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 = '1900C' 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 = '1900C' 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 FFS2003F00004Cable · frayedAIRSTAIR DOOR WOULD NOT OPEN. BROKEN CABLE PREVENTED LATCHES FROM ROTATING.SDR FFS2003F00003Cable · frayedAIRSTAIR DOOR LATCH CABLE FOUND FRAYED/DAMAGED DURING INSPECTION.SDR NSVA200200001Check Valve · failedBOS- AFTER TAXIING TO GATE THE LT ENGINE WOULD NOT SHUT DOWN. FIRE T-HANDLE WAS PULLED, NO EFFECT. THE ENGINE CONTINUED TO RUN. MAINTENANCE VERIFIED THE FIREWALL SHUTOFF VALVE WAS CLOSED. THE MANUAL SHUTOFF VALVE WAS CLOSED AS WELL WITH NO ENGINE SHUT DOWNSDR ACE1014021Pump · malfunctionedON TAKE OFF ROLL, PRIOR TO LIFT OFF, RT ENG EXPERIENCED COMPLETE LOSS OF POWER AND TAKE OFF WAS ABORTED. NR ENGINE SPOOLED DOWN, CREW SECURED IT IAW PROCEDURE. AC RETURNED TO RAMP WITHOUT FURTHER INCIDENT. POST SHUT DOWN INSP DID NOT REVEAL ANY ABNORMALITY SDR AUS20021137Tach Generator · faulty(AUS) RT PROPELLER TACH-GENERATOR FAULTY.SDR FFS2003F00002Cable · frayedAIRSTAIR DOOR LATCH CABLE FRAYED.SDR CA021016034Sleeve · fractured(CAN) PILOT REPORTED OIL PRESSURE FLUCTUATING.REDUCED POWER, OIL PRESSURE CONTINUED TO DECREASED. SHUT DOWN AND SECURED ENGINE. LANDED WITHOUT INCIDENT. OPENED AGB WITH STANDARD AERO REPRESENTATIVE.SDR CA021009025Connector · loose(CAN) WHILE EXTENDING THE LANDING GEAR DURING AN APPROACH THE FLIGHT CREW NOTICED NO GREEN INDICATION FOR THE NOSE LANDING GEAR TO BE IN THE DOWN AND LOCKED POSITION. AFTER 2 MORE APPROACHES AND HAVING THE SAME RESULTS, THE AIRCRAFT WAS THEN RETURNED TO AND LASDR ACE0822021Relay · contaminatedON APPROACH TO LANDING, THE LANDING GEAR WOULD NOT NORMALLY EXTEND. THE FLIGHT CREW USED THE ALTERNATE HAND PUMP FOR EXTENSION AND PERFORMED AND UNEVENTFUL LANDING. MAINTENANCE CONFIRMED THAT THE LANDING GEAR HYDRAULIC MOTOR RELAY WOULD FREEZE AND NOT OPERATSDR AUS20020954Landing Gear · malfunctioned(AUS) LANDING GEAR EXTENSION SYSTEM FAULTY. GEAR EXTENDED MANUALLY. INVESTIGATION AND GROUND TESTING COULD FIND NO FAULTS. AIRCRAFT RETURNED TO SERVICE.SDR YAD2003F00002Connector · shortedDURING SCHEDULED MAINTENANCE, FOUND THAT THE WING STROBE LIGHTS WERE INOPERATIVE WITH THE NAVIGATION LIGHT TURNED ON. TROUBLESHOOTING REVEALED INTERNAL SHORTING OF THE AFT PRESSURE BULKHEAD CONNECTOR. ALSO DISCOVERED THAT THE ELEVATOR ELECTRIC TRIM SERVO WISDR ACE0820021Connector · shortedDURING SCHEDULED MAINTENANCE, FOUND THAT THE WING STROBE LIGHTS WERE INOPERATIVE WITH THE NAVIGATION LIGHTS TURNED ON, TROUBLE SHOOTING REVEALED INTERNAL SHORTING OF THE AFT PRESSURE BULKHEAD CONNECTOR. DISCOVERED THAT THE ELEVATOR ELECTRIC TRIM SERVO WIRES TSDR AUS20020907Gcu · out of adjust(AUS) RT GENERATOR CONTROL UNIT (GCU) OUT OF ADJUSTMENT.SDR ACE0806021Ring Assembly · looseDURING HSI INSPECTION, THE CT VANE RING SEGMENTS WERE NOTED BEING LOOSE. THE HOT SECTION WAS REPLACED DUE TO THIS CONDITION. AS THE ASSY WAS SET ON A WORK BENCH, MULTIPLE SHROUD SEGMENTS WERE