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 9618921145Tt2 Sensor · failedDURING TAXING OUT, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AND VIBRATION. AS THE NR 1 ENGINE EGT CLIMBED TO 750 DEGREES, THE CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE, AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. REPLACED TT2 SENSOR, LEAK Sep 1, 1996 · N145US · Doug DC1040 · Engine BMEP/Torque IndicatingSDR 9619601162Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON THE FUSELAGE OVERWING EXTERNAL LONGERONS 30L, 32L, 37L, AND 32R FROM FS 1407 - FS 1548. REPAIRED LONGERONS PER EA 11-110189.Aug 31, 1996 · N162US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9618901154Engine · failedEN ROUTE, THE NR 1 ENGINE EXPERIENCED LOSS OF OIL QUANTITY AND PRESSURE. CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE, AND RETURNED TO SEA WITHOUT FURTHER INCIDENT. AT THE TIME OF SHUTDOWN, RESIDUAL PRESSURE WAS 28 PSI WITH 30 PERCENT N1 AND 20 PERCENT Aug 31, 1996 · N154US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9619241162Skin · crackedDURING T-CHECK, FOUND A CRACK IN THE NR 3 AIR CONDITIONING PACK CUTOUT SKIN UPPER AFT CORNER FS 535. REPAIRED SKIN (P/N ACA 3108-501) PER EA 11-110184.Aug 30, 1996 · N162US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9619231162Support · crackedDURING T-CHECK, FOUND A CRACK IN THE LEFT FLAP INBOARD FLAP SUPPORT BASE PLATE AT STA 1521. REPAIRED PLATE (P/N ANB 7170) PER EA 11-110179.Aug 29, 1996 · N162US · Doug DC1040 · Trailing Edge FlapsSDR 9619121162Floor Beam · crackedDURING T-CHECK, FOUND A CRACK IN THE FS 1099 FORWARD CARGO FLOOR BEAM AT LBL 60. REPAIRED BEAM (P/N ADA 0039-5) PER EA 11-106300.Aug 29, 1996 · N162US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9619581162Frame · crackedDURING T-CHECK, FOUND A .75 INCH CRACK IN THE LEFT FORWARD ACCESSORY COMPARTMENT DOOR JAMB FS 547 FRAME INBOARD CHORD. REPAIRED FRAME (P/N ACA 0051-3) PER EA 11-106313.Aug 28, 1996 · N162US · Doug DC1040 · Fuselage Main, FrameSDR 9619571162Door Jamb · crackedDURING T-CHECK, FOUND A CRACK IN THE NR 3R DOOR JAMB WEB, LOWER FORWARD CORNER. REPAIRED WEB (P/N AEA 0115-2) PER EA 11-105144.Aug 28, 1996 · N162US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9619211162Web · crackedDURING T-CHECK, FOUND THREE CRACKS IN DOOR 3L LOWER FORWARD SIDE WEB. REPAIRED WEB (P/N AEA 0115-1) PER EA 11-106311.Aug 28, 1996 · N162US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9618711162Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT FS 1781. REPAIRED LONGERON (P/N AGA7045) PER EA 11-106299.Aug 24, 1996 · N162US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9618701162Fitting · corrodedDURING T-CHECK, FOUND CORROSION ON THE LONGERON 51R END FITTING AT FS 1521 - 1531. REPLACED FITTING.Aug 23, 1996 · N162US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9617961146Position Ind · malfunctionedDURING TAKEOFF, THE GEAR RETRACTED BUT THE RED GEAR POSITIONS INDICATORS REMAINED ILLUMINATED. RECYCLED GEAR AND THE LIGHT WENT OUT. MAINTENANCE PERFORMED INSPECTIONS AND BITE TESTS, OPERATIONAL CHECK OK.Aug 15, 1996 · N146US · Doug DC1040 · Landing Gear Position and WarningSDR 9617951146Proximity Box · failedDURING TAKEOFF, ALL RED GEAR POSITION LIGHTS ILLUMINATED AND THE WARNING HORN SOUNDED WITH THE GEAR HANDLE UP. RECYCLED GEAR BUT LIGHT REMAINED ILLUMINATED