Douglas DC-10-40

Service difficulty reports · 614

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = 'DC1040'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 9506511155Switch · lack of lubeDURING TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED. LUBED AND CYCLED SPEED BRAKE HANDLE SWITCH MECHANISM.Apr 24, 1995 · N155US · Doug DC1040 · Central WarningSDR 9506451156Compressor · stalledDURING DESCENT WITH THE POWER LEVERS RETARDED, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH A RISE IN EGT FOLLOWED BY A FLAMEOUT. A RELIGHT WAS SUCCESSFUL AND ENGINE OPERATION WAS NORMAL THE REMAINDER OF THE FLIGHT. THE ENGINE WAS INSPECTED AND FUEL PApr 24, 1995 · N156US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9506441158Seat Track · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 440 - 485, RBL 9. REPLACED SEAT TRACK.Apr 24, 1995 · N158US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9506431158R3 Door · crackedDURING PERIODIC CHECK, CRACKS WERE FOUND IN THE FORWARD AND AFT LOWER DOOR 3R STRUCTURE AT FS 1260 AND 1305. STOP DRILLED AND INSTALLED DOUBLER.Apr 24, 1995 · N158US · Doug DC1040 · Emergency ExitsSDR 9506631145Roll Computer · malfunctionedDURING DESCENT WHEN DEPLOYING SPEEDBRAKES, AIRCRAFT ROLLED TO THE LEFT. VISUAL AND OPERATIONAL CHECK WAS NORMAL, NO FAULTS FOUND AND AUTO-PILOT BITE CHECK WAS NORMAL. RIGGED SPOILER CABLES AND REPLACED THE ROLL COMPUTER.Apr 23, 1995 · N145US · Doug DC1040 · Autopilot ComputerSDR 9506391158L3 Door · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE DOOR 3L AFT LOWER LIGHTENING HOLE AT FS 1305. STOP DRILLED CRACK AND INSTALLED DOUBLER.Apr 21, 1995 · N158US · Doug DC1040 · Emergency ExitsSDR 9506291158Skin · damagedDURING PERIODIC CHECK, FUSELAGE SKIN WAS FOUND DENTED AND GOUGED AT FS 1801, STR 2L TO 4L. REMOVED DAMAGED AREA AND INSTALLED DOUBLERS.Apr 20, 1995 · N158US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9505871153Nr 3 Bearing · failedDURING CLIMB AT ABOUT 7000 FEET, SMOKE AND FUMES APPEARED IN THE CABIN AND THE AIRCRAFT RETURNED TO MSP WHERE AN UNEVENTFUL LANDING WAS MADE. NO FUEL WAS DUMPED. THE NR 3 ENGINE NR 3 BEARING COMPARTMENT SHOWED EVIDENCE OF DISTRESS AND BLACK OIL WAS FOUND. TApr 16, 1995 · N153US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9505731153Bracket · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SHEAR TIE AT FS 1761 TO 1782, STR 45R AND 46R. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER EA 11-97995.Apr 13, 1995 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9505721153Angle · crackedDURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE 'TEE' ANGLE AT FS 1162, RBL 47 ABOVE ACCESS 142AZ. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER EA 11-97997.Apr 13, 1995 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9505681145Engine · malfunctionedDURING CLIMB, THE NR 1 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO LAX WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE. NO FUEL WAS DUMPED. BLACK OIL WAS FOUND AND THE AIRCRAFT WAS FERRIED TO MSP WHERE THE Apr 13, 1995 · N145US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9506231156Skin · damagedDURING OVERNIGHT INSPECTION, FOUND FUSELAGE SKIN WAS TORN JUST FORWARD OF DOOR 2L. REMOVED DAMAGE AND REPAIRED PER EA 11-96714.Apr 12, 1995 · N156US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9505691221Eel Wire · brokenDURING CRUISE, ALL EMERGENCY LIGHTS ILLUMINATED. PULLED