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 = 'PA24' 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 = 'PA24' 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 VNAA202209209992None · corrodedFLOOR SEAT RAIL AT LBL9 BETWEEN FS 485.00 AND 571.00 IS CORRODED.SDR 2020FA0000200Propeller · departedAFTER THE RUNUP AND TAKEOFF CHECKLIST COMPLETE, I ACCELERATED TO ALMOST ROTATION SPEED WHEN I HEARD A LOUD BANG. I IMMEDIATELY RETARDED THE THROTTLE TO IDLE AND BROUGHT THE AIRPLANE TO A CONTROLLED STOP ADJACENT TO, BUT OFF THE RUNWAY. THE AIRPLANE NEVER LEFSDR 2019FA0000119Mount · corrodedINTERNAL CORROSION OF THE ENGINE MOUNT ASSEMBLY P/N 20796-00.SDR 2012FA0000698Exhaust Stack · erodedTHE PILOT MADE AN INTENTIONAL GEAR-UP LDG AFTER SEVERAL UNSUCCESSFUL ATTEMPTS TO FULLY EXTEND THE LANDING GEAR. FOLLOW-UP INSPECTION OF THE ACFT REVEALED THAT A SECTION OF THE LEFT-FRONT EXHAUST STACK ASSY HAD FAILED AND SEPARATED FROM THE ENGINE EXHAUST SYS,SDR 2009FA0000762Bulkhead · crackedFOUND AFT VERTICAL FIN SPAR TO BULKHEAD BRACKET CRACKED AT STA 258.75. THIS PROBLEM HAS BEEN ADDRESSED BY AD 74-16-08 AND MFG SL 679 ON OTHER SERIES ACFT BUT NOT ON THIS ONE. (K)SDR 2007FA0000484Carburetor · wornTHE ACCELERATOR PUMP IN THE CARBURETOR FAILED. INSPECTION SHOWED THAT THE PUMP HEAD GLAND HAD SHRUNK, SO THAT IT DID NOT PROVIDE A SEAL BETWEEN THE CARBURETOR BODY AND THE PUMP ITSELF. THE RESULT WAS THAT ADVANCING THE THROTTLE DID NOT CAUSE FUEL TO BE SQUIRSDR 2005FA0001216Transmission · failedLANDING GEAR RETRACT SYS WOULD NOT EXTEND GEAR TO A DOWN AND LOCKED POSITION. SEVERAL ATTEMPTS TO CYCLE GEAR POPPED GEAR MOTOR CIRCUIT BREAKER. TRANSMISSION DECOUPLER RELEASED WHEN EMERGENCY GEAR EXTENSION WAS ATTEMPTED, GEAR WOULD NOT GO TO DOWN AND LOCKED SDR 2003FA0000835Wire · frayedREPLACED W2094304, DUE TO 4 FRAYED WIRES. FOUND AT ANNUAL. LOCATION , BEHIND LEFT GEAR WELL COVER WHERE CABLE COMES INTO WING.SDR 2004FA0000610Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE SDR 2002FA0001098Bolt · corrodedDURING ANNUAL INSPECTION STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS (PN AN175C33A) THAT ATTACHES THE STSDR 20001204SH013Stack · brokenTHE PIPER COMANCHE BROKE THE RT REAR EXHAUST STACK INSIDE THE CARBURETOR HEAT MUFF. THE PIPE BROKE INSIDE THE CUFF THAT IS WELDED TO THE STACK FOR THE MUFF TO ATTACH TO CAUSING THE STACK TO DROP AND ERODE ITS WAY THROUGH THE MUFF. THE HEAT BEING DIRECTED INSSDR 99ZZZX2930Indicator · malfunctionedFOUND BLACK AND WHITE LIGHTING WIRES SHORTED TOGETHER. THIS OCCURRED AT THE BASE OF THE LIGHTING BAR, A POSITION THAT THE MANUFACTURER WOULD HAVE ASSEMBLED AT THE FACTORY. THESE UNITS HAVE OPTIONAL LIGHTING CAPABILITIES. THE SHORT OCCURRED ON THE ASSEMBLY THSDR 98ZZZX2184Stack · brokenJUST AFTER TAKEOFF, PILOT REPORTED SMOKE IN THE COCKPIT. HE DELCARED AN EMERGENCY LANDING. AFTER TOUCH-DOWN AND REDUCING POWER, SMOKE CLEARED. AFTER SHUT DOWN, REMOVED COWLING AND FOUND EXHAUST PIPE OFF OF MUFFLER. FOUND EXHAUST PIPE BROKEN AFT OF NR 3 RISSDR 98ZZZX846Mount · crackedDISCOVERED CRACKED HORIZONTAL TUBE MEMBER ON ENGINE MOUNT. THE CRACKED MEMBER IS THE .50 INCH DIAMETER TUBE RUNNING FROM THE OUTSIDE .6250 INCH TUBE TO THE CENTER LANDING GEAR MOUNTING POSITION. THIS CONDITION WAS DISCOVERED DURING AN ANNUAL INSPECTION. NO SDR 97ZZZX4489Hub Spider · crackedCUSTOMER PURCHASED PROPELLER NEW IN 1977. IN 1991 WITH 639 HOURS, PROPELLER STRUCK A TOW BAR RESULTING IN MINOR BLADE DAMAGE. PROP WAS TAKEN IN FOR REPAIR AND AD 73-02-01 WAS C/W. IN SEPTEMBER OF 1977 WITH 876 TT HOURS, PROP WAS BROUGHT IN FOR ROUTINE OVERHSDR AU970613Throttle · wrong part(AUS) SUSPECT INCORRECT THROTTLE CONTROL FITTED - NO MICROSWITCH IS FITTED FOR THE UNDERCARRIAGE WARNING SYSTEM AND THE WIRING IS SECURED BEHIND THE INSTRUMENT PANEL - PERSONNEL/MAINTENANCE ERROR - UNAPPROVED PARTSDR CA970527013Bearing Balls · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADE BEARING BALLS WERE FOUND CORRODED AND REMOVED FROM SERVICE.SDR AU960848Switch · seized(AUS) LANDING GEAR WARNING MICROSWITCH SEIZED IN 'SAFE' POSITIONSDR CA960604001Motor · burnt(CAN) LANDING GEAR REFUSED TO EXTEND AND LOCK. EMERGENCY EXTEND SUCCESSFUL. ELECTRICAL MOTOR BURNT OUT.SDR EY2R9600538Pilot Tube · corrodedPILOT TUBE FOUND WITH CORROSION.SDR EY2R9600369Pilot Tube · corrodedPILOT TUBE FOUND CORRODED.SDR EY2R9600368Bearing · corrodedBEARING FOUND CORRODED.SDR 96ZZZX753Transmission · crackedTHE ALUMINUM CASTING OF THE MLG TRANSMISSION (PN 25720-002) WAS CRACKED IN 4 PLACES AND VERY CLOSE TO COMPLETE FAILURE. FAILURE OF THE HOUSING WOULD POSSIBLY CAUSE THE LANDING GEAR TO LOCK IN ANY POSITION. THE CRACKS WERE DISCOVERED DURING A GEAR RETRACTION
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