OBSERVED TO FALL OUT OF PLACE, HAD THIS OCCURRED DURING ENG OPERATSDR ACE0805021Pump · leakingPILOT REPORTED FUEL LEAKING FROM LEFT COWLING AFTER SHUT DOWN ON THE RAMP, MAINTENANCE REPLACED THE LOW PRESSURE FUEL PUMP DUE FUEL LEAKING FROM PRESSURE RELIEF COVER GASKET. THIS PUMP WAS IN COMPLIANCE WITH CRANE SB. CONCERNING RELIEF COVER SCREW TORQUES ANSDR AUS20020791Wire · failed(AUS) LT PROPELLER GROUND IDLE STOP SOLENOID FAILED. BROKEN CONDUCTOR AT WIRING ENTRY INTO SOLENOID BODY.SDR ACE0729021Oil Cooler · crackedMAINTENANCE FOUND OIL LEAKING FROM THE RIGHT ENGINE COWLING. INVESTIGATION REVEALED A CRACKED OIL COOLER. OIL COOLER WAS REPLACED. THE REMOVED OIL COOLER WAS INSPECTED AND A CRACK ALONG THE END PLATE WELD SEEM WAS LOCATED. THIS DEFECT IS COMMON WITH THIS PSDR FFS2003F00000Cable · frayedAIRSTAIR DOOR LATCH CABLE FRAYED.SDR FFS2003F00001Cable · frayedAIRSTAIR DOOR LATCH CABLE FOUND FRAYED DURING INSPECTION.SDR TIMR74Skin · crackedLEADING EDGE OF STABILIZER DISBONDED ON LOWER SIDE AND A CRACK FORMED JUST OFF THE END CAP AND COMPOSITE JOINT. (CONTROL NR 74)SDR ACE0603021Relay · burnedON APPROACH, THE LANDING GEAR WAS SELECTED DOWN AND THE GEAR EXTENDED NORMALLY, GIVING THREE GREEN SAFE INDICATIONS. MOMENTS AFTER GETTING THE GEAR DOWN AND SAFE INDICATION, THE LANDING GEAR PUMP CIRCUIT BREAKER POPPED. THE AIRCRAFT MADE AN UNEVENTFUL LANDINSDR ACE0531021Control Cable · brokenPILOT ATTEMPTED TO ADJUST ELEVATOR TRIM TO REDUCE CONTROL FORCES AND NOTICED THAT TRIM SYS DID NOT FEEL LIKE IT WAS WORKING NORMAL. AFTER UNEVENTFUL LANDING , PILOT ATTEMPTED TO ADJUST ELEVATOR TRIM, NOTED THAT TRIM WHEEL STARTED TO BIND. BROKEN UPPER ELEVATSDR ACE0155021Yoke · crackedWHILE PERFORMING A SCHEDULED AILERON YOKE INSPECTION. FOUND THE RT AILERON YOKE CRACKED ON ONE SIDE OF THE TAPER PIN HOLE. ALONG THE GRAIN OF THE METAL.SDR ACE0515021Yoke · crackedWHILE PERFORMING A SCHEDULED AILERON YOKE INSPECTION, FOUND THE RT AILERON YOKE CRACKED ON ONE SIDE OF THE TAPER PIN HOLE. ALONG THE GRAIN OF THE METAL. THIS COMPONENT WAS INSPECTED AT LEAST ONCE WITHIN THE PREVIOUS 2000 FLIGHT HOURS.SDR ACE0510021Windshield · crackedON CLIMB OUT, RT WINDSHIELD CRACKED. AIRCRAFT IMMEDIATELY RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. WINDSHIELD REPLACED.SDR ACE0509021Bolt · lack of lubeAT CAMP INSPECTION, WHILE PERFORMING A SPECIAL INSPECTION AS DIRECTED BY MFG. FOUND RT MLG DRAG BRACE CENTER BOLT TO BE MISSING GREASE PASSAGES. THIS IS THE EXACT CONDITION THAT REQUIRED THE SPECIAL INSPECTION. REPLACED THE (PN 1018100903) BOLT WITH A NEW SDR CA020528004Blade · damaged(CAN) DURING A ROUTINE INSPECTION MAINTENANCE DISCOVERED THE RT INBOARD INERTIA VANE LINKAGE HAD COME APART. THE RETAINING PIN AND ROD WERE NOT FOUND. UPON INSPECTION OF FIRST STAGE COMPRESSOR ONE BLADE HAD TWO NICKS. IT IS SUSPECTED THAT THE RETAINING PIN WASSDR NSVA02011Control Cable · out of rigBOS - CREW REPORTED THAT THE AIRSTAIR DOOR WOULD NOT LOCK. SECURED AIRSTAIR DOOR TO LOCKED POSITION FOR FERRY FLIGHT. SFP ISSUED