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 9702491146Tt2 Sensor · failedDURING TAKEOFF, THE NR 1 ENGINE FAILED TO ACCELERATE. TAKEOFF WAS ABORTED AT 70 KNOTS. MAINTENANCE REPLACED THE TT2 SENSOR AND RETURNED TO SERVICE.Feb 7, 1997 · N146US · Doug DC1040 · Engine BMEP/Torque IndicatingSDR 9702071143Prox Control · failedDURING TAKEOFF, THE GEAR WARNING HORN SOUNDED WITH THE STRUT EXTENSION, THE 4 RED GEAR UNSAFE LIGHTS ILLUMINATED. RECYCLED GEAR AND LIGHTS REMAINED ILLUMINATED. FLIGHT RETURNED TO MSP. MAINTENANCE REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL.Feb 2, 1997 · N133JC · Doug DC1040 · Landing Gear Position and WarningSDR 9702381154Engine · malfunctionedDURING LANDING ROLLOUT IN REVERSE THRUST, THE NR 3 ENGINE EGT BEGAN TO CLIMB. THE NR 3 ENGINE WAS SHUT DOWN AT 915 CELSIUS. MAINTENANCE PERFORMED VISUAL INSPECTION OF ENGINE, NO DISCREPANCIES NOTED. IN ACCORDANCE WITH MM 72-00-00, PG 227, NO ACTION IS REQUIFeb 1, 1997 · N154US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9701501158Pressure Switch · failedDURING TAKEOFF, THE NR 3 MANIFOLD FAIL LIGHT ILLUMINATED. DUMPED 76,500 LBS OF FUEL AND RETURNED TO IAD. REPLACED THE MANIFOLD PRESSURE SWITCH.Jan 27, 1997 · N158US · Doug DC1040 · Pneumatic Indicating SystemSDR 9701241155Compressor · stalledDURING TOP OF DESCENT FROM 33,000 FEET, NR 2 ENGINE STALLED. FLIGHT CREW NOTICED EGT RISE AND ELECTED TO SHUTDOWN NR 2 ENGINE. A SUCCESSFUL RELIGHT WAS ACCOMPLISHED BUT THE ENGINE WAS SHUTDOWN AGAIN DUE TO HIGH EGT. AN UNEVENTFUL LANDING WAS PERFORMED AT DEJan 22, 1997 · N155US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9700861141Epr Indicator · malfunctionedDURING TAKEOFF ROLL, THE NR 3 ENGINE EPR WAS LOW. TAKEOFF WAS ABORTED AT 50 KNOTS. MAINTENANCE FOUND EPR INDICATOR FAULTY. REPLACED THE EPR INDICATOR.Jan 19, 1997 · N141US · Doug DC1040 · Engine Pressure Ratio (EPR)SDR 9700961141Battery · dischargedDURING INSPECTION, FOUND THE MID CABIN EMERGENCY FLOOR LIGHT ON THE LEFT SIDE INOPERATIVE. REPLACED MID CABIN EMERGENCY BATTERY.Jan 16, 1997 · N141US · Doug DC1040 · Emergency LightingSDR 9700461156Switch · failedDURING TAKEOFF, FOUR UNSAFE GEAR UP INDICATION ILLUMINATED. RECYCLED GEAR AND RECEIVED THE SAME INDICATION. FLIGHT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 2 ENGINE THROTTLE SWITCH S1-341.Jan 11, 1997 · N156US · Doug DC1040 · Landing Gear Position and WarningSDR 9700581155Turbine · damagedDURING DESCENT, THE NR 2 ENGINE EXPERIENCED A STALL AND POWER LOSS. PILOT ELECTED TO SHUT DOWN AND THEN RESTART NR 2 ENGINE. AN UNEVENTFUL LANDING FOLLOWED. MAINTENANCE BORESCOPE INSPECTION REVEALED TURBINE SECTION DAMAGE. REPLACED NR 2 ENGINE.Jan 10, 1997 · N155US · Doug DC1040 · Turbine SectionSDR 9700541147Frame · crackedDURING L-CHECK, A CRACK WAS FOUND ON THE LOWER NOSE FUSELAGE FRAME AT FS 459 X=61. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLES PER EA 11-120645, (P/N ABA7348-3).Jan 6, 1997 · N147US · Doug DC1040 · Fuselage Main, FrameSDR 9700551147Skin · crackedDURING L-CHECK, A CRACK WAS FOUND IN THE WING FIXED LEADING EDGE AT THE NR 12 SLAT TRACK AT STA XOS 774. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLERS PER EA 11-120642.Jan 2, 1997 · N147US · Doug DC1040 · Wing, Plate/SkinSDR 9627701147Skin · crackedDURING LINE CHECK, A CRACK WAS FOUND ON THE LEFT WING FIXED LEADING EDGE SKIN AT XOS=610. