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 = '180K' 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 = '180K' 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 CA150127005Chain · detached(CAN) DURING A TRAINING FLIGHT, PILOT REPORTED THAT THE ELEVATOR TRIM WHEEL JAMMED IN FLIGHT, DURING CRUISE, WITH TRIM IN A RELATIVELY NEUTRAL POSITION. THE PILOT WAS UNABLE TO ROLL THE TRIM WHEEL FORWARD, BUT WITH CONSIDERABLE FORCE APPLIED BY THE PILOT, THE SDR CA121023006Angle · cracked(CAN) DURING INSPECTION OF HORIZONTAL STABILIZER TRIM TAB ACTUATORS, 1000 HRS OR 3 YEARS, IT WAS FOUND THAT THE TAILCONE REINFORCING LT ANGLE ASSY, PN 0712048-7 HAD A CRACK AT THE HORIZONTAL STABILIZER PIVOT POINT BOLT HOLE. CRACK RUNNING FROM TOP OF ANGLE, DOSDR CA110331026Relief Valve · broken(CAN) OIL PRESSURE VALVE HSG ON BACK OF ENGINE WAS FOUND LEAKING. MAINTENANCE REMOVED THE VALVE, BUT UPON RE-INSTALLATION, THE VALVE BROKE IN HALF. THE AREA BETWEEN THE SEAT OF THE O-RING AND THE THREADS WAS FOUND CRACKED, CAUSING THE LEAK. THE UNIT WAS REMOVSDR CA080225009Control Cable · frayed(CAN) LWR ELEVATOR CABLE FRAYED AT BULKHEAD STA 140, WHERE CABLE RIDES ON THE PHENOLIC BLOCK.SDR CA070724003Elt · corroded(CAN) BATTERY CONNECTIONS HAD EXCESSIVE CORROSION AND EVEN THOUGH THE INDICATOR LAMP INDICATED THAT UNIT WAS WORKING THE UNIT HAD NO SWEEP OUTPUT (TC NR 20070724003)SDR CA070522003Camshaft · spalled(CAN) IN REMOVING NR 1 CYLINDER TO BE CHANGED OUT THE LIFTERS WERE REMOVED TO BE BLEED DOWN, LIFTERS WERE SPAWLED. THE AME INSPECTED THE CAM AND THE EXHAUST LOBE WAS ALSO SPALLED. THE ENGINE WAS REMOVED AND PREPARED FOR SHIPMENT TO A REPAIR SHOP. UNDER FURTHERSDR AU510001674Drive Belt · looseALTERNATOR DRIVE BELT LOOSE. LOSS OF ELECTRICAL POWER.SDR CA021119006Bearing · corroded(CAN) PROPELLER WOULD NOT CHANGE PITCH. PROPELLER WAS SO BADLY CORRODED INTERNALLY THAT THE BEARING SEIZED. ENTIRE PROPELLER SCRAP DUE TO CORROSION. NO HISTORY OF PROPELLER HAVING BEEN SUBMERGED.SDR CA020726018Cylinder · cracked(CAN) AT END OF 2 RT FLT, CYL HEAD TEMP, OIL TEMP & PRESSURE ALL NORMAL. OIL TEMP SUDDENLY WENT UP ONE NEEDLE WIDTH, OIL PRESSURE WENT DOWN ONE NEEDLE WIDTH. ENGINE MADE BANGING, CLATTERING NOISE WITH WHIFF OF HOT OIL SMOKE IN COCKPIT. ENGINE RAN VERY ROUGHSDR 2002FA0000836Lifter · failedTHIS ENGINE WAS OVERHAULED 6/10/99 BY REPAIR STATION. IT NOW HAS 563.3 HOURS AND ALL THE INTAKE VALVES WERE BAD, ALL EXHAUST GUIDES WERE BAD, AND ALL LIFTERS ARE BAD. CYLINDERS WERE NEW FROM PARTS MFG AND SUPPLY. THIS AIRCRAFT HAS NOT SET FOR OVER 1 MONTH ASDR 2002FA0000835Lifter · failedTHIS ENGINE WAS OVERHAULED 6/10/99 BY REPAIR STATION. IT NOW HAS 563.3 HOURS AND ALL THE INTAKE VALVES WERE BAD, ALL EXHAUST GUIDES WERE BAD, AND ALL LIFTERS ARE BAD. CYLINDERS WERE NEW FROM PARTS MFG AND SUPPLY. THIS AIRCRAFT HAS NOT SET FOR OVER 1 MONTH ASDR 2002FA0000834Guide · failedTHIS ENGINE WAS OVERHAULED 6/10/99 BY REPAIR STATION. IT NOW HAS 563.3 HOURS AND ALL THE INTAKE VALVES WERE BAD, ALL EXHAUST GUIDES WERE BAD, AND ALL LIFTERS ARE BAD. CYLINDERS WERE NEW FROM