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 = 'SF340A' 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 = 'SF340A' 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 COMA9531170Switch · defectiveTHE MAIN PITCH TRIM IS INTERMITTENT ON PILOTS YOKE. REPLACED THE PILOTS PITCH TRIM SWITCH.SDR COMA951170Overspeed Syst · no testLT PROPELLER OVERSPEED SYSTEM DOES NOT TEST. COULD NOT DUPLICATE, SYSTEM TEST NORMAL AND ACFT CONTINUED SERVICE.SDR COMA951169Up Lock Spring · brokenWHEN LANDING GEAR RETRACTED, INTRANSIT INDICATOR REMAINED ON. REPLACED BROKEN UPLOCK SPRING ON LT MLG.SDR COMA951166Pdu · defectiveAFTER TAKEOFF, LEFT MAIN ELECTRICAL BUS FAILED. REPLACED THE LT POWER DISTRIBUTION UNIT.SDR COMA951168Windshield Seal · failedLOUD POP SOUND FOLLOWED BY HIGH AIR FLOW SOUND IN COPILOTS WINDSHIELD AREA. THE PRESSURIZATION REMAINED NORMAL. REPLACED COPILOTS WINDSHIELD BECAUSE OF DEFECTIVE SEAL.SDR PLGA92795E1Switch · out of adjustFLT NR 4561 - BOS-ACK - DURING CLIMB-OUT, THE MAIN CABIN DOOR HANDLE WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. THE DOOR WAS CONFIRMED LATCHED AND THE DOOR WARNING HANDLE LIGHT WAS DEFERRED PER MEL 57-70-1. AIRCRAFTSDR PLGA81795G1Hyd Line · failedPHL - FLT NR 4426 - DURING TAXI, THE FLIGHT CREW EXPERIENCED A LEFT TAIL PIPE HOT LIGHT FOLLOWED BY A LEFT BLEED LEAK LIGHT. THE LEFT BLEED WAS OPEN IN AUTO AND CROSSOVER BLEED VALVE WAS OPEN. FLAMES WERE CONFIRMED AT WHICH POINT BOTH ENGINE WERE SECURED. TSDR COMA9531165Governor · defectiveLT PROPELLER RPM DROPS TO 1370 DURING FINAL APPROACH. REPLACED THE PROPELLER OVERSPEED GOVERNOR.SDR COMA9531162Inner Race · spunMECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE SPUN. WHEEL ASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR.SDR COMA9531161Inner Race · spunMECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE SPUN. WHEEL SUBASSY IS BEING SENT TO ABS FOR SECOND REPAIR AND REMOVED FROM SERVICE.SDR COMA9531164Propeller · malfunctionedDURING FINAL APPROACH, THE LT PROPELLER RPM WAS 100 RPM LOW. REPLACED THE LT PROPELLER ASSY.SDR COMA9531163Eel Battery Pack · dischargedFLOOR PROXIMITY EMERGENCY LIGHTING AT ROW 5 IS INOP. REPLACED EMERGENCY LIGHTING BATTERY PACK.SDR COMA9531160Starter Gen · failedDURING START SEQUENCE, THE LEFT ENGINE DOES NOT ROTATE. REPLACED THE LT ENGINE STARTER/GENERATOR.SDR COMA9531159Ecu · defectiveDURING FLIGHT, THE LEFT ENGINE TORQUE INDICATION FLUCTUATES. REPLACED THE LEFT ENGINE ELECTRONIC CONTROL UNIT.SDR REXA95061Transducer Assy · malfunctionedBRAKES OCCASIONALLY FAIL TO STOP AIRCRAFT UNLESS ANTI-SKID SYSTEM IS TURNED OFF. SEPT 11, 1995 TO SEPT 18, 1995, THREE WRITE-UPS. SEPT 11, OHMED ALL WHEEL SPEED TRANSDUCERS AND NO DEFECTS NOTED. SEPT 14, REPLACED LEFT AND RIGHT INBOARD WHEEL SPEED TRANSDUCESDR REXA95060Adf Control Head · smokedSMOKE IN COCKPIT FROM CENTER PANEL. FOUND SMOKE TO BE COMING FROM ADF CONTROL HEAD. ADF SYSTEM ALREADY DEFERRED. PULLED AND COLLARED ADF C/B. (M)SDR COMA9531155Propeller Hub · crackedDURING ULTRASONIC INSP OF HUB REAR FACE, A FLAW WAS INDICATED AT THE BOLT HOLE ADJACENT TO BLADE PORT NR 3. PROPELLER WAS DISSEMBLED, HUB (S/N CW1044) AND REMOVED FROM SERVICE.SDR COMA9531156Seal · leakingSMOKE WAS OBSERVED COMING FROM LEFT ENGINE STARTER/GENERATOR COOLING VENT. REPLACED THE STARTER/GENERATOR DRIVE OIL SEAL.SDR COMA9531154Windshield · bird strikeBIRD STRIKE ON RT WINDSHIELD AREA. PERFORMED BIRD STRIKE INSPECTION IAW INSPECTION PROGRAM, NO DEFECTS FOUND AND AIRCRAFT RETURNED TO SERVICE.SDR SIMA952581Eel Batt Pack · dischargedSGF - FLT 3512 - RIGHT FORWARD EMERGENCY LIGHTS FOUND TO BE INOPERATIVE ON PRE-FLIGHT INSPECTION. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE. (M)SDR COMA9531158Connector · defectiveRT PROPELLER GEAR BOX OIL PRESSURE INDICATOR WAS FLUCTUATING BETWEEN 30 AND 200 PSI. REPLACED THE PGB OIL PRESSURE TRANSDUCER WIRING CONNECTOR.SDR COMA9531157Quadrant Lock · malfunctionedCONDITION LEVERS FRICTION LOCK DOES NOT HOLD SUFFICIENTLY. REPLACED THE CONTROL QUADRANT.SDR COMA9531152Pdu · defectiveLEFT MAIN ELECTRICAL BUS WILL NOT COME ON LINE. REPLACED THE RT POWER DISTRIBUTION UNIT.SDR REXA95058Window Light · terminal borkenBRAKES FAIL TO STOP AIRCRAFT ON SEVERAL OCCASSIONS, TURNING OFF ANTI-SKID FIXES PROBLEM. OHMED WHEEL SPEED TRANSDUCERS, OHMED GOOD. OHMED LEFT AND RIGHT ANTI-SKID CONTROL VALVES, ALSO OHMED GOOD. SECURED WIRING FROM ANTI-SKID COMPUTER AWAY FROM WINDOW LIGHTSDR COMA9531153Bearing · wornSHUDDER FELT THROUGH CONTROL YOKE DURING INFLIGHT TURNS. REPLACED LT AILERON BEARINGS.SDR PLGA91195J2Carbon Seal · failedFLT NR 4899 - YYZ-BDL - THE LEFT OIL PRESSURE WARNING LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO 40 PSI. FLIGHT CREW SHUTDOWN THE ENGINE AND DIVERTED INTO ROC. MAINTENANCE INSPECTED ENGINE AND DETERMINED NR 5 CARBON SEAL FAULTY, WHERE UPON THE POWER TURBISDR COMA9531151Computer · inoperativeDURING TAKEOFF ROLL, AUTO-COARSEN WARNING LIGHT ON CENTRAL WARNING PANEL CAME ON, ABORTED TAKEOFF. REMOVED AND REPLACED AUTO-COARSEN COMPUTER WITH SERVICEABLE UNIT.SDR COMA9531150Air Data Comp · inoperativeCAPTAINS AIRSPEED INDICATOR WAS SPINNING ON TAKEOFF ROLL. REMOVED AND REPLACED AIR DATA COMPUTER WITH SERVICEABLE.SDR REXA95057Eel Battery · dischargedEMERGENCY LIGHTS WILL NOT STAY ON DURING PREFLIGHT TESTING. NO DEFECTS NOTED WITH EMERGENCY LIGHTS AND THE AIRCRAFT WAS RELEASED FOR SERVICE AFTER THE BATTERIES WERE CHARGED DURING THE FERRY FLIGHT FROM FYV TO MEM. (M)SDR COMA9531149Inner Race · spunMECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR.SDR COMA9531148Inner Race · spunMECHANIC REMOVED WHEEL ASSY DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR.SDR COMA31138Conrtol Vlv · leakingHYDRAULIC FLUID LEAKING IN NOSE LANDING GEAR AREA. REPLACED THE LANDING GEAR CONTROL VALVE.SDR PLGA94951GShoot-Bolt · wornFLT NR 4471 - TAKEOFF FROM BOS, THE CREW HATCH WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BOS LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. TROUBLE SHOOTING FOUND THE SHOOT-BOLT WORN AT THE MICRO-SWITCH ACTUATING POINT. MAISDR COMA1137Eel Battery Pack · dischargedAFT LT FUSELAGE AND AFT MOST RT CABIN OVERHEAD EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK NUMBER 24LN.SDR COM31147Valve · failedTHE FUEL CROSS-FEED VALVE WILL NOT CLOSE, CIRCUIT BREAKER TRIPPED. REPLACED THE FUEL CROSS-FEED VALVE.SDR