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 9900981161Seat Track · corrodedDURING M-CHECK, FOUND GOUGING AND CORROSION ON THE OUTBOARD AFT CABIN SEAT TRACK LBL 108 AT FS 1661 TO 1700. REPAIRED PER EA 11-164769.Feb 12, 1999 · N161US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9900501149Duct · failedDURING INITIAL CLIMB AFTER TAKEOFF AT APPROXIMATELY 2000 FT MSL, THE NR 2 ENGINE FIRE WARNING ANNUNCIATED. THE ENGINE WAS SHUT DOWN PER THE FIRE WARNING CHECK LIST AND THE NR 1 FIRE BOTTLE WAS DISCHARGED. THE FIRE WARNING CEASED AFTER THE BOTTLE WAS DISCHARGFeb 11, 1999 · N149US · Doug DC1040 · Pneumatic Distribution SystemSDR 9901191161Frame · crackedDURING M-CHECK, FOUND CRACK IN FORWARD CARGO FLOOR FRAME AT FS 1099 AT LBL 38. REPAIRED PER EA 11-158134.Feb 5, 1999 · N161US · Doug DC1040 · Fuselage Main, FrameSDR 9900441154Valve · leakingHYDRAULIC QUANTITY DECREASED TO ZERO DURING FLIGHT. FLIGHT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. FOUND LOWER HORIZONTAL STABILIZER CONTROL VALVE LEAKING. REPLACED CONTROL VALVE, LEAK AND OPERATIONAL CHECK OK.Feb 5, 1999 · N154US · Doug DC1040 · Stabilizer Control SystemSDR 9901211156Floorbeam · crackedDURING M-CHECK, FOUND CRACKS ON THE FLOORBEAM UPPER CHORD AT FS 791, LBL 6 TO RBL 2. REPAIRED PER EA 11-162058.Jan 14, 1999 · N156US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9901251156Longeron · crackedDURING M-CHECK, FOUND CORROSION ON HORIZONTAL SECTION OF LONGERON 30R AT FS 1450, 1470 AND 1503. ALSO, FOUND TWO INCH CRACK ON HORIZONTAL SECTION OF LONGERON 30R AT FS 1431. REPAIRED PER EA 11-162065.Jan 13, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901281156Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 32L BETWEEN FS 1501 AND 1521. REPAIRED PER EA 11-162062.Jan 12, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901231156Longeron · crackedDURING M-CHECK, FOUND CORROSION ON HORIZONTAL SECTION OF LONGERON 31R AT FS 1471 AND 1491. CRACKS WERE ALSO FOUND ON HORIZONTAL SECTION OF LONGERON 31R AT FS 1501 AND 1531. REPAIRED PER EA 11-162069.Jan 12, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9900131158Light · smokingDURING APPROACH INTO BOS, FLIGHT ATTENDANT NOTICED SMOKE FROM CABIN LIGHT ABOVE SEAT 2H AND 2J. NOTIFIED COCKPIT AND SHUT LIGHTS OFF. SMOKE DISSIPATED. CAPTAIN DECLARED A PRECAUTIONARY EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED BALLAST ON LIGHTJan 11, 1999 · N158US · Doug DC1040 · Passenger Compartment LightingSDR 9901271156Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 34R AT FS 1521 AND 1531. REPAIRED PER EA 11-162072.Jan 10, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901241156Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 30L BETWEEN FS 1501 TO 1521. REPAIRED PER EA 11-162061.Jan 10, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901261156Longeron · corrodedDURING M-CHECK, FOUND CORROSION BEYOND SRM LIMITS ON LONGERON 44R AT FS 1601. REPAIRED PER EA 11-162068.Jan 8, 1999 · N156US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9900831141Longeron · corrodedDURING M-CHECK, FOUND CORROSION BETWEEN FS 1741 AND 1771 ON LONGERON 50L. REPAIRED PER EA 11-162749.Jan 7, 1999 · N141US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9900651141Longeron · corrodedDURING