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 = '35C33' 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 = '35C33' 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 2019FA0000248Stop Pin · backed outTHE FULL RICH STOP PIN ON FUEL INJECTION CONTROL ASSEMBLY (PN 629904-2A11) BACKED COMPLETELY OUT AFFECTING THE MIXTURE WHEN THE MIXTURE CONTROL WAS IN THE FULL RICH POSITION. THE RESULT WAS REDUCED POWER AT FULL THROTTLE THAT WAS RECOVERED BY ADJUSTING THE MIXSDR 2016FA0000036Pickup · failedELECTRIC MAGNETO FAILED. TROUBLESHOOT FOUND MAGNETIC PIC-UP CIRCUIT OPEN. REPLACED WITH NEW AND RUN CHECK SATISFACTORY. REMOVED PART APPEARS TO HAVE DEBONDED FROM CYLINDER AND THERE IS EVEDENCE THAT IT CONTACTED THE CRANK TRIGGER. OAT TEMPERATURE WAS JUST SDR 2015FA0000059Piston · brokenDURING AN ANNUAL INSPECTION, THE QUICK DRAIN OIL DRAIN VALVE WOULD NOT LOCK OPEN. A BLOCK OF WOOD WAS USED TO WEDGE UNDER THE DRAIN VALVE TO HOLD IT OPEN. AFTER THE OIL WAS DRAINED, THE VALVE WAS REMOVED AND THE VALVE LOCKED OPEN NORMALLY. LOOKED UP INTO THSDR 2010FA0000060Hub · mismanufacturedPROPELLER FACTORY NEW IN 12/10/99. PROPELLER HUB FOUND AT O/H TO BE UNAIRWORTHY DUE TO CYLINDER HOLES DEPTH DRILLED BY FACTORY TOO DEEP. 3 SMALL DIMPLES NOTED ON UNDERSIDE OF HUB ON INSPECTION. MFG HAS REJECTED HUB. FACTORY HAD TO HAVE IMPROPERLY DRILLED HUSDR 2008FA0000907Cylinder · crackedANNUAL INSP REVEALED A LARGE QUANITY OF VERY BLACK OIL RUNNING DOWN THE ENGINE MOUNT LEG AND AIRFRAME STRUCTURE. FURTHER INVESTIGATION FOUND THE LEAK TO ORIGINATE AT THE HEAD TO BARREL CONNECTIONS OF CYLINDERS NR 1, AND NR 3. COMPRESSION CHECK USING AN INPUTSDR 2008FA0000714V-Belt · departedPILOT REPORTED LOSS OF ELECTRICAL POWER IN CRUISE FLIGHT DURING NIGHT VFR. V-BELT OBSERVED MISSING FROM ACCESSORY CASE ABSENT FROM ALTERNATOR PULLEY. V-BELT APPARENTLY LOST IN FLIGHT THROUGH OPENING IN LOWER COWLING. OWNER REPORTS THAT ONLY 25-30 HOURS WAS PUTSDR 2003FA0001005Adapter · wornENGINE DEVELOPED OIL LEAK, FOUND THIS ADAPTER LEAKING AT THREADS, LOCKING NUT SAFETY WAS INTACT, TORQUE DOPE WAS INTACT. ALL REQUIREMENTS OF AD 96-12-22 WERE MET AS PREVIOUSLY INSPECTED 18 HOURS BEFORE FAILURE.SDR AUS20030676Spar · corroded(AUS) WING SPARS PN 35110061-1 (LT) AND PN 351100612 (RT) CONTAINED EXFOLIATION CORROSION IN THE UPPER AND LOWER SPAR CAPS.SDR 2001FA0000367Antenna · crackedA/C ARRIVED WITH AN ANTENNA 'FLUTTERS' SQUAK. UPON INSPECTION OF VHF COMM ANTENNA, IT WAS NOTED THAT THE ANTENNA WAS INSTALLED WITH NO SUPPORTING DOUBLER. UPON ANTENNA REMOVE, A 5.5 INCH RADIAL CRACK WAS DISCOVERED AROUND THE ANTENNA BASE. THE ADJOINING STRSDR 