Douglas DC-10-40

Service difficulty reports · 614

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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 = '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 9710721156Compressor · stalledDURING TAKEOFF ROLL, PASSENGERS REPORTED A FLASH AND FLAME BALL FROM LEFT WING. ALSO, TOWER REPORTED HEARING A LOUD NOISE. TAKEOFF WAS ABORTED AT 80 KNOTS. CREW SUSPECTED NR 1 ENGINE COMPRESSOR STALL BUT REPORTED NO ABNORMAL INDICAITONS. MAINTENANCE INSPECJun 4, 1997 · N156US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9710681152Prbc · failedDURING DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED WITH RISING EGT. ENGINE WAS SHUT DOWN AT MAX EGT OF 650C. NR 2 ENGINE RESTART AND SUBSEQUENT OPERATION WERE NORMAL. MAINTENANCE REPLACED THE PRBC AND RAN ENGINE TO TAKEOFF POWER. ALL PARAMETERS WERE NORMALJun 3, 1997 · N152US · Doug DC1040 · Compressor Bleed ValveSDR 9710511156Disagree Light · illuminatedDURING TAKEOFF, THE SLAT DISAGREEMENT LIGHT ILLUMINATED. ABORTED TAKEOFF. MAINTENANCE REPLACED THE FLAP POSITION INDICATOR AND INSTALLED THE DC10 SLAT DISAGREE TEST PANEL PER MM 27-84-00. GROUND AND FLIGHT OPERATIONAL CHECK OK.May 28, 1997 · N156US · Doug DC1040 · Leading Edge Slat Position Indicating SystemSDR 9710311147Engine · overtempON LANDING WITH ALL ENGINES IN REVERSE THRUST, NR 1 ENGINE OVERTEMPED REACHING MAX EGT 980 CELSIUS. THE NR 1 ENGINE WAS SHUTDOWN WITH REVERSER UNLOCK LIGHT STILL ILLUMINATED. MAINTENANCE INSPECTED INLET AND EXHAUST, RAN ENGINE AT IDLE, AND CYCLED REVERSER SEMay 27, 1997 · N147US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9710481156Prox Contl Box · failedDURING TAKEOFF, THE SLAT DISAGREEMENT LIGHT ILLUMINATED WITH THE TAKEOFF WARNING HORN. ABORTED TAKEOFF. MAINTENANCE REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL BOX AND THE FLAP POSITION INDICATOR.May 26, 1997 · N156US · Doug DC1040 · Leading Edge Slat Position Indicating SystemSDR 9710501158Prox Box · malfunctionedDURING TAKEOFF, GEAR VIBRATION WAS FELT UPON RETRACTION AND ALL UNSAFE GEAR LIGHTS REMAINED RED. RECYCLED GEAR AND OPERATION WAS NORMAL. MAINTENANCE REPLACED BOTH NOSE GEAR TIRES. RESET MAIN LANDING GEAR PROXIMITY BOX AND NO FAULTS WERE FOUND WITH GEAR INDIMay 25, 1997 · N158US · Doug DC1040 · Landing Gear Position and WarningSDR 9710391161Transducer · seizedDURING FLAP RETRACTION AFTER TAKEOFF, STICK SHAKER ACTIVATED, SLAT DISAGREE LIGHT AND RESET LIGHT ILLUMINATED AND COULD NOT GET SLATS TO RETRACT. DUMPED 10,000 LBS OF FUEL AND RETURNED TO SFO. MAINTENANCE REPLACED THE STALL TRANSDUCER, OPERATIONAL CHECK OK.May 25, 1997 · N161US · Doug DC1040 · Stall Warning SystemSDR 9710951154Skin · corrodedDURING L-CHECK, FOUND CORROSION ON FUSELAGE SKIN FS 1853 TO 1871 AT LONGERON 43L. REPAIRED PER EA 11-124093.May 24, 1997 · N154US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9710211143Engine · malfunctionedNR 1 ENGINE EGT ROSE RAPIDLY AFTER THE REVERSER WAS STOWED. ENGINE WAS SHUTDOWN, EGT PEAKED AT 780 CELSIUS. MAINTENANCE RAN NR 1 ENGINE, OPERATED REVERSER AND ALL INDICATIONS WERE NORMAL.May 24, 1997 · N133JC · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9710941154Spar · corrodedDURING L-CHECK, FOUND CORROSION ON UPPER T-CHORD OF AFT SPAR FROM XORS 1077 TO 1086. REPAIRED PER EA 11-150360.May 23, 1997 · N154US · Doug DC1040 · Wing SparSDR 9710111158Compressor · stalledAT 1,400 FEET DURING TAKEOFF, THE NR 2 ENGINE COMPRESSOR STALLED TWICE WITH EGT MOMENTARILY REACHING 900C ON BOTH OCCASIONS. NO OTHER ABNORMAL