M-CHECK, FOUND CORROSION AT FS 1738 ON LONGERON 50L. REPAIRED PER EA 11-162749.Jan 7, 1999 · N141US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9900641141Lever · corrodedDURING M-CHECK, FOUND CORROSION UNDER AND AROUND PIVOT BEARING SUPPORT BUSHING ON INBOARD FLAP DRIVE LEVER. REPAIRED PER EA 11-162743.Jan 7, 1999 · N141US · Doug DC1040 · Wing, Landing Gear Attach FittingsSDR 9901221156Floorbeam · crackedDURING M-CHECK, FOUND CRACK ON THE FLOORBEAM UPPER CHORD AT FS 879 LBL 7. REPAIRED PER EA 11-162057.Jan 3, 1999 · N156US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9811481141Frame · crackedDURING M-CHECK, FOUND FUSELAGE FRAME CRACKED AT FS 1921 AT ATTACH TO LEFT CARGO TRACK. REPAIRED PER EA 11-162429.Dec 17, 1998 · N141US · Doug DC1040 · Fuselage Main, FrameSDR 9810531162Battery Pack · dischargedDURING LINE CHECK, LEFT AND RIGHT AISLE ESCAPE PATH LIGHTS OUT FROM ROW 22 TO 27. REPLACED BATTERY PACK AND CHARGER, OPERATIONAL CHECK OK.Nov 27, 1998 · N162US · Doug DC1040 · Emergency LightingSDR 9811101159Skin · corrodedDURING M CHECK, FOUND CORROSION ON INTERIOR SURFACE SKIN AT CENTER WHEEL WELL, LONGERON 48L TO 48R, FS 1509 TO 1521. REPAIRED PER EA 11-161113, MFG PART NUMBER AYB7065-.Nov 20, 1998 · N159US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9810271144Line · failedON DEPARTURE FROM HNL, LOST ALL HYDRAULIC FLUID IN NR 3 SYSTEM. FOLLOWED COM PROCEDURE AND RETURNED TO HNL. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 4 BRAKE LINE CHAFED THROUGH. REPLACED BRAKE LINE AND SERVICED SYSTEM. OPERATIONAL CHECK OK.Oct 13, 1998 · N144JC · Doug DC1040 · Hydraulic System, MainSDR 9811451159Frame · crackedDURING M-CHECK, FOUND FRAME CRACKED AT FS 454, RBL 64. REPAIRED PER EA 11-161107.Oct 2, 1998 · N159US · Doug DC1040 · Fuselage Main, FrameSDR 9811261161Power Supply · inopDURING LINE CHECK, FOUND EMERGENCY LIGHTS WOULD NOT TEST. REPLACED OVERWING POWER SUPPLY. OPERATIONAL CHECK OK.Sep 30, 1998 · N161US · Doug DC1040 · Emergency LightingSDR 9810201160Frame · crackedDURING M-CHECK, FOUND CRACK ON LOWER NOSE FUSELAGE FRAME AT FS 459. REPAIRED PER EA 11-157988.Sep 24, 1998 · N160US · Doug DC1040 · Fuselage Main, FrameSDR 9811251161Power Supply · inopDURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING FROM DOOR 3L AND 3R TO ROW 32 INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY AND CONTROL UNIT. OPERATIONAL CHECK OK.Sep 22, 1998 · N161US · Doug DC1040 · Emergency LightingSDR 9810211160Floorbeam · crackedDURING M-CHECK, FOUND CRACK AT THE AFT CARGO FLOORBEAM UPPER CHORD UNDER THE LEFT SEAT TRACK AT FS 1821. REPAIRED PER EA 11-161103.Sep 21, 1998 · N160US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9811271161Battery Pack · dischargedDURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE FROM DOOR 3L AND 3R TO ROW 32. REPLACED BATTERY PACK ABOVE DOOR 3L. OPERATIONAL CHECK OK.Sep 18, 1998 · N161US · Doug DC1040 · Emergency LightingSDR 9810221160Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON INBOARD FLANGE UPPER SIDE AT FS 1159-1179, LONGERON 27L. REPAIRED PER EA 11-160045.Sep 17, 1998 · N160US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9810051160Support · corrodedDURING M-CHECK, FOUND CORROSION ON THE FLOOR SUPPORT ON FRAME 999 ABOVE STR 