICATED IAW FEDEX EA 1-5510- 71836, STABILIZERS- HORIZONTAL STABILIZER BARREL NUT BORES- CORROSION REMOVAL- BORE 26 LEFT- FITTING ALC8107-1- FABRICATION AND INSTALLED AS PER SRM 51-33-01VOL II.
Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 42,860 hrs · 9,165 cycles
SNRM N0883 : LT HORIZONTAL STABILIZER NR 10 BORE CORROSION EXCEEDED LIMIT AFTER REWORK. CORROSION REMOVED AND REPAIR CARRIED OUT IAW EA NR 1-5510-69392.
Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 42,860 hrs · 9,165 cycles
LEFT HORIZONTAL STABILIZER NR 4 BORE CORROSION EXCEEDED LIMIT AFTER REWORKED. CORROSION ON LEFT HORIZONTAL STABILIZER NR 4 BORE REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-69395, TITLE: STABILIZERS- HORIZONTAL STABILIZER BARREL NUT BORES- CORROSION REMOVAL- BORE 4 LEFT.
Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 42,860 hrs · 9,165 cycles
LEFT HORIZONTAL STABILIZER NR 2 BORE CORROSION EXCEEDED LIMIT AFTER REWORKED. CORROSION ON LEFT HORIZONTAL STABILIZER NR 2 BORE REMOVED AND REPAIRED CARRIED OUT AS PER EA 1-5510-69394 (TITLE : STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL - BORE 2 LEFT).
Part: FITTING — CORRODED (HORIZ STAB) · airframe 42,860 hrs · 9,165 cycles
EMPENNAGE - LEFT HORIZONTAL STABILIZER NR 14 BORE BOTTOM CORROSION EXCEEDED LIMIT. EMPENNAGE - LEFT HORIZONTAL STABILIZER NR 14 FITTING FABRICATED IAW FEDEX EA 1-5510-71835 - STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSION REMOVAL - BORE 14 LEFT - FITTING ALC8106-1 - FABRICATION.
Part: BUSHING — LOOSE (TE FLAP HINGE) · airframe 42,860 hrs · 9,165 cycles
RIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE INBOARD ACTUATOR LUG BUSHING FOUND LOOSE. RT WING OUTBOARD FLAP OUTBOARD AFT HINGE INBOARD ACTUATOR LUG LOOSE BUSHING REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: BUSHING — LOOSE (TE FLAP HINGE) · airframe 42,860 hrs · 9,165 cycles
LEFT WING OUTBOARD FLAP AFT HINGE OUTBOARD PIVOT LUG BUSHING FOUND LOOSE. LEFT WING OUTBOARD FLAP AFT HINGE OUTBOARD PIVOT LUG BUSHING REPLACED IAW FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: BUSHING — LOOSE (T/E FLAP) · airframe 42,860 hrs · 9,165 cycles
RT WING OUTBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT LUG BUSHING FOUND LOOSE. RT WING OUTBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT LUG LOOSE. BUSHING REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: BUSHING — LOOSE (T/E FLAP) · airframe 42,860 hrs · 9,165 cycles
RIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT LUG LOOSE BUSHING. REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: BUSHING — LOOSE · airframe 42,860 hrs · 9,165 cycles
LT WING OUTBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG BUSHING FOUND LOOSE. LEFT WING OUTBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT LUG LOOSE BUSHING REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: HINGE — CORRODED (T/E FLAP) · airframe 42,860 hrs · 9,165 cycles
LEFT WING OUTBOARD FLAP INBOARD AFT HINGE AT FLAP SIDE INBOARD PIVOT LUG BORE OUTER SURFACE FOUND CORRODED. LEFT WING OUTBOARD FLAP INBOARD AFT HINGE AT FLAP SIDE INBOARD PIVOT LUG BORE OUTER SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-69352.
Part: HINGE — CORRODED (LE FLAP) · airframe 42,860 hrs · 9,165 cycles
RIGHT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE FOUND CORROSION. RIGHT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5750-69354 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET REPAIR.