INDICATIONS. MAINTENANCE CONTROL RECOMMENDED DIVERSION TO BOS FOR MAINTENANCE. INSPECTION FOUND COMPRESSOR BLADE PMay 21, 1997 · N158US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9709911144Switch · stickingDURING LANDING, LOWERED LANDING GEAR HANDLE AND RED UNSAFE LIGHT ILLUMINATED AND DID NOT GO OUT. RECYCLED GEAR AND OPERATION WAS NORMAL. MAINTENANCE CLEANED AND LUBED GEAR HANDLE SWITCH.May 12, 1997 · N144JC · Doug DC1040 · Landing Gear Position and WarningSDR 9709461152Skin · corrodedDURING LINE CHECK, FOUND CORROSION ON FUSELAGE SKIN UNDER LEFT BODY FAIRING FS 1741 - 1761. REPAIRED PER EA 11-124146.May 7, 1997 · N152US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9709171148Compressor · stalledDURING TAKEOFF ROLL WITH POWER APPLICATION, THE NR 3 ENGINE COMPRESSOR STALLED. TAKEOFF WAS ABORTED WITH NO ENGINE LIMITS EXCEEDED. SECOND TAKEOFF WITH SLOWER POWER APPLICATION WAS NORMAL. MAINTENANCE VISUALLY INSPECTED ENGINE PER MM 71-00-00. NO DEFECTS WMay 7, 1997 · N148US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9709631155Tr Unit · malfunctionedWHEN POWER PUSHED UP TO TAKEOFF LEVEL, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE DEFERRED NR 3 THRUST REVERSER PER MEL 78-1A. SPECIFIC PART CAUSING PROBLEM TO BE DETERMINED.May 1, 1997 · N155US · Doug DC1040 · Engine Thrust ReverserSDR 9708341160Tr Light · illuminatedDURING TAKEOFF ROLL, THE NR 2 ENGINE AMBER REVERSER UNLOCK LIGHT ILLUMINATED AND TAKEOFF WAS ABORTED. MAINTENANCE VERIFIED REVERSER WAS STOWED AND ALL LOCKPLATES INSTALLED. MEL 78-2A WAS ADDED. SPECIFIC PART CAUSING PROBLEM TO BE DETERMINED.Apr 27, 1997 · N160US · Doug DC1040 · Engine Thrust ReverserSDR 9709471143Skin · crackedDURING 'M' CHECK, FOUND CRACKS IN LEADING EDGE SKIN AT EXTINGUISHER BOTTLE ACCESS INBOARD AND OUTBOARD FORWARD CORNER. REPAIRED PER EA 11-122890.Apr 19, 1997 · N141US · Doug DC1040 · Wing, Plate/SkinSDR 9708001143Frame · crackedDURING M-CHECK, FOUND CRACK IN FRAME AT FS 1851, LONGERON 11R. REPAIRED PER EA 11-098840.Apr 19, 1997 · N141US · Doug DC1040 · Fuselage Main, FrameSDR 9709491143Doubler · crackedDURING 'M' CHECK, FOUND CRACK IN DOUBLER BETWEEN LONGERON 4R AND 5R, FS 1129. REPAIRED PER EA 11-122888.Apr 18, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9708661143Frame · crackedDURING M-CHECK, FOUND CRACK IN FRAME AT FS 1851 AT LONGERON 10L TO 11L. REPAIRED PER EA 11-098839.Apr 18, 1997 · N141US · Doug DC1040 · Fuselage Main, FrameSDR 9708021143Frame · crackedDURING M-CHECK, FOUND CRACK IN FRAME AT FS 1841 JUST BELOW LONGERON 12L. REPAIRED PER EA 11-123994.Apr 18, 1997 · N141US · Doug DC1040 · Fuselage Main, FrameSDR 9708011143Frame · crackedDURING M-CHECK, FOUND CRACK IN FRAME AT FS 1851 AT LONGERON 10R. REPAIRED PER EA 11-098840.Apr 18, 1997 · N141US · Doug DC1040 · Fuselage Main, FrameSDR 9707731154Bleed Solenoid · malfunctionedAFTER LANDING, WHILE COMING OUT OF REVERSE THRUST, NR 2 ENGINE EGT ROSE RAPIDLY. NR 2 ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED ENGINE PER MM 72-00-00, PG 227 AND REPLACED BLEED OVERRIDE SOLENOID. THE NR 2 ENGINE WAS GROUND RUN AND CHECKED OK.Apr 18, 1997 · N154US · Doug DC1040 · Compressor Bleed ControlSDR 9709481143Frame · corrodedDURING 'M' CHECK, FOUND CORROSION LOWER AFT SKIN ATTACH ANGLE IN SILL ACCESS FS 1708, RBL 70. REPAIRED PER EA 11-124021.Apr 17, 1997 · N141US · Doug DC1040 · Fuselage Main, FrameSDR 9707741154Compressor · stalledDURING TOP OF DESCENT, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL. THE NR 3 ENGINE WAS SHUT DOWN. THE NR 3 ENGINE WAS RESTARTED AT 25,000 