UNITL PASSING 10,000 FEET. MAINTENANCE REPLACED THE MAIN LANDING GEAR PROXIMITY BOX.Aug 15, 1996 · N146US · Doug DC1040 · Landing Gear Position and WarningSDR 9617741160Indicator · failedDURING CLIMB, CABIN WOULD NOT PRESSURIZE. FLIGHT RETURNED TO SEA. MAINTENANCE REPLACED THE CABIN DIFFERENTIAL PRESSURE INDICATOR, OPERATIONAL CHECK OK.Aug 15, 1996 · N160US · Doug DC1040 · Cabin Pressure IndicatorSDR 9617921151Skin · corrodedDURING T-CHECK, FOUND CORROSION ON THE UNDER WING BARREL SKIN FROM FS 1509 TO 1531, LONGERONS 49L TO 49R AND ON THE BULKHEAD T-ANGLE. REPAIRED THE SKIN (P/N AYB7065-1) AND T-ANGLE (P/N AEA7079-1) PER EA 11-106295.Aug 14, 1996 · N151US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9617901151Skin · crackedDURING T-CHECK, FOUND A CRACK IN THE RIGHT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-501) PER EA 11-106298.Aug 13, 1996 · N151US · Doug DC1040 · Wing, Plate/SkinSDR 9618661151Seat Track · corrodedDURING T-CHECK, FOUND CORROSION ON THE RBL 75 SEAT TRACK AT FS 1841. REPAIRED TRACK (P/N S 4929147) PER EA 11-106212.Aug 9, 1996 · N151US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9618651151Doubler · corrodedDURING T-CHECK, FOUND CORROSION ON THE RADIO ALTIMETER MOUNTING PLATES, NR 1-2, TRANSMIT AND RECEIVE. REPAIRED PLATES (P/N AYB7022-1, AYB7053-1, AND AYB7053-501) PER EA 11-106221.Aug 9, 1996 · N151US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9617151158Engine · overtempDURING LANDING ROLLOUT, THE NR 1 ENGINE EGT WENT ABOVE RED LIMIT LINE FOR ABOUT THREE SECONDS. THE ENGINE WAS THEN SHUTDOWN WHILE STILL IN REVERSE AND A/C TAXIED TO GATE WITHOUT FURTHER INCIDENT. PERFORMED ENGINE OVER TEMPERATURE INSPECTION AND NO DISCREPANCAug 7, 1996 · N158US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9616011157Oil Press Transm · failedDURING TAKEOFF, THE NR 3 ENGINE OIL PRESSURE DROPPED TO 20 PSI. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 ENGINE OIL PRESSURE TRANSMITTER AND OIL PRESSURE INDICATOR. PERFORMED LEAK AND Jul 25, 1996 · N157US · Doug DC1040 · Engine Oil PressureSDR 9615471143Engine · stalledEN ROUTE LAX-HNL, THE NR 2 ENGINE EXPERIENCED TOP OF DESCENT STALL WHEN POWER WAS RETARDED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND FLIGHT CONTINUED TO HNL WITHOUT FURTHER INCIDENT. VISUAL INSPECTION OF THE NR 2 ENGINE REVEALED NO DISCREPANCIES. BORESJul 16, 1996 · N133JC · Doug DC1040 · Turbine Engine Compressor SectionSDR 9615461159Power Supply · inoperativeDURING LINE INSPECTION, FOUND THE ESCAPE EMERGENCY FLOOR LIGHT AT DOOR 3L AND 3R INTERMITTENT. REPLACED BATTERY POWER SUPPLY.Jul 16, 1996 · N159US · Doug DC1040 · Emergency LightingSDR 9615111162Transmitter · leakingDURING CLIMB, THE NR 2 HYDRAULIC SYSTEM SHOWED A SLOW LEAK. RETURNED TO HNL, DUMPED 38,000 LBS OF FUEL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 PRESSURE TRANSMITTER.Jul 13, 1996 · N162US · Doug DC1040 · Hydraulic Quantity SensorSDR 9615891158Skin · crackedDURING L-CHECK, FOUND A CRACK IN THE RIGHT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-502) PER EA 11-105354.Jul 11, 1996 · N158US · Doug DC1040 · Wing, Plate/SkinSDR 9615881158Skin · crackedDURING L-CHECK, FOUND A CRACK IN THE LEFT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-501) PER EA 11-105353.Jul 11, 1996 · N158US · Doug DC1040 · Wing, Plate/SkinSDR 9615001159Engine · malfunctionedDURING