Mcdonnell Douglas MD-11

Service difficulty reports · 7,956

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'MD11'
  ORDER BY difficulty_date DESC"

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SDR WRLA20090926225Beam · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LEFT MAIN LANDING GEAR TRUCK BEAM PIVOT PIN. REMOVED THE LEFT MAIN LANDING GEAR TRUCK BEAM PIVOT PIN IAW AMM 32-12-20-000-908 REV 65. INSTALLED THE LEFT MAIN LANDING GEAR TRUCK BEAM PIVOT PIN IAW AMM 32-12-20Sep 26, 2009 · N271WA · Doug MD11 · Main Landing Gear Strut/Axle/TruckSDR WRLA20090926221Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 925-968, X=-75.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926220Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 840-870, X=-27.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926217Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 820-864, X=-8.50. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 REPAIR 1 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926214Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D FLOOR SUPPORT AT STA 1880, X=36. REPLACEMENT FLOOR SUPPORT IAW MD-11 SRM 51-31-01 REV41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926211Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D CABIN FLOOR SUPPORT, STA 1878 X=-36. REPLACEMENT FLOOR SUPPORT IAW MD-11 SRM 51-31-01 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926254Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON LONGERON SPLICE FITTING, CENTER CARGO, STA 5-123, L4R. PART REPLACED PER WOA EI W2009P53B-1134 REV 00.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR WRLA20090926219Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 457, X=-33.5. CLEAN-UP CORROSION AREA MEASURE THE ORIGINAL AND REWORK THICKNESS RESULT: 0.090-0.082" (REF JOB CARD ATTACHING SHEET 074291) WITHIN LIMITS PER MD-11 SRM 53-00-00 PAGE 206 RESep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926209Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 453-455, X=-27.5. CLEAN-UP CORROSION AREA MEASURE THE TRACK AREA THICKNESS: 0.100" (REF JOB CARD ATTACHING SHEET 074290) WITHIN LIMITS PER SRM 53-00-52 REV 41. APPLY PROTECTION COATING PSep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926228Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION M/D CABIN SEAT TRACK, STA1875 Y=8.5. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926215Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1881, X=-47.50. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926213Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1878, X=27.50. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926212Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D CABIN SEAT TRACK, STA 1881 Y=-8.50. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926210Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1880, X=-27.50. REPAIR THE SEAT TRACK PER MD-11 SRM 53-00-52 REV 41, APPLY PROTECTION COATING PER MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090919208Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK BETWEEN STA 1351 AND STA 1361, X=107.