TO FERRY AIRCRAFT FROM BOS TO HYA. HYA MAINTENANCE RIGGED THE AIRSTAIR DOOR CABLE IAW BMM 52-10-00, OPERATIONAL CHECK WAS SATISFSDR NSVA0212Control Cable · brokenLEB - CREW REPORTED THAT THE AIRSTAIR DOOR HANDLE WOULD NOT SECURE CLOSED. FOUND BROKEN CABLE INSIDE AIRSTAIR DOOR LATCH MECHANISM. MAINTENANCE ACCOMPLISHED TEMP FIX TO SECURE DOOR. SFP ISSUED TO FERRY AIRCRAFT FROM LEB TO HYA. HYA MAINTENANCE REPLACED AIRSDR ACE0425021Diaphragm · leakingON THE RAMP, THE PILOT REPORTED FUEL LEAKING FROM THE INBOARD NR 1 ENGINE DRAIN LINE. MAINTENANCE DISCOVERED THE LOW PRESSURE FUEL PUMP WAS REPLACED. DISASSEMBLY OF THE PUMP REVEALED THAT THE DIAPHRAGM IN THE PRESSURE ADJUSTING VALVE HAD A HOLE IN IT. FURTHSDR CA020913008Engine · making metal(CAN) ON DESCENT, NR 1 ENGINE TORQUE DROPPED BY 200 LBS. WHEN THE PILOT RETARDED THE POWER LEVER THE TORQUE DROPPED OFF ANOTHER 2000 LBS AND THE LOW OIL PRESSURE LIGHT ILLUMINATED. THE PILOT SHUTDOWN THE ENGINE AND CONTINUED THE APPROACH AND LANDING WITHOUT SDR ACE0419021Valve · mismanufacturedON ROUTINE INSPECTION, FOUND ENGINE FORWARD AND AFT COMBUSTION CASE DRAIN VALVE LINES OVERHEATED. REMOVED DRAIN VALVES AND INSPECTED FOR CONDITION. DETERMINED THAT BOTH DRAIN VALVES HAD BEEN PREVIOUSLY INSTALLED WITH MISSING INTERNAL COMPONENTS. A TOTAL OF SDR FFS2002F00005Tire · separatedA WALK AROUND CHECK REVEALED A SECTION OF TREAD APPROXIMATELY 16 INCH X 5 INCH MISSING FROM RIGHT HAND INBOARD TIRE. APPARENTLY THE TREAD HAD SEPARATED UPON LANDING AND IMPACTED THE RIGHT INBOARD FLAP SEGMENT DAMAGING THE FLAP NACELLE FAIRING, LOWER AFT SKIN SDR CA020403002Tire · unbonded(CAN) AIRCRAFT DEPARTED PRINCE GEORGE,PILOTS FELT VIBRATION THRU AIRFRAME. AS IT DID NOT DIMINISH THEY ELECTED TO RETURN. MAINTENANCE INSPECTED AIRCRAFT AND WITH NO VISIBLE DEFECTS THE AIRCRAFT WAS TEST FLOWN. NO NOTICEABLE VIBRATION WAS FELT AND AIRCRAFT RETUSDR NSVA0209Odor · detectedBOS - FAINT SMELL OF OIL COMING FROM ENVIRONMENTAL SYSTEM. MAINTENANCE INSPECTED LT AND RT ENGINE INTAKES FOR OIL RESIDUE, OIL FOR PROPER LEVEL AND DUCT OUTLETS FOR RESIDUE, NONE FOUND. SFP ISSUED TO HYA. MAINTENANCE INSPECTED ACM FOR OIL LEAKS, NO DEFECTS SDR ACE0319021Shaft · shearedAFTER LANDING, PILOT REPORTED INTERIOR CABIN DOOR HANDLE INOPERATIVE. MAINTENANCE REMOVED THE HANDLE AND FOUND THE DRIVE SHAFT SHEARED. MAINTENANCE REPLACED THE HANDLE ASSEMBLY AND FOUND NO OTHER PROBLEMS.SDR ACE0318021Switch · out of adjustON APPROACH TO LANDING, GEAR WARNING SYSTEM (REDUCED POWER WITH GEAR UP) DID NOT FUNCTION EVEN WITH POWER LEVERS FULLY RETARDED. MAINTENANCE CORRECTED THE PROBLEM BY ADJUSTMENT OF THE POWER LEVER GEAR UNSAFE WARNING MICRO SWITCHES.SDR ZKG2002F00001Cooler · crackedPRECOOLER CRACKED ON RIGHT ENGINE INBOARD AFT. THIS IS THE 2ND AC WITH THE SAME TROUBLE IN LESS THAN ONE WEEK.SDR ACE0225021Shaft · shearedAFTER LANDING, THE FLIGHT CREW WAS UNABLE TO OPEN THE FORWARD AIRSTAIR DOOR USING THE INTERIOR HANDLE. THE PILOT WROTE UP THE AIRSTAIR DOOR HANDLE AS INOPERATIVE. MAINTENANCE REPLACED