Part: FITTING — CORRODED (TE FLAP HINGE) · airframe 42,860 hrs · 9,165 cycles
LEFT WING (FLAP SIDE) - INBOARD T/E FLAP, OUTBOARD AFT HINGE FITTING FOUND PIVOT BEARING MOUNT HOLE OUTBOARD SIDE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69357 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT INBOARD FLAP HINGE BRACKET REPAIR.
Part: STABILIZER — CORRODED (ZONE 300) · airframe 42,860 hrs · 9,165 cycles
LT HORIZONTAL STABILIZER NR 36 BARREL NUT BORE FOUND WITH CORROSION ON BEARING, SIDEWALL AND BOTTOM SURFACE. BOTTOM SURFACE BLEND OUT CORROSION UP TO MAXIMUM LIMIT CORROSION STILL PRESENT. CORROSION ON LT HORIZONTAL STABILIZER NR 36 BARREL NUT BORE REMOVED AND REPAIR CARRIED OUT IAW EA 1-5510-69391.
Part: HINGE BRACKET — CORRODED (T/E FLAP) · airframe 42,860 hrs · 9,165 cycles
RIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE FOUND CORROSION. RIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5740-71734 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED.
Part: FITTING — CORRODED (TE FLAP HINGE) · airframe 42,860 hrs · 9,165 cycles
LEFT WING (FLAP SIDE) - OUTBOARD T/E FLAP, INBOARD AFT HINGE FITTING FOUND PIVOT BEARING MOUNT HOLE OUTBOARD SIDE CORRODED. LEFT WING (FLAP SIDE) - OUTBOARD T/E FLAP, INBOARD AFT HINGE FITTING PIVOT BEARING MOUNT HOLE OUTBOARD SIDE CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1- 5750-69352 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: HINGE — CHIPPED (LE FLAP) · airframe 42,860 hrs · 9,165 cycles
RIGHT WING INBOARD FLAP OUTBOARD FWD HINGE PIVOT LUG BORE AT INBOARD LOWER SIDE FOUND CHIPPED OFF. RIGHT WING INBOARD FLAP OUTBOARD FWD HINGE PIVOT LUG BORE AT INBOARD LOWER SIDE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69363 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS.
Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 42,860 hrs · 9,165 cycles
LT WING (WING SIDE) - OUTBOARD TRAILING EDGE FLAP, INBOARD HINGE FITTING FOUND HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORRODED. LT WING (WING SIDE) - OUTBOARD TRAILING EDGE FLAP, INBOARD HINGE FITTING HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORROSION REPAIR CARRIED-OUT IAW EA 1-5750-69355 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP, INBOARD HINGE BRACKET REPAIR.
Part: FITTING — CORRODED (LT WING) · airframe 42,860 hrs · 9,165 cycles
LEFT WING (WING SIDE) - OUTBOARD T/E FLAP, OUTBOARD HINGE FITTING FOUND HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORRODED. LEFT WING (WING SIDE) - OUTBOARD T/E FLAP, OUTBOARD HINGE FITTING HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORROSION REPAIR IAW FEDEX EA 1-5750- 69356 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.
Part: HINGE — CORRODED (LE FLAP) · airframe 42,860 hrs · 9,165 cycles
RIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE INBOARD FOUND CORROSION. RIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE INBOARD CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5740-71734 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,860 hrs · 9,165 cycles
MAIN DECK - AT BS 695, LEFT X=8.5, FLOOR TRACK CRACKED. MAIN DECK - AT BS 695 TO BS745 X=8.5 LT CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,860 hrs · 9,165 cycles
MAIN DECK - AT BS 755, LEFT X=8.5, FLOOR TRACK CRACKED. MAIN DECK - BS 755, LT X=8.5 SEAT TRACK REPAIRED AS PER SRM 53-70-00,VOL I.
Part: HINGE — CORRODED (ZONE 600) · airframe 42,860 hrs · 9,165 cycles
RT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE INBOARD FOUND CORROSION. SNRM N0613: RT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE INBOARD CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5750-69354 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.
