Boeing MD-11F

Service difficulty reports · 31,320

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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 = 'MD11F'
  ORDER BY difficulty_date DESC"

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SDR IPXA13M79643Doubler · crackedINSPECTION TYPE :1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 544 REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS542 -547 IAW SRM 57-40-02. REPAIR 15 FIG 206. (MAJOR)Jul 29, 2013 · N290UP · Doug MD11F · Wing, Plate/SkinSDR IPXA13M79617Doubler · crackedINSPECTION TYPE: 1C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 613 REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 610 -616 IAW SRM 57-40-02 REPAIR 15 FIG 206. (MAJOR)Jul 29, 2013 · N290UP · Doug MD11F · Wing, Plate/SkinSDR IPXA3M79576Actuator · leakingHYDRAULIC SYS 3 LEAK, RT INBD ELEVATOR ACTUATOR LEAKING. COMPLETED LMECA 21940 AND 21941. R & R RT INBD ELEVATOR ACTUATOR, REF MM 27-33-20.Jul 29, 2013 · N271UP · Doug MD11F · Elevator Control SystemSDR FDEA201307281676Power Supply · failedON PREFLIGHT, RECEIVED A LEVEL ONE EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED EMERGENCY LIGHT TEST AND ALL TEST PASSED. NEXT MORNING RECEIVED THE MESSAGE AGAIN. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY. CHECKED GOOD IAW AMM CH 33-51-01-4.Jul 28, 2013 · N598FE · Doug MD11F · Emergency LightingSDR FDEA201307281675Power Supply · inoperativePERFORMED EMERGENCY LIGHTS TEST AND ALL TEST PASSED. TESTED AGAIN AND REPRODUCED PROBLEM. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY.Jul 28, 2013 · N598FE · Doug MD11F · Emergency LightingSDR FDEA201307281674Power Supply · failedDURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTS TEST WILL NOT PASS. REPLACED EMERGENCY LIGHT POWER SUPPLY REF MM 33-51-01-4 , TESTED NORMAL.Jul 28, 2013 · N574FE · Doug MD11F · Emergency LightingSDR WRLA20130727601Wedge · debondedDISBOND WAS FOUND ON LT WING OTBD FLAP, NRC6753-503L, WEDGE UPPER SKIN AT STA X OF 614.25 TO 676.5. PERFORM THE LT WING OTBD FLAP WEDGE UPPER SKIN REPAIR IAW EI W2013A57B-2048, REV: 0. CHECK CONDITION SATISFACTORY.Jul 27, 2013 · N382WA · Doug MD11F · Trailing Edge FlapsSDR WRLA201310020600Skin · crackedCRACK ON RT WING FIXED L/E NOSE SKIN AT STA XOS 776. REPAIR RT WING FIXED L/E NOSE SKIN IAW EI W2013A57B-1995, REV 1. CONDITION CHECKED NORMAL.Jul 27, 2013 · N382WA · Doug MD11F · Wing, Plate/SkinSDR WRLA20130727599Skin · crackedCRACK ON LT WING FIXED L/E NOSE SKIN AT STA XOS 944. REPAIR THE DAMAGE AREA, IAW EI W2013A57B-1989, REV1. CONDITION CHECKED NORMAL.Jul 27, 2013 · N382WA · Doug MD11F · Wing, Plate/SkinSDR IPXA3M79512Lamp · inoperativeL1 DOOR SLIDE TEST LIGHT INOPERATIVE. TROUBLESHOT IAW MM 25-61-00. REPLACED PTT LAMP. OPS CHECKED GOOD.Jul 26, 2013 · N293UP · Doug MD11F · Escape SlideSDR FDEA201307251661Skin · crackedEIGHT FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 53, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 25, 2013 · N521FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201307251660Skin · crackedSEVEN FASTENER HOLES FOUND WITH CRACK INDICATIONS. DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 53. REPAIR CJul 25, 2013 · N521FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201307251663Warning Light · false activationDURING PRE-FLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY LIGHTS, EMERGENCY LIGHTS TEST PASS, AND OPERATE NORMALLY. ACFT OK TO CONTINUE.Jul 25, 2013 · N574FE · Doug MD11F · Emergency LightingSDR FDEA201307241655Rib · damagedRT WING NR 8 LEADING SLAT TRACK RIB DRIVE ATTACH LUG BORE HOLES XOS 1113.252 FOUND DAMAGED. REPAIRED IAW EA1-5750-16614. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201307241652Skin · dentedRIGHT WING L/E NR 8 SLAT FWD INBD AREA DENTED. REPAIRED IAW EA 1-5750-166141. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307241651Rib · damagedAFTER RT WING L/E NR 8 SLAT LOWER INNER SKIN REMOVAL, FOUND INTERNAL NR 5 RIB DAMAGED AT XOS 1030.5. REPAIRED IAW EA 1-5750-166142. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307241650Rib · damagedAFTER RT WING L/E NR 8 SLAT LOWER INNER SKIN REMOVAL, FOUND INTERNAL NR 4 RIB DAMAGED AT XOS 1025. REPAIR IAW EA 1-5750-166142. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307241649Rib · damagedAFTER RT WING L/E NR 8 SLAT LOWER INNER SKIN REMOVAL, FOUND INTERNAL NR 1 RIB, DAMAGED AT XOS 1010.5. REPAIRED IAW EA 1-5750-166142. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 24, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307241672Power Supply · inoperativeDURING PRE-FLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY ONE LOW WARNING. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY LIGHTS, EMERGENCY LIGHTS TEST PASS, AND OPERATE NORMALLY. ACFT OK TO CONTINUE.Jul 24, 2013 · N574FE · Doug MD11F · Emergency LightingSDR FDEA201307241657Indicator · inoperativeLEFT EVACUATION SLIDE, REMOTE PUSH TO TEST INDICATOR INOPERATIVE.Jul 24, 2013 · N612FE · Doug MD11F · Escape SlideSDR FDEA201307241646Solenoid · crackedREMOVED NR 3 RT EDP DUE TO LOST OF HYD FLUID AND PART REMOVAL FROM A/C ONLY, NO INSTALLATION. REPLACED NR 3 RT EDP DEPRESS SOLENOID VALVE AND FUNCTION CHECK OK IAW MM 29-11-21-4. ACFT OK FOR SERVICE.Jul 24, 2013 · N589FE · Doug MD11F · Hydraulic System, MainSDR FDEA201307231642Rib · damagedON REMOVAL OF RIGHT WING L/E NR 8 SLAT LOWER SKIN, NR 2 RIB FROM INBD WAS FOUND DAMAGED AT APPROX XOS 1015. REPAIRED IAW EA 1-5750-166142. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 23, 2013 · N521FE · Doug MD11F · Leading Edge DevicesSDR FDEA201307221626Structure · corrodedLEFT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE ACTUATOR INBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08, REV 76. REPAIR CARRIED OUT IAW EA 1-5750-166143, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221625Structure · corrodedLEFT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE UPPER MOUNT OTBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-08, REV 76. REPAIR CARRIED OUT IAW EA 1-5750-166143, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221624Structure · corrodedLEFT WING OTBD FLAP INBD FORWARD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORRODED. BARREL NUT BORE SURFACE REWORKED IAW CMM 20-10-6, REV 76. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08, REV 76. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221623Structure · corrodedRIGHT WING OTBD FLAP, INBD FORWARD (WING SIDE) HINGE UPPER MOUNT INBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 76, REPAIRED IAW EA 1-5750-T0301348, PART 1 STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221622Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE UPPER MOUNT OTBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 76. REPAIRED IAW EA 1- 5750-T0301348, PART 1, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221621Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE ACTUATOR INBD BORE CORRODED. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 76. REPAIRED IAW EA 1-5750-T0301348, PART 1, STEP 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221617Structure · corrodedRIGHT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL MOUNT LOWER BORE CORRODED. BORE NR 7 REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1- 5750-T0301349, PART 1, STEP 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221615Structure · corrodedRIGHT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE BARREL MOUNT UPPER BORE CORRODED. BORE NR 7 REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 76. REPAIRED IAW EA 1- 5750-T0301349, PART 1, STEP 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221614Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE UPPER MOUNT INBD BORE CORRODED. REPAIRED IAW EA 1- 5750-T0301349 PART 1 STEP 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA3M79516Battery · warning lightEMERGENCY LIGHT BATTERY ONE LOW MESSAGE. TROUBLESHOT IAW FIM 33-51-00. EMERGENCY LIGHT TEST PASSED IAW AMM 33-51-00. SYS OK.Jul 22, 2013 · N270UP · Doug MD11F · Emergency LightingSDR IPXA13M79446Skin · crackedTWO INCH CRACK ON LT WING LWR SURFACE OF L/E SKIN. REPAIRED IAW EO MD11-5730-50299-B.Jul 22, 2013 · N286UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201307221632Tee Fitting · corrodedLT OTBD FLAP VANE TEE FITTING "B" MOUNTING HOLE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02 REPAIR 5 FIG.201 REV 53. REPAIRED IAW EA 1-5750-T0301579 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221631Tee Fitting · corrodedRT OTBD FLAP VANE TEE FITTING "F" MOUNTING HOLE CORRODED. FOUND EXCEEDED LIMIT IAW SRM 57-50-02, REPAIR 5, FIG 201, REV 53. REPAIRED IAW EA 1-5750-T0301580, PART 1 STEP 1.B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221630Tee Fitting · corrodedRIGHT OTBD FLAP VANE TEE FITTING "C" MOUNTING HOLE CORROSION. FOUND EXCEEDED LIMITS IAW SRM 57-50-02, REPAIR 5, FIG 201, REV 53. REPAIRED IAW EA1-5750-T0301580, PART 1 STEP 1.A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221629Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD AFT (FLAP) HINGE PIVOT HOLE INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-52-04, REV 76. REPAIRED IAW EA 1-5750-166144. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221628Bushing · wornRIGHT WING FLAP OTBD HINGE (FLAP SIDE), PIVOT OTBD BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76 AND FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. NEW BUSHING FABRICATED BY MACHINING AND INSTALLED EA 1-5750-102153C, PART 3, STEP 2. REPAIRJul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221627Bushing · wornRIGHT WING: RT INBD FLAP OTBD HINGE (FLAP SIDE) , PIVOT INBD BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 76. NEW BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-102153C, PART 3, STEP Jul 22, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307221619Bushing · wornRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR, OUTBOARD BORE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 76. NEW BUSHING AND REPAIR WASHER FABRICATED AND INSTALLED IAW EA 1-5750-T0301349, PART 1Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221618Bushing · wornRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR INBD BORE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0301349, PART 1, STEP 3. REPAIR CLAJul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307221616Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FORWARD (WING) HINGE BARREL MOUNT HAS SURFACE CORROSION. REWORKED IAW CMM 20-10-6, REV 76. FOUND WITHIN DWG NR ARC0503 AND CMM 57-44-09, REV 19, TABLE 601 LIMITS. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 116.Jul 22, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA13M79440Attach Fitting · crackedINSPECTION TYPE:1C, LT LOWER WINGLET FWD ATTACH FITTING CRACKED. REPLACED BOTH LT LOWER WINGLET ATTACH FITTINGS BY INSTALLING KIT SB11570063-3 IAW EO MD11-5720-27680-C, APPX D.Jul 21, 2013 · N255UP · Doug MD11F · Wing, Attach FittingsSDR FDEA201307201601Switch · failedSLIDE PRESSURE LIGHT IN L1 DOOR WAS INOPERATIVE, REPLACED LIGHT SWITCH ASSY IAW MM 25-61-04-4. OPS CHECKED NORMAL.Jul 20, 2013 · N579FE · Doug MD11F · Passenger/Crew DoorsSDR IPXA2016080206622Spar Cap · corrodedINSPECTION TYPE: 1C, LT WING REAR SPAR CAP HAS CORROSION BETWEEN XORS. 784.5 TO 829. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6374 REV. I/R AND EO MD11-5710-61421-A.Jul 19, 2013 · N278UP · Doug MD11F · Wing SparSDR FDEA201307191590Hinge Fitting · crackedRIGHT WING T/E OTBD FLAP INBD FORWARD HINGE BRACKET SIDE LOAD FITTING CRACKED. R & R IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 19, 2013 · N521FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201307191588Support Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT FOR OPEN HOLE INSPECTION FOUND TWO CRACK INDICATIONS ON NR 1 MAIN DECK CARGO DOOR LOWER FRAME SUPPORT FITTING AT HOLE "C" AND "D". R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVISION 116.Jul 19, 2013 · N521FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201307191593Wedge · delaminatedRIGHT WING -OTBD FLAP INBD T/E WEDGE FOUND DELAMINATED AT XOFH 458.240 TO XOFH 465.49. REPAIRED IAW EA 1-5750-T0301239 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Jul 19, 2013 · N642FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307191591Stop Fitting · crackedLEFT WING OTBD FLAP STOP FITTING CRACKED. STOP FITTING REMOVED IAW SRM 51-31-01, REV 53, HOLES PICKED UP ON NEW STOP FITTING IAW DWG ARC4125, REV G AND SRM 51-31-02 REV 53 NEW STOP FITTING INSTALLED IAW SRM 51-33-01, REV 53. REPAIR CLASSIFIED MAJOR IAW GMM 6Jul 19, 2013 · N521FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307191589Web · canningCENTER LANDING GEAR WHEEL WELL, OIL CANNING FOUND AT RT KEELBEAM WEB, ABOVE FORWARD DOOR HINGE LINE. REPAIRED IAW EA 1-5310-T0301311, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jul 19, 2013 · N521FE · Doug MD11F · Fuselage Miscellaneous Structure
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