THE INTERIOR DOOR HANDLE ASSEMBLY AFTER FINDING THE SQUARE HANDLE SHAFT SHSDR ACE0220021Light · brokenUPON LANDING GEAR RETRACTION AFTER TAKEOFF, LANDING GEAR DOWN AND LOCK GREEN LIGHTS REMAINED ILLUMINATED. GEAR WARNING HANDLE LIGHTS CONTINUED TO WORK CORRECTLY. AIRCRAFT MADE UNEVENTFUL LANDING IN ANCHORAGE AND MAINTENANCE REPLACED THE DEFECTIVE LAMP MODULESDR 2002F00863Angle · crackedANGLE LOCATED ABOVE THE ICE DOOR HINGE, THIS ANGLE HOLDS THE LOWER FIRE SEAL BULKHEAD. WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK. (M)SDR ACE0208021Oil Cooler · crackedPILOT REPORTED THAT, AFTER LANDING, HE OBSERVED ENGINE OIL LEAKING FROM THE NR 2 ENGINE. THE OIL LEVEL WAS VERIFIED TO BE JUST INDICATIONS OF OIL PRESSURE LOSS, FLUCTUATION OR HIGH TEMP. MAINTENANCE REPLACED THE OIL COOLER AND LATER VERIFIED THAT IT WAS CRACKSDR ACE0206021Downlock Switch · inoperativePILOT REPORTED THAT ON APPROACH TO ANCHORAGE, WHEN THE LANDING GEAR WAS SELECTED DOWN. THE NOSE GEAR, GREEN DOWN AND LOCK LAMP FAILED TO ILLUMINATE (THE GEAR UNSAFE LIGHTS WERE NOT ILLUMINATED). THE GEAR WAS CYCLED AND AFTER A 30 SECOND DELAY, THE NOSE GEAR SDR ACE0118021Yoke · crackedWHILE PERFORMING A SCHEDULED AILERON YOKE INSPECTION, FOUND THE RT AND LT AILERON YOKES CRACKED ON TWO SIDES (TOP AND BOTTOM) OF THE TAPER PIN HOLES, ALONG THE GRAIN OF THE METAL. THE CAUSE OF THE FAILURES WAS NOT EVIDENT.(K)SDR ACE0124021Connector · dirtyAFTER DEPARTURE FROM ANCHORAGE, THE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER SELECTING GEAR UP. THE FLIGHT CREW RETURNED FOR AN UNEVENTFUL LANDING IN ANCHORAGE. MAINT COULD NOT DUPLICATED THE DISCREPANCY WITH THE AIRCRAFT ON JACKS. MAINT CLEANED SYSTESDR ACE0119021Line · crackedFLIGHT CREW REPORTED THAT THE NR 2 ENGINE FLAMED OUT EN ROUTE. ATTEMPTED RESTART WAS UNSUCCESSFUL. THE ENGINE WAS SECURED AND ACCOMPLISHED UNEVENTFUL LANDING. MAINTENANCE LOCATED A CRACKED P3 ENGINE CONTROL AIR LINE AND REPLACED SAME. MAINTENANCE ALSO DETESDR ACE0117021Relay · burnedTHE PILOT REPORTED THAT AFTER DEPARTURE FROM HPB, THE LANDING GEAR SELECTOR HANDLE WAS INOPERATIVE AND WOULD NOT RAISE THE LANDING GEAR. THE FLIGHT CONTINUED, WITH THE GEAR EXTENDED. AN UNEVENTFUL LANDING WAS MADE AND MAINTENANCE REPLACED THE LANDING GEAR POSDR ACE0102021Wire · brokenAFTER TAKEOFF, NR 2 ENGINE OIL PRESSURE INDICATED (0) UNTIL POWER WAS REDUCED TO 1700 LBS TORQUE. RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. MAINTENANCE REPAIRED A BROKEN WIRE AT THE NR ENGINE OIL PRESSURE TRANSMITTER CONNECTOR.SDR NSVA0203Line · crackedRKD - ON TAKEOFF ROLL OUT HYD LOW ANNUNCIATOR LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE AT RKD DECLARED THAT FLUID LEVEL WAS OK FOR 'M' ACTION AND HEF MAINTENANCE CONTROL DEFERRED IT IAW MEL 32-7 CAT 'C'. PILOT WROTE UP THAT SDR NSV2002F00000Line · chafedMECHANIC FOUND EVIDENCE OF FUEL DRIPPING FROM LEFT ENGINE NACELLE. REMOVED AND REPLACED FUEL LINE, RAN UP, LEAK CHECKED GOOD. (CONTROL NR NSVA 02-03)
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