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLERS PER EA 11-120641 (P/N ARB2887-501).Dec 31, 1996 · N147US · Doug DC1040 · Wing, Plate/SkinSDR 9627401162Epr Indicator · malfunctionedDURING TAKEOFF, THE NR 3 ENGINE EPR INDICATION WAS LOW. TAKEOFF WAS ABORTED. MAINTENANCE REPLACED THE EPR INDICATOR. ENGINE GROUND RUN CHECKED GOOD.Dec 30, 1996 · N162US · Doug DC1040 · Engine Pressure Ratio (EPR)SDR 9627201153Reverser System · malfunctionedDURING TAKEOFF ROLL, ENGINE NR 2 AMBER REVERSE UNLOCK LIGHT ANNUNCIATED. TAKEOFF ABORTED AT 120 KNOTS. MAINTENANCE PERFORMED REJECTED TAKEOFF INSPECTION, NO DAMAGE FOUND. REVERSER ON MEL.Dec 28, 1996 · N153US · Doug DC1040 · Engine Thrust ReverserSDR 9627631153Skin · corrodedDURING TRANSITION CHECK, CORROSION WAS FOUND ON THE UNDERWING BARREL SKIN AT FS 1509 TO 1531, LBL 49 TO RBL 49. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLERS PER EA 11-120126 (P/N AYB7065-1).Dec 23, 1996 · N153US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9627621153Skin · delaminatedDURING PERIODIC CHECK, DELAMINATION OF THE VERTICAL STABILIZER SKIN AT STR 375 TO 405 RIGHT SIDE. REPAIRED PER EA 11-120122 (P/N ANC7047-2).Dec 23, 1996 · N153US · Doug DC1040 · Vertical Stabilizer, Plate/SkinSDR 9627641153Support · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE LEFT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. REMOVED AND REPLACED PIVOT SUPPORT PER EA 11-120135 (P/N AJC7230-1).Dec 20, 1996 · N153US · Doug DC1040 · Horizontal Stabilizer StructureSDR 9627551153Doubler · gougedDURING PERIODIC CHECK, GOUGES WERE FOUND ON THE FORWARD CARGO LOWER JAMB SKIN DOUBLER AT FS 911.97. BLENDED OUT GOUGES AND INSTALLED REPAIR DOUBLER PER EA 11-120623.Dec 19, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9627561153Angle · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FORWARD CARGO JAMB ANGLE AT FS 1002, LONGERON 43R. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER EA 11-120622 (P/N ADA0233-7).Dec 18, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9626741150Transmitter · intermittentDURING POWER APPLICATION FOR TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED. TAXIED OFF THE RUNWAY AND RETURNED TO GATE. MAINTENANCE FOUND THE FLAP TRANSMITTER INTERMITTENT, AND REPLACED.Dec 18, 1996 · N150US · Doug DC1040 · Trailing Flap Position Indicating SystemSDR 9627611153Longeron · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FUSELAGE OVERWING EXTERNAL LONGERONS AT FS 1404 TO 1515. BLENDED OUT CORROSION AND INSTALLED DOUBLERS PER EA 11-120121.Dec 16, 1996 · N153US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9627571153Doorframe · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE CENTER CARGO DOOR JAMB FRAME AT FS 1787, LONGERON 43R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS AND SHIMS PER EA 11-120612(PN AFA3876-3).Dec 16, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9627581153Mounting Rings · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON THE RADIO ALTIMETER ANTENNA MOUNTING RINGS. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER EA 11-120609 (P/N AYB7053-1).Dec 12, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9627601153Support · crackedDURING PERIODIC CHECK, THE FLOOR PANEL ATTACH TAB WAS FOUND CRACKED AT FS 475, LBL 36 FLOOR SUPPORT RAIL. REMOVED DAMAGED AREA AND INSTALLED REPAIR CHANNEL AND FILLERS PER EA 11-105163 (P/N NCA6042-33).Dec 4, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9625751147Pt 7 Line · brokenDURING TAKEOFF ROLLOUT, THE NR 3 ENGINE EXHIBITED LOWER POWER. THE TAKEOFF WAS ABORTED AND A/C RETURNED TO GATE. MAINTENANCE FOUND A BROKEN PT7 LINE BETWEEN 6 AND 8 O'CLOCK POSITION. REPAIR WAS DEFERRED PER