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 RPR 1 REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV41.Sep 19, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090918205Skin · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK WITH FASTENER HOLE WORN OUT ON INBD/OUTBD SKIN (P/N: AUB7562-5 AND AUB7652-6) OF NR 3 PYLON FWD FAIRING. PERFORM EI W2009A54B-1109, REV 00 TO REPAIR THE DAMAGED AREA.Sep 18, 2009 · N271WA · Doug MD11 · Nacelle/Pylon, Plate/SkinSDR WRLA20090917203Skin Panel · crackedDURING 2C CHECK, EGAT MECHANIC FOUND SKIN BULGE ON RT NOSE FUSELAGE UPPER, STA 275, X=-10. INSTALLED SKIN REPAIR IAW EI W2009A53B-1120 REV 00.Sep 17, 2009 · N271WA · Doug MD11 · Fuselage Main, Plate/SkinSDR WRLA20090917202Doubler · crackedCRACK - DURING 2C CHECK, EGAT MECHANIC FOUND THE STIFFENER DOUBLER AT THE CENTER GEAR W/W WEB Y:1381, X:-31.50 HAS CRACKED FROM THE FASTENER AREA (RIGHT STIFFENER). ACCORDING TO EI W2009A53B-1115 REV 00 TO FABRICATE REPAIR PARTS. RE-INSTALLED FASTENERS PER MSep 17, 2009 · N271WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA20090917201Doubler · crackedCRACK - DURING 2C CHECK, EGAT MECHANIC FOUND THE STIFFENER DOUBLER AT THE CENTER GEAR W/W WEB Y:1382, X:+31.50 HAS CRACKED FROM THE FASTENER AREA (LEFT STIFFENER). ACCORDING TO EI W2009A53B-1114 REV 00 TO FABRICATE REPAIR PARTS. REINSTALL FASTENERS PER MD-11Sep 17, 2009 · N271WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA20090917204Fitting · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON NLG TRUNNION SUPPORT FITTING, Y=582, X=24. CRACK LENGTH MEASURED 1 INCH. REPAIR THE NLG TRUNNION SUPPORT FITTING IAW MD-11 SRM 53-10-14 FIGURE 202, REPAIR 2, REV 41.Sep 17, 2009 · N271WA · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR WRLA20090916200Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF LEFT OUTBOARD T/E FLAP CRACK. ACCOMPLISH EI NR:W2009A57B-1093, REV 00 AND EI NR:W2009A57B-1205.Sep 16, 2009 · N271WA · Doug MD11 · Trailing Edge FlapsSDR WRLA20090916199Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF RIGHT OUTBOARD T/E FLAP CRACK. ACCOMPLISH E.I NO:W2009A57B-1092, REV 00 AND E.I NR :W2009A57B-1207 REV 00.Sep 16, 2009 · N271WA · Doug MD11 · Trailing Edge FlapsSDR FDEA200909143298Door · out of alignmentDURING LWR AFT CARGO DOOR OPERATION FOUND DOOR UNABLE TO CLOSE DUE TO INTERFERENCE AT FWD LWR CORNER. AFT CARGO DOOR REMOVED AND REINSTALLED IAW AMM 52-33-04-4 REVISION 64. AFT CARGO DOOR HINGE REPAIR BUSHING FABRICATED AND INSTALLED IAW SRM 52-30-16 FIG 1Sep 14, 2009 · N573FE · Doug MD11 · Cargo/Baggage DoorsSDR FDEA200909143297Skin · erodedLT WING - NR 5 SPOILER T/E LWR SURFACE FOUND 02 EACH LOCATIONS, ERODED. REPAIR CARRIED OUT IAW EA 1-5770-132216. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 107.Sep 14, 2009 · N573FE · Doug MD11 · SpoilersSDR FDEA200909063264Skin · corrodedLT WING UPPER SKIN AT STA, XORS 378 FOUND CORROSION. REPAIR IAW EA 1-5710-132212 TITLE: "WINGS-LT WING UPPER SKIN SURFACE CORROSION - REPAIR"Sep 6, 2009 · N580FE · Doug MD11 · Wing, Plate/SkinSDR FDEA200908243075Skin · gougedFUSELAGE SKIN ADJACENT TO NOSE JACK POINT FOUND WITH DEEP SCRATCH MARK, SKIN. REPAIR CARRIED OUT IAW SRM 53-20-01 REPAIR 2, FIG 201, REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 107.Aug 24, 2009 · N573FE · Doug MD11 · Fuselage Main, Plate/SkinSDR FDEA200908193047Seat Track · corrodedCABIN - LT SEAT TRACK CROWN AREA AT STA 6-10 TO STA 6-30, X = -8.5 FOUND SURFACE CORROSION. REMOVED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52, FIG 201, REVISION 41. SEAT TRACK SPLICE REPAIR CARRIED OUT FROM STA 6-0 TO STA 6-25, X = -8.5 IAW SRM 53-00-52, Aug 19, 2009 · N573FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908193046Skin · corrodedAFT ACCESSORY COMPARTMENT RT SKIN BETWEEN STA 2140 AND STA 2163 (ACCESS PANEL NR347DF LWR ANCHOR NUT MOUNTING AREA) FOUND WITH SEVERE CORROSION. REPAIRED AS PER SRM 53-70-01 FIGURE 201 REVISION 41. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Aug 19, 2009 · N573FE · Doug MD11 · Fuselage Main, Plate/SkinSDR FDEA200908173033Structure · unknownRT HORIZONTAL STABILIZER AFT OPERATING BULKHEAD TRIMMED FOR BARREL NUT HOLE NR 35R REWORK ACCESS AND FOUND EXCEEDED EO LIMITS. COMPLIED WITH EA NR 1-5510-131640, TITLE: STABILIZER - HORIZ (AD 2003-22-08, EO 1-5510-7-5000) - RT OPERATING BULKHEAD FITTING TRIAug 17, 2009 · N573FE · Doug MD11 · Horizontal Stabilizer StructureSDR FDEA200908173032Hinge Bracket · corrodedLT WING OTBD FLAP, OTBD HINGE (WING SIDE) SIDELINK LWR HOLE FOUND CORRODED. COMPLIED WITH EA 1-5750-132180. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 17, 2009 · N573FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA200908163026Support Fitting · crackedCRACK INDICATION FOUND DURING HEFC OPEN HOLE INSPECTON ON LEFT WING OUTBOARD FLAP HINGE SUPPORT FITTING, MOST OUTBOARD FASTENER HOLE AT 3 O' CLOCK POSITION LOOKING AFT. REPAIR CARRIED OUT IAW EA NR 1-5750-132199. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMMAug 16, 2009 · N573FE · Doug MD11 · Wing Miscellaneous StructureSDR FDEA200908163025Support Fitting · crackedCRACK INDICATION FOUND DURING HEFC OPEN HOLE INSPECTON ON RIGHT WING OUTBOARD FLAP HINGE SUPPORT FITTING MOST OUTBOARD FASTENER HOLE AT 7 O'CLOCK POSITION LOOKING AFT. REPAIR CARRIED OUT IAW EA NR 1-5750-132200. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-Aug 16, 2009 · N573FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA200908163024Skin · damagedLEFT WING NR 8 SLAT INTERIOR SURFACE SKIN INBOARD TOP CORNER FOUND CHIPPED-OFF AT XOS 1005. CARRIED OUT REPAIR IAW SRM 57-40-01 FIG 201 REPAIR 3, REV 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 16, 2009 · N573FE · Doug MD11 · Leading Edge DevicesSDR FDEA200908153021Skin · corrodedHORIZONTAL STABILIZER LEFT PLANK 36L BARREL NUT BORE BEARING AREA CORROSION REWORK EXCEEDED E.O. 1-5510-7-5000D1 PART 1 LIMITATIONS. REPAIR CARRIED OUT AS PER E.A. 1-5510-131639, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Aug 15, 2009 · N573FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WRLA20090814255Skin · damagedTHE RT DETACHABLE ELEVATOR WAS DAMAGED DUE TO CONTACT WITH GROUND EQUIPMENT. THE UPPER AND LOWER SKINS WERE DAMAGED ON THE TRAILING EDGE. THE INBD CORNER WAS CRACKED AND WAS REMOVED THROUGH ALL PLIES. IN ADDITION, THE INNERMOST PLY OF THE OUTER SKIN IS DAMAAug 14, 2009 · N271WA · Doug MD11 · Elevator, Plate/SkinSDR FDEA200908132997Skin · misrepairedEXISTING EXTERNAL REPAIR DOUBLER FOUND AT RT WING NR 5 SLAT L/E EXTERIOR SKIN. EXISTING EXTERNAL REPAIR DOUBLER AT RT WING NR 5 SLAT L/E EXTERIOR SKIN EVALUATED AND FOUND NOT IAW SRM REPAIR. REPAIR CARRIED OUT IAW EA NR 1-5750-133822, TITLE: WINGS - FLIGHTAug 13, 2009 · N573FE · Doug MD11 · Leading Edge DevicesSDR FDEA200908132996Skin · misrepairedEXISTING EXTERNAL REPAIR DOUBLER FOUND AT RT WING SLAT NR 7 L/E EXTERIOR SKIN. EXISTING EXTERNAL REPAIR DOUBLER AT RT WING SLAT NR 7 L/E EXTERIOR SKIN EVALUATED AND FOUND NOT IAW SRM REPAIR. RT WING NR 7 SLAT ASSY REMOVED AND REPLACED IAW AMM 27-80-30-4, RAug 13, 2009 · N573FE · Doug MD11 · Wing, Plate/SkinSDR WRLA20090813197Engine · oil consumptionEN ROUTE TO ATL, AIR SYSTEM PRODUCED OILY SMELL. SHUT DOWN PACK NR 1 AND SMELL WENT AWAY. OIL QUANTITY OF NR 1 ENGINE DECREASED FROM 16 TO 3 QUARTS DURING 13 HOURS OF FLIGHT. REPLACED NR 1 ENGINE.Aug 13, 2009 · N270WA · Doug MD11 · Engine (Turbine/Turboprop)SDR FDEA200908133003Skin · corrodedHORIZONTAL STABILIZER LEFT HAND UPPER PLANK 02L BARREL NUT BORE BEARING AREA CORROSION REWORKED EXCEEDED E.O. 