Part: FITTING — CORRODED (ZONE 600) · airframe 42,860 hrs · 9,165 cycles
RT WING OUTBOARD FLAP VANE 2ND VANE MOUNT FITTING FROM INBOARD FOUND MOUNT HOLE AND BUSHING WITH CORROSION. REPAIR CARRIED OUT AT RT WING OUTBOARD FLAP VANE 2ND VANE MOUNT FITTING FROM INBOARD MOUNT HOLE AS PER EA 1-5750-71731 : WINGS - RIGHT AND LEFT OUTBOARD FLAP VANE - NR 2 VANE TO TRACK SUPPORT CORRODED.
Part: SKIN PANEL — CORRODED (CENTER WING) · airframe 42,860 hrs · 9,165 cycles
MAIN DECK - BETWEEN BS 1215-1235, RIGHT XCW 0-50, CENTER WING UPPER PANEL STRUCTURE FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK.
Part: FITTING — CORRODED (TE FLAP HINGE) · airframe 42,860 hrs · 9,165 cycles
LEFT WING - OUTBOARD T/E FLAP, FWD OUTBOARD HINGE FITTING FOUND HYDRAULIC ACTUATOR ASSEMBLY MOUNT HOLE INBOARD SIDE WITH CORROSION (WING SIDE FITTING). REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69356 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.
Part: HINGE — CORRODED (ZONE 600) · airframe 42,860 hrs · 9,165 cycles
RT WING INBOARD FLAP AFT HINGE INBOARD PIVOT LUG BORE FOUND CORROSION. RT WING INBOARD FLAP AFT HINGE INBOARD PIVOT LUG BORE CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69360 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT INBOARD FLAP HINGE BRACKET ASSEMBLY REPAIR.
Part: SKIN PANEL — CORRODED (ZONE 200) · airframe 42,860 hrs · 9,165 cycles
MAIN DECK - BETWEEN BS 1215-1235, LEFT XCW 75-115, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK.
Part: SKIN PANEL — CORRODED (CENTER WING) · airframe 42,860 hrs · 9,165 cycles
MAIN DECK - BETWEEN BS 1215-1235, LEFT XCW 0-50, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING/UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK.
Part: SKIN — CORRODED (WING BOX) · airframe 42,860 hrs · 9,165 cycles
MAIN DECK - BETWEEN BS 1160-1170, RIGHT XCW 80-100, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK.
Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 42,860 hrs · 9,165 cycles
LT WING - OUTBOARD TRAILING EDGE FLAP VANE, NR 2 TRACK SUPPORT ASSY FOUND FORWARD MOUNT BOLT HOLE SURFACE WITH CORROSION (NUMBERED FROM INBOARD). REPAIR CARRIED OUT AT LT WING OUTBOARD TRAILING EDGE FLAP VANE NR 2. TRACK SUPPORT ASSY FWD MOUNT BOLT HOLE IAW EA 1-5750-71731 : WINGS - RIGHT AND LEFT OUTBOARD FLAP VANE - NR 2 TO TRACK SUPPORT CORRODED.
Part: SKIN — CORRODED (CENTER WING) · airframe 42,860 hrs · 9,165 cycles
MAIN DECK - BETWEEN BS 1215-1235, RIGHT XCW 50-115, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK.
Part: HINGE — CORRODED (ZONE 600) · airframe 42,860 hrs · 9,165 cycles
RT WING INBOARD FLAP AFT HINGE OUTBOARD PIVOT LUG BORE FOUND CORROSION. RT WING INBOARD FLAP AFT HINGE OUTBOARD PIVOT LUG BORE CORROSION REPAIR CARRIED OUT IN ACCORDANCE WITH FEDEX EA 1-5750-69360 - WINGS TRAILING EDGE AND TRAILING EDGE DEVICES - RT INBOARD FLAP HINGE BRACKET ASSEMBLY - REPAIR.
