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 9611391154Hyd Pump · broken plugDURING CLIMBOUT, LOST THE NR 1 HYDRAULIC SYSTEM FLUID. FLIGHT DUMPED 40,000 LBS OF FUEL AND RETURNED TO HNL. MAINTENANCE REPLACED THE RIGHT HYDRAULIC PUMP AND THE AIRCRAFT RETURNED TO SERVICE.May 26, 1996 · N154US · Doug DC1040 · Hydraulic Pump (Electric/Engine), MainSDR 9611401149Fail Light · illuminatedAFTER TAKEOFF POWER WAS APPLIED, THE NR 2 ENGINE FAIL LIGHT ILLUMINATED AT 48 PERCENT N1. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. INSPECTED THE NR 2 ENGINE FOR DISCREPANCIES AND NON WERE FOUND. AIRCRAFT RETURNED TO SERVICE, THE NR 2 ENGINE FAIL LIGHTMay 23, 1996 · N149US · Doug DC1040 · Central WarningSDR 9611291155Tr Unit · malfunctionedDURING TAKEOFF ROLLOUT, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 3 REVERSER AND FOUND IT TO BE NORMAL. DURING REVERSER OPERATION WITH GROUND AIR, REVERSER DEPLMay 20, 1996 · N155US · Doug DC1040 · Engine Thrust ReverserSDR 9611221155Compressor · stalledDURING LANDING ROLLOUT, THE NR 1 AND NR 3 ENGINES EXPERIENCED COMPRESSOR STALLS IN REVERSE. MAXIMUM TEMPERATURE WAS AT 700 DEGRESS CELSIUS FOR BOTH ENGINES. BOTH ENGINES WERE SHUT DOWN AND RESTARTED. CREW FOLLOWED COCKPIT PROCEDURE AND TAXIED TO THE GATE WIMay 20, 1996 · N155US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9610651159Wire · failedDURING CRUISE, MULTIPLEX SYSTEM POWER CABLE SHORTED AND SPARKED BETWEEN SEATS 33DE. MECHANIC ON BOARD DISCONNECTED THE POWER SOURCE FROM THE MUX BOX. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. REPLACED SEATS, CABLES, AND SEAT BOXES.May 15, 1996 · N159US · Doug DC1040 · Entertainment SystemSDR 9611061145Web · crackedDURING T-CHECK, FOUND A CRACK IN THE RIGHT NOSE LANDING GEAR WHEELWELL WEB FS 481 - FS 496, WATER LINE -60 TO -70. REPAIRED WEB (P/N NCA 6246-28) PER EA 11-104263.May 14, 1996 · N145US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9612691145Jamb Doubler · corrodedDURING T-CHECK, FOUND CORROSION IN THE AFT CARGO DOOR JAMB LOWER AFT CORNER DOUBLERS AND RAIL. REPAIRED DOUBLERS (P/N AFA7052-1, AFA7083-501) AND THE RAIL (P/N AFA7029-1) PER EA 11-104264.May 13, 1996 · N145US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9611611145Seat Track · corrodedDURING T-CHECK, FOUND CORROSION ON THE RIGHT OUTBOARD SEAT TRACK FROM FS 1990 - FS 2005, RBL 67. REPAIRED TRACK (P/N NFA 6222-9) PER EA 11-104266.May 13, 1996 · N145US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9611031145Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 45R AT FS 1690. REPAIRED LONGERON (P/N AFA 7097-1) PER EA 11-104262.May 13, 1996 · N145US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 96104311596Battery Pack · dischargedDURING LINE INSPECTION, FOUND THE EMERGENCY ESCAPE PATH LIGHT FROM DOOR 3L TO ROW 28 DIM. REPLACED EMERGENCY LIGHT BATTERY PACK.May 13, 1996 · N159US · Doug DC1040 · Emergency LightingSDR 9611591145Track · corrodedDURING T-CHECK, FOUND CORROSION ON THE LEFT OUTBOARD SEAT TRACK FROM FS 1521 - FS 1541, LBL 107. REPAIRED TRACK PER EA 11-099327.May 11, 1996 · N145US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9611001145Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT FS 1652. REPAIRED LONGERON (P/N AFA 7078-1) PER EA 11-104261.May 11, 1996 · N145US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9611581145Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON EXTERNAL LONGERON 31R AT FS 1504. REPAIRED LONGERON (P/N AEA 7136-2) PER EA 11-105391.May 9, 1996 · N145US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9610411155Engine · malfunctionedDURING LANDING ROLLOUT, THE NR 3 ENGINE EXPERIENCED REVERSE STALL WITH A SUBSEQUENT TAILPIPE FLAME WHICH WAS REPORTED BY THE CONTROL TOWER. THE NR 3 ENGINE WAS SHUTDOWN AND FIRE BOTTLE DISCHARGED AS EGT CLIMBED TO 915 DEGREES CELSIUS. HOWEVER, THERE WAS NO FMay 9, 1996 · N155US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9612681145Jamb Web · crackedDURING T-CHECK, FOUND TWO CRACKS 2.5 AND 1.75 LONG 3L IN THE DOOR 3L AFT LOWER DOOR JAMB WEB. REPAIRED WEB (P/N AEA0112-1) PER EA 11-105390.May 8, 1996 · N145US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9611571145Skin · corrodedDURING T-CHECK, FOUND CORROSION ON THE EXTERIOR SKIN FS 1343 - FS 1368, LBL 51 - RBL 51, AT THE POPPET DRAIN PLUGS. REPAIRED SKIN (P/N AYB 7065/NYB 6208) PER EA 11-105372.May 8, 1996 · N145US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9611561145Jamb · crackedDURING T-CHECK, FOUND A CRACK IN THE 3R LOWER FORWARD DOOR JAMB WEB. REPAIRED WEB (P/N AEA 0115-2) PER EA 11-105389.May 8, 1996 · N145US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9611541145Skin · crackedDURING T-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE SKIN AT THE FUELING ACCESS CUT-OUT XOS 611. REPAIRED SKIN (P/N ARB 2887-501) PER EA 11-105388.May 7, 1996 · N145US · Doug DC1040 · Wing, Plate/SkinSDR 9609471158Fuel Control · malfunctionedWHILE WAITING FOR TAKEOFF, THE NR 1 ENGINE COMPRESSOR STALL OCCURRED AT ENGINE IDLE POWER. EGT TEMPERATURE REACHED 700 CELSIUS AND THE NR 1 ENGINE WAS SHUTDOWN. AIRCRAFT RETURNED TO THE GATE. GROUND MAINTENANCE REPLACED THE ENGINE VANE CONTROL, PERFORMED ENApr 30, 1996 · N158US · Doug DC1040 · Fuel Control/Turbine EnginesSDR 9609321143Compressor · stalledAT TOP OF DESCENT, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THE ENGINE WAS SHUTDOWN AND A HIGH ALTITUDE RAPID RESTART WAS ATTEMPTED BUT DID NOT START. A SECOND RESTART WAS SUCCESSFUL AND FLIGHT CONTINUED TO MCO WITHOUT FURTHER INCIDENT. MAINTENANCE PApr 28, 1996 · N133JC · Doug DC1040 · Turbine Engine Compressor SectionSDR 9609301143Air Data Comp · failedDURING TAKEOFF ROLL, THE CAPTAIN'S AIRSPEED READ 20 KNOTS HIGHER THAN THE FIRST OFFICER'S AIRSPEED INDICATOR. ABORTED TAKEOFF AND RETURED TO THE GATE. DURING TAXI THE CAPTAIN'S ALTIMETER READ 120 FEET HIGHER THAN THE FIRST OFFICER'S ALTIMETER. REPLACED THE Apr 28, 1996 · N133JC · Doug DC1040 · Air Data ComputerSDR 9609281153Wire · failedDURING LINE INSPECTION, FOUND THE FLOOR TRACK LIGHT INOPERATIVE ON THE RIGHT SIDE OF THE FIRST CLASS CABIN. REPAIRED TRACK WIRING AT DOOR 2R.Apr 25, 1996 · N153US · Doug DC1040 · Light System WiringSDR 9609111155Bleed Valve · malfunctionedAT TOP OF DESCENT, THE NR 2 ENGINE EXPERIENCED COMPRESSOR STALL. THE EGT ROSE TO 800 DEGREES AND BACK TO NORMAL WITHIN A MINUTE. ALSO, WITH LOW FUEL FLOW N1 AND N2 WOULD NOT RESPOND TO THROTTLE MOVEMENTS. CREW FOLLOWED COCKPIT OPERATING MANUAL AND CONTINUEDApr 21, 1996 · N155US · Doug DC1040 · Compressor Bleed ValveSDR 9608911151Power Pack · inoperativeDURING LINE INSPECTION, THE EMERGENCY FLOOR PATH LIGHTS OVER THE AFT WING AREA WERE INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERIES.Apr 18, 1996 · N151US · Doug DC1040 · Emergency LightingSDR 9608821146Header · crackedDURING L-CHECK, FOUND A .75 INCH CRACK IN THE FORWARD CARGO DOOR CUTOUT UPPER HEADER FS 938. REPAIRED HEADER (P/N ADA0217) PER EA 11-103925.Apr 17, 1996 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9608811146Skin · crackedDURING L-CHECK, FOUND A .5 INCH CRACK IN THE UPPER