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 FDEA201703150882Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 661 - 667 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 15, 2017 · N589FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201703150896Doubler · crackedLEFT WING LEADING EDGE CAVITY AT XOS 667, RIB DOUBLER CRACKED. THE RIB DOUBLER WAS REMOVED IAW SRM 51-31-01-0G. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REVISION K, AND INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 15, 2017 · N589FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201703150895Frame · dentedCABIN, MDCC FRAME REPAIR FOUND DENTED AT BS 1681, LONGERON 12R. REPAIRED IAW SRM 51-33-01-0G AND SRM 53-00-07-2R, FIG 201, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 15, 2017 · N589FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201703150894Frame · dentedMDCC FRAME REPAIR FOUND DENTED AT BS 1701, LONGERON 12L. REPAIRED IAW SRM 51-33-01-0G, AND SRM 53-00-07-2R, FIG 201, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 15, 2017 · N589FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201703150893Seat Track · crackedLOWER FWD CARGO COMPARTMENT CEILING AREA AT STA 755, X =47 SEAT TRACK ASSEMBLY FOUND CRACKED LOWER FWD CARGO COMPARTMENT CEILING AREA CRACKED SEAT TRACK AT STA 755, X =47. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE AT STA 625 TO STA. 7Mar 15, 2017 · N589FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201703150892Seat Track · crackedLOWER FWD CARGO COMPARTMENT CEILING AREA AT STA 715, X =47 SEAT TRACK ASSEMBLY FOUND CRACKED LOWER FWD CARGO COMPARTMENT CEILING AREA CRACKED SEAT TRACK AT STA 715, X =47. REPAIRED PER SRM 53-00-52 FIG. 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Mar 15, 2017 · N589FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201703150891Seat Track · crackedLOWER FWD CARGO COMPARTMENT CEILING AREA AT STA 635, X =47 SEAT TRACK ASSEMBLY FOUND CRACKED LOWER FWD CARGO COMPARTMENT CEILING AREA CRACKED SEAT TRACK AT STA 635, X =47 REPAIRED AT STA 625 TO STA 765, X=47 AS PER SRM 53-00-52 FIG 201 REPAIR 1. REPAIR CLASSIFMar 15, 2017 · N589FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201703150889Seat Track · crackedLOWER FWD CARGO COMPARTMENT CEILING AREA AT STA 635, X =-8 SEAT TRACK ASSEMBLY FOUND CRACKED. REPAIRED FROM STA 665 TO EXISTING SPLICE AT STA. 625, X=-8 AS PER SRM 53-00-52 FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Mar 15, 2017 · N589FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2017031615216Sign · detachedR2 EMERGENCY EXIT SIGN FELL OFF THE DOOR. INSTALLED THE EMERGENCY EXIT LIGHT OVER DOOR.Mar 15, 2017 · N255UP · Doug MD11F · Emergency LightingSDR IPXA2017040715895Stringer · crackedINSPECTION TYPE: 3C, RT WING STRINGER 14 CRACKED, XORS 506 - 538. REPAIRED THE WING STRINGER IAW EA 011-5710-01-A6726, REV IR, AND EO MD11-5710-63835-A (MAJOR).Mar 14, 2017 · N289UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2017032715553Fitting · corrodedINSPECTION TYPE: 3C, LONGERON 23L END FITTING CORRODED AT BS 1501. REMOVCED, FABRICATED, AND INSTALLED A REPLACEMENT END FITTING IAW DWG AEA0349, AND SRM 51-33-01.Mar 14, 2017 · N289UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017031415146Pin · damagedL1 DOOR STUCK HALF WAY UP. DOOR WILL NOT OPERATE ELECTRICALLY, L1 DOOR CLOSED MANUALLY. REPLACED THE L2 DOOR LOCK PIN IAW AMM 52-10-06.Mar 14, 2017 · N279UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2017031415122Skin · damagedDAMAGE TO THE RT WING FIXED LEADING EDGE SKIN. REPAIR IAW EO MD11-5730-63591.Mar 14, 2017 · N296UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017040715920Stringer · crackedINSPECTION TYPE: 3C, RT WING UPPER STRINGER 6 AT XORS 980.8 IS CRACKED. REPAIRED THE STRINGER IAW EA 011-5710-01-A6721-IR, AND EO MD11-5710-63826-A.Mar 13, 2017 · N289UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2017033115710Stringer · crackedINSPECTION TYPE: 3C, RIGHT WING TANK STRINGER 5 IS CRACKED BETWEEN XORS 1070 - 1094, INSIDE PANELS 639FB & 639GB. REPAIRED THE STRINGER IAW EA 011-5710-01-A6719, REV IR, AND EO MD11-5710-63758-A. (MAJOR)Mar 13, 2017 · N289UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2017032915645Spar Cap · corrodedINSPECTION TYPE: 3C, LEFT WING T/E REAR SPAR LOWER CAP HAS CORROSION OTBD OF THE OTBD FLAP OTBD HINGE. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6717, REV IR, AND EO MD11-57-63677-A.Mar 13, 2017 · N289UP · Doug MD11F · Wing SparSDR IPXA2017032915651Door Frame · crackedINSPECTION TYPE: 3C, LOWER AFT WEB ON THE R3 DOOR FRAME CRACKED, UPPER AFT SIDE. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.Mar 13, 2017 · N289UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2017032915650Door Frame · crackedINSPECTION TYPE: 3C, FWD LOWER WEB ON L3 DOOR FRAME FOUND CRACKED ON LOWER AFT SIDE. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.Mar 13, 2017 · N289UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2017032715565Beam · crackedINSPECTION TYPE: 3C, RT WING T/E VERTICAL SUPPORT BEAM CRACKED ADJACENT TO THE INBD AILERON OTBD HINGE. REMOVED AND REPLACED THE BEAM IAW SRM 51-33-01Mar 13, 2017 · N289UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2017031315081Skin · crackedA CRACK WAS FOUND ON THE LEFT WING LOWER SURFACE LEADING EDGE SKIN. INSTALLED A REPAIRED DOUBLER IAW EO MD11-5720-63578-A.Mar 13, 2017 · N294UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017031315083Battery Pack · dischargedEMERGENCY LIGHT BATTERY LOW. R & R THE BATTERY PACK IAW AMM 33-51-01 PB 401. EMERGENCY LIGHT TEST PASSED.Mar 13, 2017 · N292UP · Doug MD11F · Emergency LightingSDR FDEA201703130871Door Frame · crackedMAIN DECK CARGO BAY L3 DOOR FORWARD LOWER FUSELAGE FRAME WEB CRACKED AT BS 1255, BETWEEN LONGERON 26 AND 27L. REPAIRED IAW SRM 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 13, 2017 · N589FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201703130870Door Frame · crackedMAIN DECK CARGO BAY R3 DOOR FORWARD LOWER FUSELAGE FRAME WEB CRACKED AT BS 1255, BETWEEN LONGERON 26 - 27R. REPAIRED. CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 13, 2017 · N589FE · Doug MD11F · Fuselage Main, StructureSDR IPXA2017032815617Skin · crackedINSPECTION TYPE: 3C, LEFT WING L/E LOWER SKIN CRACKED AT ACCESS PANEL 519CB. REPAIRED THE SKIN IAW SRM 57-40-01, REPAIR 18, FIG. 201. MAJOR.Mar 12, 2017 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017032815614Skin · crackedINSPECTION TYPE: 3C, LEFT WING L/E LOWER SKIN CRACKED AT ACCESS PANEL 518FB. REPAIRED THE SKIN IAW SRM 57-40-01, REPAIR 17, FIG. 201. MAJOR.Mar 12, 2017 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017040715919Skin · gougedINSPECTION TYPE: 3C, RT WING FIXED L/E SKIN UPPER SURFACE BETWEEN XOS 1121.389 AND 1100.593 IS GOUGED. REPAIRED IAW EA 011-5730-01-A6732-IR, AND EO MD11-5730-63840-A.Mar 11, 2017 · N289UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017032715577Skin · gougedINSPECTION TYPE: 3C, RT WING NR 5 SLAT TRAILING EDGE GOUGED. REPAIRED IAW EA 011-5754-01-A6720 REV.IR, AND EO MD11-5750-63699-AMar 11, 2017 · N289UP · Doug MD11F · Leading Edge DevicesSDR IPXA2017032415471Longeron · corrodedINSPECTION TYPE: 3C, AFT CARGO BAY LONGERON 46R IS CORRODED BETWEEN BS 1997 - 2007. REMOVED, FABRICATED AND REPLACED THE LONGERON IAW EA 011-5310-01-A6714, REV I/R, AND EO MD11-5310-63706-A. (MAJOR)Mar 11, 2017 · N287UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017031515181Plate · missingR1 DOOR SLIDE PRESS TO TEST COVER PLATE MISSING. REPLACED LAMP ASSY IAW AMM 25-61-04. OPS NORMAL.Mar 11, 2017 · N275UP · Doug MD11F · Escape SlideSDR IPXA2017031415124Buss · no testNO EMERGENCY AC NOR DC BUSSES TEST DURING PREFLIGHT ANNUNCIATOR LIGHTS TEST. PERFORMED ANNUCIATOR CONTROL UNIT TEST WITH BAF SWITCH ON IAW MM 33-15-01. OPS CHECKED GOOD. ALL LIGHT ILLUMINATED.Mar 11, 2017 · N257UP · Doug MD11F · Electrical Power SystemSDR IPXA2017031515183Compressor · stalledEMERGENCY DECLARED DUE TO THE NR 2 ENGINE COMPRESSOR STALLED. CREW SHUTDOWN THE ENGINE. REPLACED THE NR 2 ENGINE.Mar 10, 2017 · N280UP · Doug MD11F · Turbine Engine Compressor SectionSDR IPXA2017032115388Support · crackedINSPECTION TYPE: 3C, LEFT ELEVATOR CAM ROLLER SUPPORT HAS EDGE DAMAGE. REPAIRED THE SUPPORT IAW EA 011-5510-01-A6712, REV I/R, AND