Douglas DC-10-40

Service difficulty reports · 614

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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 9722511146Tr Unit · malfunctionedON TAKEOFF ROLL AS POWER WAS APPLIED, THE NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROXIMATELY 30 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A.Dec 3, 1997 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9722411160Compressor · stalledDURING LANDING ROLLOUT, THE NR 3 ENGINE COMPRESSOR STALLED, EGT REACHED 1000C FOR 1 TO 2 SECONDS BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE DEACTIVATED THE THRUST REVERSER PER MEL AND INSPECTED THE INLET AND EXHAUST WITH NO DAMAGE FOUND. THE BORESCOPE INSPDec 2, 1997 · N160US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9722521144Tr Unit · malfunctionedDURING TAKEOFF ROLL, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AT 70 KTS WITH THE INDICATION EXTINGUISHING WITH POWER REDUCTION. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A AND THE AIRCRAFT RETURNED TO SERVICE.Dec 1, 1997 · N144JC · Doug DC1040 · Engine Thrust ReverserSDR 9722201146Thrust Reverser · malfunctionedDURING LANDING ROLLOUT, THE NR 1 ENGINE THRUST REVERSER FAILED TO STOW. THE CREW RECYCLED THE REVERSER AND A COMPRESSOR STALL OCCURRED. MAX EGT WAS 650C. THE ENGINE WAS SHUT DOWN. THE OUTBOARD REVERSER SLEEVE DEPARTED THE AIRCRAFT. MAINTENANCE LOCKED OUT Nov 26, 1997 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9722871146Web · crackedDURING L-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL, LEFT AND RIGHT CORNER WEB AROUND FASTENERS FS 488. REPAIRED PER EA 11-153553.Nov 21, 1997 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9721301141Fitting · corrodedDURING L-CHECK, FOUND CORROSION ON LONGERON 44R END FITTING AT FS 1701. REPLACED FITTING EPR SRM 51-00-00.Nov 10, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9720781157Compressor · stalledDURING LANDING ROLLOUT WHILE COMING OUT OF REVERSER THRUST, THE NBR 1 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 850C AND THE ENGINE WAS SHUT DOWN. THE CREW STATED THERE WAS A TAIL CROSSWING DURING LANDING. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NNov 5, 1997 · N157US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9720491149Compressor · stalledDURING TAKEOFF ROLL AND WHILE INCREASING POWER, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL. N2 WAS AT 70 PERCENT AND EPR WAS 1.35 WITH NO ABNORMAL ENGINE INDICATIONS. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED TNov 1, 1997 · N149US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9720191150Compressor · stalledDURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. EGT ROSE TO 950C AND THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE INCLUDING A BORESCOPE AND FOUND NO DEFECTS. THE RABS SYSTEM AND FUEL PUMP CHECKED NORMAL.Oct 27, 1997 · N150US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9720181150Compressor · stalledDURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 2 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 950C AND THE ENGINE WAS SHUT DOWN. MAINTENANCE PERFORMED A BORESCOPE, CHECKED THE RABS OPERATION AND THE FUEL PUMP PRESSURE WITH ALL CHECKING NORMAL.Oct 27, 1997 · N150US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9719781148Prox Box · malfunctionedDURING APPROACH, THE SAFE AND UNSAFE GEAR INDICATION LIGHTS DID NOT ILLUMINATE. APPROACH WAS ABORTED. DUE TO WEATHER AND FUEL CONCERNS FLIGHT PROCEEDED TO CDG. RECYCLED GEAR AND INDICATION NORMAL. MAINTENANCE RESEATED LANDING GEAR PROXIMITY BOX, NO FAULTS Oct 22, 1997 · N148US · Doug DC1040 · Landing Gear Position and WarningSDR 9719831141Fuel