Part: HINGE — CORRODED (LT WING) · airframe 42,860 hrs · 9,165 cycles
LT WING - OUTBOARD T/E FLAP, OUTBOARD FWD HINGE FITTING FOUND OUTBOARD LOWER REAR SPAR ATTACH MOUNT HOLE WITH CORROSION (WING SIDE FITTING). REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69356 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP. OUTBOARD HINGE BRACKET REPAIRS.
Part: FITTING — CORRODED (TE FLAP HINGE) · airframe 42,860 hrs · 9,165 cycles
LEFT WING - OUTBOARD T/E FLAP, OUTBOARD FWD HINGE FITTING FOUND INBOARD SIDE ARM, BARREL NUTS MOUNT HOLES WITH CORROSION (WING SIDE FITTING). LEFT WING - OUTBOARD T/E FLAP, OUTBOARD FWD HINGE FITTING INBOARD SIDE ARM BARREL NUTS MOUNT HOLES (WING SIDE FITTING) CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5750-69356 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP, OUTBOARD HINGE BRACKET REPAIRS.
Part: HINGE — CORRODED (ZONE 500) · airframe 42,860 hrs · 9,165 cycles
LT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FORWARD HINGE FITTING FOUND HYDRAULIC ACTUATOR ASSEMBLY MOUNT HOLE INBOARD SIDE WITH CORROSION (WING SIDE FITTING). LT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FORWARD HINGE FITTING HYDRAULIC ACTUATOR ASSY MOUNT HOLE INBOARD ( WING SIDE FITTING ) CORROSION. REPAIR CARRIED OUT IAW EA NR 1-5750-69355. WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.
Part: SUPPORT — CORRODED (FLAP TRACK) · airframe 42,860 hrs · 9,165 cycles
LEFT WING - OUTBOARD TRAILING EDGE FLAP VANE, NR 1 TRACK SUPPORT FOUND AFT HOLE AND EXTERIOR SURFACE AREA CORRODED (NUMBERED FROM INBOARD). LT WING OUTBOARD TRAILING EDGE FLAP VANE NR 1 TRACK SUPPORT REMOVED AND REPLACED AS PER MM 27-50-32-4.
Part: SKIN — CHAFED (ZONE 500) · airframe 42,860 hrs · 9,165 cycles
SNRM N0344 : LH WING - INBOARD T/E MAIN FLAP HAS CHAFING MARK AT L/E SKIN APPROX. 3 INCHES FROM INBOARD EDGE. CHAFING MARK SMOOTHENED AND FOUND OUT OF LIMIT IAW SRM 57-00-01 VOL.I AND REPAIR CARRIED OUT AT LH WING INBOARD TRAILING EDGE MAIN FLAP LEADING EDGE SKIN IAW SRM 57-00-01 FIG.7 VOL.I
Part: HINGE — CORRODED (ZONE 500) · airframe 42,860 hrs · 9,165 cycles
LT WING, INBOARD TRAILING EDGE FLAP, OUTBOARD AFT HINGE FITTING FOUND PIVOT BEARING MOUNT HOLE INBOARD SIDE CORRODED (FLAP SIDE). REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5750-69357 WINGS - TRAILING EDGE & TRALING EDGE DEVICES - LT INBOARD FLAP HINGE BRACKET REPAIR.
Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 42,860 hrs · 9,165 cycles
SUSPECT HAIRLINE CRACK ON LT WING NR 16 SLAT TRACK INBOARD FITTING. REMOVED AND REPLACED RIB AT LT WING LEADING EDGE INBOARD SLAT TRACK NR 16 SUPPORT IAW SRM 51-31-01 VOL. II AND DRAWING NR ARC2850.
