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 COMA9531207Control Assy · malfunctionedLANDING GEAR INTRANSIT LIGHT REMAINED ON WHEN GEAR SELECTED UP. COULD NOT DUPLICATE, REPLACED THE LANDING GEAR CONTROL ASSY FOR TROUBLESHOOTING.SDR COMA9531204Weu · defectiveLEFT ENGINE INTAKE HEAT FAILED INDICATION. REPLACED THE WARNING ELECTRONIC UNIT.SDR COMA9531212Bearing Race · spunWHEEL ASSEMBLY WAS REMOVED FROM A/C FOR TIRE WORN TO LIMITS. UPON DISASSEMBLY AND INSPECTION OF WHEEL, FOUND BEARING RACE IN HUB ASSEMBLY TURNING. SUB-ASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR.SDR COMA9531205Controls · lack of lubeAILERONS ARE BINDING. INSPECTED AILERON SYSTEM AND NO FAULTS FOUND. LUBRICATED AILERON CENTERING CAMS AND ACFT RETURNED TO SERVICE.SDR COMA9531201Prop Hub · bolt hole dmgFOUND MULTIPLE FLAW INDICATIONS DURING ULTRASONIC INSPECTION IN COMPLIANCE WITH AD93.19.01. PROPELLER WAS DISASSEMBLED AND HUB, S/N CW1042, REMOVED FROM SERVICE.SDR COMA9531203Wheel · crackedMECHANIC REMOVED NOSE WHEEL TIRE DUE TO TIRE ROTATING ON RIM. WHEEL WAS TAKEN TO THE TIRE SHOP FOR INSPECTION. WHEEL WAS DISASSEMBLED, CLEANED AND INSPECTED. THE MECHANIC FOUND THE CRACK BY USING EDDY CURRENT. CRACK .50 INCH LONG. WHEEL HAS BEEN REMOVED FSDR COMA9531202Wheel · crackedMECHANIC REMOVED NOSE WHEEL TIRE DUE TO TIRE ROTATING ON RIM. WHEEL WAS TAKEN TO THE TIRE SHOP FOR INSPECTION. WHEEL WAS DISASSEMBLED, CLEANED AND INSPECTED. THE MECHANIC FOUND A 3.50 INCH CRACK IN THE BEAD AREA ON THE OUTBOARD SUBASSEMBLY BY USING EDDY CURSDR COMA9531200Control Valve · malfunctionedUNCOMMANDED FLAP EXTENSION AND RETRACTION DURING FLIGHT. FLAPS WOULD OSCILLATE 3 DEGREES EVERY TEN MINUTES. REPLACED THE FLAP HYDRAULIC CONTROL VALVE.SDR COMA9531198Efis Tube · smokingDURING ENGINE START PILOT'S EFIS TUBES WENT BLANK AND SMOKE WAS NOTICED FROM GLARESHIELD AREA. REPLACED THE PILOT'S EAD2-EFD-86.SDR COMA9531199Engine · high oil consumpLEFT ENGINE OIL CONSUMPTION IS VERY HIGH. REPLACED THE LT ENGINE.SDR PLG120495E1Lower Duct · damagedFLT NR 4401 - PQI-BOS - DURING FLIGHT, THE LEFT INTAKE HEAT FAILED. DUE TO EXISTING WEATHER CONDITIONS, THE AIRCRAFT DIVERTED INTO PWM AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE LOWER DUCT DSDR SIMA953321Swivel Fitting · brokenDFW - FLT 3537 - SHORTLY AFTER TAKEOFF, AIRCRAFT HAD A COMPLETE HYDRAULIC SYSTEM FAILURE. CREW PUMPED GEAR DOWN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE SWIVEL FITTING ON THE RT MAIN GEAR FAILED. REPLACED FITTING, OPS CHECK GOOD. THE AIRCSDR COMA9531197Weu · defectiveCON FIG WARNING, DURING TAKEOFF ROLL. REPLACED THE WARNING ELECTRONIC UNIT AND ACFT RETURNED TO SERVICE.SDR COMA9531196Switch · defectivePITCH TRIM FUNCTION FROM COPILOTS POSITION IS INTERMITTENT. REPLACED THE COPILOTS PITCH TRIM SWITCH.SDR COMA9531194Ahrs Computer · defectiveLEFT H.S.I. HEADING IS SLEWING OUT OF TOLERANCE. REPLACED THE NR 1 AHRS COMPUTER.SDR COMA9531195Flight Controls · vibrationDURING TAKEOFF, A FORE AND AFT VIBRATION WAS NOTED IN CONTROL YOKES. FLIGHT CONTROL SYSTEM WAS INSPECTED AND NO DEFECTS NOTED. ACFT RELEASED FOR FLIGHT CHECK WHICH WAS SATISFACTORY.SDR PLG111795E1Door Warning · illuminatedDURING DEPARTURE FROM BOS, FLT NR 4414, HAD A FORWARD CABIN DOOR WARNING LIGHT ILLUMINATE. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE DOOR WARNING SYSTEM AND FOUND NO FAULT. THE SYSTEM WAS OPS CHECKED AND ALL INDICATSDR COMA9531192Computer · defectiveHEADING COMPARATOR WARNING. REPLACED THE NR 1 AHC.SDR REXA95067Smoke Detector · false warningCARGO SMOKE 'CWP' WARNING ILLUMINATED IN FLIGHT, STAYED ON, DISCHARGED CARGO FIRE EXTINGUISHER. REMOVED AND REPLACED CARGO FIRE BOTTLE AND CARTRIDGE. OPS CHECKED SMOKE DETECTOR IAW AMM. CHECKED GOOD, OK FOR SERVICE. NO EVIDENCE OF FIRE. (M)SDR COMA9531191Pcu · defectiveRT PROPELLER WILL NOT MAINTAIN 100 PERCENT RPM DURING TAKEOFF AND APPROACH. REPLACED THE PROPELLER PITCH CONTROL UNIT.SDR COMA9531190Compressor · damagedLEFT ENGINE IS MAKING A HIGH PITCHED WHINE DURING TAKEOFF. FOUND COMPRESSOR TO HAVE FOD DAMAGE, REPLACED ENGINE.SDR SIMA953121Light · failedLAW - FLT 3798 - DURING THE PROCESS OF PREPARING AIRCRAFT FOR DEPARTURE FROM GATE AREA, SMOKE WAS DETECTED COMING FROM VICINITY OF WINDOW LIGHT AT SEAT 11A. MAINTENANCE INSPECTED AND FOUND THE WINDOW LIGHT FIXTURE HAD FAILED. THE LIGHT FIXTURE AND FLUORESCENSDR COMA9531189Aoa Vane · defectiveTHE LEFT ALPHA LIGHT ILLUMINATED DURING FLIGHT. REPLACED THE LEFT AOA VANE.SDR COMA9531188Wire · shortedTHE CABIN PRESSURIZATION AND AUTO DUMP CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. REPAIRED SHORTED WIRING IN THE RIGHT WHEEL WELL.SDR PLG11595G1Roll Trim Tab · out of adjustFLT NR 4743 - PSM - AFTER TAKEOFF, THE AIRCRAFT ROLLED TO THE LEFT REQUIRING STANDBY TRIM TO MAINTAIN STRAIGHT AND LEVEL FLT. THE AIRCRAFT DIVERTED TO MHT LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND RERIGGED THE MAIN ROLL TURN TASDR COMA9531186Retract Mech · out of adjustFLAP FAULT ON CAUTION WARNING PANEL. PERFORMED FLAP CONTROL SYSTEM RIGGING AND ADJUSTMENT.SDR COMA9531187Trim Actuator · failedTHE MAIN ELEVATOR PITCH TRIM IS INOPERATIVE. REPLACED THE MAIN ELEVATOR PITCH TRIM ACTUATOR.SDR COMA9531183Weu · defectiveTHE LEFT ENGINE AIR VALVE LIGHT ILLUMINATED DURING FLIGHT. REPLACED THE WARNING ELECTRONIC UNIT.SDR COMA9531185Adc · defectiveTHE LEFT AIRSPEED INDICATOR FAILED. REPLACED THE AIR DATA COMPUTER.SDR COMA9531184Power Contl Quad · defectiveDURING LANDING AND ROLLOUT, THE RIGHT PROPELLER R.P.M. DETERIORATES TO 1100 R.P.M. REPLACED THE POWER CONTROL QUADRANT.SDR COMA9531179Weu · defectiveTHE RIGHT WINDSHIELD HEAT DOES NOT WORK. REPLACED THE WARNING ELECTRONIC UNIT.SDR PLG103095G3Squibb · failedFLT 4719 - ON APPROACH, CREW RECEIVED 2 INTERMIT CARGO SMOKE DETECT LIGHT WARN. APPROX 500 FEET, CARGO WARN LIGHT REMAINED ILLUMINATED. THE CARGO FIRE EXTINGUISHER SWITCH SELECTED. AFTER ACTUATING THE SWITCH, THE SMOKE DETECT WARNING LIGHT REMAINED ILLUMINASDR COMA9531180Pos Transmitter · defectiveUNCOMMANDED MOVEMENT OF FLAPS DURING FLIGHT. REPLACED THE LT AND RT FLAP POSITION TRANSMITTER.SDR 95ZZZM757Smoke Det · failedFLT 4719 - ON APPROACH, CREW RECEIVED 2 INTERMIT CARGO SMOKE DETECT LIGHT WARN. APPROX 500 FEET, CARGO WARN LIGHT REMAINED ILLUMINATED. THE CARGO FIRE EXTINGUISHER SWITCH SELECTED. AFTER ACTUATING THE SWITCH, THE SMOKE DETECT WARNING LIGHT REMAINED ILLUMINASDR PLG103095G1Garrett Vlv · malfunctionedFLT NR 4483 - EN ROUTE TO BOS, RECEIVED A RIGHT ENGINE ANTI-ICE VALVE LIGHT AND THE CAPTAINS AIRSPEED INDICATOR FAILED. THE AIRCRAFT RETURNED TO HPN, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE CLEANED THE CANNON PLUG ASDR COMA9531182Efd 86 · failedTHE PILOT'S LEFT EADI TOP TUBE IS INOPERATIVE. REPLACED THE PILOT'S EFD-86.SDR COMA9531181Starter Gen · failedTHE LEFT ENGINE WOULD NOT ROTATE DURING START CYCLE. REPLACED THE LEFT ENGINE STARTER/GENERATOR.SDR COMA9531178Inner Race · spunMECHANIC REMOVED WHEEL ASSY FROM AIRCRAFT DUE TO TIRE WORN TO LIMITS. DURING INSPECTION, FOUND THAT THE INNER RACE HAD SPUN. SUBASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR.SDR COMA9531177Computer · defectiveLEFT AND RIGHT HEADING COMPARATOR YELLOW FLAG DURING FLIGHT. REPLACED THE NR 1 AHRS COMPUTER.SDR COMA9531176Contl Valve · defectiveLEFT DUCT OVERHEAT WARNING DURING FLIGHT. REPLACED THE DUAL TEMPERATURE CONTROL VAVLE.SDR COMA9531175Generator · failedTHE RIGHT AC GENERATOR FAILED DURING FLIGHT. REPLACED THE RT AC GENERATOR.SDR 95ZZZX6319Tab Washer · failedGEAR CASE WAS RECEIVED DUE TO IDLER GEAR SHIFTED FORWARD WHICH RESULTED IN WEARING A HOLE THROUGH THE FORWARD GEAR CASE HOUSING. DISASSEMBLY REVEALED THE RIGHT IDLER GEAR NUT, PN 775770-1, HAD COME OFF THE RT IDLER GEAR, PN 775754-5. THE TABS ON THE TAB WASHSDR 96ZZZX27Wheel · crackedAIRCRAFT'S MAIN WHEEL ASSY EXHIBITING NUMEROUS BEAD SEAT FAILURES. SUBMITTER STATED CIRCUMSTANCES OR CAUSES ARE NOT APPARENT, BUT THE RECURRENCE SEEMS TO INDICATE A FATIGUE OR POSSIBLE MANUFACTURING DEFECT.SDR COMA9531174Gcu · defectiveTHE LEFT ENGINE WILL NOT ROTATE DURING START CYCLE. REPLACED THE LEFT DC GENERATOR CONTROL UNIT.SDR SIMA952961Smoke Detector · failedDFW - FLT NR 3515 - AVIONICS SMOKE WARNING AFTER TAKEOFF. REMOVED AND INSTALLED AVIONICS SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. (M)SDR COMA9531173Connectors · dirtyAUTO COARSEN FAILED DURING TAKEOFF. CLEANED CONNECTIONS AT THE P3 ARMING SWITCHES.SDR SIMA952912Prop Blade · crackedLAW - PROP DOWTY MODEL R3894-123-F25, S/N CW1157, WAS REMOVED FROM AIRCRAFT FOR SLINGING GREASE. DURING SHOP TEARDOWN, NR 2 BLADE P/N 6607132886/ S/N SF340-132-1530, WAS FOUND TO HAVE A CRACK OF APPROX 5.5 INCHES LONG IN THE AREA BETWEEN THE COUNTER WEIGHT MOSDR REXA95064Smoke Detector · malfunctionedCARGO SMOKE CAUTION IN FLIGHT, FOLLOWED CHECK LIST, FIRED CARGO EXTINGUISHER. RETURNED TO MEM. REPLACED CARGO DETECTOR. (M)SDR COMA9531172Trim Actuator · failedLEFT AILERON TRIM DOES NOT WORK. REPLACED THE LEFT AILERON TRIM ACTUATOR.SDR COMA9531171Controller · defectiveFLAP DISAGREEMENT INDICATOR FLASHES WITH EACH FLAP POSITION SELECTION. REPLACED THE FLAP CONTROL UNIT.
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