Douglas DC-10-40
Service difficulty reports · 614
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 9602151154Handle · lack of lubeDURING GEAR EXTENSION, THE GEAR HANDLE BUTTON STUCK IN PLACE IN DOWN POSITION WITH AN UNSAFE GEAR INDICATION. RECYCLED GEAR AND MANUALLY PUSHED HANDLE IN AND GOT NORMAL GEAR INDICATIONS. LUBED GEAR HANDLE RELEASE BUTTON AND GEAR HANDLE PIVOTS.SDR 9602391150Fitting · corrodedDURING L-CHECK, FOUND CORROSION ON THE LONGITUDINAL FITTING AT FS 1513 TO 1517, LBL 29 IN THE CENTER LANDING GEAR WHEEL WELL AFT SHELF. REPLACED FITTING PER SRM 51-00-00 PG 2.SDR 9602271141Compressor · stalledDURING LANDING ROLL-OUT (CDG), THE NR 3 ENGINE EXPERIENCED A SLIGHT REVERSE STALL. CREW FOLLOWED COCKPIT OPERATING PROCEDURE BY SHUTTING THE ENGINE DOWN AND PROCEEDED WITH LANDING WITHOUT FURTHER INCIDENT. REPLACED THE NR 3 ENGINE AND CHECK WAS NORMAL.SDR 9601751162Gear Box · leakingAFTER TAKEOFF, THE NR 2 ENGINE OIL DECREASED RAPIDLY. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND RETURNED TO MSP. REPLACED STARTER DRIVE SEAL, BOTH HYDRAULIC PUMP DRIVE SEALS, GEAR BOX, AND BREATHER VALVE. PERFORMED LEAK CHECK. ENGINE RUN-UP WAS NORMAL.SDR 9601461148Solenoid · failedDURING LANDING, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL. EGT INCREASED TO TOP OF SCALE. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, SHUT NR 1 ENGINE DOWN AND MOTORED UNTIL EGT IS BELOW 100C. BORESCOPED NR 1 ENGINE AND INSPECTED PER MM 71-00-00. REPLACESDR 9601141161Controller · failedDURING CRUISE, THE TANK OVER FILLED LIGHT ILLUMINATED AND FUEL WAS STREAMING FROM THE LEFT DUMP NOZZLE. DUMPED 92,500 LBS OF FUEL AND RETURNED TO DTW. REPLACED FUEL CONTROLLER.SDR 9601661157Longeron · corrodedDURING L-CHECK, FOUND CORROSION ON THE RBL 7 LONGERON FITTING FROM FS 1509 TO 1521 IN THE CENTER GEAR WHEEL WELL. REPLACED THE FITTING PER SRM 51-00-00 FIG 2.SDR 9600891160Compressor · stalledDURING LANDING WITH REVERSER DEPLOYED, THE NR 1 ENGINE EXPERIENCED A REVERSE STALL. EGT WENT TO 950 DEGREES AND THE ENGINE WAS SHUTDOWN. PERFORMED INSPECTION ON THE INLET AND EXHAUST, INSPECTION WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR 9600771154Fitting · crackedDURING T-CHECK, FOUND A CRACK IN THE NR 4 BANJO FITTING, FORWARD RIGHT FLANGE IN THE RADIUS. REPAIRED PER SRM 55-20-00, SHEETS 1-17.SDR 9600721154Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERONS 29R TO 31R BETWEEN FS 1401 TO 1521. REPAIRED LONGERONS PER EA 11-104451.SDR 9600711154Skin · corrodedDURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1661 TO 1681, LONGERONS 51L AND 51R BENEATH THE ANTI-COLLISION BEACON. REPAIRED SKIN (P/N NFA 6214) PER EA 11-99375.SDR 9600651154Bulkhead · crackedDURING T-CHECK, FOUND VERTICAL CRACKS IN A FS 1787 BULKHEAD STANCHION AT LBL 9, 10 INCHES ABOVE THE CARGO FLOOR LINE. REPAIRED STANCHION PER EA 11-104463.SDR 9600371154Splice Fitting · corrodedDURING T-CHECK, FOUND CORROSION ON THE STR 52 SPLICE FITTING AT FS 1718. FABRICATED AND INSTALLED PER AFA 7102-1 AND SRM 53-10-00.SDR 9600621154Seat Track · corrodedDURING T-CHECK, FOUND CORROSION IN THE MAIN CABIN SEAT TRACK FS 1878 TO 1908 AT LBL 100. REPAIRED TRACK (P/N AFA 7789-503) PER EA 11-104452.SDR 9600611154Web · corrodedDURING T-CHECK, FOUND CORROSION IN THE FLOOR WEB AND DOUBLER AT FS 1908 TO 1921 LBL 88. REPAIRED WEB (P/N AGA 3807-5) PER EA 11-104450.SDR 9600451158Power Supply · failedDURING LINE CHECK, FOUND THE AFT EMERGENCY LIGHT POWER SUPPLY FAILED BITE TEST. REPLACED THE AFT POWER SUPPLY AND BATTERY PACK.SDR 9522231154Doubler · corrodedDURING