Part: FITTING — CORRODED (TE FLAP HINGE) · airframe 42,860 hrs · 9,165 cycles
LEFT WING - OUTBOARD T/E FLAP, INBOARD AFT HINGE FITTING FOUND PIVOT BEARING MOUNT HOLE INBOARD SIDE CORRODED (FLAP SIDE). LEFT WING - OUTBOARD T/E FLAP, INBOARD AFT HINGE FITTING PIVOT BEARING MOUNT HOLE INBOARD SIDE CORROSION (FLAP SIDE) REPAIR CARRIED-OUT IAW FEDEX EA 1-5750- 69352 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: HINGE — CORRODED (TE FLAP) · airframe 42,860 hrs · 9,165 cycles
RIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR OUTBOARD LUG FOUND PITTING CORROSION. RIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR OUTBOARD LUG REPAIRED AS PER FEDEX EA 1-5750-69353 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT AND RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: RIB — CRACKED (ZONE 600) · airframe 42,860 hrs · 9,165 cycles
RT WING OB FLAP IB UP STOP NOSE SUPPORT RIB ISLAND FOUND CRACKED. REMOVED AND REPLACED RT WING OUTBOARD FLAP INBOARD UP STOP NOSE SUPPORT RIB AS IAW SRM 51-31-01 VOL. II. COMPLIED WITH EA 1-5750-71834 - WINGS - TRAILING EDGE FLAPS - OB TRAILING EDGE FLAP - SECONDARY UP STOP - REPAIR.
Part: RIB — CRACKED (ZONE 500) · airframe 42,860 hrs · 9,165 cycles
LT WING - O/B T/E FLAP ASSY FOUND NR 2 TRACK STOP ISLAND RIB CRACKED AT BARREL NUT MOUNT AREA. REMOVED AND REPLACED RIB AT LT WING OUTBD TRAILING EDGE FLAP IAW SRM 51-31-01 VOL. II AND EA 1-5750-71834 - WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAP - SECONDARY UP STOP - REPAIR.
Part: SUPPORT FITTING — CRACKED (ZONE 600) · airframe 42,860 hrs · 9,165 cycles
RT WING L/E SLAT NR 16 IB TRACK FITTING CRACKED. REMOVED AND REPLACED RIB AT RT WING LEADING EDGE INBOARD SLAT TRACK NR 16 SUPPORT IAW SRM 51-31-01 VOL. II AND DRAWING NO. ARB2850.
Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,860 hrs · 9,165 cycles
FLOOR SEAT TRACK AT STA 635 LH X=8.5 CRACKED. CORRECTIVE ACTION SNRM N0163 : CABIN - FLOOR TRACK AREA AT BS 625 TO BS 745 LT X=8.5 CARRIED OUT SEAT TRACK REPAIR IAW SRM 53-70-00 VOL.I
Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,860 hrs · 9,165 cycles
FLOOR SEAT TRACK AT STA 635 LH X=27.5 CRACKED. DAMAGED FLOOR TRACK AREA FROM BS625 TO BS 665 LH X=27.5 CARRIED OUT SEAT TRACK REPAIR IAW SRM 53-70-00 VOL. I.
Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,860 hrs · 9,165 cycles
FLOOR SEAT TRACK AT STA 635 LH X=47.5 CRACKED. FLOOR TRACK AT STA 635 LH X=47.5 CARRIED OUT REPAIR IAW SRM 53- 70-00 VOL.I.
2002
Part: MODULE — MALFUNCTIONED (AUTOTHROTTLE SYS) · airframe 39,542 hrs · 8,406 cycles
DURING CRUISE AT FL330, SMOKE BEGAN POURING FROM THROTTLE QUADRANT. DISCONNECTED AUTOTHROTTLES, AUTOPILOT & SMOKE QUICKLY DISSIPATED. EMERGENCY DECLARED AND REQUESTED PRIORITY HANDLING TO STANSTED UK. PER CREW DEBRIEF SMOKE DISAPPEARED SIMULTANEOUSLY WITH MANUAL DISCONNECTION OF AUTOTHROTTLES. PERFORMED FCC-1 THRUST CONTROL MODULE RTS TEST PER MM 22-00-00-5. TEST FAILED FOR A/T SERVO WITH NO THROTTLE MOVEMENT DURING TEST. PERFORMED FCC-2 THRUST CONTROL MODULE RTS TEST PER MM 22-00-00-5 & ALL TESTS PASSED. SUSPECT NR 1 A/T SERVO FAILURE WITHIN THE TCM WAS CAUSE OF SMOKE. REQUIRES REPLACEMENT OF THE THRUST CONTROL MODULE.
