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 = 'PA31P' 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 = 'PA31P' 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 97ZZZX4206Bearing · flakedENGINE REMOVED AFTER FINDING BEARING MATERIAL IN OIL SCREEN. DISASSEMBLED, FOUND ABOUT 1.5 SQUARE INCHES OF MATERIAL FLAKED OFF OF BEARING. SUSPECT POOR BOND TO BEARING.SDR 97ZZZX3868Pump · inoperativeLEFT MAIN TRANSFER PUMP OVERHAULED BY 2-14-96, INSTALLED 7-8-96. PUMP INOPERABLE. SENDING TO RAPCO FOR DETERMINATION OF PROBLEM. SHORT SERVICE LIFE.SDR 97ZZZX3163Stud · failedFOUR CYLINDER ATTACH STUDS ON NR 3 CYLINDER FOUND BROKEN FOLLOWING ENGINE RUNNING ROUGH. FOUND NO EVIDENCE OF DETONATION ON TEAR DOWN.SDR 97ZZZX3151Valve Seat · looseLEFT ENGINE RUNNING ROUGH. CHECKED COMPRESSION, 0/80, NR 3 CYLINDER. CHECKED WITH BORESCOPE, FOUND EXHAUST VALVE SEAT LOOSE. REMOVED CYLINDER ASSY WHICH WAS OVERHAULED BY ECI. SUSPECT FIT BETWEEN CYLINDER AND SEAT WAS NOT TIGHT ENOUGH AT ASSEMBLY.SDR AU971332Cylinder · cracked(AUS) ENGINE CYLINDER CRACKED FROM INDUCTION TUBE FACE TOWARDS THE INLET VALVE SEAT. CRACK LENGTH 31.75MM (1.25IN)SDR AU971333Cylinder · cracked(AUS) ENGINE CYLINDER CRACKED FROM INDUCTION TUBE MOUNT FACE TOWARDSTHE INLET VALVE SEAT. CRACK LENGTH 25.4MM (1IN).SDR 97ZZZX2337Diaphragm Valve · looseSCREW THAT SECURES NEEDLE VALVE TO DIAPHRAGM IN FUEL PRESSURIZATION VALVE CAME LOOSE ALLOWING NEEDLE VALVE TO COME LOOSE WHICH SHUT ENGINE DOWN. SCREW STILL HAD EVIDENCE OF LOC-TITE ON THREADS. SUSPECT THAT FUEL MAY HAVE SOFTENED LOC-TITE WHICH ALLOWED SCREWSDR 97ZZZX2052Cylinder · crackedDURING ROUTINE MAINTENANCE, NR 1 AND NR 3 CYLINDERS WERE FOUND CRACKED IN THE INTAKE PORT AREA. CRACKS WERE BETWEEN FIRST AND SECOND COOLING FINS FROM THE TOP AND PROGRESSED TO THE THINNER AREA OF THE PORT. CRACKS NOTED BY A GREENISH TO BLACK STAIN LOOKING FSDR 97ZZZX2051Cylinder · crackedDURING ROUTINE MAINTENANCE, NR 1 AND NR 3 CYLINDERS WERE FOUND CRACKED IN THE INTAKE PORT AREA. CRACKS WERE BETWEEN FIRST AND SECOND COOLING FINS FROM THE TOP AND PROGRESSED TO THE THINNER AREA OF THE PORT. CRACKS NOTED BY A GREENISH TO BLACK STAIN LOOKING FSDR 97ZZZX2050Cylinder · crackedDURING MAINTENANCE WITH INTAKE PIPE REMOVED, INTAKE GUIDE WAS FOUND MOVING WITH THE VALVE. CYLINDER REPLACED, TEAR DOWN REPORT REQUESTED FROM ENGINE OVERHAULER. REPORT STATED A CRACK HAD CAUSED THE PROBLEM. OUT OF 4 ENGINES OF THIS TYPE MAINTAINED BY THIS FSDR 97ZZZX1945Alternator · failedALTERNATOR FAILED AT 5-1/2 MONTHS AND 185.3 HRS TT. WAS OVERHAULED 9-19-96. CONTINUE TO HAVE VERY SHORT SERVICE LIFE OF THESE UNITS.SDR 97ZZZX1218Alternator · shaft failedALTERNATOR QUIT WORKING. REMOVED, FOUND SHAFT THROUGH ROTOR ASSY WOULD TURN WITHOUT TURNING ROTOR. UNIT OVERHAULED 1-13-97.SDR 97ZZZX1217Starter · shortedSTARTER INOPERABLE. FOUND SHORTED OUT. TIME 