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 = '95A55' 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 = '95A55' 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 CA150113033Diaphragm · failed(CAN) FOUND ACCUMULATOR DIAPHRAGM FAILED, OIL ON PRESSURE SIDE.SDR CA141209004Elt · inoperative(CAN) WHILE TESTING THE ELT ON ITS ANNUAL CERTIFICATION AS PER CAR 571 APPENDIX G FOUND NO OUTPUT POWER OR MODULATION FOR THE 121.5 MHZ FREQUENCY. THE UNIT RETURNED FOR REPAIR.SDR 2004FA0000563Clip · failedLT THROTTLE CONTROL LEVER FAILED TO CHANGE POWER DURING CHANGE FROM TAKE-OFF TO CRUISE POWER SETTING. IT WAS DISCOVERED THT THE CRIMPING HAS FAILED ON THE CLIP THROTTLE CONTROL PN RA1039C WHICH IS PART OF THE THROTTLE CABLE ASSY PN 50-389012-15. THIS CLIP ISSDR IS4R269MCombustion Head · defectiveHEATER CORE RETURNED TO US BY CUSTOMER AFTER PURCHASING AN EXCHANGE/OVERHAUL HEATER. TEAR-DOWN/CLEANING OF CORE REVEALED COMBUSTION HEAD WITH A 3/16 X 1/4 INCH HOLE IN THE WALL OF THE COMBUSTION HEAD. THIS IS THE THIRD HEAD WE HAVE FOUND WITH A HOLE IN IT. A PSDR UZ22003F00000Cylinder · separatedNR 4 CYLINDER TOP CAME OFF OF BARREL IN FLIGHT UNKNOWN CAUSE OR HOW TO PREVENT.SDR 2003FA0000827Drain · failedQUICK DRAIN FAILED, CAUSING TOTAL LOSS OF ENGINE OIL. AFTER SHUTDOWN OF ENGINE, BROKEN OFF PART WAS FOUND. AFTER REMOVING OIL PAN, ENGINE OIL WAS CHECKED AT TIME OF OIL LOSS AND HAD 4 QUARTS REMAINING, BUT WAS STILL DRAINING.SDR CA020719005Skin · cracked(CAN) WHILE COMPLETING A 100 HR INSPECTION THE LEADING EDGE SKIN OF FLAP WAS FOUND CRACKED AT ACTUATOR ATTACH POINT.CRACKS EXTENDED INBOARD & OUTBOARD APPROXIMATELY 1INCH FROM THE FORWARD ATTACHMENT HOLE FOR FLAP ACTUATOR. - CRACKS WERE DETECTED AFTER CLEANINGSDR 2002FA0000134Shock Mount · missingFOUND RIGHT FORWARD ENGINE VIBRATION ISOLATOR MOUNT AND ATTACH HARDWARE MISSING FROM RIGHT ENGINE.SDR CA010627053Bolt · failed(CAN) UPON MPI IT WAS FOUND THAT 2 OF 4 WING BOLTS FAILED INSPECTION. IT WAS THANDETERMINED TO CHANGE ALL THE BOLTS. LOG ENTRY INDICATES BOLTS WERE LAST CHANGED IN 1992. THER IS NO RECORD OF BOLT INSPECTION SINCE THAT TIME ALTHOUGH INSPECTION IS CALLED FOR AFTSDR CA010625052Retainer · missing(CAN) DURING SCHEDULED MAINTENANCE IT WAS FOUND THAT THE LOWER CONTROL ARM RETAINER WAS MISSING. UPON FURTHER INVESTIGATION, IT WAS FOUND LYING IN THE BELLY OF THE AIRPLANE. IT WAS ALSO NOTED THAT THE UPPERCONTROL ARM RETAINER WAS ATTACHED WITH ONLY ONE OF TWOSDR 20001229SH008Bearing · delaminatedENGINE WAS DISASSEMBLED FOR PROPELLER STRIKE INSPECTION, FOUND NR 6 ROD BEARING SURFACE MATERIAL DELAMINATING FROM BEARING EXPOSING BABBITT MATERIAL AND REMAINING BEARINGS SHOWING SIGNS OF THIS CONDITION FORMING ON THEM. ALL BEARINGS WERE SENT TO TELEDYNE CONSDR 20000505SH006Connecting Rod · bentNR 6 EXHAUST PUSHROD BENT, BROKEN AND WORN HALFWAY THRU FROM RUBBING ON INSIDE OF THE PUSHROD HOUSING. NR 6 INTAKE PUSHROD BROKEN IN TWO. CYL HAS 190 HRS SINCE NEW AND BOTH VALVES MOVED FREELY IN GUIDES. NR 6 CONNECTING ROD FOUND VISIBLY BENT. INTAKE MANIFSDR 20000505SH005Pushrod · bentNR 6 EXHAUST PUSHROD BENT, BROKEN AND WORN HALFWAY THRU FROM RUBBING ON INSIDE OF THE PUSHROD HOUSING. NR 6 INTAKE PUSHROD BROKEN IN TWO. CYL HAS 190 HRS SINCE NEW AND BOTH VALVES MOVED FREELY IN GUIDES. NR 6 CONNECTING ROD FOUND VISIBLY BENT. INTAKE MANIFSDR 99ZZZX2758Blade · crackedBLADE CRACKED IN THE V-SHANK AREA OF PROPELLER.SDR AU990110Bracket · broken(AUS) GENERATOR MOUNT BRACKET BROKEN AT BOTH ENDS. GENERATOR UPPER STAY ALSO BROKEN. LOWER STAY WORE THROUGH THE BRASS ELBOW ON THE FUEL PUMP.SDR 98ZZZX2166Rod Bolt · failedROD BOLT WAS MAGNAFLUXED AND CLEANED 75.8 HOURS PRIOR TO FAILURE. TT UNKNOWN, SUSPECT UNDETECTED METAL FATIGUE. BOLT BROKE UNDER FULL POWER AND HIGH RPM. SUGGEST CHANGING OUT ROD BOLTS WITH NEW BOLTS AT EACH MAJOR OVERHAUL.SDR 97ZZZX4866Control Cable · brokenRIGHT MIXTURE CABLE WORKING FINE AND SMOOTH. MADE FLIGHT, ENGINE WOULD NOT SHUT DOWN. FOUND CABLE BROKEN AT WELD JOINT ON ENGINE END UNDER SOLID SHEATH. INSTALLED NEW CABLE.SDR 98ZZZX116Control Cable · failedMIXTURE CABLE FAILED ON SHUT DOWN AFTER FLIGHT. NO PREVIOUS INDICATION OF PROBLEM. INSPECTION SHOWED UNDER SHEATH WELD BROKE THAT SECURES SOLID END TO CABLE PORTION. CANNOT INSPECT HERE DUE TO SHEATH COVERING. NEW SAME PART NUMBER INSTALLED.SDR EY2R9601174Split Bearing · corrodedCORROSION FOUND ON SPLIT BEARING.SDR EY2R9600912Ferrule · corrodedFERRULE CORRODED.SDR 95ZZZX829Elt · corrodedTHIS UNIT WAS REMOVED FOR INSPECTION PER 91.207(D) DURING ANNUAL INSPECTION. CORROSION (WHITE POWDER TYPE RESIDUE AROUND NEG. TERMINAL, BLUE RESIDUE INSIDE NEG. TERM.) WAS FOUND DURING INSPECTION OF CIRCUIT BOARD. UNIT WAS RECOND. AND CERTIFIED BY MANUFACTUR
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