SKIN OF THE RIGHT INBOARD ELEVATOR. REPAIRED SKIN PER EA 11-104237.Apr 17, 1996 · N146US · Doug DC1040 · Elevator, Plate/SkinSDR 9608791146Web · crackedDURING L-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL LEFT AND RIGHT SIDE WEBS AT FS 495, Z= -64. REPAIRED WEBS (P/N NCA6246-25, -27) PER EA 11-102158.Apr 16, 1996 · N146US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9608541161Tach Generator · malfunctionedDURING CLIMBOUT, THE NR 3 ENGINE N1, N2 AND NR 3 EPR BECAME ERRATIC, ALL OTHER INDICATIONS NORMAL. CREW FOLLOWED COCKPIT OPERATING PROCEDURES AND RETURNED TO DTW WITHOUT FURTHER INCIDENT. REPLACED THE N1 AND N2 INDICATORS. ALSO, REPLACED THE NR 3 N2 TACH GEApr 13, 1996 · N161US · Doug DC1040 · Engine RPM Indicating SystemSDR 9608421160Skin · corrodedDURING C-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 869, LONGERON 39R, UNDER THE PRIMARY STATIC PORT. REPAIRED SKIN (P/N ADA7030-1) PER EA 11-103927.Apr 9, 1996 · N160US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9608171152Battery Pack · dischargedDURING INSPECTION, FOUND THE EMERGENCY LIGHTS IN THE FORWARD CABIN FAILED THE SELF-TEST. REPLACED THE BATTERY PACK.Mar 22, 1996 · N152US · Doug DC1040 · Emergency LightingSDR 9605781149Engine · fodDURING TAXIING, THE NR 3 ENGINE GENERATOR CAME OFF-LINE FOLLOWED BY HIGH EGT OF 840 DEGREES. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE GATE. GROUND CREW AND SEVERAL PASSENGERS NOTED WHAT APPEARED LIKE A PIECE OF PLASTIC BEING SUCKED INTO THE Mar 9, 1996 · N149US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9605701150Compressor · stalledAT TOP OF DESCENT, THE NR 3 ENGINE COMPRESSOR STALLED AND EGT ROSE TO 750 DEGREES. THE ENGINE WAS SHUT DOWN AND A SUCCESSFUL RESTART WAS ACCOMPLISHED. FLIGHT CONTINUED TO DTW WITHOUT FURTHER INCIDENT. VISUAL INSPECTION AND BORESCOPE OF NR 3 ENGINE HIGH PRESMar 6, 1996 · N150US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9605011144Compressor · stalledDURING LANDING ROLLOUT, THE NR 3 ENGINE EXPERIENCED REVERSE STALL. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND NR 3 ENGINE SHUTDOWN WAS ACCOMPLISHED WITHOUT FURTHER INCIDENT. BORESCOPE INSPECTION OF NR 3 ENGINE HPC 13TH AND 15TH STATOR STAGES REVEALED NO DMar 1, 1996 · N144JC · Doug DC1040 · Turbine Engine Compressor SectionSDR 9605611149Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 46R AT FS 1781. REPAIRED LONGERON (P/N AFA 7098-1) PER EA 11-103255.Feb 29, 1996 · N149US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9605571149Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 48L AT FS 1964. REPAIRED LONGERON (P/N AGA 7047-1) PER EA 11-103940.Feb 28, 1996 · N149US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9605561149Splice · corrodedDURING T-CHECK, FOUND CORROSION ON THE LONGERON 50L SPLICE AT FS 1156. REPAIRED SPLICE (P/N ADA 7313) PER EA 11-103956.Feb 27, 1996 · N149US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9605551149Jamb · corrodedDURING T-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB AT FS 999, LONGERON 43L. REPAIRED JAMB (P/N S2929817) PER EA 11-103895.Feb 27, 1996 · N149US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9604631150Compressor · stalledDURING DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED AND INFLIGHT SHUTDOWN WAS ACCOMPLISHED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND CONTINUED FLIGHT TO PHX. INSPECTION AND RUNUP OF NR 2 ENGINE ON GROUND WAS NORMAL.Feb 25, 1996 · N150US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9605491149Blkhd Web · corrodedDURING