CIRCUIT BREAKER AND LIGHTS EXTINGUISHED. AIRCRAFT CONTINUED TO DESTINATION. REPAIRED WIRE ON CANNON PLUG P1-1789. OPERATIONAL CHECK OK.Apr 12, 1995 · N221NW · Doug DC1040 · Emergency LightingSDR 95005701146Rccb · failedDURING PREFLIGHT CHECK, THE AIRCRAFT EMERGENCY POWER FAILED TO TEST. FOUND REMOTE CONTROL CIRCUIT BREAKER (RCCB) B1-189 STUCK OPEN. REPLACED RCCB, OPERATIONAL CHECK OK.Apr 12, 1995 · N146US · Doug DC1040 · DC Generating SystemSDR 9505491145Computer · malfunctionedDURING CRUISE WITH A BANK ANGLE OF 10 DEGREES, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL TO 30 DEGREES. ADDITIONALLY, DURING APPROACH WITH 20 DEGREES SELECTED, THE AIRCRAFT EXPERIENCED ANOTHER UNCOMMANDED ROLL TO 35 DEGREES. REPLACED THE AUTO-PILOT CONTROApr 9, 1995 · N145US · Doug DC1040 · Autopilot ComputerSDR 9507751158Frame · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME AT FS 879, LBL 38. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER EA 11-98027. MFG PART NUMBER: ADA7034-3.Apr 4, 1995 · N158US · Doug DC1040 · Fuselage Main, FrameSDR 9505141141Engine · malfunctionedDURING DESCENT FL280 AT IDLE POWER, THE NR 1 ENGINE ENCOUNTERED WAKE TURBULENCE AND A SURGE FOLLOWED BY RISING EGT. THE ENGINE WAS SHUTDOWN, AND A RELIGHT WAS SUCCESSFUL. OPERATION WAS NORMAL THE REMAINDER OF THE FLIGHT. THE ENGINE WAS INSPECTED AND A BORESMar 30, 1995 · N141US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9504961153Engine · flame outDURING TAXI OUT, THE NR 2 ENGINE EXPERIENCED A SURGE AND FLAMED OUT WITH THE EGT GOING TO MAX FOR THREE SECONDS. TAIL WIND GUSTS TO 25 KTS WERE BEING EXPERIENCED. THE ENGINE WAS INSPECTED AND BOROSCOPE WAS ACCOMPLISHED. AN ENGINE CHANGE HAS BEEN SCHEDULED.Mar 26, 1995 · N153US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9504731152Angle · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE 'J' ANGLE AT FS 1781, RBL 20 - LBL 15 BELOW THE SUMP FLOOR. REMOVED CORROSION AND INSTALLED DOUBLER.Mar 25, 1995 · N152US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9504751152Bulkhead · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE BULKHEAD AT FS 1157, STR 51R AND 50R IN THE CENTER ACCESSORY COMPARTMENT. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS AND FILLERS PER EA 11-97898.Mar 24, 1995 · N152US · Doug DC1040 · Fuselage Main, BulkheadSDR 9504741152Longeron · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON LONGERON 52 AT FS 1139 - 1156 IN CENTER ACCESSORY COMPARTMENT. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS PER EA 11-97898.Mar 24, 1995 · N152US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9505191152Skin · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FUSELAGE SKIN AND BULKHEAD AFT OF CENTER LANDING GEAR AT FS 1509 - 1531, LONGERONS 50L AND 50R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS PER EA 11-97918.Mar 23, 1995 · N152US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9504801150Engine · failedDURING CLIMB, THE NR 3 ENGINE OIL QUANTITY BEGAN TO DECREASE, THE OIL STRAINER LIGHT ILLUMINATED, AND THE ENGINE WAS SHUT DOWN. 30,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO HNL WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE. METAL AND BLACK OIMar 23, 1995 · N150US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9504891152Bulkhead · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE CENTER WING PRESSURE BULKHEAD AND LONGERON 52 IN THE CENTER ACCESSORY