PARTS MFG AND SUPPLIER. THIS AIRCRAFT HAS NOT SET FOR OVER 1 MONTH SDR 2002FA0000833Intake Valve · failedTHIS ENGINE WAS OVERHAULED 6/10/99 BY REPAIR STATION, IT NOW HAS 563 HOURS AND ALL THE INTAKE VALVES WERE BAD, ALL EXHAUST GUIDES WERE BAD, AND ALL LIFTERS ARE BAD. CYLINDERS WERE NEW FROM PARTS MFG AND SUPPLY. THIS AIRCRAFT HAS NOT SET FOR OVER 1 MONTH AT ASDR 2001FA0000658Gasket · looseTHIS AIR FILTER ASSEMBLY HAS THE MANUFACTURING DEFECT DESCRIBED IN AD. WITH THE GASKET COMING LOOSE. FOUND IT DURING ANNUAL INSPECTION AND DISCOVERED THAT IT (BA 8110) IS NOT COVERED BY THE AD.SDR 2002FA0001387Bellcrank · bentAIRCRAFT WAS INVOLVED IN AN ACCIDENT ON LANDING DUE TO LOSS OF CONTROL. CFI WAS FLYING FROM THE RT SEAT. AIRCRAFT LEFT THE RUNWAY TO THE RT EVEN THOUGH PILOT APPLIED FULL LT RUDDER. DURING INSPECTION. DISCOVERED THAT THE LT RUDDER PEDAL WOULD UNLOCK (STOWSDR CA001018011Bearing · failed(CAN) PROPELLER PARTS CORRODED BEYOND REPAIR. BLADE BEARING RACES AND BALLS. BLADE SPLIT RETAINING RINGS. PISTON AND PISTON PINS. CYLINDER ACTUATING PINS. NOTE: THESE PARTS CORRODED AFTER 6 YEARS, NOW REGULATION IS 10 YEARS. (X)SDR 20000623SH018Bushing · erodedRECENTLY INSTALLED TAILSPRING BUSHINGS FOUND EXTRUDED AFTER ONLY 8 HOURS OF OPERATION. SUBMITTER KNOWS OF ONE OTHER LOW TIME FAILURE OF THESE BUSHINGS. (X)SDR AU981594Spar · cracked(AUS) VERTICAL FIN REAR SPAR CRACKED UNDER DOUBLERS AS INDICATED IN CESSNA SE-80-85.SDR CA980908004Spreader Bar · corroded(CAN) SPREADER BARS AT THE FLOAT WERE SPLIT ON THE RIGHT HAND SIDE IN OUTSIDE TUBING. CONDITION COULD NOT BE DETECTED WITHOUT DISMANTLING THE FAIRING IN BETWEEN THE FLOATS. THE INSIDE SLEEVE IN THE ATTACHMENT AREA COVERS THE INSIDE OF THE SPREADER BAR TUBINGSDR CA980330017Cylinder · scratched(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE CYLINDER WAS FOUND SCRATCHED AND THE BLADE PITCH LOCK DISTRIBUTION WAS FOUND OUT OF MANUFACTURERS LIMITS AS PER THE OVERHAUL MANUAL.SDR 97ZZZX5139Bracket · brokenPILOT REPORTED LEFT FLAP WOULD NOT FULLY EXTEND. AN INSPECTION WAS CONDUCTED AND THE FLAP PULLEY BRACKET WAS FOUND BROKEN. THIS CONDITION CAUSED FLAP CABLE TO HAVE EXCESSIVE SLACK.SDR 98ZZZX961Selector · corrodedFOUND FUEL SELECTOR VALVE CORRODED AND FLAKING ON ONE SIDE. THE ONLY WAY TO SEE THIS SIDE OF THE VALVE IS WITH A MIRROR THROUGH THE INSPECTION PANEL ON THE BOTTOM OF THE AIRCRAFT. AIRCRAFT IS ON FLOATS.SDR 97ZZZX3383Vent · pluggedAT ANNUAL INSPECTION, NOTICED CORROSION ON THE MAIN ELECTRICAL CONTACTOR AND THE STARTER RELAY. SUSPECT THE BATTERY WAS VENTING OUT BY THE CABLES. CHECKING THE BATERY BOX VENT, IT WAS FILLED WITH MUD DAUBER LARVA. THIS AIRCRAFT HAD ACCUMULATED 36 HOURS SINCSDR EY2R9601207Bearing · corrodedCORROSION FOUND ON BEARING RACE.SDR 96ZZZX2769Brake Disc · failedUPON STARING TAKEOFF ROLL, LOUD NOISE AND LEFT BRAKE MALFUNCTION OCCURRED. TAKEOFF ABORTED. LEFT MAIN BRAKE DISC HAD BROKEN LOOSE FROM MAIN WHEEL BOLTS. SUSPECT CAUSE WAS CRACKS IN DISC. SUBMITTER RECOMMENDS INSPECTION OF DISC FOR CRACKS.
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