Mcdonnell Douglas MD-11

Service difficulty reports · 7,956

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  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 9WGA2021041951301Warning Message · illuminatedCABIN ALTITUDE ALERT ON DESCENT AT FL190.Apr 19, 2021 · N513SN · Doug MD11 · Cabin Pressure Control SystemSDR FDEA202012160235Floor Panel · damagedMAIN CABIN FLOOR - PANEL 241GF - CHAFFING DAMAGE TO UPPER FACE SHEET OF FLOORBOARD. REMOVED AND REPLACED DAMAGED FLOORBOARD 241GF IAW MM 53-21-09-04 FIG. 201 AND MM 53-21-06-4. INSPECTED, OK. REMOVED AND REPLACED DAMAGED FLOORBOARD 241GF IAW MM 53-21-09-Dec 16, 2020 · N523FE · Doug MD11 · Fuselage Floor PanelSDR FDEA202012160234Floor Panel · damagedMAIN CABIN FLOOR - PANEL 241FF - CHAFFING DAMAGE AND CRACK TO UPPER FACE SHEET OF FLOOR BOARD. REMOVED AND REPLACED DAMAGED FLOORBOARD 241FF IAW MM 53-21-09-04 FIG. 201 AND MM 53-21-06-4. INSPECTED, OK. MAJOR REPAIR.Dec 16, 2020 · N523FE · Doug MD11 · Fuselage Floor PanelSDR FDEA2020081081825Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY AT XOS 630 BEADED DOUBLER FOUND CRACKED.Aug 8, 2020 · N625FE · Doug MD11 · Wing, Plate/SkinSDR FDEA202007301719Seat Track · damagedMAIN DECK SEAT TRACK CROWN DAMAGED AT BS 755 , X = 8.5 .Jul 30, 2020 · N582FE · Doug MD11 · Fuselage Floor PanelSDR FDEA202007131493Wire Harness · failedAFTER TAKEOFF APPROXIMATELY 200 FT, ENGINE 2 ANTI ICE DUCT ILLUMINATED, FOLLOWED QRH & SHUTDOWN NR 2 ENG. RETURNED TO LAND. PERFORMED LEAK CHECK OF NR 2 ENG ANTI-ICE DUCT IAW AMM 30-22-09-5. NO LEAKS FOUND, PRESSURE HELD WITH NO LOSS. COMPLIED WITH FIM 30-Jul 13, 2020 · N618FE · Doug MD11 · Engine Bleed Air System WiringSDR FDEA202006021107Sprocket · damagedFOUND RH THS DRIVE CHAIN OUTBOARD IDLER SPROCKET DAMAGED AND MISSING BEARING. FOUND DURING HORZ STAB LUBE R&R SPROCKET ASSEMBLY.Jun 2, 2020 · N601FE · Doug MD11 · Horizontal Stabilizer StructureSDR FDEA2020061622615Skin · corrodedAFT ACCESSORY COMPARTMENT HAS EVIDENCE OF CORROSION ON R/H SIDEWALL. REPAIR IN REF. TO MD11 SRM 53-70-01-2R; FIG. 201.Oct 12, 2019 · N617FE · Doug MD11 · Fuselage Main, Plate/SkinSDR FDEA2019101782491Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 1282 X = 47.5 FOUND CROWN DAMAGEDOct 8, 2019 · N597FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019101842684Skin · chafed#2 ENGINE - LOWER RIGHT AFT INLET - SKIN WORN THROUGH AT APPROXIMATELY 5:45 POSITION, WHERE THE RIGHT FAN COWL MAKES CONTACT WITH SKIN SURFACE (MARKED). REPAIRED WORN SKIN PER SRM 54-20-15-2R SHT.3.Oct 4, 2019 · N631FE · Doug MD11 · Nacelle/Pylon, Plate/SkinSDR DALA2019061790008Beam · wornPD:WHILE INSPECTING THE PN 221-0261-501 AFT MOUNT BEAM, DELTA FOUND WEARCOMMON TO THE SIDE WALL THAT IS BEYOND THE LIMITS OF CMM 71-20-05. THE CA:O/H PER CMM 221-0260-501, COMPLIED WITH ER/A 578346-14. DAMAGE WASCLEANED, VISUALLY AND FPI INSPECTED,BLENDED AND May 15, 2019 · Doug MD11 · Engine Mount SectionSDR SRXR201808220026Door · crackedFWD TAILCONE UPPER RT AFT DOOR WAS CRACKED. REPAIRED IAW EA 011-5246-52-A7329 I/R.Aug 22, 2018 · N412SN · Doug MD11 · Aerodynamic FairingsSDR 9WGA20180806001Longeron · corrodedLONGERON 52 CORRODED BETWEEN FRAMES BS 1039 - 1059, IN FORWARD CARGO BAY.Aug 6, 2018 · N411SN · Doug MD11 · Fuselage Main, Longeron/StringerSDR SRXR201806050041Doubler · corrodedRIGHT WING L/E BEADED DOUBLER WAS CRACKED AT WS 584. REMOVED, FABRICATED AND INSTALLED A NEW BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15.Jun 5, 2018 · N415JN · Doug MD11 · Wing, Plate/SkinSDR SRXR201805310037Skin · corrodedRH WING UPPER SKIN HAD CORROSION AT XORS 676 TO XORS 792, STRINGER 6 AND 7. ACCOMPLIHED BLEND OUT REPAIR IAW EA 011-5720-52-A7274 I/R.May 31, 2018 · N415JN · Doug MD11 · Wing, Plate/SkinSDR SRXR201805310036Skin · corrodedLEFT WING UPPER SKIN HAD CORROSION AT XORS 197. ACCOMPLISHED A BLEND OUT REPAIR IAW EA 011-5710-52-A7233 I/R.May 31, 2018 · N415JN · Doug MD11 · Wing, Plate/SkinSDR SRXR201805300035Longeron · corrodedCORROSSION FOUND ON LONGERON 38L AT BS 460 TO 595. REMOVED, FABRICATED, AND INSTALLED A NEW LONGERON IAW SRM 51-31-01, AND EA 011-5300-52-A7260 I/R.May 30, 2018 · N415JN · Doug MD11 · Fuselage Main, Longeron/StringerSDR SRXR201805240027Drag Angle · corrodedRH FUSELAGE WING BARREL CANTED PANEL DRAG ANGLE IS CRACKED AT STA 1236 STGR 43. REPAIRED IAW EA 011-5310-52-A7215, I/R3May 24, 2018 · N415JN · Doug MD11 · Fuselage Main, StructureSDR FDEA201805231279Seat Track · gougedMAIN DECK SEAT TRACK CROWN AT BS 1421, LBL 47.5 DAMAGED. REPLACED THE SEAT TRACK FROM BS 1390 TO 1431 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 23, 2018 · N620FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR SRXR201805180023Skin · corrodedLEFT WING UPPER SURFACE FWD SKIN HAS CORROSION AT XORS 130. ACCOMPLISHED A REPAIR IAW EA 011-5720-52-A7223, IR.May 18, 2018 · N415JN · Doug MD11 · Wing, Plate/SkinSDR SRXR201805150022Stringer · crackedCENTER WING UPPER AUX FUEL TANK LOWER STRINGER 47 IS CRACKED AT XCW -46.50, XCW -17, XCW 17.00,XCW -46.50 XCW 46.50. ACCOMPLISHED REPAIRS ON CENTER WING UPPER AUX FUEL TANK LOWER STRINGER 47 BETWEEN XCW -17.00 XCW 17.00, XCW -46.50, XCW 46.50, XCW 64, XCW -64May 15, 2018 · N415JN · Doug MD11 · Fuselage Main, Longeron/StringerSDR SRXR201805150021Stringer · crackedCENTER WING UPPER AUX FUEL TANK LOWER STRINGER 52 IS CRACKED AT XCW 17.00 AND XCW 46.50. ACCOMPLISHED REPAIR ON CENTER WING UPPER AUX TANK LOWER STRINGER 52 AT XCW 0 TO XCW 64 PER MD-11 SRM 57-10-03 REPAIR 1 FIG 201 REF VT SAA NRC#A040936.May 15, 2018 · N415JN · Doug MD11 · Fuselage Main, Longeron/StringerSDR SRXR201805150020Stringer · crackedCENTER WING UPPER AUX TANK LOWER STRINGER 48 IS CRACKED AT XCW 17.00 AND 46.50. ACCOMPLISHED REPAIR ON CENTER WING UPPER AUX TANK LOWER STRINGER 48 PER MD-11 SRM 57-10-03 REPAIR 1 FIG 201 REF VT SAA NRC# A040935.May 15, 2018 · N415JN · Doug MD11 · Fuselage Main, Longeron/StringerSDR FDEA201802010287Panel · departedDURING POST FLIGHT, MX WALKAROUND FOUND THE NR 1 ENGINE INBOARD PYLON PANEL SHEARED OFF. FABRICATED THE PANEL AND REPLACED THE LAND ASSY. INSTALLED THE PANEL IAW EA 1-5410-T0338185 B, PART 3.Feb 1, 2018 · N573FE · Doug MD11 · Nacelle/Pylon, Plate/SkinSDR FDEA201801260228Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 617, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 26, 2018 · N576FE · Doug MD11 · Wing, Plate/SkinSDR FDEA201710263055Seat Track · crackedMAIN DECK SEAT TRACK BS 715, LBL 8.5 FOUND