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 = '182T' 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 = '182T' 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 2005FA0000611Pin · looseG-1000-3 PIN CONNECTOR FOR MANIFOLD PRESSURE TRANSDUCER, THE PINS WILL GET LOOSE AND CAUSE THE MANIFOLD PRESSURE INDICATION TO JUMP FROM 7.7 TO 55 MP PSI. TROUBLESHOT, WITH THIS IN THE FUTURE DUE TO VIBRATION OF AIRCRAFT. NOTE: NEVER HAD A RED-X OVER MP INDISDR 2005FA0000752Pump · obstructedRECEIVED BOOST PUMP FOR WARRANTY CREDIT WITH A CUSTOMER COMPLAINT OF (BREAKER POPS WHEN FUEL PUMP IS TURNED ON). PRELIMINARY INSPECTION OF THE PUMP REVEALED FOREIGN MATERIAL IN THE INLET PORT. FURTHER INSPECTION OF THE PUMP REVEALED THE FOREIGN MATERIAL TRIESDR 2005FA0000086Pin · out of adjustTRANSIT CUSTOMER HAD RUDDER TRIM STICK IN FULL RT TRIM CONDITION AND COULD NOT TRIM LT. FOUND THAT IF TRIMMED TOO FAR TO RT. THE INDICATOR PIN WOULD JUMP OUT OF TRIM WHEEL TRACK AND COULD LOCK TRIM WHEEL. WE READJUSTED INDICATOR PIN AND CENTERED CONTROLS. SDR FGQ2004F00001Inertia Reel · crackedENERTIAL REEL FOR SHOULDER HARNESS MOUNT STRIPS CRACKED THROUGH TAPPED HOLES.SDR 2005FA0000101Exhaust Valve · seizedUPON TAKEOFF, PILOT REPORTED POWER LOSS AND ROUGH RUNNING ENGINE. INVESTIGATION FOUND NR 3 CYLINDERS EXHAUST VALVE SEIZED. THIS WAS 4TH OCCURENCE SINCE NEW (1999). INSTITUTED 300 HOUR VALVE GUIDE REAM AND 25 HOUR OIL CHANGE. MFG DENIED REQUEST TO INCREASE SDR 2004FA0000151Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000158Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000157Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TOT HE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000156Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000155Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000154Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000153Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000152Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000150Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000005Camshaft · spalledENGINE MAKING METAL, MFG DETERMINED IT TO BE CAMSHAFT/ LIFTER MATERIAL ENGINE RETURNED TO FACTORY FOR REPAIR. THIS IS THE SECOND OCCURRANCE OF CAMSHAFT/ LIFTER SPALLING AND 5TH OCCURANCE OF ENGINES MAKING METAL IN A FLEET OF 5. POSSIBLE MANUFACTURING AND MATSDR 2003FA0000249Skin · crackedBELLY SKIN CRACKED AT NUTPLATE FOR FAIRING AFT OF NOSE GEAR. CAUSED BY VIBRATION OF FAIRING. INCREASE STRUCTURE STRENGTH INSTEAD OF USING .025 2024 USE .032 2024 T-3.SDR 2004FA0000167Magneto · failedIT APPEARS THAT THE IMPULSE COUPLING FAILED, THEREFORE SEIZING THE MAGNETO AND SHEARING GUIDE SHAFT OF RETAINER GEAR ASSEMBLY AND BREAKING APART (INTO PIECES) THE RETAINER ASSEMBLY, ITSELF. SENDING PIECES OF METAL INTO THE ACCESSORY CASE AND POSSIBLY INTO THE
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