Aerospatiale SA330J
Service difficulty reports · 69
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 = 'SA330J' 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 = 'SA330J' 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 3S8R2011041600011Stringer · deformedSTRINGER IN REAR TRANSVERSAL FUEL TANK COMPARTMENT DEFORMED. TO BE REPLACED WITH NEW.SDR 3S8R2011041600010Stringer · deformedSTRINGER IN REAR TRANSVERSAL FUEL TANK COMPARTMENT DEFORMED. TO BE REPLACED WITH NEW.SDR 3S8R2011041600009Stringer · deformedSTRINGER IN REAR TRANSVERSAL FUEL TANK COMPARTMENT DEFORMED. TO BE REPLACED WITH NEW .SDR 3S8R2011041600008Wedge · corrodedLEFT WEDGE CORRODED AT FS 5905. WILL REQUIRE REPLACEMENT.SDR 3S8R2011041600005Attach Fitting · crackedRIGHT ANGLE OF TAILBOOM ATTACH FITTING CRACKED. REPLACED WITH NEW, TAILBOOM FRAME 9000, RE-WORK SHEET 330530604.SDR 3S8R2011041600004Angle · crackedHORIZONTAL STABILIZER INTERNAL ANGLE CRACKED. TO BE REPLACED WITH NEW.SDR 3S8R2011041600003Angle · corrodedRIGHT INTERNAL UPPER ANGLE BETWEEN FRAME X3855 AND X5295 CORRODED BEYOND LIMITS. TO BE REPLACED WITH NEW.SDR 3S8R2011041600002Angle · corrodedLEFT ANGLE BETWEEN FRAME X3855 AND X5295 IN LEFT FUEL TANK COMPARTMENT CORRODED BEYOND LIMITS. TO BE REPLACED WITH NEW.SDR 3S8R2011041600001Angle · corrodedRT ANGLE BETWEEN FRAME X3855 AND X5295 CORRODED, TO BE REPLACED WITH NEW.SDR P4YA2010120900001Engine · failedDURING SOUTHBOUND CRUISE, THE SIC CALLED OFF THE POWER SETTING. 95 PERCENT WAS SET NG, THERE WAS A SUDDEN BOOM FROM THE ENGINE AND A SLIGHT YAW. POWER WAS REDUCED, GAUGES CHECKED, THEN THE CREW CHIEF TOLD THE PILOTS THE NR 1 ENGINE WAS MAKING 92 PERCENT AND SDR P4YA2010120300001Connector · dirtyWHILE ON SHORT FINAL, LANDING, THE RT FIRE LIGHT ILLUMINATED AND AURAL TONE CAME ON. FLIGHT CREW THEN SCANNED THE INSTRUMENT PANEL FOR SECONDARY INDICATIONS OF FIRE AND FOUND NONE. CREW THEN COMPLETED THE APPROACH AND UPON LANDING RETARDED NR2 ENGINE TO IDLE PSDR P4YA2010070600001Oil Cooler · leaking4 MILES OUT, MGB WARNING LIGHT ILLUMINATED. NOTICED PRESSURE DROP TO .5 BAR. UPON FINAL, NOTICED TEMP TO BE 115°C. ALL SEQUENCE OF EVENTS WITHING 2:20 MIN. UPON INSP ON GROUND, FOUND OIL COOLER ASSY LEAKING AND FURTHER NOTICED PLUG BLOW OUT OF BACK OF OIL COOSDR P4YA2010022300001Door · openAFTER DEPARTING, AIRBORNE, PRIOR TO REACHING CRUISE SPEED AND ALTITUDE. RT REAR DOOR CAME OPEN IN FLIGHT. ACTION WAS TO SLOW DOWN TO NEAR VTOSS AIRSPEED AND RETURN BACK TO DEPARTURE AIRBORNE. AFTER LANDING, DOOR WAS REMOVED AND ACFT INSPECTED, THEN RESTARTEDSDR P4YA2010021800001Oil Cooler · destroyedAFTER 1 HOUR AND 40 MINUTES OF INSTRUMENT TRAINING A LOUD NOISE WAS HEARD FROM THE REAR OF THE ACFT AND A SLIGHT VIBRATION WAS FELT BY THE CREW. AFTER A COUPLE OF MINUTES, 1 OF THE MAIN GEAR BOX OIL COOLER FAN BELTS LIGHT ILLUMINATED. AN IMMEDIATE TURN TO THSDR CA040528004Freewheel Unit · failedON START UP, ROTORS BEGAN TURNING. A LOUD BANG HEARD. START ABORTED. INSPECTION REVEALED T/R SHAFT SEGMENT TWISTED AT NR 5 SHAFT. FREEWHEEL SLIPPED MOMENTARILY AND RE-ENGAGED. TRANSMISSION SENT TO FRANCE FOR DISASSEMBLY. SPRING IN FREEWHEEL FOUND BROKEN.SDR 20001101SH018Freewheel Unit · failedMAIN GEARBOX FIREEWHEEL FAILURE CAUSING OVERTORQUE TO INTERMEDIATE GEARBOX. (X)SDR 20001101SH017Freewheel Unit · failedMAIN GEARBOX FREEWHEEL FAILURE. (X)SDR 20001101SH019Freewheel Unit · failedMAIN GEARBOX FREEWHEEL FAILURE CAUSING OVERTORQUE TO TAILROTOR GEARBOX. (X)SDR AU961027Blade · faulty(AUS) TAIL ROTOR BLADE LEADING EDGE EROSION STRIP SEPARATED FROM BLADE CAUSING HIGH FREQUENCY VIBRATION - SUSPECT CAUSED BY DEFECTIVE BOND BETWEEN BLADE LEADING EDGE AND EROSION STRIP
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