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 = 'U206G' 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 = 'U206G' 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 AU960015Flap · corroded(AUS) ENGINE RH COWL FLAP ASSEMBLY CORRODED INTERNALLY BEYOND REPAIR - AIRCRAFT OPERATES AS A SEAPLANE IN A SALT LADEN ENVIRONMENTSDR 96ZZZX592Cooler · leaksSUBMITTER STATED THIS IS THE EIGHTH OIL COOLER OF THIS TYPE TO LEAK BETWEEN 100-HOUR AND 200-HOUR TT'S.SDR CA960115201Fuel Drains · corroded stem(CAN)WHILE COMPLYING WITH CAP 28-30-01 THE FUEL DRAINS ON THE RIGHT HAND WING AND BOTH RESERVE TANKS WERE FOUND TO BE BADLY CORRODED AND THE INTERNAL SPRINGS WERE STICKING. THE FUEL DRAINS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 96ZZZX88Cooler · leakingOIL COOLER CORE WAS FOUND LEAKING AFTER RETURNING FROM A FLIGHT. THIS IS THE SECOND COOLER FOUND LEAKING ON THIS ENGINE. FIRST LEAK OF COOLER WAS AT 395.0 HOURS TOTAL TIME. TOTAL TIME ON ENGINE NOW IS 502.0 HOURS.SDR CA951127201Trim Rod End · mis repaired(CAN) PILOTS REPORTED THAT THE AIRCRAFT HAD POOR STEERING ON THE GROUND. MAINTENANCE FOUND THE RUDDER CONTROL CABLE TENSION LOW. AN UNAUTHORIZED REPAIR WAS MADE TO THE TRIM BUNGEE ROD END BY WAY OF WELDING WHICH SHORTENED THE THREADED PORTION AND THUS THE ADJUSDR 96ZZZX89Cooler · leakingOIL COOLER FOUND LEAKING. THIS IS THE SECOND OIL COOLER ON THIS ENGINE. THE FIRST STARTED LEAKING AT 353.0 HOURS TOTAL TIME. THE SECOND AT 549.5 HOURS TOTAL TIME.SDR 96ZZZX87Cooler · leakingOIL COOLER CORE WAS FOUND LEAKING.SDR 95ZZZX6085Hub · crackedPROPELLER INSPECTION FOUND CRACK IN BLADE SOCKET NR 1, 4TH THREAD.SDR 95ZZZX4554Control Rod · loose rivetsDURING ROUTINE INSPECTION, FOUND PILOT YOKE PUSH ROD CONTROL TUBE ASSY WITH LOOSE RIVETS. NOTED .05 INCH PLAY IN CONNECTION. NEW PART RECEIVED FROM CESSNA AND INSPECTION REVEALED ALUMINUM RIVETS USED DURING ASSEMBLY IN PLACE OF CARBON STEEL. CESSNA FACTORY VESDR 96ZZZX86Cooler · leakingOIL COOLER CORE WAS FOUND LEAKING.SDR 95ZZZX4564Oil Tube · extender crackedTHE EXTENDER CRACKED AT BOTTOM FLANGE AND THE TUBE FELL OFF THE ENGINE CAUSING OIL TO COME OUT OF ENGINE. SUBMITTER SUGGESTS LARGER WELDS WOULD HELP HOLD IT TOGETHER BETTER.SDR 96ZZZX90Cooler · leakingOI COOLER CORE WAS FOUND LEAKING.SDR 95ZZZX4432Valve Guide · looseINSPECTION FOUND EXHAUST VALVE GUIDE EXCESSIVELY LOOSE IN CYLINDER.SDR 95ZZZX822Rotor Coil · wornROTO-COILS EXTREMELY WORN, AND ELONGATED. FOUND DURING TOP OVERHAUL OF ENGINE.SDR 95ZZZX943Roto Coil · wornDURING TOP OVERHAUL, INSPECTION REVEALED WORN OUT EXHAUST AND INTAKE VALVE SPRING RETAINING ROTO-COILS.
Back to Cessna U206G