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 = 'U206D' 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 = 'U206D' 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 2013FA0000712Cylinder Head · unserviceableCYLINDER HEAD SEPARATED FROM CYLINDER BARREL WHILE IN LEVEL CRUISE FLIGHT. A SAFE LANDING WAS ACCOMPLISHED AT APPROXIMATELY 6 MILES FROM POINT OF FAILURE.SDR CA130220010Channel · corroded(CAN) DURING DISASSEMBLY FOR PAINT, CORROSION WAS NOTED UNDERNEATH THE BALANCE WEIGHT. AFTER REMOVAL OF THE BALANCE WEIGHT, CORROSION, HEAVY PITTING WAS FOUND ON THE MATING SURFACE OF THE CHANNEL. THE BALANCE WEIGHT CHANNELS ON THE RT AND LT ELEVATORS WERE RESDR CA130220008Hinge · corroded(CAN) DURING DISASSEMBLY FOR PAINT, THE RT AND LT ELEVATOR OTBD HINGES WERE FOUND TO BE UNSERVICEABLE DUE TO CORROSION. NEW HINGES INSTALLED TO RECTIFY DEFECT.SDR CA130220006Spar · corroded(CAN) DURING REMOVAL OF THE ELEVATOR ATTACHMENT HINGE FOR REPLACEMENT, CORROSION WAS FOUND ON BOTH OTBD ENDS OF THE HORIZONTAL STABILIZER REAR SPAR. THE AREA WAS REPAIRED IAW THE SRM TO RECTIFY DEFECT.SDR 2012FA0000275Cylinder Head · separatedJUST AFTER REACHING CRUISING ATTITUDE OF 2500 FT MSL, THE ENGINE BEGAN PRODUCING A LOUD NOISE, ACCOMPANIED BY LOSS OF POWER AND EXTREME VIBRATION. A SAFE LANDING WAS ACCOMPLISHED, WHERE IT WAS DETERMINED THT THE CYLINDER HEAD ON THE NR3 CYLINDER HAD SEPARATEDSDR WVBACL020311Push-Pull Cable · bindingFLAP PUSH PULL CONTROL CABLE, PN 9860058-7, WAS FOUND TO BE BINDING AND NOT MOVING SMOOTHLY IN ITS HOUSING. UPON REMOVAL OF CABLE, ALSO FOUND CRACKED T/E RIB, PN 0523233-6, DAMAGED AGAIN AFTER A VERY POOR PREVIOUS REPAIR. RIB WAS REPAIRED USING POORLY FORMEDSDR CA091026002Hub · cracked(CAN) DURING PROPELLER OVERHAUL PROCESS, EDDY CURRENT INSPECTION CARRIES OUT ON HUB UNIT THREADED BLADE SOCKET AREA`S AS PER. MANUFACTURER INSTRUCTIONS, WHERE THE INDICATIONS WERE FOUND. HUB REPLACED. (TC 20091026002)SDR CA090112004Selector · leaking(CAN) FUEL SELECTOR CLOSED DUE TO FLEX HOSES IN ENGINE COMPARTMENT BEING REPLACED. AFTER HOSES INSTALLATION FUEL SELECTOR OPEN TO CHECK FOR LEAKS, FUEL LEAK FOUND ON BELLY. FUEL SELECTOR WAS LEAKING ON THE TOP, SOURCE OF LEAK SHAFT ON THE TOP. SELECTOR WAS SDR CA020801011Muffler · separated(CAN) THE MUFFLER INSTALLED MAY 27, 2002 SEPARATED AT THE BELL FLANGE (UPPER ATTACH POINT). THE TAILPIPE CLAMP REMAINED CONNECTED. THE MUFFLER WAS REMOVED AND REPLACED ON JULY 4, 2002 WITH A NEW OVERHAULED MUFFLER AND NEW ATTACHING HARDWARE. THE AIRCRAFT WASSDR CA000928037Crankcase · failed(CAN) NR 2 MAIN BEARING HAD STARTED TO SPIN IN CRANKCASE CAUSING ALUMINUM IN FILTER. CRANKCASE SENT OUT FOR REPAIR. ENGINE ASSEMBLED WITH NEW CRANKCASE. (X)SDR CA000928036Lifter · chipped(CAN) A LARGE AMOUNT OF ALUMINUM WAS FOUND IN THE OIL SCREEN. A CYLINDER DIFFERENTIAL COMPRESSION CHECK WAS PERFORMED AND FOUND TO BE ALL ABOVE 70/80. STARTER DRIVE WAS REMOVED AND INSPECTED, NO DAMAGE FOUND AT THIS TIME (SUSPECTED USING ONLY A BORESCOPE). SDR CA000830042Hub · cracked(CAN) CRACK IN RETENTION THREAD. SEE MCCAULEY SB # 205BSDR CA000128042Cylinder · cracked(CAN) CYLINDER FOUND CRACKED AT UPPER SPARK PLUG HOLE MOVING FWD PAST THE INBRD SIDE OF THE INJECTOR HOLE.SDR AU000128042Cylinder · cracked(AU) CYLINDER FOUND CRACKED AT UPPER SPARK PLUG HOLE MOVING FORWARD PAST THE INBOARD SIDE OF THE INJECTOR HOLE.SDR CA951221012Strut Fitting · cracked(CAN)WHILE CARRYING OUT SEB 93-5 ON THE LOWER LEFT HAND DOOR POST STRUT FITTING, A CRACK WAS FOUND AT THE WING STRUT SUPPORT FITTING. CESSNA SERVICE KIT SK 206-42C WAS INSTALLED AND THE AIRCRAFT RETURNED T O SERVICE.SDR CA960312201Crankshaft · broken(CAN)ENGINE TEARDOWN FOLLOWING SUDDEN FAILURE. CRANKSHAFT BROKEN IN THREE PIECES. THE BREAKS ARE THROUGH THE NUMBER 4 AND 6 CRANK CHEEKS. ALSO SEVERE DAMAGE TO SEVERAL CONRODS, COUNTERWEIGHTS AND INTERIOR OF CASE. CRANKSHAFT DID NOT SHOW ANY SIGNS OF LACK OF
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