T-CHECK, FOUND CORROSION ON THE FS 2007 AFT PRESSURE BULKHEAD WEB AND STIFFENER AT LBL 32, Z = -40. REPAIRED WEB (P/N NJC6040-501) AND STIFFENER (P/N NJC6040-109) PER EA 11-99304.Feb 22, 1996 · N149US · Doug DC1040 · Fuselage Main, BulkheadSDR 9606711149Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON EXTERNAL LONGERONS 29R TO 31R FROM FS 1501 TO 1521. REPAIRED LONGERONS (P/N AEA7133-2, 7132-2, AND 7136-2, RESPECTIVELY) PER EA 11-103946.Feb 21, 1996 · N149US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9605441149Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 47R AT FS 1156. REPAIRED LONGERON (P/N ADA7308-502) PER EA 11-103951.Feb 17, 1996 · N149US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9603941162Seal · leakingDURING DESCENT, THE NR 2 ENGINE WAS SHUTDOWN DUE TO OIL PRESSURE DROPPING BELOW 35 PSI AND OIL QUANTITY DROPPING TO 1 GALLON. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND CONTINUED FLIGHT TO HNL WITHOUT FURTHER INCIDENT. REPLACED THE RIGHT GARLOCK SEAL THATFeb 14, 1996 · N162US · Doug DC1040 · Turbine Engine Oil SystemSDR 9603551157Computer · failedDURING TAKEOFF, CAPTAIN'S AIRSPEED INDICATOR FROZE AT 100 KNOTS WHILE THE FIRST OFFICER'S INDICATOR READ 60 KNOTS. TAKEOFF WAS ABORTED. THE CAPTAIN'S AIR DATA COMPUTER WAS SWAPPED WITH THE NR 3 COMPUTER AND AIRCRAFT RETURNED TO SERVICE.Feb 12, 1996 · N157US · Doug DC1040 · Air Data ComputerSDR 9603601150Tr Unlock Light · illuminatedDURING TAKEOFF, THE NR 1 REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 1 REVERSER AND FOUND NORMAL. PLACARD NR 1 REVERSER INDICATION PER MEL 78-2A.Feb 11, 1996 · N150US · Doug DC1040 · Engine Thrust ReverserSDR 9603531161Power Supply · inoperativeDURING LINE CHECK, THE EMERGENCY LIGHT TEST LIGHT WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY AND BATTERY.Feb 10, 1996 · N161US · Doug DC1040 · Emergency LightingSDR 9603121156Bleed Converter · malfunctionedAT TOP OF DESCENT, THE NR 3 ENGINE EXPERIENCED COMPRESSOR STALL. THE NR 3 ENGINE WAS SHUTDOWN AND RESTARTED. FLIGHT CONTINUED TO LGW WITHOUT FURTHER INCIDENT. REPLACED BLEED CONVERTER AND PS4 RESTRICTOR. PERFORMED ENGINE RUNUP AND ALL PARAMETERS WERE NORMAFeb 10, 1996 · N156US · Doug DC1040 · Compressor Bleed ControlSDR 9603331143Compressor · stalledDURING DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUTDOWN AND RESTARTED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND CONTINUED TO LAX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE AND CHECK WAS NORMAL.Feb 8, 1996 · N133JC · Doug DC1040 · Turbine Engine Compressor SectionSDR 9605301157Compressor · stalledDURING TAKEOFF, THE NR 3 ENGINE STALLED AND TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE AND BORESCOPE OF NR 3 ENGINE REVEALED NO TROUBLE. REPLACED THE NR 3 EVC AND PRECISION TRIMMED. OPERATIONAL CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE.Feb 4, 1996 · N157US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9602921159Battery · dischargedDURING LINE CHECK, FOUND THE FORWARD SECTION OF THE EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED THE FORWARD BATTERY PACK.Feb 4, 1996 · N159US · Doug DC1040 · Emergency LightingSDR 9602801146Stall Transducer · malfunctionedDURING TAKEOFF, AUTO SLAT WOULD NOT RETRACT AND STICK SHAKER ACTIVATED. DUMPED 16,000 LBS OF FUEL AND RETURNED TO DTW. REPLACED AT/SC COMPUTER (11-2232-9-0001, SN 10201) AND THE NR 1 STALL TRANSDUCER (11-3418-9-0001, SN 00438).Feb 4, 1996 · N146US · Doug DC1040 · Stall Warning System
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