CRACKED. THE SEAT TRACK WAS REPLACED FROM BS 705 TO 745, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 26, 2017 · N587FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201707192001Line · leakingDURING CRUISE, THE HYD 3 PRESSURE HIGH ALERT. HYD 3 OFF. TEMP WENT TO 120 DEGREE C AND PRESS TO 3720. THEN IN SERVICE QTY HYD 3 WENT TO O PSI. LEAK APPEARS TO BE FROM THE NR 3 HYD PRESSURE LINE FROM PYLON UNDER 617AB. REMOVED AND INSPECTED RT ENGINE CJul 19, 2017 · N594FE · Doug MD11 · Hydraulic System, MainSDR FDEA201705031346Transmitter · failedDURING CLIMBOUT AT SLAT RETRACTION, RECEIVED AN AUDIBLE WARNING FOR THE LANDING GEAR. WARNING CONTINUED UNTIL CAWS TO/LDG/CABIN ALT, CIRCUIT BREAKER WAS PULLED. CYCLED LANDING GEAR PRIOR TO PULLING CIRCUIT BREAKER. THE WARNING STOPPED, BUT WHEN GEAR WAS RMay 3, 2017 · N604FE · Doug MD11 · Leading Edge Slat Position Indicating SystemSDR FDEA201701030007Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT AT STATION XOS 700 FOUND BEADED DOUBLER CRACKED.Jan 3, 2017 · N591FE · Doug MD11 · Wing, Plate/SkinSDR FDEA201612144454Light · inoperativeREMOTE BOTTLE LIGHT INOPERATIVE ON THE R1 DOOR.Dec 14, 2016 · N595FE · Doug MD11 · Emergency EquipmentSDR FDEA201612144453Light · inoperativeREMOTE BOTTLE LIGHT INOPERATIVE ON THE R1 DOOR.Dec 14, 2016 · N595FE · Doug MD11 · Emergency EquipmentSDR FDEA201612124394Controller · failedCAPT'S WINDSHIELD COMPLETELY COLD SOAKED AND APPEARS W/S HEAT INOP AND FOGGED OVER DURING DESCENT AND APPROACH. SEVERE FOGGING TO POINT OF CAPTS VISIBILITY SERIOUSLY REDUCED AND UNSAFE. REPLACED LT WINDSHIELD HEAT CONTROLLER PER AMM 30-41-01-4. OP CHK OK.Dec 12, 2016 · N608FE · Doug MD11 · Windshield/Door Rain/Ice RemovalSDR FDEA201611234215Hinge Fitting · corrodedRIGHT WING, FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE FOUND CORRODED.Nov 23, 2016 · N603FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA201607152453Spar · crackedAFTER PANEL 364RR, EMPENNAGE, INSIDE PANEL 364RR AFT SPAR WEB FOUND CRACK AT STA Y = 2164.Jul 15, 2016 · N582FE · Doug MD11 · Standard Practices/StructuresSDR FDEA201607082331Spar Cap · crackedDURING 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 - VERTIJul 8, 2016 · N582FE · Doug MD11 · Vertical Stabilizer, Spar/RibSDR FDEA201607082330Spar Cap · crackedDURING 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.Jul 8, 2016 · N582FE · Doug MD11 · Vertical Stabilizer, Spar/RibSDR FDEA201607082321Skin · delaminatedLEFT WING OUTBOARD AILERON TRAILING EDGE WEDGE UPPER SURFACE INBOARD SIDE. FOUND DELAMINATION ABOUT 4" X 4". REPAIRED IAW EA 1-5750-T0326653, PART: 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI: 57504046 FOR WORK DETAILS.Jul 8, 2016 · N605FE · Doug MD11 · AileronsSDR FDEA201607012217Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT OUTBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944". REPAIR BUSHING FABRICAJul 1, 2016 · N602FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA201607012216Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE UPPER MOUNT INBOARD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 0.942", FINAL HOLE DIA: 0.950", MAXIMUM ALLOWABLE HOLE DIA: 0.944", REPAIR BUSHING FABRICATEDJul 1, 2016 · N602FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA201607012215Hinge · corrodedLEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE PIVOT HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.317", MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTAJul 1, 2016 · N602FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA201605131564Seat Track · corrodedCABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSIONS, AT RT STATION 1556, X=-27.5. CORRODED SEAT TRACK REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 13, 2016 · N595FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201510253349Seat Track · corrodedMAIN DECK CABIN FLOOR CURVED SEAT TRACK AT BS 1887 - 1994, X= -107 FOUND CORROSION. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK SEGMENT REPLACEMENT FROM STA 1771 TO STA.2007 X = -107 PER SRM 53-00-52-2R FIGURE 201 REPAIR #6. REPAIR CLASSIFIED AS MAJOR PEROct 25, 2015 · N609FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2016041802315Fitting · corrodedINSPECTION TYPE:2C, RCB FLOOR FITTING HAS CORROSION DAMAGE ALONG LOWER EDGE ACCOMPLISHED. BLEND REPAIR ON RCB FLOOR FITTING BS 488 X=85.5 IAW EA 011-5310-01-A6203, REV I/R AND EO MD11-5340-60492-A.Mar 26, 2015 · N256UP · Doug MD11 · Fuselage Main, Attach FittingsSDR FDEA201407091681Pseu · faultySLAT DISAG ON ROTATION ON TAKEOFF. AT SLAT RETRACTION SPEED DURING CLIMB SLAT DISAG EXTINGUISHED. 30 SECONDS LATER SLAT DISAG LIGHT CAME ON. LIGHT STAYED ON UNTIL SLATS EXTENDED FOR LANDING, THEN LIGHT EXTINGUISHED, NORMAL LANDING. TROUBLE SHOT IAW FIM 31Jul 9, 2014 · N620FE · Doug MD11 · Leading Edge Slat Position Indicating SystemSDR FDEA201404160739Pump · failedLEVEL OFF AT FL350, RECEIVED LEVEL ONE TANK 3 TIP TRAPPED & TANK 3 FUEL QTY LOW. SHORTLY FOLLOWED BY FUEL CROSSFEED 3 DISAGREE. TRANSFER PUMP INOPERATIVE. TAIL FUEL MANAGEMENT INOPERATIVE. OPS NOT AUTHORIZED ABOVE 78 N LAT OPERATE FSC IN MANUAL. RESET CBApr 16, 2014 · N614FE · Doug MD11 · Aircraft Fuel Distribution SystemSDR FDEA201311272881Doubler · chafedCABIN LT STATION 535 LONGERON 24 LT FRAME EXISTING REPAIR DOUBLER FOUND CHAFFED. DOUBLER REMOVED AND REPAIR CARRIED OUT AS PER SRM 53-20-07 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.Nov 27, 2013 · N597FE · Doug MD11 · Fuselage Main, FrameSDR FDEA201311262872Web · crackedCABIN LT STATION 1259 LONGERON 26 LT, DOOR 3 LT FWD JAMB LOWER WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.Nov 26, 2013 · N597FE · Doug MD11 · Fuselage Miscellaneous StructureSDR FDEA201311262871Web · crackedCABIN RT STATION 1259 LONGERON 26 RT, R3 DOOR FWD JAMB LOWER WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.Nov 26, 2013 · N597FE · Doug MD11 · Fuselage Miscellaneous StructureSDR FDEA201311262870Web · crackedCABIN RT STATION 1310 LONGERON 26 RT, R3 DOOR AFT JAMB LOWER WEB FOUND CRACKED.Nov 26, 2013 · N597FE · Doug MD11 · Fuselage Miscellaneous StructureSDR FDEA201311262869Frame · dentedCABIN LT STATION 535 LONGERON 19 LT FRAME FOUND WITH DENT. FRAME REPAIRED AS PER SRM 53-20-07 FIGURE 202 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100 REVISION 118.Nov 26, 2013 · N597FE · Doug MD11 · Fuselage Main, Frame
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