EO MD11-5510-63644-A.Mar 9, 2017 · N287UP · Doug MD11F · Elevator StructureSDR IPXA2017030914922Warning Message · illuminatedEMERGENCY BATTERY 1 LOW. R & R R & R MSC IAW AMM 31-42-01 OPS CHECKED NORMAL.Mar 9, 2017 · N272UP · Doug MD11F · Emergency LightingSDR FDEA201703090829Hydraulic Line · damagedUPON GEAR EXTENSION LOST HYD SYSTEM NR 3. ACCOMPLISHED PLUMBING REPAIRES IN RT WW TO NR 3 HYD BRAKE SUPPLY SYS REF MM 20-10-01-2, RECLOCKED NR 3 BRAKE TRANSDUCER CONNECTOR, ALL OPEN SYSTEMS ARE CLOSED. ALL REQUIRED LEAK AND OPS CHECKS COMPLIED WITH SATISFACTOMar 9, 2017 · N523FE · Doug MD11F · Hydraulic System, MainSDR FDEA201703070803Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.226", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHINGMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070802Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.226" MAXIMUM ALLOWABLE HOLE DIA 1.220", OVERSIZED BUSHING Mar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070801Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.402" , MATERIAL REMOVED 0.008", REMAINING THICKNESS 0.394". MINIMUM ALLOWABLMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070800Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.220 INCH; FINAL HOLE DIAMETER 1.234 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INCMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070799Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.220 INCH; FINAL HOLE DIAMETER 1.234 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070798Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.219 INCH; FINAL HOLE DIAMETER 1.226 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070797Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACHED INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.219 INCH; FINAL HOLE DIAMETER 1.226 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 IMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070796Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) FORWARD MOUNT OUTBOARD LUG SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS: 0.380" MATERIAL REMOVED: 0.003" REMAINING THICKNESS: 0.377" MINIMUM ALLOWABLEMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070795Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.222", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHINGMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070794Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44--09 EXISTING HOLE DIA 1.281", FINAL HOLE DIA 1.285", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING Mar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070793Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT LOWER BOLT H0LE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIAMETER 0.406 INCH; FINAL HOLE DIAMETER 0.422 INCH; MAXIMUM ALLOWABLE DIAMETER 0.391 INCHMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070792Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44--09 EXISTING HOLE DIA 0.405", FINAL HOLE DIA 0.422", MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZED BUSHING FAMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070791Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.410", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.405". MINIMUM ALLOWABLE Mar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070790Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 2.316", FINAL HOLE DIA 2.320", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSHING FABRICATED AND IMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2017031014964Bracket · failedPBE IN SUPERNUMERARY AREA CAME OFF WALL DURING TAKEOFF. R & R THE PBE BRACKET ASSY IAW AMM 35-31-01.Mar 7, 2017 · N279UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017031014951Sensor · failedLEVEL 2 ALERT FOR ICE SENSOR FAIL DISPLAYED, COMPLETED QRH PROCEDURE. R & R THE NR HIGH STAGE AND NR 1 INTERMEDIATE PRESSURE SENSOR CFDS FAULT PE2, PE3B AND PI3. T2-1215, T2-1218 AND T2-1185 IAW MM 36-11-05 PERFORMED PSC 1 AND PSC2, RETURNED TO SERVICE IAW 36Mar 7, 2017 · N284UP · Doug MD11F · Air Intake Anti/De-Ice System
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