44L. REPAIRED PER EA 11-160661.Sep 1, 1998 · N160US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9810001155Web · crackedDURING M-CHECK, FOUND CRACK IN WEB UPPER STRUCTURE IN LOWER RADIUS. REPLACED WEB DOUBLER PER EA 11-159807.Aug 27, 1998 · N155US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9810021155Bracket · corrodedDURING M-CHECK, FOUND CORROSION IN UPPER FASTENER BRACKET IN RUDDER. REPAIRED PER EA 11-160285.Aug 25, 1998 · N155US · Doug DC1040 · Rudder StructureSDR 9810011160Skin · corrodedCENTER LANDING GEAR WHEEL WELL REAR SHELF AREA HAS EXPOSED METAL AND CORROSION AT FS 1509 TO 1521 FROM LEFT KEEL WEB TO RIGHT KEEL WEB. REPAIRED PER EA 11-158662.Aug 25, 1998 · N160US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9811281151Battery Pack · dischargedDURING LINE CHECK, ZONE 'C' EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK.Aug 15, 1998 · N151US · Doug DC1040 · Emergency LightingSDR 9810041155Angle · corrodedDURING M-CHECK, FOUND LOWER CHORD ANGLE CORRODED ON INBOARD END. REPAIRED PER EA 11-158027.Jul 14, 1998 · N155US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9809961155Skin · corrodedDURING M-CHECK, FOUND CORROSION ON OUTER SKIN FROM FS 1510 TO 1531, STR 45R TO 45L. REPAIRED PER EA 11-158670.Jul 1, 1998 · N155US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9809951155Skin · crackedDURING M-CHECK, FOUND TWO INCH CRACK IN INBOARD EDGE OF LEADING EDGE FLEX SKIN. REPAIRED PER EA 11-155651.Jun 19, 1998 · N155US · Doug DC1040 · Wing, Plate/SkinSDR 9809601162Proximity Box · failedRECEIVED NOSE GEAR UNSAFE INDICATION WHEN GEAR EXTENDED FOR LANDING. RECYCLED GEAR AND FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. VISUALLY CONFIRMED GEAR DOWN. FLIGHT LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC BOX. FOUND NOSE GEAR DOWJun 19, 1998 · N162US · Doug DC1040 · Landing Gear Position and WarningSDR 9809561141Fuel Line · crackedWHILE AT CRUISE FL330, THE NR 2 ENGINE COMPRESSOR STALLED. ALL NR 2 PARAMETERS ROLLED BACK TO FLIGHT IDLE. THE ENGINE DID NOT RESPOND TO POWER LEVER INPUTS AND WAS SHUT DOWN. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. THE CREW DID ATTEMPT ONJun 16, 1998 · N141US · Doug DC1040 · Engine Fuel DistributionSDR 9809551153Engine · failedDURING CLIMB-OUT, THE NR 2 ENGINE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED AND THE INDICATED OIL TEMPERATURE WAS INCREASING. THE ENGINE WAS SHUT DOWN. 50,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO LAX WITHOUT FURTHER DIFFICULTY. THE AIRCRAFT Jun 12, 1998 · N153US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9809521149Line · failedDURING CRUISE, NR 1 HYDRAULIC SYSTEM INDICATED TOTAL LOSS OF FLUID. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 ENGINE HYDRAULIC KIT AND REPLACED LINE IN CENTER WHEEL WELL. LEAK AND OPERATIONAL CHECK OK.Jun 11, 1998 · N149US · Doug DC1040 · Hydraulic System, MainSDR 9809131149Engine · flamed outWHILE IN CRUISE FLIGHT AT FL340, THE AIRCRAFT ENCOUNTERED MODERATE TURBULENCE, POSSIBLY WAKE TURBULENCE, AND THE NR 1 ENGINE FLAMED OUT. THE ENGINE WAS SECURED PER ENGINE FAILURE CHECKLIST AND A DESCENT FROM FL340 WAS STARTED. AT FL300, A RESTART WAS ACCOMPLMay 11, 1998 · N149US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9809071157Compressor · stalledDURING TAKEOFF ROLL, THE NR 3 ENGINE COMPRESSOR STALLED WITH FLAMES REPORTED FROM THE TAILPIPE. THE TAKEOFF WAS ABORTED AT 25 KTS. THE EGT REACHED A MAXIMUM OF 800C AND THE ENGINE RECOVERED. MAINTENANCE INSPECTED THE ENGINE INCLUDING A BOROSCOPE WITH NO TROMay 10, 1998 · N157SU · Doug DC1040 · Turbine Engine Compressor SectionSDR 9808911150Tr Rigging · out of adjustUPON APPLICATION OF TAKEOFF POWER, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE ADJUSTED THE REVERSER VENT VALVE RIGGING AND FOUND ALL INDICATIONS NORMAL. AIRCRAFT DEPARTED WITMay 10, 1998 · N150US · Doug DC1040 · Engine Thrust ReverserSDR 9808921141Compressor · stalledDURING THE LANDING ROLLOUT, THE NR 3 ENGINE COMPRESSOR STALLED WHILE IN REVERSE THRUST. THE EGT REACHED 970C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE PERFORMED A BORESCOPE INSPECTION AND FOUND DAMAGE TO THE HIGH PRESSURE COMPRESSOR. THE AIRCRAFT WAS REMOMay 7, 1998 · N141US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9808621162Compressor · stalledDURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 880C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER TAFI STALL PROCEDURE WITH NO TROUBLE FOUND. RABS CHECK WAS NOT ACCOMPLISHED AND THMay 6, 1998 · N162US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9808211160Compressor · stalledDURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT REACHED 800C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER TAFI 71-00-00 WITH NO DEFECTS NOTED. THE THRUST REVERSER WAS PLACED ON MEL 78-1A UMay 2, 1998 · N160US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9807741160Engine · flamed outAT TOP OF DESCENT FL330, THE NR 3 ENGINE FLAMED OUT. THE ENGINE WAS SUCCESSFULLY RESTARTED ON THE SECOND ATTEMPT. THE DESCENT AND LANDING WAS WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE ENGINE PER TAFI 71-00-00 AND PERFORMED A HIGH POWER ENGINE RUN, ALL WApr 29, 1998 · N160US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9807601156Rccb · inoperativeDURING CRUISE, LOST GROUND SERVICE BUS, VIDEO SYSTEM BECAME INOPERATIVE AND ALSO TOILETS. WATER QUANTITY INDICATED ZERO AND WATER PRESSURE INDICATED LOW. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RCCB BI-339, OPERATIONAL CHECKApr 26, 1998 · N156US · Doug DC1040 · AC Power Distribution SystemSDR 9806981152Compressor · stalledDURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 1 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN WITH THE EGT REACHING A MAXIMUM OF 940C. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE.Apr 20, 1998 · N152US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9806901162Compressor · stalledDURING LANDING ROLLOUT WHILE COMING OUT OF REVERSE THRUST AT 80 KTS, THE NR 3 ENGINE COMPRESSOR STALLED. EGT PEAKED AT 1000C BEFORE THE ENGINE WAS SHUT DOWN AND THE COM COMPLIED WITH. MAINTENANCE INSPECTED THE ENGINE PER MAINTENANCE MANUAL INCLUDING A BORESCApr 17, 1998 · N162US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9806911148Tr Unit · malfunctionedDURING TAKEOFF ROLL, THE NR 2 ENGINE REVERSER UNLOCKED LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A.Apr 16, 1998 · N148US · Doug DC1040 · Engine Thrust Reverser
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