Control · malfunctionedWHILE DESCENDING THRU FL350, THE NR 3 ENGINE EGT ROSE TO 880C. THE ENGINE WAS SHUT DOWN. THE SECOND RESTART ATTEMPT WAS SUCCESSFUL WITH NORMAL OPERATION FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE BORESCOPED THE ENGINE WITH NO DEFECTS NOTES. THE FUEL CONTOct 21, 1997 · N141US · Doug DC1040 · Fuel Control/Turbine EnginesSDR 9719081141Wire · brokenDURING LIGHT INSPECTION FOUND THE EMERGENCY FLOOR LIGHT INOPERATIVE IN LEFT SIDE IN B-ZONE. MAINTENANCE REPAIRED A BROKEN WIRE IN THE TRACK WIRING.Oct 13, 1997 · N141US · Doug DC1040 · Light System WiringSDR 9718791157Bleed Duct · damagedAT ROTATION, THE NR 1 ENGINE FIRE LIGHT ILLUMINATED FOLLOWED BY THE REVERSER UNLOCK LIGHT. WITH POWER REDUCED TO IDLE ON THE NR 1 ENGINE, THE FIRE LIGHT WENT OUT. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED WITHOUT INCIDENT. MAINTENANCE FOUND AN ENGINE BLEED Oct 5, 1997 · N157US · Doug DC1040 · Pneumatic Distribution SystemSDR 9718781143Compressor · stalledAT TOP OF DESCENT FL280, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WITH EGT RISING TO 900C. THE ENGINE WAS SHUT DOWN AND TWO RESTART ATTEMPTS WERE UNSUCCESSFUL. MAINTENANCE INSPECTED THE ENGINE PER MM 71-00-00 FOR TOP OF DESCENT STALL WITH NO DEFECTS NOct 5, 1997 · N133JC · Doug DC1040 · Turbine Engine Compressor SectionSDR 9720411157Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 51R AT FS 1119. REPAIRED PER EA 11-152790.Oct 4, 1997 · N157US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9720421157Skin · corrodedDURING M-CHECK, FOUND CORROSION ON FUSELAGE SKIN FS 1509 TO 1531 AND LONGERON 49L TO 49R. REPAIRED PER EA 11-150758.Oct 1, 1997 · N157US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9718241158Selector · failedDURING CLIMB, UNABLE TO CONTROL CABIN PRESSURE. FLIGHT RETURNED TO DTW. MAINTENANCE REPLACED THE CABIN PRESSURE SELECTOR.Oct 1, 1997 · N46767 · Doug DC1040 · Cabin Pressure Control SystemSDR 9718641157Skin · corrodedDURING M CHECK, FOUND CORROSION ON SKIN DOUBLER AT FS 1157 BETWEEN LONGERON 51L AND 50L. REPAIRED PER EA 11-152199.Sep 30, 1997 · N157US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9718631157Skin · corrodedDURING M CHECK, FOUND CORROSION ON FUSELAGE SKIN AT FS 1148 BETWEEN LONGERONS 51R AND 52. REPAIRED PER EA 11-152199.Sep 30, 1997 · N157US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9718111141Tach Ind · failedON TAKEOFF ROLL, THE NR 3 ENGINE N1 INDICATION SPIKED WHILE AT MAXIMUM POWER. THE TAKEOFF WAS ABORTED AT APPROXIMATELY 40 KNOTS. ALL OTHER PARAMETERS WERE NORMAL. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE DEFERRED THE N1 INDICATION UNDER MEL 77-1BSep 28, 1997 · N141US · Doug DC1040 · Engine RPM Indicating SystemSDR 9718981157Seat Track · corrodedDURING M-CHECK, FOUND CORROSION ON SEAT TRACK (P/N AEA7325-11) BETWEEN FS 1288 AND 1301 AT DOOR 3L. REPAIRED PER EA 11-152198.Sep 25, 1997 · N157US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9718421157Floorbeam · crackedDURING M CHECK, FOUND CRACK ON FLOORBEAM UPPER CAP AT RBL 5, FS 791. REPAIRED PER EA 11-150759.Sep 24, 1997 · N157US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9717941141Power Supply · inoperativeDURING LINE INSPECTION, FOUND THE EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AFT OF DOOR 2L. MAINTENANCE REPLACED POWER SUPPLY.Sep 23, 1997 · N141US · Doug DC1040 · Emergency LightingSDR 9717821154Engine · failedDURING CRUISE, THE NR 1 ENGINE EGT CLIMBED AT LEAST 100 CELSIUS ABOVE THE OTHER ENGINES. ALL OTHER INDICATIONS WERE NORMAL. THE FLIGHT DIVERTED TO MSP AS A PRECAUTION. THE ENGINE FAILED A BORESCOPE INSPECTION AND WAS REPLACED.Sep 20, 1997 · N154US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9717721150Battery · dischargedDURING LINE INSPECTION, FOUND THE AFT CABIN FLOOR EMERGENCY LIGHT AND SIGNS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (61-0478-9) AND THE POWER SUPPLY (60-1321-7).Sep 17, 1997 · N150US · Doug DC1040 · Emergency LightingSDR 9717691152Power Supply · inoperativeDURING LINE INSPECTION, FOUND THE EMERGENCY ESCAPE LIGHTS INOPERATIVE AT DOORS 3L AND 3R AND ROWS 22-27 (BOTH AISLES). MAINTENANCE REPLACED THE POWER SUPPLY, BATTERY PACK, AND REPAIRED THE CANNON PLUG.Sep 17, 1997 · N152US · Doug DC1040 · Emergency LightingSDR 9717701141Battery Pack · dischargedDURING LINE INSPECTION, FOUND THE FLOOR EMERGENCY LIGHT BETWEEN DOORS 2L AND 2R INOPERATIVE. REPLACED BATTERY PACK.Sep 15, 1997 · N141US · Doug DC1040 · Emergency LightingSDR 9720431157Skin · corrodedDURING M-CHECK, FOUND CORROSION ON FUSELAGE SKIN AT LOWER BEACON MOUNTING AREA. REPAIRED PER EA 11-150583.Sep 11, 1997 · N157US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9717361144Handle · lack of lubeDURING APPROACH, UNABLE TO GET ALL GREEN LIGHTS ON THE LANDING POSITION. RECYCLED GEAR TWICE WITH NO HELP. USED ALTERNATE GEAR EXTENSION AND ALL GREEN LIGHTS ILLUMINATED. MAINTENANCE FOUND LANDING GEAR HANDLE STICKING. LUBED GEAR HANDLE.Sep 11, 1997 · N144JC · Doug DC1040 · Landing Gear SelectorSDR 9717151161Cadc · failedDURING CRUISE, THE NR 2 AIR DATA COMPUTER FAILED, (NR 3 CADC WAS ON PREVIOUS MEL). FLIGHT DIVERTED INTO BOS. MAINTENANCE REPLACED NR 2 CADC.Sep 10, 1997 · N161US · Doug DC1040 · Air Data ComputerSDR 9716621151Apu · failedAFTER TAKEOFF, CABIN BEGAN TO FILL WITH SMOKE. CREW ISOLATED PACKS AND FOLLOWED SMOKE REMOVAL CHECK LIST. SMOKE CLEARED AND FLIGHT CONTINUED TO DESTINATION. MAINTENANCE PURGED THE PNEUMATIC SYSTEM AND REPLACED THE APU.Aug 25, 1997 · N151US · Doug DC1040 · APU Core EngineSDR 9716251144Tr Light · illuminatedON TAKEOFF ROLL, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AT 100 KNOTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE DEFERRED THE REVERSER INDICATION SYSTEM UNDER MEL 78-2A WITH THE REVERSER STOWED AND LOCKED. EAug 25, 1997 · N144JC · Doug DC1040 · Engine Thrust ReverserSDR 9716191149Power Supply · inoperativeDURING LINE INSPECTION, FOUND THE FIRST CLASS EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY PACK.Aug 23, 1997 · N149US · Doug DC1040 · Emergency LightingSDR 9716201155Ins Connector · brokenDURING TAKEOFF ROLL, THE NR 2 INS FAILED WITH THE NR 3 INS ON MEL. FLIGHT RETURNED TO MSP. MAINTENANCE REPAIRED CANNON PLUGS ON BOTH NR 2 AND NR 3 INS SYSTEMS.Aug 22, 1997 · N155US · Doug DC1040 · Inertial Guidance SystemSDR 9716051148Tr Cable · out of adjustWHILE ADVANCING THROTTLES TO TAKEOFF POWER, THE NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE LOCKED OUT THE NR 2 THRUST REVERSER AND PLACED IT ON MEL 78-1A. AIRCRAFT THEN DEAug 21, 1997 · N148US · Doug DC1040 · Engine Thrust ReverserSDR 9715881156Wire · brokenDURING LINE INSPECITON, FOUND 'B' ZONE LEFT AISLE FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROWS 10AB TO 20AB. MAINTENANCE REPAIRED BROKEN WIRE TO THE EMERGENCY PATH LIGHTING AT DOOR 2L.Aug 18, 1997 · N156US · Doug DC1040 · Light System WiringSDR 9715651151Compressor · stalledON INITIAL POWER UP FOR TAKEOFF, THE NR 3 COMPRESSOR STALLED, MAX EGT WAS 600C AND EPR WAS 1.18. THE TAKEOFF WAS ABORTED AT 20 KNOTS. MAINTENANCE INSPECTED THE ENGINE PER MM 71-00-00 FOR A CONDITION 1 TYPE 'A' STALL WITH NO DEFECTS NOTED. THERE WAS A 90 DEGAug 18, 1997 · N151US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9715571161Engine · failedWHILE CLIMBING THRU 2000 FEET AFTER TAKEOFF, THE NBR 2 ENGINE EGT WENT OFF SCALE HIGH AND EPR DROPPED. ENGINE WAS SHUT DOWN AND 55,000 LBS OF FUEL WAS DUMPED. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE WITH NO DEFEAug 14, 1997 · N161US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9715581149Tr Unit · malfunctionedDURING LANDING ROLLOUT, THE NR 3 ENGINE THRUST REVERSER DID NOT STOW. THE NR 3 ENGINE EGT CLIMBED TO 920C AND THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER MM 70-00-00. EGT WAS WITHIN LIMITS AND NO DEFECTS WERE NOTED. GROUND RUN OF ENGINE Aug 13, 1997 · N149US · Doug DC1040 · Engine Thrust ReverserSDR 9713421157Compressor · stalledWHEN NR 2 ENGINE POWER ADVANCED TO 1.2 EPR AND STABLE FOR A CROSSBLEED START, THE NR 2 ENGINE COMPRESSOR STALLED. EGT WAS RISING THROUGH 680 CELSIUS WHEN THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED ENGINE PER MM 71-00-00 FOR STALL WITH NO DEFECTS NOTED. Jul 9, 1997 · N157US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9713141152Battery Pack · dischargedDURING LINE INSPECTION, MID CABIN EMERGENCY LIGHT BATTERY FAILED BITE TEST. MAINTENANCE REPLACED BATTERY PACK.Jul 5, 1997 · N152US · Doug DC1040 · Emergency LightingSDR 9713601144Roll Computer · failedDURING CRUISE, COULD NOT ENGAGE AUTO PILOTS WITHOUT ENCOUNTERING ROLLING INPUT TO THE AILERONS. AIRCRAFT DIVERTED TO LGW. MAINTENANCE REPLACED BOTH ROLL COMPUTERS (11-2211-9-0001, S/N 90034 AND 56026) AND THE DIRECTIONAL CONTROL PANEL (11-2216-9-00005, S/N 9Jun 29, 1997 · N144JC · Doug DC1040 · Autopilot ComputerSDR 09712131148Engine · malfunctionedCREW ABORTED TAKEOFF AT 110 KNOTS WHEN THE NR 1 ENGINE WOULD NOT REACH TAKEOFF EPR. TAKEOFF EPR WAS SET TO 1.51, BUT NR 1 ENGINE ONLY REACHED 1.45. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW RAN ENGINE TO TAKEOFF EPR OF 1.51 AND PERFORMED BLEED CHECK PEJun 22, 1997 · N148US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9711981157Egt Indication · risingON LANDING ROLLOUT WHILE COMING OUT OF REVERSE THRUST, THE NR 3 ENGINE EGT STARTED RISING RAPIDLY. THE ENGINE WAS SHUT DOWN WITH A MAX EGT OF 650C. MAINTENANCE CHECKED REVERSER OPERATION PER MM 78-30-00, WITH NO DEFECTS NOTED. EGT WAS WITHIN LIMITS PER MM 7Jun 19, 1997 · N157US · Doug DC1040 · Engine EGT/TIT Indicating SystemSDR 9711781152Altimeter · failedDURING CRUISE, FIRST OFFICER'S ALTIMETER OFF FLAG CAME INTO VIEW AND SMOKE COMING FROM THE UNIT. PULLED CIRCUIT BREAKERS AND RETURNED TO HNL. MAINTENANCE REPLACED THE ALTIMETER INDICATOR.Jun 16, 1997 · N152US · Doug DC1040 · Altimeter, Barometric/EncoderSDR 9711911154Fire Detector · malfunctionedDURING TAXI WHILE TRYING TO START APU, FIRE INDICATION LIGHT ANNUNCIATED. CREW DISCHARGED FIRE BOTTLE. MAINTENANCE FOUND NO EVIDENCE OF FIRE. REPLACED APU FIRE BOTTLE AND APU FIRE DETECTOR CONTROL UNIT (P/N 11-2611-9-0001, 90004).Jun 14, 1997 · N154US · Doug DC1040 · Fire DetectionSDR 9711421146Tr Unit · locked outDURING TAKEOFF ROLL, NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT 90 KNOTS. MAINTENANCE VERIFIED THAT THE THRUST REVERSER WAS LOCKED OUT AND CHANGED THE MEL TO 78-2A.Jun 14, 1997 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9711661150Longeron · crackedDURING L-CHECK, FOUND CRACK IN STR 41 AT RIGHT WING STA XORS 344. REPAIRED PER EA 11-150363.Jun 12, 1997 · N150US · Doug DC1040 · Wing, Longeron/StringerSDR 9711121160Duct · looseAT APPROXIMATELY V1 SPEED, THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AND AT 800 FT AGL THE NR 1 REVERSER UNLOCK LIGHT ILLUMINATED. THE NR 1 ENGINE WAS SHUT DOWN PER IAW COM PROCEDURES AND FUEL WAS DUMPED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOJun 6, 1997 · N160US · Doug DC1040 · Pneumatic Distribution System
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