MEL 77-3.Dec 2, 1996 · N147US · Doug DC1040 · Engine Pressure Ratio (EPR)SDR 9627681155Frame · crackedDURING L-CHECK, A CRACK WAS FOUND ON THE LOWER NOSE FUSELAGE FRAME AT STA 459 AND X=61. REPAIRED PER EA 11-12013, (P/N ABA7348-3).Nov 27, 1996 · N155US · Doug DC1040 · Fuselage Main, FrameSDR 9624641154N 1 Transmitter · failedDURING TAKEOFF ROLLOUT, THE NR 3 ENGINE N1 WOULD NOT REACH TAKEOFF POWER WITH ENGINE FAIL LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 N1 TRANSMITTER.Nov 15, 1996 · N154US · Doug DC1040 · Engine RPM Indicating SystemSDR 9624451146Compressor · stalledDURING POWER REDUCTION AT FL210, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL. AS EGT CLIMBED TO 750 DEGREES, THE ENGINE WAS SHUT DOWN AND RESTARTED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND CONTINUED FLIGHT TO PHL WITHOUT FURTHER INCIDENT. VISUAL ANNov 14, 1996 · N146US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9624011158Compressor · stalledAT FL310 WHEN POWER WAS REDUCTED FOR DESCENT, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THERE WAS A SUBSEQUENT VIBRATION UNTIL THE ENGINE WAS SHUT DOWN. NO ABNORMAL EGT OR FUEL FLOW INDICATION AT THE TIME OF INCIDENT. FLIGHT CONTINUED TO DTW WITHOUT FNov 10, 1996 · N158US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9623541161Fitting · corrodedDURING L-CHECK, FOUND THE LONGERON 48L, 49L, AND 48R END FITTINGS CORRODED FROM FS 1509 - 1521. REPLACED BOTH FITTINGS.Oct 28, 1996 · N161US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9623061151Compressor · stalledDURING LANDING ROLLOUT, THE NR 1 ENGINE EXPERIENCED REVERSE STALL. THE ENGINE WAS SHUT DOWN AS EGT ROSE OVER 950 DEGREES WITHIN THIRTY SECONDS. MAINTENANCE PERFORMED BORESCOPE INSPECTION AND NO DISCREPANCIES WERE FOUND. CHECKED REVERSER ACTUATED BLEED SYSTEOct 28, 1996 · N151US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9623521161Skin · crackedDURING L-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT THE LEFT AIR CYCLE MACHINE DOOR JAMB UPPER AFT CORNER, FS 587. REPAIRED SKIN (P/N ACA 3108) PER EA 11-110287.Oct 27, 1996 · N161US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9623501161Skin · crackedDURING L-CHECK, FOUND A 1.6258 INCH CRACK IN THE RIGHT WING LOWER LEADING EDGE SKIN AT XOS 611. REPAIRED SKIN (P/N ARB2887-502) PER EA 11-110210.Oct 25, 1996 · N161US · Doug DC1040 · Wing, Plate/SkinSDR 9621781150Compressor Blade · damagedDURING CRUISE AT FL350, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND RECOVERED. EPR INCREASED AND N1 FLUCTUATED. CREW FOLLOWED COM PROCEDURES AND CONTINUED FLIGHT TO SEA WITHOUT FURTHER INCIDENT. BORESCOPE INSPECTION REVEALED DAMAGE TO THE 8TH STAGE HOct 12, 1996 · N150US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9621731146Tr Light · illuminatedDURING TAKEOFF ROLLOUT, THE NR 3 THRUST REVERSER LIGHT ILLUMINATED AT 60 KNOTS. CREW ABORTED TAKEOFF AND WHILE TAXING, REALIZED THAT THE REVERSER WAS ON MEL FROM A PREVOUS INCIDENT. FLIGHT DEPARTED AND TO BOS WITHOUT FURTHER INCIDENT.Oct 10, 1996 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9621741146Rev Unlock Light · illuminatedDURING TAKEOFF ROLLOUT, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED THE REVERSER AND DEFERRED REPAIR PER MEL 78-1A.Oct 8, 1996 · N146US · Doug DC1040 · Engine Thrust ReverserSDR 9621511161Compressor · stalledDURING APPLICATION OF POWER FOR TAKEOFF, THE NR 3 ENGINE EXPERIENCED COMPRESSOR STALL. CREW ABORTED THE TAKEOFF AS EGT CLIMBED TO 990 DEGREES WITHIN ONE SECOND. AIRCRAFT RETURNED TO THE