COMPARTMENT. REPAIRED BULKHEAD PER EA N11-97898.Mar 21, 1995 · N152US · Doug DC1040 · Fuselage Main, BulkheadSDR 9504481152Rib · damagedDURING PERIODIC CHECK, FOUND THE RIGHT DETACHABLE ELEVATOR RIB DAMAGED AT FS XE =67.226, 49.5 INCHES FROM TRAILING EDGE. REPAIRED PER SRM 55-20-00.Mar 21, 1995 · N152US · Doug DC1040 · Elevator, Spar/RibSDR 9504471152Roller Tray · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE ROLLER TRAY IN THE FORWARD CARGO COMPARTMENT AT FS 759, RBL 28. REMOVED CORROSION AND INSTALLED DOUBLER AND FILLER PER EA 11-97896.Mar 21, 1995 · N152US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9503701144Skin · crackDURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE LEFT WING LEADING EDGE SKIN AT THE FORWARD INBOARD CORNER OF FUELING ACCESS DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 11-89870.Mar 12, 1995 · N144JC · Doug DC1040 · Wing, Plate/SkinSDR 9503691144Frame · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE LOWER CHORD OF FRAME AT FS 1099, STRINGER 51R AND 52R. REMOVED DAMAGED AREA AND INSTALLED SPLICES PER EA 11-97861.Mar 12, 1995 · N144JC · Doug DC1040 · Fuselage Main, FrameSDR 9504201144Skin · damagedDURING PERIODIC INSPECTION, DAMAGE WAS FOUND ON THE RIGHT DROOPED LEADING EDGE. REMOVED DAMAGE AND REPAIRED PER EA 11-96662.Mar 11, 1995 · N144JC · Doug DC1040 · Wing, Plate/SkinSDR 9503721144Frame · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON FRAME AT FS 1902 LONGERON 51R TO 50L AND FS 1997 LONGERON 51L TO 48R. REMOVED CORROSION AND INSTALLED DOUBLER PER EA 11-97827.Mar 11, 1995 · N144JC · Doug DC1040 · Fuselage Main, FrameSDR 9503711144Floorbeam · corrodedDURING PERIODIC INSPECTION, DAMAGE WAS FOUND ON THE FLOORBEAM AT FS 939 IN FORWARD CARGO COMPARTMENT.Mar 9, 1995 · N144JC · Doug DC1040 · Fuselage Main, Floor BeamSDR 9504221144Bulkhead · crackedDURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE LEFT AND RIGHT SIDE FUEL TANK BULKHEAD TEE AT FS 1159, X = 50. REMOVED CORROSION AND INSTALLED REPAIR ANGLES PER EA 11-97796.Mar 7, 1995 · N144JC · Doug DC1040 · Fuselage Main, BulkheadSDR 9504231144Longeron · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE CENTER FUSELAGE EXTERNAL LONGERONS 30L-32L, FS 1386-1523. REMOVED CORROSION AND INSTALLED REPAIR ANGLES PER EA 11-96668.Mar 6, 1995 · N144JC · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9503551153Compressor · stalledDURING TAKEOFF, THE NR 2 ENGINE COMPRESSOR STALLED AND SHUT DOWN. DUMPED 43,000 LBS OF FUEL AND RETURNED TO LAX. FERRIED AIRCRAFT TO MSP AND REPLACED THE NR 2 ENGINE.Mar 6, 1995 · N153US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9503431151Engine · failedDURING INITIAL CLIMB, THE NR 1 ENGINE EXPERIENCED LOSS OF OIL QUANTITY AND PRESSURE AND WAS SHUT DOWN. 70,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO SFO WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS ACCOMPLISHED. BLACK OIL WAS FOUND AND THE AIRCRAFMar 4, 1995 · N151US · Doug DC1040 · Turbine Engine Oil SystemSDR 9504641144Longeron · crackedDURING PERIODIC INSPECTION, CRACKS WERE FOUND ON LONGERON 28L AT FS 514. LONGERON IS MADE FROM .050 INCH THICK 7075-T6 ALUMINUM. TRIMMED LONGERON AND INSTALLED DOUBLER PER EA11-96648.Mar 2, 1995 · N144JC · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9503221149Power Cables · malfunctionedDURING LANDING THE NR 2 ENGINE POWER LEVER COULD NOT BE RETARDED AND THE ENGINE WAS SHUT DOWN DURING ROLLOUT. THE THROTTLE BOOT