341.1 HOURS SMOH. ONE YEAR IN SERVICE.SDR 97ZZZX817Crankshaft · fracturedAT OIL CHANGE 7 FERROUS PIECES .430 INCH LONG .095 INCH THICK AND BETWEEN .125 INCH AND .250 INCH WIDE WERE FOUND IN SUCTION SCREEN ALONG WITH ALUMINUM SHAVINGS. OIL PAN REMOVAL AND VISUAL INSPECTION REVEALED A BROKEN CORNER OFF THE COUNTERWEIGHT BLADE ON THESDR 96ZZZX6140Gear Tooth · brokenENGINE SOUNDED ROUGH ON SHUT DOWN. FOUND EXCESSIVE PLAY IN PROPELLER. DRAINED OIL, PULLED SUCTION SCREEN, FOUND PIECE OF TOOTH IN SCREEN. ENGINE TORN DOWN, FOUND BROKEN TEETH ON PROP SHAFT DRIVE GEAR, ALSO, DRIVE GEAR DAMAGED. SUBMITTER SUSPECTS PREVIOUS CSDR 96ZZZX6139Pump · failedVAC PUMP REMOVED FOR ENGINE REPAIR. SHAFT VERY HARD TO TURN AND UNIT SQUEALED.SDR 96ZZZX6099Counter Weight · crackedPULLED SUCTION SCREEN FOLLOWING OIL CHANGE, FOUND BROKEN PIECE OF SNAP RING, P/N 71906. REMOVED SUMP, FOUND COUNTER WT NR 5 SNAP RING AFT SIDE INBOARD BROKE AND COUNTER WT CRACKED AT BUSHING HOLE. SCREEN WAS PULLED FOLLOWING FAILURE OF NR 5 CYL (DROPPED EXHASDR 96ZZZX6082Valve Seat · looseENGINE RUN-UP AND ROUGH. CHECKED COMPRESSION, FOUND NR 5 CYLINDER 0/80. REMOVED CYLINDER, FOUND EXHAUST VALVE SEAT LOOSE IN HEAD FOLLOWING VALVE DURING VALVE MOVEMENT.SDR 96ZZZX5901Dowel · looseFOUND DOWEL FOR CRANKSHAFT SPLINE BUSHING IN SUMP AT OIL SCREEN. UPON TEAR DOWN FOUND ONLY 1 OF 3 DOWELS STILL IN CRANKSHAFT. BUSHING WAS STARTING TO TWIST IN BETWEEN CRANKSHAFT AND SPLINE BUSHING. NO OTHER INDICATION OF PROBLEMS. ENGINE RAN GOOD, FILTER WSDR 96ZZZX5837Pump · shaft shearedPUMP WAS INSTALLED ON FRESH O/H ENG 9-15-95, PUMP NEW FROM AIRBORNE, FAILED AT 369.6 HRS 10-30-96. SEIZED AND SHEARED SHAFT. FAILURE RATE ON THESE PUMPS FROM SUBMITTERS EXPERIENCE IS QUITE HIGH. ABOUT 50 PERCENT FAIL JUST PAST THIS WARRANTY TIME OF 1 YR OR SDR 96ZZZX4142Cylinder · crackedHOBBS - 3,213.6 HOURS. OIL APPEARED AROUND NR 1 CYLINDER PUSH ROD TUBES. SEALS REPLACED, GROUND CHECK OPS GOOD. AFTER FLIGHT, OIL APPEARED AGAIN. REMOVED NR 1 CYLINDER, FOUND CYLINDER SLEEVE CRACKED APPROXIMATELY THREE-FOURTHS OF CIRCUMFERENCE. LOG REVEALSDR EY2R9601489Hub · damagedPROP ASSY HUB DAMAGEDSDR 96ZZZX1513Pump · shaft failedDRIVE COUPLING SHEARED FOLLOWING PUMP FAILURE. PUMPS SEEM TO ONLY RUN ABOUT 400 HOURS PRIOR TO FAILURE. SUBMITTER HAS 5 AIRCRAFT RUNNING 2 EACH PER AIRCRAFT.SDR 96ZZZX787Control Cable · brokenRIGHT PROPELLER CONTROL CABLE BROKE ABOUT 12 INCHES AFT OF GOVERNOR ATTACHMENT. NO PRIOR INDICATION OF CABLE FAILURE. PROPELLER CONTROL OPERATED SMOOTHLY.SDR 96ZZZX479Valve · loose crimp nutINSPECTION OF OIL TEMPERATURE BYPASS VALVE REVEALED LOOSE NUT. REF: LYC SB 518C, 5-2-95. THIS SB LISTS P/N 53E19980, S/N 159, AND HIGHER AS N/A. SUBMITTER SUGGESTS SB BE REVISED TO INCLUDE ALL PART NUMBERED AND SERIAL NUMBERED VALVES UNTIL LATEST STYLE PARSDR 95ZZZX6542Clamp · crackedFOUND CLAMP CRACKED