Part: ANTENNA — FAILED · airframe 38,351 hrs · 8,119 cycles
02-70 BOTH WX RADARS FAILED AFTER T/O. R&R WX RADAR ANTENNA PER MM 34-41-07-4.
Part: NUT — LOOSE (LT & RT MLG) · airframe 38,212 hrs · 8,084 cycles
CLC LT & RT BOLTS LOOSE. REMOVED AND REPLACED TRUNNION NUTS PER CMM. 32-15-01.
2001
Part: FIRE LOOP — FAULTY (NR 1 ENGINE) · airframe 35,433 hrs · 7,425 cycles
AFT T/O LEVEL 1 ALERT FIRE DET NR 1 FAIL ILLUMINATED. NR 1 ENG A-LOOP DEFERRED. *S/D* REMOVED AND REPLACED LWR RAIL WHICH INCLUDED DH8 & DH5 PER MD11 MM 26-11-03-4 B-LOOP. CHECK GOOD.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,661 hrs · 7,244 cycles
AFT FUSELAGE COMPARTMENT ZONE 312 BS 2014 CROWN AREA, ANGLE FOUND CRACKED. *S/D* REMOVED AND REPLACED PER SRM 51-35-01 & 51-33-01 VOL II AND DWG AJC 7372.
Part: CLIP — CRACKED (FUSELAGE) · airframe 34,661 hrs · 7,244 cycles
AFT FUSELAGE COMPARTMENT ZONE 312 BS Y 2092 CANT, CROWN AREA, CLIP CRACKED. *S/D* REMOVED AND REPLACED CLIP PER SRM 51-35-01 & 51-33-01 VOL II AND DWG AJC 7028.
Part: CLIP — CRACKED (FUSELAGE) · airframe 34,661 hrs · 7,244 cycles
AFT FUSELAGE COMPARTMENT ZONE 312 BS Y 2060 CANT, CROWN AREA, TOP SIDE CHANNEL AND LWR SIDE CLIP FOUND CRACKED. *S/D* REMOVED AND REPLACED CHANNEL AND CLIP PER SRM 51-35-01 & 51-33-01 VOL II AND DWG AJC 7372 & AJC 7029. NEW CHANNEL HEAT TREAT CARRIED OUT PER DPS 7.00-01 AND HARDNESS RESULT HRB 83 AS PER DPS 1.05-3.
Part: CLIP — CRACKED (FUSELAGE) · airframe 34,661 hrs · 7,244 cycles
AFT FUSELAGE COMPARTMENT ZONE 312 BS Y 2046 CANT, CROWN AREA, CLIP FOUND CRACKED. *S/D* REMOVED AND REPLACED CLIP PER SRM 51-35-01 & 51-33-01 VOL II AND DWG AJC 7021.
2000
Part: ACTUATOR — INOPERATIVE (ELEVATOR)
DURING CLIMBOUT AC STARTED TO PITCH UP AND DOWN AT FAST RATE. REMOVED AND REPLACED NR 1 FCC PER MM 2-01-03-4. OPS CK NORMAL. REMOVED AND REPLACED ELECTRICAL CONNECTORS ON LIB ELEVATOR ACTUATOR.
1999
Part: FITTING — CRACKED (VERTICAL STAB)
WHILE ACCOMPLISHING EO 1-5510-7-3304 PART 2 AT RT AFT MOST BOTTOM HOLE, WHILE REAMING TO CLEAR-OFF CRACK FOUND A SLEEVE BUSHING ON THE HOLE SKIN SIDE. (SLEEVE BUSHING HAD COME OUT DURING REAMING PROCESS). RT AFT MOST BOTTOM HOLE REPAIR CARRIED OUT AS PER FED EX ENG AUTH NR 1-5530-48153.
Part: FITTING — CRACKED (ELEVATOR)
EDDY CURRENT INSP CARRIED OUT ON NR 4 BANJO FITTING FOUND CRACKS. *S/D* REPAIRS CARRIED OUT PER FEDEX ENG AUTH 1-5530-48154.