COM31146Weu · defectiveCABIN PRESSURE WARNING ON CWP, DURING TAKEOFF. REPLACED THE WARNING ELECTRONIC UNIT.SDR COM31145Bearing · wornDURING FLIGHT, VERY NOTICEABLE VIBRATION IN CONTROL YOKE. AILERONS SEEM TO HAVE DELATED RESPONSE TO RT ROLL INPUT COMMAND. INSPECTED AILERON CONTROL SYSTEM AND FOUND NO DEFECTS. REPLACED WORN BEARINGS ON RT ELEVATOR TRIM TAB.SDR COM31143Switch · defectiveAUTO COARSEN WARNING DURING TAKEOFF. REPLACED THE AUTO COARSEN ARMING P3 PRESSURE SWITCH.SDR SIMA952381W.E.U. · malfunctionedOKC - FLT 3554 - DURING TAKEOFF, NR 1 ENGINE FIRE WARNING CAP ILLUMINATED. NO FIRE HANDLE LIGHT, NO ENGINE FIRE DETECTED. RETURNED TO OKC. MAINTENANCE REPLACED THE W.E.U. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 5,981.0. (X)SDR COM31144Engine · malfunctionedLEFT ENGINE WILL NOT ACHIEVE 100 PERCENT TORQUE. REPLACED THE LT ENGINE.SDR COM31142Control System · out of adjustFLAP WARNING ON CWP ACTIVATED. RIGGED THE FLAP CONTROL SYSTEM IAW M/M SPECIFICATIONS AND AIRCRAFT TO SERVICE.SDR COM31141Governor · inoperativeRIGHT PROPELLER COMES OUT OF FEATHER VERY SLOW. ACTION: FERRIED AIRCRAFT TO CVG, FOUND RIGHT PROPELLER OVERSPEED GOVERNOR BAD. REMOVED AND REPLACED GOVERNOR WITH SERVICEABLE UNIT.SDR COM31140Control Cable · brokenRIGHT INBOARD MAIN GEAR DOOR WOULD NOT RETRACT AFTER GEAR EXTENSION. ACTION: FOUND RELEASE CABLE ON TELESCOPING ROD, BROKEN, REPLACED CABLE WITH SERVICEABLE UNIT.SDR COM31138Starter Gen · inoperativeON TAXI OUT, THE LT ENGINE FAILED TO SHOW ANY RPM DURING START ATTEMPT. REMOVED AND REPLACED STARTER/GENERATOR.SDR SIMA952311Eel Power Supply · inoperativeDFW - FLT 3961 - EMERGENCY LIGHTS GO OUT AFTER A FEW SECONDS OF ILLUMINATION. MAINTENANCE REPLACED POWER SUPPLY. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 3,713.0. (X)SDR COM31139Engine · overtempNR 1 ENGINE ITT EXCEEDED 930 DEGREES DURING TAKEOFF. THE OUTSIDE AIR TEMPERATURE 89 DEGREES, TQ 105 PERCENT, ITT 940 DEGREES FOR 3 SECONDS. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY.SDR PLGA81895G1Connector Pin · failedFLTN 4787 - ON FINAL INTO PWM, THE RIGHT PROP RPM DROPPED TO 1160 WITH THE CONDITION LEVER AT MAX. ON THE GROUND, THE CREW WAS UNABLE TO FEATHER THE PROPELLER WITH THE CONDITION LEVER. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND THAT THE BALL JOINT SDR SIMA952291Linear Actuator · out of adjustOKC - FLT NR 3553 - DESCENT FOR LANDING INTO OKC, AIRCRAFT EXPERIENCED SEVERE ROLL RIGHT. CREW RECOVERED AND CONTINUED FOR AN UNEVENTFUL LANDING. FOLLOWING LANDING WHEN CREW RESET THE GUST LOCK, IT WAS NOTED THAT THE AILERONS WERE IN A DISCONNECT CONFIGURATISDR COM31137Hub · crackedDURING ULTRASONIC INSPECTION OF PROP HUB S/N 110935, SEVERAL FLAWS WERE DETECTED WHILE PERFORMING SB 61-58 APPENDIX C SCAN B. PROPELLER WAS DISASSEMBLED AND HUB WAS REMOVED FROM SERVICE.SDR PLGA71195J1Static Seal · excess clearanceHIGH OIL TEMPERATURE, OIL PRESSURE FLUCTUATION AND LOSS IS BELIEVED TO BE THE RESULT OF EXCESSIVE CLEARANCE BETWEEN THE NR 3 LABRYNTH SEAL AND ITS ASSOCIATED STATIC SEAL, THE A-SUMP SUPPORT SEAL, WHICH CAUSED SUMP AIRFLOWS INSUFFICIENT TO PREVENT EXCESSIVE LOS
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