FEET AND OPERATED NORMALLY FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE BOROSCOPE INSPECTED NR 3 ENGINE, NO TROUBLEApr 17, 1997 · N154US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9708161143Bracket · corrodedDURING M-CHECK, FOUND CORROSION ON AFT SHEAR TIE AT FS 945 BETWEEN LONGERONS 45R TO 46R. REPAIRED PER EA 11-122908.Apr 16, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9708101143Spar Chord · crackedDURING M-CHECK, FOUND CRACK IN RADIUS AT AFT UPPER SPAR CHORD WING STA XW 948-946 LEFT WING. REPAIRED PER EA 11-123995.Apr 16, 1997 · N141US · Doug DC1040 · Wing SparSDR 9707601147Battery · dischargedDURING LINE INSPECTION, FOUND THE FORWARD SECTION OF THE AFT ZONE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY.Apr 15, 1997 · N147US · Doug DC1040 · Emergency LightingSDR 9708651143Aft Shelf · corrodedDURING M-CHECK, FOUND CORROSION ON SKIN IN CENTER WHEEL WELL AFT SHELF INBOARD AND OUTBOARD OF RBL 27 'T' CHORD. REPAIRED PER EA 11-122905.Apr 14, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9707431160Erp Indicator · malfunctionedDURING TAKEOFF, NR 1 ENGINE EPR LOW. TAKEOFF WAS ABORTED AT 100 KNOTS. MAINTENANCE REPLACED EPR INDICATOR. ENGINE GROUND RUN AND EPR INDICATION AT IDLE AND TAKEOFF POWER WAS NORMAL.Apr 13, 1997 · N160US · Doug DC1040 · Engine Pressure Ratio (EPR)SDR 9707441161Prox Control · failedDURING GEAR RETRACTION, ALL LANDING GEAR UNSAFE LIGHTS ILLUMINATED WITH GEAR HANDLE UP. RECYCLED GEAR, NO HELP. GEAR VISULALY CHECKED UP. MAINTENANCE REPLACED MAIN LANDING GEAR PROXIMITY CONTROL.Apr 11, 1997 · N161US · Doug DC1040 · Landing Gear Position and WarningSDR 9707401148Air Data Comp · failedDURING TAKEOFF ROLL, THE CAPTAIN'S AIRSPEED INDICATOR READ ZERO WHILE THE COPILOT'S READ 120. ABORTED TAKEOFF. MAINTENANCE REPLACED THE AIR DATA COMPUTER.Apr 10, 1997 · N148US · Doug DC1040 · Air Data ComputerSDR 9708641143Jamb · crackedDURING M-CHECK, FOUND CRACK IN DOOR JAMB FOR DOOR 3R IN THE FORWARD LOWER WEB AT THE LOWER LIGHTENING HOLE. REPAIRED PER EA 11-122885.Apr 4, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9707031153Engine · malfunctionedAFTER LANDING WHILE COMING OUT OF ENGINE REVERSER, THE NR 1 ENGINE EGT EXCEEDED LIMITS. THE NR 1 ENGINE WAS SHUT DOWN. MAINTENANCE BORESCOPE INSPECTED ENGINE AND PERFORMED RAB'S SYSTEM CHECK IN ACCORDANCE WITH MM 75-30-00, PG 201-203. NO DISCREPANCIES WERE Apr 2, 1997 · N153US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9707021145Compressor · stalledAFTER AIRCRAFT PUSHBACK FROM GATE, NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WHILE AT IDLE POWER. FLIGHT CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED ENGINE AND FOUND NO DISCREPANCIES. ENGINE WAS GROUND RUN AND ALL PARAMETERS Apr 2, 1997 · N145US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9706711154Compressor · stalledAT TOP OF DESCENT, NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL. ENGINE WAS SHUT DOWN AT 31,000 FEET DUE TO RISING EGT. ENGINE WAS RESTARTED AT 29,000 FEET. AN UNEVENTFUL LANDING WAS PERFORMED AT DESTINATION AIRPORT. MAINTENANCE INSPECTED ENGINE PER MM 71-00-Mar 31, 1997 · N154US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9707051153Engine · malfunctionedAFTER LANDING WHILE COMING OUT OF ENGINE REVERSE THRUST, THE NR 3 ENGINE EGT BEGAN TO EXCEED LIMITS. ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED ENGINE PER MM 72-00-00, PG 227. NO DISCREPANCIES WERE NOTED.Mar 24, 1997 · N153US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9706051144Battery · dischargedDURING LINE INSPECTION, FOUND THE EMERGENCY LIGHT IN MID CABIN FLOOR AND CEILING INOPERATIVE. REPLACED BATTERY PACK.Mar 23, 1997 · N144JC · Doug DC1040 · Emergency LightingSDR 9708171143Bulkhead Channel · corrodedDURING M-CHECK, FOUND CORROSION IN SEVERAL AREAS ON THE FOURTH AND FIFTH CHANNELS DOWN FROM THE TOP OF THE BS 2007 BULKHEAD. PRIMED AND INSTALLED REPAIR PER EA 11-122886.Mar 22, 1997 · N141US · Doug DC1040 · Fuselage Main, BulkheadSDR 9706061162Prox Control · failedDURING LANDING, FOUR RED GEAR LIGHTS ILLUMINATED. RECYCLED GEAR, THE FOUR GREEN LIGHTS ILLUMINATED. MAINTENANCE REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL.Mar 19, 1997 · N162US · Doug DC1040 · Landing Gear Position and WarningSDR 9706071159Switch · bentDURING TAKEOFF, ALL THE GEAR RED UNSAFE LIGHTS ILLUMINATED. FOLLOWED COM PROCEDURE AND VERIFIED GEAR UP AND LOCKED. FLIGHT PROCEEDED TO PHX. MAINTENANCE REPLACED THE THROTTLE SWITCHES S1-342.Mar 18, 1997 · N159US · Doug DC1040 · Landing Gear Position and WarningSDR 9704791157Switch · malfunctionedDURING TAKEOFF, RECEIVED THE GEAR WARNING AND 3 RED LIGHTS. RECYCLED GEAR AND RECEIVED 3 RED LIGHTS. REPLACED MAIN LANDING GEAR PROXIMITY CONTROL WITH NO HELP. NEXT FLIGHT DURING TAKEOFF, RED UNSAFE LIGHTS REMAINED ILLUMINATED. FOLLOWED COM AND VERIFIED LAMar 6, 1997 · N157US · Doug DC1040 · Landing Gear Position and WarningSDR 9705451146Web · crackedDURING LINE CHECK, MULTIPLE CRACKS WERE FOUND IN THE NCA6246-28 NOSE GEAR SUPPORT WEB AT THE UPPER FORWARD CORNERS OF BOTH LEFT AND RIGHT WEBS. REPAIRED PER EA 11-123544.Mar 1, 1997 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9704011160Compressor · stalledSHORTLY AFTER TAKEOFF, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AT 300 FEET. ENGINE EGT BRIEFLY REACHED 985 AND THEN ALL INDICATIONS RETURNED TO NORMAL. FLIGHT CREW DECIDED TO RETURN TO DEPARTURE AIRPORT. PRIOR TO AN UNEVENTFUL LANDING, 110,000 LBS OFFeb 26, 1997 · N160US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9704941148Skin · crackedDURING L-CHECK, FOUND CRACK IN WING SKIN AT FORWARD INBOARD CORNER OF REFUELING DOOR AT STA XORS506. REPAIRED PER EA 11-121770.Feb 25, 1997 · N148US · Doug DC1040 · Wing, Plate/SkinSDR 9703731149Oil Quantity · lowDURING CRUISE FLIGHT, THE NR 3 ENGINE LOW OIL QUANTITY AND OIL PRESSURE DEVELOPED. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO YMX. AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE CHECKED FOR OIL LEAKS, INSPECTED CHIP DETECTORS, ADDED ENGINEFeb 22, 1997 · N149US · Doug DC1040 · Turbine Engine Oil SystemSDR 9703081146Compressor · stalledDURING LANDING, THE NR 3 ENGINE COMPRESSOR STALLED WHILE IN REVERSE. ENGINE WAS SHUT DOWN WHILE STILL IN REVERSE. PERFORMED INSPECTION WITH NO FAULTS FOUND, OPERATIONAL CHECK OK.Feb 12, 1997 · N146US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9702811152Fire Warning · illuminatedDURING CLIMB, THE NR 3 ENIGNE FIRE INDICATION ILLUMINATED. SHUT DOWN ENGINE AND FIRE BOTTLE DISCHARGED. DUMPED 16,800 LBS AND RETURNED TO LAX. AIRCRAFT TO BE FERRIED TO MSP.Feb 9, 1997 · N152US · Doug DC1040 · Fire DetectionSDR 9702801146Tr System · malfunctionedDURING TAKEOFF, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. RERIGGED REVERSER SYSTEM.Feb 9, 1997 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9702791158Apu · failedDURING BOARDING, THE APU FAILED, FIRE BOTTLES WERE FIRED AND CABIN FILLED WITH SMOKE. REPLACED APU, WATER SEPARATOR BAGS AND PURGED PACKS.Feb 9, 1997 · N158US · Doug DC1040 · APU Core Engine
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