DURING INSPECTION OF ALL EXHAUST COMPONENTS FOR CONDITION FOLLOWING PURCHASE OF AIRCRAFT BY CUSTOMER. ADVISE CLAMPS BE INSPECTED VERY CLOSELY AS THIS CLAMP LOOKED LIKE A GOOD CLAMP UNTIL CLOSE INSPECTION REVEALED APPROXIMATELY A 2 INCH CRASDR 95ZZZX6767Cylinder · boss brokenEXHAUST VALVE INBOARD ROCKER ARM SHAFT BOSS BROKEN OFF CYLINDER ASSY. ROCKER ARM AND SHAFT LIFTED UP CRACKING CYLINDER ON OUTBOARD SIDE WHERE SHAFT PASSES THROUGH CYLINDER. SUBMITTER SUSPECTED DEFECTIVE CASTING AS THERE IS NO EVIDENCE OF PREVIOUS CRACK.SDR 95ZZZX6403Pump · shaft shearedPRESSURE PUMP SHEARED DRIVE SHAFT. UNIT SEIZED.SDR 95ZZZX6402Cylinder · boss brokenNR 5 CYLINDER ON LT ENGINE INBOARD EXHAUST ROCKER SHAFT ARM BOSS BROKE OFF CYLINDER. NO EVIDENCE OF PREVIOUS CRACK. NO INDICATION OF VALVE CONTACTING PISTON. SUSPECT CASTING DEFECT AT MANUFACTURER.SDR 95ZZZX5935Turbocharger · oil lossENGINE LOST OIL PRESSURE ON APPROACH TO AIRPORT. UPON INSPECTION ON THE GROUND, FOUND NO OIL IN ENGINE. OIL ON TURBO CENTER HOUSING AND OVERBOARD EXHAUST STACK. FOUND NO OTHER EVIDENCE OF LEAKAGE. PRESSURE TESTED ALL OIL LINES AND HOSES, FOUND NO OTHER LEASDR 95ZZZX5601Stack · brokenNR 6 EXHAUST STACK BROKEN AT FLANGE. LEAKING EXHAUST GASSES DAMAGED WIRING AND COWL NEXT TO STACK. PROBLEM OCCURRED DURING CLIMB-OUT, ENGINE WAS SECURED AND AIRCRAFT LANDED WITHOUT INCIDENT. TIME ON STACK UNKNOWN. BREAK APPEARED TO HAVE OCCURRED OVER A SHOSDR 96ZZZX716Breaker Points · not openingMAGNETO DEFECTIVE. BREAKERS NOT OPENING AT THE CORRECT GAP. ALSO, NOT LUBRICATED. NEED TO LUBRICATE BREAKERS AND SET CORRECT GAP. ALSO, FOUND BAD CAPACITOR.SDR 95ZZZX3458Crankcase · bolts looseENGINE OVERHAULED 2-3-94. INSTALLED IN AIRCRAFT 4-1-94. AT 1,800 RPM CRUISE POWER, OIL PRESSURE AT 55 PSI, 190 DEGREES, OIL TEMPERATURE, WHICH IS ON THE TOP OF YELLOW ARC, BOTTOM OF GREEN ARC, AT HIGHER OIL TEMP, OIL PRESSURE WOULD DROP INTO YELLOW ARC. REMSDR 95ZZZX4313Downlock Hook · bindingDURING ROUTINE FLT, LT MLG FAILED TO EXTEND PROPERLY. GREEN 'DOWN & LOCKED' LIGHT FAILED TO ILLUM & RED 'TRANSITION' LIGHT REMAINED LIT. AFTER DETERMINING GRN LIGHT NOT AT FAULT & UNSUCCESSFUL ATTEMPTS TO EXTEND GEAR (MANUAL EXTENSION, G-LOADING, FISH-TAILINSDR 95ZZZX1891Crankshaft · ctweight failedDURING CRUISE, LT ENGINE LOST POWER, OIL PRESSURE OKAY. ENGINE SHUT DOWN AND SAFE LANDING MADE. FOUND BOLTS BROKE ON NR 3 CYCLINDER CONNECTING ROD. ALSO, NR 4 COUNTERWEIGHT BROKE LOOSE FROM CRANKSHAFT DUE TO FAILURE OF ATTACH POINT ON CRANKSHAFT. NO PRIOR SDR 95ZZZX1221Valve Cover · crackedOPERATOR/OWNER COMPLAINED OF OIL LEAK ON LEFT ENG. REMOVED COWLING AND FOUND OIL AROUND 2-4-6 CYLINDER AREAS. WASHED DOWN ENGINE. RAN AND SHUT DOWN ENGINE, FOUND OIL SEEPING FROM AROUND NR 4 CYLINDER VALVE COVER/GASKET. WASHED AREA AND RAN ENGINE AGAIN. F
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