Aerospatiale AS332L
Service difficulty reports · 62
Newest first. General aviation reporting is voluntary.
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 = 'AS332L' 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 = 'AS332L' 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 AU000085Gearbox · corroded(AUS) MAIN ROTOR GEARBOX LEAKING OIL FROM THE AREA OF THE ROTOR BRAKE ATTACHMENT LUGS. INVESTIGATION FOUND CORROSION AROUND THE STAINLESS STEEL SLEEVE.SDR AU990151Transmission · making metal(AUS) MAIN ROTOR GEARBOX METAL CONTAMINATION. PART TC: 1,704.SDR AU981162Harness · failed(AUS) NR 1 ENGINE NTL HARNESS FAULTY. PART TC: 6,171.SDR AU981124Bearing · loose(AUS) MAIN ROTOR HEAD TEFLON BEARINGS HAD EXCESSIVE PLAY. PART TC: 1,142.SDR CA980325049Blade · damaged(CAN) DURING DAILY INSPECTION AFTER FLIGHT IT WAS NOTICED THAT THE ELT ANTENNA WAS MISSING AND THAT ONE TAIL ROTOR BLADE WAS DAMAGED. THE DAMAGED AREA WAS APPROXIMATELY MID POINT OF THE INNER SURFACE OF THEBLADE. IT APPEARS THAT THE ELT ANTENNA MAY HAVE PUNCTUSDR AU980493Coupling · leaking(AUS) NR 2 ENGINE FUEL SUPPLY LINE QUICK DISCONNECT FITTING LEAKING. SUBMITTER SUSPECTS CAUSED BY A WORN COUPLING.SDR AU980494Filter · contaminated(AUS) NR 2 ENGINE FUEL FILTER CONTAMINATED.SDR AU971654Fcu · faulty(AUS) NO2 ENGINE FUEL CONTROL UNIT FAULTY.SDR CA971121004Sleeve · cracked(CAN) FRENCH AD T97-303-066, REQUIRED INSPECTION OF THE SLEEVE, SPLINED SHAFT. INSPECTION INCLUDED A DYE PENETRANT OF SHAFT WHICH DETECTED TWO SMALL WEAR MARKS ON THE FRONT OF THE SHAFT ABOUT 120 DEGREES APART. FURTHER INVESTIGATION FOUND THAT THESE WEAR MARSDR AU960957Pipe · cracked(AUS) NO2 HYDRAULIC SYSTEM PIPE CRACKED AND LEAKING - LOSS OF HYDRAULICFLUIDSDR AU960956Cylinder · loose(AUS) LIFE JACKET CO2 INFLATION BOTTLES UNSCREWED FROM FIRING MECHANISM- LIFE JACKET SERIAL NUMBERS 9409871 AND 9409866 - ANTI-TAMPERING INDICATORS WERE STILL IN PLACESDR AU960036Engine · over temp(AUS) ENGINE OVERTEMPED ON START - EGT WAS BELOW 900 DEGREES C FOR 38 SECONDS - EGT LIMITS ON START 810 DEGREES C TO 900 DEGREES C FOR 2 SECONDS - SUSPECT START FOLLOWED ABORTED START WHICH LEFT A SUBSTANTIAL AMOUNT OF FUEL IN THE ENGINE
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