2001F00363Antenna · crackedAIRCRAFT ARRIVED WITH AN ANTENNA 'FLUTTERS' SQUAWK. UPON INSPECTION OF VHF COMM ANTENNA, IT WAS NOTED THAT THE ANTENNA WAS INSTALLED WITH NO SUPPORTING DOUBLER. UPON ANTENNA REMOVAL, A 5.5 INCH RADIAL CRACK WAS DISCOVERED AROUND THE ANTENNA BASE. THE ADJOINSDR SW15200110536Bulkhead · crackedDURING 100 HOUR INSPECTION FOUND CRACKS IN THE DOUBLER TAIL, A CRACK ON THE RIGHT HAND SKIN SECTION AND A CRACK ON THE AFT BULKHEAD APPROX 1 INCH AT THE BEGINNING OF THE RADIUSED AREA RADIATING OUTBOARD .7500 ON THE RIGHT SIDE AND .5000 ON THE LEFT SIDE. THESDR SW15200110535Bushing · improper partTHE INCORRECT BUSHING WAS IDENTIFIED DURING DEMINSIONAL INSPECTION OF THE COUNTER- WEIGHT PRIOR TO INSTALLATION.SDR SW15200110531Doubler · crackedDURING 100 HOUR INSPECTION FOUND CRACKS IN THE DOUBLER TALL PN 002440000143. THE DOUBLER IS CRACKED JUST FORWARD OF THE AFT BULKHEAD APPROX 1 INCH JUST BEFORE THE RADIUSED AREA EXTENDING OUTBOARD .2500.SDR 20000620SH031Bulkhead · crackedCRACKS FORMED AROUND 4 OF ATTACHING BOLTS IN BULKHEAD IN USE LESS THAN 100 HOURS. ATTACHING FLANGE APPEARS TO BE RUBBING AGAINST HUB. FLANGE IS MISFORMED. MANUFACTURING DEFECT. (X)SDR AU990714Spar · corroded(AUS) LEFT AND RIGHT WING UPPER SPARS CONTAINED SEVERE INTERGRANNULAR CORROSION. ON THE LT WING A SECTION OF THE REAR HINGE HAD BEEN REMOVED WITH NO MATERIAL REPLACED. ON THE RT WING A SUSPECT REPAIR HAD BEEN CARRIED OUT WITH A DOUBLER ADDED. SUBMITTER SUSPESDR AU980599Bracket · corroded(AUS) LT MAIN LANDING GEAR UPLOCK BRACKET CORRODED IN THE AREA OF THE UPLOCK PIVOT POINT. PART 5,634.SDR AU980158Valve · leaking(AUS) NO1 CYLINDER EXHAUST VALVE LEAKING AND VALVE GUIDE WORN (STILLWITHIN LIMITS). NO3 CYLINDER INLET VALVE LEAKING.SDR AU971466Hose · faulty(AUS) ALL FLUID HOSES IN ENGINE COMPARTMENT NOT PROTECTED BY FIRE SLEEVES. PERSONNEL/MAINTENANCE ERROR.SDR 97ZZZX3154Hub · crackedPROPELLER RECEIVED FOR INSPECTION OF RED DYE OIL LEAK (SMALL). DISASSEMBLED PROPELLER, INSPECTED HUB WITH 10X POWER MICROSCOPE, FOUND CRACK IN NR 2 BLADE SOCKET, LAST THREAD IN 8 O'CLOCK POSITION, 1.50 INCHES TO 2 INCHES LONG. NOTE: THIS PROPELLER HAS TTSN SDR 97ZZZX1200Shuttle Valve · failedCHECK VALVE FAILED ON ENGINE DRIVEN VACUUM PUMP. SIDE RIVET HEAD SEPARATED FROM VALVE ASSEMBLY. RENDERED VALVE INOP.SDR 95ZZZX3611Spar · crackedPERFORMING AD 93-24-03 FOUND UPPER RUDDER SPAR CRACKED.SDR 96ZZZX960Spar · crackedPERFORMING AD 93-24-03 FOUND CRACKED RUDDER SPAR UNDER UPPER HINGE BRACKET.SDR 95ZZZX946Hub · crackedPROPELLER IN FOR 5 YEAR TBO FOUND DURING OHC. FOUND HUB CRACKED.
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