GATE AND VISUAL INSPECTION REVEALED NO DISCREPANCIES. BORESCOPE INSPECTOct 8, 1996 · N161US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9620671152Fitting · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT THE CENTER WHEEL WELL AFT SHELF FS 1509 TO 1521. REPLACED FITTING (P/N AYB 7063-501) PER SRM 51-00-00.Sep 24, 1996 · N152US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9620341143Evc · malfunctionedEN ROUTE, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL DURING DESCENT. THE ENGINE WAS SHUT DOWN AND RESTARTED. CREW FOLLOWED COM PROCEDURES AND CONTINUED FLIGHT TO MSP WITHOUT FURTHER INCIDENT. ENGINE BORESCOPE WAS ACCOMPLISHED AND NO DISCREPANCIES WERE FSep 22, 1996 · N133JC · Doug DC1040 · Compressor Bleed ControlSDR 9620461152Fitting · corrodedDURING T-CHECK, FOUND CORROSION ON THE LONGERON 48R ATTACH FITTING AT FS 1509 TO 1521. REPLACED FITTING (P/N AYB 7061-1).Sep 21, 1996 · N152US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9620641152Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON THE OVERWING EXTERNAL LONGERONS 29R AND 30R FROM FS 1432 TO 1501. REPAIRED LONGERONS PER EA 11-110221.Sep 20, 1996 · N152US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9621191152Floor Beam · crackedDURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR BEAM AT FS 1099, LBL 58. REPAIRED BEAM (P/N ADA 0039-5) PER EA 11-110248.Sep 19, 1996 · N152US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9621171152Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 46R FROM FS 1754 - 1812. REPAIRED LONGERON (P/N AFA 7098-1) PER EA 11-110220.Sep 18, 1996 · N152US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9621161152Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 48R FROM FS 1964 - 1970. REPAIRED LONGERON (P/N AGA 7047-501) PER EA 11-110251.Sep 17, 1996 · N152US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9620621152Seat Track · corrodedDURING T-CHECK, FOUND CORROSION ON THE RBL 65 SEAT TRACK AT FS 1841. REPAIRED TRACK (P/N NFA 6222-39) PER EA 11-110225.Sep 17, 1996 · N152US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9619841152Fitting · corrodedDURING T-CHECK, FOUND CORROSION ON THE LONGERON 52 END FITTING AT FS 1521. REPLACED FITTING PER SRM 53-00-01.Sep 15, 1996 · N152US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9619931145Sensor · failedDURING LANDING ROLLOUT, THE NR 1 AND NR 3 ENGINES EXPERIENCED REVERSE STALL SIMULTANEOUSLY. BOTH ENGINES WERE SHUT DOWN DUE TO INCREASING EGT AND AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BORESCOPE INSPECTION OF THE NR 3 ENGINE Sep 14, 1996 · N145US · Doug DC1040 · Fuel Controlling SystemSDR 9620611152Door Jamb · crackedDURING T-CHECK, FOUND TWO CRACKS IN THE NR 3R DOOR JAMB FORWARD WEB FS 1250 TO 1256 AT THE FLOOR LEVEL. REPAIRED WEB (P/N AEA 0155-2) PER EA 11-110246.Sep 12, 1996 · N152US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9619781153Fire Wire · chafedDURING INITIAL CLIMB, THE NR 3 ENGINE B-LOOP LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND CONTINUED FLIGHT AS SCHEDULED. ON FINAL APPROACH, THE NR 3 ENGINE FIRE WARNING INDICATION ILLUMINATED AGAIN. CREW SHUT THE ENGINE DOWN AND MADE A TWO ENGINE LANDSep 12, 1996 · N153US · Doug DC1040 · Fire DetectionSDR 9619821152Skin · corrodedDURING T-CHECK, FOUND CORROSION AND A SHEARED BOLT IN THE 4L DOOR CUTOUT SPLICE FS 1851 AT LONGERON 15L. REPLACED BOLT PER SRM 51-31-01.Sep 11, 1996 · N152US · Doug DC1040 · Fuselage Main, Plate/Skin
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