T-CHECK, FOUND CORROSION ON THE NR 1 RADIO ALTIMETER DOUBLERS AT FS 1177. REPAIRED THE DOUBLERS PER EA 11-104443.SDR 9522221154Beam · crackedDURING T-CHECK, FOUND A CRACK IN THE FS 761 FLOORBEAM AT LBL 8, SEAT TRACK ATTACH HOLE. REPAIRED BEAM (P/N ADA 7226-505) PER EA 11-99295.SDR 9521751154Fitting · crackedDURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR LIFT ACTUATOR FITTING, FORWARD LOWER LUG. REPLACED FITTING.SDR 9522201154Door Jamb · corrodedDURING T-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB LOWER OUTBOARD SILL BEAM BELOW LONGERON 43R FROM FS 1035 TO 1039. REPAIRED THE BEAM (P/N ADA 0250-1) PER EA 11-104446.SDR 9521201150Coalescer Bags · contaminatedAFTER TAKEOFF, CABIN BEGAN TO FILL WITH SMOKE, PILOT BEGAN DUMPING FUEL AND RETURNED TO DEPARTURE AIRPORT. AIRCRAFT LANDED, TAXIED TO GATE AND DEPLANED PASSENGERS THROUGH JETWAY WITHOUT FURTHER INCIDENT. MAINTENANCE INSTALLED NEW COALESCER BAGS AND RAN AIRCRSDR 9521331150Apu · failedPRIOR TO DEPARTURE, A LARGE CLOUD OF SMOKE DISCHARGED OUT OF APU EXHAUST DUCT. NO UNUSUAL COCKPIT INDICATIONS. APU WAS SHUTDOWN, AT WHICH TIME THE CABIN BEGAN TO FILL WITH SMOKE. PASSENGERS DEPLANED THROUGH MAIN CABIN DOOR WITHOUT INCIDENT. APU PLACED ON MSDR 9520631158Pneu Manifold · failedDURING CLIMB, THE NR 2 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED INTERMITTENTLY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ITEM ENTERED IN MINIMUM EQUIPMENT LIST AND AIRCRAFT APPROVED FOR SERVICE.SDR 9520251156Compressor · stalledDURING LANDING WHILE IN REVERSE THRUST, THE NR 1 AND NR 3 ENGINES COMPRESSOR STALLED WITH THE EGTS GOING TO 980 DEGREES FOR 5 SECONDS BEFORE THE ENGINES WERE SHUTDOWN. THE ENGNE WAS INSPECTED, BORESCOPED AND A GROUND RUNUP CONFIRMED PROPER OPERATION OF THE ENSDR 9519771150Oil Filter · dirtyDURING APPLICATION OF TAKEOFF POWER, THE NR 1 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED AND THE TAKEOFF WAS ABORTED. THE OIL FILTER AND PRESSURE SWITCH WERE REPLACED. THE SYSTEM CHECKED OK DURING A GROUND RUN-UP.SDR 9519761158Pt2 Probe · crackedDURING START OF DESCENT, THE NR 2 ENGINE EGT WENT TO 1010 DEGREES FOR 90 SECONDS. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT CONTINUED TO AN UNEVENTFUL TWO-ENGINE LANDING AT MSP. THE PRBC AND EVC WERE REPLACED AND A PT2 PROBE WAS FOUND CRACKED AND REPLACED. SDR 9519011146Compressor · stalledDURING CRUISE, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL WITH THE EGT GOING TO MAX FOR 30 SECONDS. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO BOS WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS ACCOMPLISHED. NO FUEL WAS DUMPED. THE AIRCRAFT WAS FESDR 9518341145Eel Power Supply · failedDURING LINE CHECK, MID CABIN EMERGENCY FLOOR LIGHTS FAILED TEST. REPLACED THE POWER SUPPLY AND BATTERY.SDR 9518271149Tr Unit · malfunctionedTHE NR 3 ENGINE REVERSER LIGHT ILLUMINATED AT 80 KNOTS AND THE TAKEOFF WAS ABORTED. THE REVERSER WAS LOCKED OUT AND PLACED ON MEL.SDR 9517961159Fuel Control · failedDURING TAXI OUT, THE NR 2 ENGINE EGT WENT TO 1,000 DEGREES FOR 30 SECONDS AND THE ENGINE WAS SHUTDOWN. THE ENGINE WAS INSPECTED AND THE EPR INDICATOR WAS REPLACED. DURING THE SECOND TAXI OUT THE FUEL FLOW PEGGED AND THE EGT AGAIN ROSE. THE FUEL CONTROL AND SDR 9517531160Link · failedDURING CLIMB, THE AIRCRAFT EXPERIENCED EXCESSIVE VIBRATION. AIRCRAFT DUMPED 120,000 LBS OF FUEL AND RETURNED TO DTW. REPLACED LEFT FORWARD CENTER GEAR DOOR DRIVE LINK AND OPERATIONAL CHECK OK.SDR 9516921161Slat Sensor · malfunctionedDURING TAKEOFF, THE SLAT DISAGREE LIGHT AND THE TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO GATE. ADJUSTED SLAT SENSORS AND REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL BOX.SDR 9516881159Longeron · crackedDURING T-CHECK, FOUND A THREE INCH CRACK IN LONGERON 45L AT FS 2160. REPAIRED LONGERON (P/N AJC 7208-1) PER EA 11-103208.SDR 9516861159Door Jamb · corrodedDURING T-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB INNER BEAM FS 882 AT LONGERON 43L. REPAIRED BEAM (P/N ADA 0251-1) PER EA 11-99322.SDR 9516851159Frame · corrodedDURING T-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB FRAMES AT LONGERON 41R, FS 895 AND 1002. REPAIRED FRAMES (P/N ADA 0233-3, -4) PER EA 11-99323.SDR 9516831159Mounting Plates · corrodedDURING T-CHECK, FOUND CORROSION ON BOTH FORWARD RADIO ALTIMETER MOUNTING PLATES. REPAIRED RINGS (P/N AYB 7022, 7053) PER EA 11-103171.SDR 9516821159Frame · crackedDURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME AT FS 879, LBL 33. REPAIRED FRAME (P/N ADA 7034) PER EA 11-99361.SDR 9516801159Web · corrodedDURING T-CHECK, FOUND CORROSION IN THE LEFT OUTBOARD FLOOR WEB AND DOUBLER AT FS 1900 - 1928, LBL 90.SDR 9516791159Floor Beam · crackedDURING T-CHECK, FOUND 0.5 INCH CRACKS IN THE FS 791 FLOOR BEAM UPPER CAP, LBL 20 - RBL 20. REPAIRED CAP (P/N ADA 7226-13) PER EA 11-99329.SDR 9515661160Tee · crackedDURING CRUISE, UNABLE TO TRANSFER FUEL FROM THE AUXILIARY TANK, DUMPED 35,000 LBS OF FUEL AND RETURNED TO BOS. REPLACED THE CENTER TANK FILL LINE TEE ASSEMBLY.SDR 9515231148De-Oiler Shaft · failedDURING CRUISE, THE NR 3 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED, OIL QUANTITY WENT TO ZERO AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT DIVERTED TO BOS WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS ACCOMPLISHED, NO FUEL WAS DUMPED. THE DE-OILER SHAFT WAS FOUND SSDR 9514971153Pneu Ind Loop · failedDURING CRUISE, THE NR 2 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED. FLIGHT RETURNED TO HNL. FOUND THE NR 2 LOOP BAD, DEFERRED PER MEL 36-10A.SDR 9515871147Angle · crackedDURING T-CHECK, FOUND A 4.3 CRACK IN THE RIGHT WING FRONT SPAR TO FUSELAGE ATTACH ANGLE FS 1159 AT LONGERON 28R. REPAIRED ANGLE (P/N ANB 7353-1), PER EA 11-99276.SDR 9515861147Skin · corrodedDURING T-CHECK, FOUND CORROSION IN THE FUSELAGE SKIN FS 1661 TO 1681, LONGERONS 51L TO 51R BENEATH THE ANTI-COLLISION LIGHT. REPAIRED SKIN (P/N NFA 6214-1), PER EA 11-99325.SDR 9515831147Frame · crackedDURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME FS 879 AT RBL 38. REPAIRED FRAME (P/N ADA 7034), PER EA 11-99259.SDR 9515771147Frame · crackedDURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME FS 879 AT LBL 33. REPAIRED FRAME (P/N ADA 7034), PER EA 11-99255.SDR 9515761147Blkhd Skin · corrodedDURING T-CHECK, FOUND CORROSION ON THE CENTER WING FRONT SPAR PRESSURE BULKHEAD FS 1156 AT THE SKIN BETWEEN LONGERONS 47R TO 48R. REPAIRED BULKHEAD PER EA 11-98963.SDR 9515741147Mounting Rings · corrodedDURING T-CHECK, FOUND CORROSION ON THREE RADIO ALTIMETER MOUNTING RINGS. REPAIRED RINGS, AYB 7022 AND AYB 7053 PER EA 11-99260.SDR 9515731147Seat Track · corrodedDURING T-CHECK, FOUND CORROSION IN THE SEAT TRACK AT FS 1530, LBL 107. REPAIRED TRACK PER EA 11-99277.SDR 9514191156Compressor · stalledTOP OF DESCENT, NR 3 ENGINE COMPRESSOR STALLED AND WAS SHUTDOWN. ENGINE WAS RESTARTED AND LANDED WITHOUT FURTHER INCIDENT. THE ENGINE WAS INSPECTED, BORESCOPED AND AN INFLIGHT BLEED CHECK IS SCHEDULED. THE PRBD, EVC REMOVAL AND PRECISION TRIM IS ON DEFERRAL
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