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 IPXA3M78499Cap · corrodedINSPECTION TYPE:4C, CORROSION ON PANEL LANDING AT PANEL ACCESS 541JB LT WING STA XORS 372 TO 433. REPAIRED LT WING T/E BEAM ASSY LOWER CAP BETWEEN XW314 AND XW373 REF STASA EA 011-5710-01-A4599 IR, EO MD11-5720-50639-A AND FORM 8 110-3.Apr 29, 2013 · N271UP · Doug MD11F · Wing Main, Frame StructureSDR FDEA201304290881Floor Support · crackedFLOOR SUPPORT CRACKED AT BS 2000-2007 X=20. R & R WITH NEW FLOOR SUPPORT IAW AMM 20-50-02 REV 75.2 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 116.Apr 29, 2013 · N608FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201304280879Skin · crackedRIGHT WING - L/E LOWER SURFACE NR 12 SLAT TRACK CUT-OUT SKIN FOUND CRACKED AT XOS 777. DURING OTBD SLAT DRIVE CABLES INSPECTION. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7 REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201304280878Frame · dentedBS 1661 LONGERON 12R FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201304280877Door Frame · crackedL3 DOOR FORWARD FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201304280876Door Frame · crackedR3 DOOR AFT FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201304280875Door Frame · crackedR3 DOOR FORWARD FRAME WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, StructureSDR IPXA3M78075Fire Detector · inoperativeFIRE DETECTOR NR 3 FAULT ILLUMINATED ON STATUS PAGE AT TOP OF DESCENT. T/S PER FIM 26-11-00-101. CONFIRMED FIRE LOOP DH23 IS INOP AND RESPONDER BROKEN. REMOVED NR 3 ENG UPPER LEFT FIRE DETECTOR ASSY. REPLACED LEFT UPPER RESPONDER AND POSITION LOOP ASSY. PERFOApr 26, 2013 · N254UP · Doug MD11F · Fire DetectionSDR FDEA201304260865Skin · crackedLEFT WING INBD FLAP UPPER SURFACE FOUND CRACKED AT XIFH 177 AND 58" FROM T/E. REPAIRED IAW EA 1-5750-166124. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.Apr 26, 2013 · N580FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201304260863Skin · looseLEFT WING INBD FLAP UPPER SURFACE, SEVERAL FASTENERS AT XIFH 159 FOUND LOOSE. R & R WITH NEW FASTENERS IAW SRM 51-35-01, REV 52. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.Apr 26, 2013 · N580FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201304260862Seat Track · corrodedEXFOLIATION CORROSION FOUND ON SEAT TRACK BASE AT BS 491 TO 502, X= -27.5. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 26, 2013 · N580FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201304240840Skin · misrepairedRT WING FIXED L/E SURFACE TELESCOPIC DUCT CUT-OUT AREA MISREPAIRED. REPAIRED IAW SRM 57-40-01, REPAIR 10, FIGURE 201, REV 52 AND EA 1-5730-166121. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 24, 2013 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201304240843Skin · delaminatedRIGHT WING OTBD FLAP T/E WEDGE INBD EDGE FORM DELAMINATED FROM XOFH 458.690 TO XOFH 468.690. REPAIRED IAW EA 1-5750-166120. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.Apr 24, 2013 · N580FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201304240842Skin · crackedLT WING INBD FLAP UPPER SKIN AT XIFH= 171, 52" FROM T/E FOUND WITH 1 INCH CRACK. REPAIRED IAW EA 1-5750-166124. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 24, 2013 · N580FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201304240841Skin · crackedRT WING NR 5 SLAT LOWER SURFACE FOUND CRACK ABOUT 5 INCHES LONG AT XOS 717. REPAIRED IAW EA 1-5750-166127, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 24, 2013 · N580FE · Doug MD11F · Leading Edge DevicesSDR FDEA201304240839Access Panel · corrodedRT WING T/E LOWER ACCESS PANEL 641JB CUT-OUT FWD EDGE LOWER CAP SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5710-166116. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 24, 2013 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201304230831Frame · misrepairedFRAME MISREPAIRED AT CABIN BS 535, L24L. REPAIRED IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 23, 2013 · N580FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201304230830Frame · misrepairedFRAME MISREPAIRED AT CABIN STATION 535, L19L. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 52. EO 1-5100-7-5001B3, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 23, 2013 · N580FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201304230832Door Frame · corrodedCARGO DOOR CUTOUT LOWER FRAME UPPER SURFACE BS 660 FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 52 AND DRAWING ACA7224 REVISION G. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Apr 23, 2013 · N608FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201304220825Seat Track · corrodedBS 5-49 X= -8.5 SEAT TRACK LOBE FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 5 SHEET 2 OF 3 REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.Apr 22, 2013 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR CLCA20130422001Hydraulic Line · looseDURING CRUISE, LEVEL 1 HYD PUMPS 1L, 2L, 3L OFF APPEAR ON SD AND ENG HYD PUMP CONTROL RIGTH CB POPPED OUT. LEVEL 1 SEL HYD SYS MAIN DURING FLIGHT. PRIOR TO LANDING MIA, LEVEL 2, HYD 3 FAIL DUE TO LOSS OF ALL HYD FLUID. MANUALLY EXTENDED LG, LANDED WITHOUT IApr 22, 2013 · N984AR · Doug MD11F · Hydraulic System, MainSDR IPXA13M78122Skin · nickedINSPECTION TYPE:1C, LT INBD FLAP LWR SKIN SURFACE HAS TWO NICKS AT APPX 58.5" FROM INBD EDGE. REPAIRED LT INBD LWR SKIN AT 58.5" FROM INBD EDGE REF SRM 57-50-01, REPAIR 1, FIG 201.Apr 21, 2013 · N277UP · Doug MD11F · Trailing Edge FlapsSDR IPXA13M78120Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED L/E BEADED DOUBLER CRACKED 18" INBD OF NR 12 SLAT TRACK. REPAIRED RT WING L/E BEADED DOUBLER 18" INBD OF NR 12 SLAT TRACK REF SRM 57-40-02, REPAIR 15, FIG 203.Apr 21, 2013 · N277UP · Doug MD11F · Wing, Plate/SkinSDR WRNA201300010Battery · defectiveDURING TOP OF CLIMB, CREW NOTICED AIRCRAFT BATTERIES NR 1 & 2 INDICATING LOW VOLTS. THEY WERE INSTRUCTED BY MAINTENANCE CONTROL TO RETURN SINCE THEY WERE 45 MINUTES OUT. ACFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH NR 1 & 2 Apr 21, 2013 · N952AR · Doug MD11F · Battery/Charger SystemSDR FDEA201304210822Paint · peelingRT OTBD AILERON UPPER AND LOWER SURFACES PAINT PEELED. SURFACE PAINT TOUCHED UP IAW SRM 51-21-02, REV 52. REPAIR CLASSIFIED AS MINOR IAW GMM -6-2-100, REV 116.Apr 21, 2013 · N583FE · Doug MD11F · AileronsSDR IPXA13M78118Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E XOS 640.7174 BEADED DOUBLER FOUND CRACKED. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS 640.7174 REF SRM 57-40-02, REPAIR 15, FIG 203.Apr 20, 2013 · N277UP · Doug MD11F · Wing, Plate/SkinSDR IPXA13M78116Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E XOS 613.1502, BEADED DOUBLER FOUND CRACKED. REPAIRED BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.Apr 20, 2013 · N277UP · Doug MD11F · Wing, Plate/SkinSDR IPXA3M78090Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR STA XOS627. REPAIRED LT WING L/E INNER BEADED DOUBLER BETWEEN STA XOS 625-629 IAW EO MD11-5730-48222-A (MAJOR).Apr 20, 2013 · N277UP · Doug MD11F · Wing, Plate/SkinSDR IPXA3M78089Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR STA XOS 646 REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 643-648 IAW UPS EO MD11-5730-48222-A (MAJOR).Apr 20, 2013 · N277UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201304200821Seat Track · corrodedBS 1219 -1259 X= -75.25. SEAT TRACK FOUND CORRODED. REPAIRED IAW 53-00-52 FIGURE 201 REPAIR 1REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116Apr 20, 2013 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201304200819Seat Track · corrodedBS 5-65 X= 8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 52 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116Apr 20, 2013 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201304200818Bulkhead Web · crackedCENTER CARGO AFT BULKHEAD PANEL FOUND CRACKED AT BS 1841 X= - 52. BULKHEAD WEB REMOVED AND REPLACED WITH NEW FABRICATED WEB AS PER SRM 51-31-01 REVISION 52 NEW WEB FABRICATED AS PER DRAWING AGA7170 REVISION T. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-10Apr 20, 2013 · N608FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201304200817Bulkhead Web · crackedCENTER CARGO AFT BULKHEAD PANEL CRACKED AT BS 1841 X= -20. BULKHEAD WEB REMOVED AND REPLACED WITH NEW FABRICATED WEB AS PER SRM 51-31-01 REVISION 52 NEW WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REVISION T. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVIApr 20, 2013 · N608FE · Doug MD11F · Fuselage Main, BulkheadSDR IPXA3M78076Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR STA XOS696. REPAIRED LT WING L/E INNER BEADED DOUBLER BETWEEN STA XOS 692-698 IAW EO MD11-5730-48222-A.Apr 20, 2013 · N277UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201304200873Wire · damagedSHORTLY AFTER STARTING APU AUTO SHUTDOWN WITH FIRE HANDLE ILLUMINATED. NO AURAL WARNING. NO INDICATION OF ACTUAL FIRE. REPAIRED WIRING INSULATION IAW SWPM 20-10-01. OPS AND LEAK CHECKED GOOD. FIRE WARNING TEST OF APU GOOD.Apr 20, 2013 · N601FE · Doug MD11F · Fire Protection System WiringSDR FDEA201304200820Frame · dentedBS 1721 L12L FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52, REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIApr 20, 2013 · N608FE · Doug MD11F · Fuselage Main, FrameSDR IPXA3M78079Access Panel · crackedINSPECTION TYPE:1C, 9 CRACKED FASTENER HOLES IN RT WING LWR SKIN AT FUEL TANK ACCESS PANEL BETWEEN XORS683.4 -713.6. REPAIRED CRACKED FASTENER HOLES IAW SRM 57-20-02, REPAIR 5 (MINOR).Apr 18, 2013 · N253UP · Doug MD11F · Wing, Plate/SkinSDR IPXA3M78078Skin · crackedINSPECTION TYPE:1C, LT WING LOWER SKIN CRACKED AT 4 FUEL TANK ACCESS PANEL FASTENER HOLES BETWEEN STA XORS 683.4 - 713.6. REPAIRED CRACKED FASTENER HOLES IAW SRM 57-20-02, REPAIR 5 (MINOR).Apr 18, 2013 · N253UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201304180805Structure · corrodedLT WING T/E LOWER CAP AT 541JB CUT OUT ACCESS FOUND SURFACE CORROSION AT XW326. REMOVED AND REPLACED WITH NEW CAP AS PER SRM 51-33-01 REVISION 52. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Apr 18, 2013 · N608FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201304180803Skin · delaminatedRIGHT OTBD AILERON INBD T/E UPPER SURFACE FROM XOA 841 TO XOA 860 FOUND DELAMINATED. EA 1-5750-166115 AND SRM 57- 60-80 REPAIR 1 PARA. 4A HAS BEEN COMPLIED WITH. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Apr 18, 2013 · N608FE · Doug MD11F · AileronsSDR FDEA201304180804Trunnion · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON STOP DRILL IN THE LT NLG TRUNNION FITTING AND FOUND CRACK PROPAGATION FROM THE SLOT OUT APPROX .2500 INCHES IN LENGTH. TRUNNION REPAIRED IAW SRM 53-10-14, FIG 202, REPAIR 2, REV 52. REPAIR CLASSIFIED MAApr 18, 2013 · N608FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201304180802Mechanism · dirtyAFTER TAKEOFF, RECEIVED RED PRIMARY & SECONDARY LIGHTS WITH THE GEAR HANDLE UP. RAN QRH AND RED LIGHT WENT OUT. TRIED TO WIGGLE AND PUSH GEAR HANDLE PRIOR TO CYCLING GEAR. ALL LIGHTS STAYED ON. PUT GEAR HANDLE DOWN, HANDLE WAS STUCK OUT AND NEEDED TO BE Apr 18, 2013 · N599FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR IPXA13M78115Trunnion · crackedINSPECTION TYPE:1C NLG LT TRUNNION CRACKED ON LOWER END. REPAIRED TRUNNION IAW SRM 53-10-14, REPAIR 2, FIG 202.Apr 17, 2013 · N277UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA3M77911Relay · inoperativeLEVEL 1, TR 3 FAIL ALERT. AT FLIGHT LVL 310, LEVEL 1 FIRE DET 2 FAULT. DISPLAYED 4,5,6 AND MCDU 2 ON F/O SIDE FAILING MULTIPLE TIMES ACFT POSITION INVALID IN FLIGHT DISPLAYED ON MCDU. DISPLAY 4 SHOWED INTERMITTENT RED X. MCDU 2 FAIL. R & R BAT CHARGER TRAApr 17, 2013 · N260UP · Doug MD11F · Battery/Charger SystemSDR WRNA201300009Carbon Seal · brokenNR 1 ENGINE OIL QTY LOW, TEMP AND PRESSURE NORMAL. DURING CLIMBOUT FROM MIA TO LIM. PILOTS NOTICED NR 1 ENGINE HAD LOSS OIL QUANTITY WITH TEMP AND PRESSURE NORMAL. CREW FOLLOWED SHUTDOWN PROCEDURES FOR NR 1 ENGINE, DUMPED 27000KGS FUEL, AND RETURNED TO MIA Apr 16, 2013 · N952AR · Doug MD11F · Turbine Engine Oil SystemSDR FDEA201304130781Seat Track · corrodedDURING REMOVAL OF FLOOR PANEL FOR ACCESS. FOUND BS 1880, X= 47.25 SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52. REPAIR 1, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 13, 2013 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201304130778Seat Track · corrodedDURING LOWER AFT CARGO BAY CEILING INSPECTION FOUND CABIN SEAT TRACK CORRODED AT BS 1975, X= -107. SEAT TRACK BS 1897 -2007, R & R IAW SRM 53-00-52, REPAIR 6, REV 52 AND SRM 51-31-01 REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 13, 2013 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201304130777Floor Support · corrodedDURING LOWER AFT CARGO COMPARTMENT CEILING INSPECTION, FOUND CABIN FLOOR SUPPORT WITH CORROSION AT BS 1887, X= -75. FLOOR SUPPORT REMOVED IAW AMM 20-50-02, REV 75.2. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7551, REVISION G. NEW FLOOR SUPPORT INSTALLED IAW AMApr 13, 2013 · N583FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201304130780Skin · crackedFIVE FASTENER HOLES, NR 8, 10, 13, 29, 32 FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 -713.6. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLASSIFIED AS MAJApr 13, 2013 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201304130779Skin · crackedTHREE FASTENER HOLES, NR 6, 8, 10 FOUND TO HAVE A CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION ON LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 - 713.6. REPAIRED IAW SRM 57-20-02. REPAIR 5, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM Apr 13, 2013 · N583FE · Doug MD11F · Wing, Plate/Skin
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