Part: BRACKET — CRACKED (RT WING)
RT WING O/B TRAILING EDGE FLAP, AFT REMOVAL OF FWD FAIRING 635AL FOUND I/B HINGE BRACKET FWD O/B END CRACKED. *S/D* REMOVED AND REPLACED PER MM 57-53-01 AND O/B FLAP ASSY REMOVED AND REPLACED PER MM 27-50-30-4.
Part: SUPPORT — CHAFFED (RT WING)
RIGHT WING TRAILING EDGE FLAP AFT REMOVAL FWD FAIR 635AL FOUND HINGE UNDRWING SUPPORT FITTING FWD SIDE I/B AND O/B EDGE WITH DEEP CHAFE MARK. INBD AND OTBD MATERIAL ORIG THICKNESS - 0.210 AFT BLEND-OUT, MATERIAL REMAIN - 0.096 FOR I/B & 0.168 FOR O/B. *S/D* CHAFING MARK REMOVED PER SRM 57-00-01 VOL 1. REPAIRED SUPPORT FITTING PER ENG AUTH NR 1-5720-48152.
Part: ELEVATOR — DAMAGED (LEFT)
LEFT O/B ELEVATOR WITH DAMAGE, O/B END BROKEN OFF. ALSO, LT HORIZONTAL STAB RIB CRACKED. *S/D* REPLACED LT AND RT O/B ELEVATOR PER 27-30-30-4.
Part: LOCK ACTUATOR — INOP (RT MLG)
RT MAIN GEAR DID NOT RETRACT. JACKED A/C PER MM 07-11-00-2 AND SWING LANDING GEAR PER MM 32-31-00-5. REMOVED AND REPLACED RT MAIN LANDING GEAR DOWNLOCK CYLINDER ASSY PER MM 32-33-02-4. REMOVED AND REPLACED RT RESTRICTOR ASSY PER MM 32-33-01-4.
Part: BUNGEE CYLINDER — FAILED (LT MLG)
LEFT MAIN GEAR UNSAFE WARNING SWAP LML BUNGEE CYLINDER WITH RML. REPLACED RML BUNGEE CYLINDER PART FLOWN IN FROM SIN. REMOVED AND REPLACED ABOVE PER MM 32-33-02-04. BLED NR 3 HYD SYS USING NR 3 AUX PUMP. GREASED LMG PIVOT POINTS, CYCLE GEAR 10 TIMES PER MM 32-31-00.
Part: TRIM CYLINDER — FAILED (LT MLG)
LT MAIN GEAR DID NOT RETRACT. REMOVED AND REPLACED LT MAIN GEAR BEAM TRIM CYLINDER FOR MX PREVENTION PER MM 32-37-01-4. LEAK CK COND NORMAL. CANNIBALIZED TRIM CYLINDER FROM AC 617.
1998
Part: PIPE — CRACKED (NR 3 ENGINE)
DECREASE FLUID IN HYD RES NR 3 BOTH PUMPS SHUTDOWN. REMOVED AND REPLACED PUMP CASE DRAIN PIPE PER MM 29-11-20-4. LEAK CHECK, NONE FOUND. REL PER MEL. REPLACED BOTH ENG DRIVEN PUMPS, FILTERS AND BROKEN LINE.
Part: PROX SENSOR — FAILED (LT MLG)
98-0099 NRT:LEFT GEAR UNSAFE INDICATION ON LANDING. RECYCLED GEAR ARM SAME ON LANDING CONFIGURATION PAGE INDICATION GEAR DOWN WITH FLOOR VIEW. REMOVED AND REPLACED DOWN LOCK PROXIMITY SENSOR PER M/M 32-61-15 RETURN TO SERVICE TEST CHECK GOOD.
1997
Part: DOOR ASSY — MISSING (WING)
SLAT DRIVE ACCESS PANEL MISSING, OCCURRED DURING TEST FLIGHT. REMOVED HINGE AND INSTALLED NEW ASSEMBLY. INSTALLED NEW HINGE AND NEW PANEL ASSY. REPAIRED COMPLIED WITH 6-25-97.