LANDING ROLLOUT, THE NR 3 ENGINE EXPERIENCED REVERSE STALL. WITH EGT INCREASING TO 1,000 DEGREES, CREW FOLLOWED COM PROCEDURE AND SHUT DOWN THE ENGINE WHILE STILL IN REVERSE. AIRCRAFT WAS TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. BORESCOPE INSPECTJul 9, 1996 · N159US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9615861141Skin · crackedDURING L-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE SKIN AT THE ANTI-ICE DUCT DOOR CUTOUT XOS 467. REPAIRED SKIN PER EA 11-105129.Jul 3, 1996 · N141US · Doug DC1040 · Wing, Plate/SkinSDR 9614511154Battery · dischargedDURING LINE INSPECTION, FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED FOUR BATTERIES.Jul 1, 1996 · N154US · Doug DC1040 · Emergency LightingSDR 9614331148Switch · brokenDURING CLIMB, PLACED THE GEAR HANDLE IN THE UP POSITION. THE 4 UNSAFE LIGHTS REMAINED ILLUMINATED. FOLLOWED COM 2.32.16 AND VERIFIED GEAR UP. MAINTENANCE REPLACED THE S1-342 SWITCH.Jun 30, 1996 · N148US · Doug DC1040 · Landing Gear Position and WarningSDR 9615301161Skin · crackedDURING LINE CHECK, FOUND A CRACK IN THE LEFT OUTBOARD AILERON UPPER SKIN AT THE NR 5 RIB. REPAIRED PER EA 11-105126.Jun 27, 1996 · N161US · Doug DC1040 · AileronsSDR 9614181150Unlock Light · illuminatedEN ROUTE DTW-MSP, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE, AND CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED VIBRATION AND WINDMILLING CHECKS. REVERSER WAS ALSO CHECKED FOR STOW Jun 26, 1996 · N150US · Doug DC1040 · Engine Thrust ReverserSDR 9614121159Power Supply · inoperativeDURING LINE CHECK, FOUND THE FORWARD 'B' ZONE AND AFT ZONE EMERGENCY FLOOR LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND POWER SUPPLY.Jun 24, 1996 · N159US · Doug DC1040 · Emergency LightingSDR 9613741160Dnlock Switch · failedDURING CLIMB, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON WITH THE GEAR HANDLE UP. RECYCLED GEAR AND VERIFIED LEFT MAIN GEAR DOOR WAS UP AND LOCKED. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DOWNLOCK PROXIMITY SWITCH.Jun 24, 1996 · N160US · Doug DC1040 · Landing Gear Position and WarningSDR 9613851144Power Supply · inoperativeDURING LINE INSPECTION, FOUND THE OVERWING EMERGENCY LIGHT POWER SUPPLY FAULTED. MAINTENANCE REPLACED THE OVERWING EMERGENCY POWER SUPPLY AND BATTERY.Jun 20, 1996 · N144JC · Doug DC1040 · Emergency LightingSDR 9613631152Oil Fill Line · looseTHE NR 1 ENGINE OIL QUANTITY BEGAN TO DECREASE AND AT FIVE GALLONS, THE ENGINE WAS SHUT DOWN. CREW FOLLOWED COM PROCEDURE AND RETURNED TO HNL. ALSO, ON TAXIING TO GATE, APU FIRE WARNING LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND FIRED BOTTLE. INSPEJun 18, 1996 · N152US · Doug DC1040 · Turbine Engine Oil SystemSDR 9613321141Cables · wornDURING TAKEOFF, DOOR 1L ANNUNCIATOR LIGHT ILLUMINATED, ABORTED TAKEOFF. MAINTENANCE REPLACED BOTH TRANSLATOR CABLES.Jun 15, 1996 · N141US · Doug DC1040 · Door Warning SystemSDR 9613101146Apu · firePRIOR TO PUSHBACK, APU TAILPIPE FIRE DEVELOPED. AIRCRAFT APU FIRE BOTTLES WERE DISCHARGED AND FLAMES EXTINGUISHED. THE PASSENGERS WERE DEPLANED THROUGHT THE JETWAY WITHOUT INCIDENT. NO SMOKE WAS PRESENT IN CABIN. MAINTENANCE INSPECTED APU AND SURROUNDING SJun 15, 1996 · N146US · Doug DC1040 · Airborne Auxiliary Power Unit (APU) SystemSDR 9613111141Compressor · stalledAT TOP OF DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED WHEN THROTTLE WAS RETARDED. AT THE TIME OF STALL, TEMPERATURE REACHED 750 DEGREES CELSIUS. FLIGHT CONTINUED TO LGW WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED INSPECTION PER 71-00-00 AND NO DAMAGE WAJun 14, 1996 · N141US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9613581144Bulkhead · corrodedDURING T-CHECK, FOUND CORROSION ON THE PRESSURE BULKHEAD CAP FS 1369 IN THE CENTER MAIN LANDING GEAR WHEEL WELL. REPAIRED CAP (P/N AYB 7080-5) PER EA 11-105427.Jun 11, 1996 · N144JC · Doug DC1040 · Fuselage Main, BulkheadSDR 9613571144Frame · corrosionDURING T-CHECK, FOUND CORROSION ON THE FS 1360 FRAME FROM LONGERON 51L TO 51R. REPAIRED FRAME (P/N AYB 7031-3) PER EA 11-105407.Jun 9, 1996 · N144JC · Doug DC1040 · Fuselage Main, FrameSDR 9613561144Frame · crackedDURING T-CHECK, FOUND A 4.625 INCH CRACK IN THE FS 1561 FRAME SPLICE AT LONGERON 44L. REPAIRED SPLICE (P/N AEA 7296-11) PER EA 11-102166.Jun 6, 1996 · N144JC · Doug DC1040 · Fuselage Main, FrameSDR 9613551144Frame · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 43R AT FS 1561. REPAIRED LONGERON (P/N AFA 7070-1) PER EA 11-105418.Jun 6, 1996 · N144JC · Doug DC1040 · Fuselage Main, FrameSDR 9613541144Skin · crackedDURING T-CHECK, FOUND CRACKS IN BOTH THE LEFT AND RIGHT WING LEADING EDGE SKIN XOS 290 AND 330. REPAIRED SKIN (P/N ARB 2984-501, -502) PER EA 11-105409.Jun 6, 1996 · N144JC · Doug DC1040 · Wing, Plate/SkinSDR 9613971144Frame · corrodedDURING T-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB FRAME AT THE LOWER FORWARD CORNER FS 895, LONGERON 41R. REPAIRED FRAME (P/N ADA 0233) PER EA 11-105379.Jun 4, 1996 · N144JC · Doug DC1040 · Fuselage Main, FrameSDR 9613521144Skin · crackedDURING T-CHECK, FOUND A .9 INCH CRACK IN THE RIGHT WING LEADING EDGE SKIN AT XOS 603. REPAIRED SKIN (P/N ARB 2887-502) PER EA 11-105398.Jun 4, 1996 · N144JC · Doug DC1040 · Wing, Plate/SkinSDR 9613511144Bulkhead · corrodedDURING T-CHECK, FOUND CORROSION ON THE CENTER ACCESSORY PRESSURE BULKHEAD WEB AT FS 1156, LBL 9. REPAIRED WEB (P/N NPB 6280-3) PER EA 11-105414.Jun 4, 1996 · N144JC · Doug DC1040 · Fuselage Main, BulkheadSDR 9613501144Frame · crackedDURING T-CHECK, FOUND A 3.625 INCH CRACK IN THE FS 1841 FRAME BETWEEN LONGERON 12L TO 13L EXTENDING COMPLETELY THROUGH THE INBOARD FLANGE AND 2.25 INCH INTO THE FRAME WEB. REPAIRED FRAME (P/N AGA 3783-501) PER EA 11-105412.Jun 4, 1996 · N144JC · Doug DC1040 · Fuselage Main, FrameSDR 9612861144Fitting · corrodedDURING T-CHECK, FOUND CORROSION ON THE SPLICE FITTING JUST INBOARD OF THE LOWER FORWARD CORNER OF THE FORWARD CARGO DOOR JAMB. REPLACED FITTING (P/N ADA 7109-501).Jun 4, 1996 · N144JC · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9612581144Fitting · crackedDURING T-CHECK, FOUND A CRACK IN THE LEFT WHEEL WELL GEAR SUPPORT FITTING AT THE REAR SPAR XORS 240. REPLACED FITTING (P/N ARB198-501).Jun 1, 1996 · N144JC · Doug DC1040 · Wing, Landing Gear Attach FittingsSDR 9611881159Throttle Switch · broken armDURING CLIMB, PLACED THE GEAR HANDLE IN THE UP POSITION, THE WARNING HORN SOUNDED AND ALL FOUR GEAR LIGHTS STAYED RED. GEAR WAS RECYCLED AND VISUALLY CHECKED IN THE UP POSITION WITH THE RED GEAR UNSAFE LIGHT STILL ILLUMINATED. FLIGHT CONTINUED TO MSP AND LANDMay 30, 1996 · N159US · Doug DC1040 · Landing Gear Position and Warning
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