1-5510-4-5000D1 PT1 LIMITATION. REPAIR CARRIED OUT AS PER E.A. 1-5510-131652, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Aug 13, 2009 · N573FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR FDEA200908122995Skin · misrepairedEXISTING EXTERNAL REPAIR DOUBLER FOUND AT LT WING INBD FLAP LWR SKIN BETWEEN STA (XIFH 153.300) AND (XIFH 159.300). EXISTING EXTERNAL REPAIR DOUBLER AT LT WING INBD FLAP LWR SKIN BETWEEN STA (XIFH 153.300) AND (XIFH 159.300) EVALUATED AND FOUND NOT IAW SRM REAug 12, 2009 · N573FE · Doug MD11 · Trailing Edge FlapsSDR FDEA200908122992Fitting · crackedLEFT HAND WING LEADING EDGE FRONT SPAR VICINITY NR 16 SLAT TRACK OUTBOARD RIB SUSPECTED CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01, REV 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 107.Aug 12, 2009 · N573FE · Doug MD11 · Wing, Rib/BulkheadSDR FDEA200908122991Longeron · corrodedCENTER CARGO COMPARTMENT DOORWAY BILGE LONGERON 50 LT AT STA 1701 FOUND CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-05, FIG 201, REV 41 AND EA NR 1-5310-132191. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 107.Aug 12, 2009 · N573FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR FDEA200908122990Longeron Splice · crackedMAIN DECK - STA 1997 LONGERON 23L, LONGERON SPLICE SUSPECTED CRACKED. MAIN DECK-LONGERON 23L AT STA 1997. CRACKED LONGERON SPLICE REMOVE AND REPLACED IAW SRM 51-31-01 REVISION 41. NEW SPLICE FABRICATED IAW DWG AJC7253, REVISION C. REPAIR CLASSIFIED AS MAug 12, 2009 · N573FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR FDEA200908122989Structure · damagedBARREL NUT HOLES INSPECTION/ RPAIR - ACCESS TO TRIM LEFT HAND STABILIZER AFT OPERATING BULKHEAD FOR 35L REWORK. COMPLIED WITH E.A. 1-5510-131637, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Aug 12, 2009 · N573FE · Doug MD11 · Horizontal Stabilizer StructureSDR FDEA200908122988Hinge Bracket · corrodedRIGHT HAND WING OUTBOARD INBOARD HINGE (WING SIDE) LOWER OUTBOARD ATTACH HOLE FOUND CORRODED. COMPLIED WITH EA 1-5750-132179. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 12, 2009 · N573FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA200908112971Hinge Fitting · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE FOUND WITH PITTING CORROSION. COMPLIED WITH EA 1-5750-132282. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.Aug 11, 2009 · N573FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA200908112970Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND WITH PITTING CORROSION HINGE FITTING. COMPLIED WITH EA 1-5750-132282. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.Aug 11, 2009 · N573FE · Doug MD11 · Trailing Edge FlapsSDR FDEA200908112969Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE FOUND WITH PITTING CORROSION. COMPLIED WITH EA 1-5750-132283. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 11, 2009 · N573FE · Doug MD11 · Trailing Edge FlapsSDR FDEA200908112968Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND WITH PITTING CORROSION HINGE FITTING. COMPLIED WITH EA 1-5750-132283. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.Aug 11, 2009 · N573FE · Doug MD11 · Trailing Edge FlapsSDR FDEA200908092960Hinge Fitting · crackedRIGHT HAND WING - LEADING EDGE STRUCTURE RIB APPROXIMATELY XOS 910 FOUND CRACKED AT STA XOS 1003.124. REMOVED AND REPLACED IAW SRM 51-33-01, REVISION 41 AND DWG ARB2921, REVISION A. REPAIR CLASSIFIED AS MINOR GMM 6-2-100, REV 107.Aug 9, 2009 · N573FE · Doug MD11 · Wing, Control Surface Attach Fittings
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