WAS CLEANED, DRIED WITH ALCOHOL, AND THE OPERATION CHECKED OK. LATER AT MSP, THE LONG AND SHORT ENGINE PUSH/PULL CABLES WERE REPLAFeb 24, 1995 · N149US · Doug DC1040 · Power LeverSDR 9503211149Pwr Lever Cable · lack of lubeDURING LANDING (AMS), THE NR 2 ENGINE POWER LEVER COULD NOT BE RETARDED AND THE ENGINE WAS SHUT DOWN DURING ROLLOUT. THE POWER LEVER CABLE WAS CLEANED, LUBRICATED, AND OPERATION CHECKED OK.Feb 23, 1995 · N148US · Doug DC1040 · Power LeverSDR 9502751148Transmitter · failedDURING TAKEOFF, THE NR 1 ENGINE FAIL LIGHT ILLUMINATED AND THE TAKEOFF WAS ABORTED. REPLACED THE NR 1 ENGINE N1 TRANSMITTER.Feb 20, 1995 · N148US · Doug DC1040 · Engine RPM Indicating SystemSDR 9502651157Air Duct · rupturedDURING INITIAL CLIMB, THE NR 1 ENGINE EXPERIENCED THE REVERSER UNLOCK LIGHT ILLUMINATE THEN GO OUT FOLLOWED BY THE FIRE LIGHT AND BELL COMING ON. POWER WAS REDUCED TO IDLE AND THE LIGHTS EXTINGUISHED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO SEA WFeb 16, 1995 · N157US · Doug DC1040 · Engine Thrust ReverserSDR 9502631151Frame · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FRAME TEE AT FS 979, STR 44L - 45L IN FORWARD CARGO COMPARTMENT. REMOVED CORROSION AND REPAIRED PER EA 11-9385.Feb 16, 1995 · N151US · Doug DC1040 · Fuselage Main, FrameSDR 9502421151Window Reveal · crackedDURING PERIODIC CHECK, CRACKS WERE FOUND ON THE WINDOW REVEALS AT WINDOWS 1, 13, 23, AND 26. INSTALLED DOUBLERS PER EA 11-93858.Feb 15, 1995 · N151US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9504051151Intercostal · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND IN THE INTERCOSTAL WEB OF THE LEFT CENTER FUSELAGE DOOR JAMB AT STA 1310.Feb 10, 1995 · N151US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9501791146Intercostal · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE FUSELAGE BELT FRAME TO INTERCOSTAL STRAP AT FS 445, LBL 25 TO THE ACCESS DOOR 115AZ. REPLACED STRAP.Feb 2, 1995 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9501781146Floor Beam · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE FLOOR BEAM AT FS 879, RBL 29 - 37. REMOVED DAMAGE AND REPAIRED PER EA 11-96621.Feb 2, 1995 · N146US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9501531146Doubler · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE INNER SKIN STIFFENER AT FS 1156, STR 50L AND 51L. INSTALLED NEW DOUBLER PER EA 11-96638.Jan 28, 1995 · N146US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9501551146Longeron · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON LONGERON AT STR 44L, FS 1581. INSTALLED REPAIR STRAP PER 11-96601.Jan 27, 1995 · N146US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9501541146Longeron · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE END FITTING AT LONGERON 18R, FS 1988 AND LONGERON 19R, FS 1990. INSTALLED STRAP DOUBLERS PER EA 11-96271.Jan 27, 1995 · N146US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9503181146Longeron · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE LONGERON 44L, FS 1581. REMOVED CORROSION AND INSTALLED DOUBLER PER EA 11-96601.Jan 25, 1995 · N146US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9501281146Bulkhead Angle · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SUPPORT ANGLE OF THE FORWARD BULKHEAD IN THE CENTER WHEEL WELL, AT RBL 10-29. INSTALLED REPAIR ANGLE PER EA 11-93766.Jan 23, 1995 · N146US · Doug DC1040 · Fuselage Main, Bulkhead
Back to Douglas DC-10-40