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 = '310J' 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 = '310J' 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 2023FA0000263Roller · seizedNOSE LANDING GEAR STRAIGHTENER CAM ROLLER PN CR10-1 SEIZED WHICH BENT THE NOSE LANDING GEAR STRAIGHTENER PN 0842000-58 BRACKET CAUSING NOSE LANDING GEAR TO BE UNABLE TO CENTER AAND UNABLE TO EXTEND OR RETRACT FULLY. AIRCRAFT LANDED WITH MLG RETRACTED AND NLG PSDR LCPR20220119001None · defectiveAFTER INCIDENT ON 12/21/2021 AT KBCT. PER REQUEST AIRCRAFT WAS JACKED AND FUNCTIONAL CHECKS (GEAR SWINGS) WERE PERFORMED ON THE AIRCRAFT. AFTER MULTIPLE FUNCTIONAL CHECKS (GEAR SWINGS) IT WAS FOUND THAT THE NOSE GEAR WOULD NOT LOCK OUT AND A GRINDING NOISE WASSDR 2007FA0000195Limit Switch · failedUP LIMIT SWITCH FAILED ON LANDING GEAR ACTUATOR, CAUSING OVER EXTENSION OF NOSE GEAR SYSTEM. THIS CAUSED THE INTERMEDIATE TORQUE TUBE TO BEND. (K)SDR 2005FA0001244Attach Fitting · corrodedDURING THE ANNUAL INSPECTION, THE WING FITTING WAS FOUND TO BE CORRODED SO SEVERE THAT IT WAS ALMOST .2500 OF THE WAY THRU THE FITTING. PICTURES ENCLOSED THAT SHOW DAMAGE. FITTING WAS LOCATED ON THE LT SIDE, AFT TOP FITTING. (K)SDR 310EESupport Bracket · brokenRH LANDING GEAR COLLAPSED ON LANDING. FOUND THAT THE UPPER BELLCRANK BRACKETT P/N 0811303-1 WHICH SUPPORTS AND GUIDES THE RT MAIN LANDING GEAR PUSH/PULL TUBES FROM GEAR BOX TO GEAR ASSEMBLY SEPERATED FROM BULKHEAD DUE TO MOUNTING RIVET FAILURE. THIS SEPERATIONSDR 2003F00141Switch · failedON APPROACH TO ELP THE PILOT DID NOT HAVE A GREEN LIGHT AFTER SELECTING GEAR DOWN. A FLY BY INDICATED GEAR APPEARED IN NORMAL DOWN POSITION. PILOT LANDED WITHOUT INCIDENT. THE LEFT HAND MICRO SWITCH PN 1SE3-3 FAILED INTERNALLY. REMOVED AND REPLACED SWITCH.SDR 2001FA0000595Bushing · separatedRIGHT MAIN LANDING GEAR UPPER AND LOWER TORQUE LINKS BECAME DISCONNECTED FROM EACH OTHER DURING TAKEOFF ROLL. IT APPEARS THAT A PRESSED IN BUSHING, SEPARATED FROM THE LOWER TORQUE LINK ALLOWING THE BOLT HEAD AND WASHER TO PASS THROUGH THE ENLARGED HOLE NORMALSDR 2002FA0000045Shimmy Dampener · damagedPILOT MADE A HARD LEFT TURN CAUSEING DAMAGE TO THE NOSE GEAR AREA. BENT ROD ON THE SHIMMY DAMPER CAUSING INTERNAL DAMAGE TO THE COMPONENT.SDR 20010412CW009Cylinder · leakingAIRCRAFT LANDED. OIL LEAKING FROM LEFT ENGINE. INSPECTION REVEALED NR 4 CYLINDER VALVE COVER BROKEN DUE TO VALVE ROCKER ASSEMBLY BROKEN FROM CYLINDER BOSS. PROBABLE CAUSE STUCK VALVE OR METAL FATIGUE AT BOSS.SDR 20000817SH012Hub · crackedHUB CRACKED IN BOTH THREADED BLADE SOCKETS. PROPELLER WAS LEAKING, IN FOR RE-SEAL. (X)SDR 20000626SH003Spar · corrodedEXFOLIATION CORROSION AT LEAST .01 INCH TO .1250 INCH DEEP AND GROWING. SUBMITTER STATES THAT AIRCRAFT WAS BASED IN SAN FRANCISCO BAY AREA AND SALT AIR MAY HAVE CONDENSED INSIDE THE AIRCRAFT INSULATION AND DRIPPED DOWN ON THE FITTINGS. HOWEVER, SUBMITTER BELSDR 20000626SH002Fitting · corrodedEXFOLIATION CORROSION AT LEAST .01 INCH TO .1250 INCH DEEP AND GROWING. SUBMITTER STATES THAT AIRCRAFT WAS BASED IN SAN FRANCISCO BAY AREA AND SALT AIR MAY HAVE CONDENSED INSIDE THE AIRCRAFT INSULATION AND DRIPPED DOWN ON THE FITTINGS. HOWEVER, SUBMITTER BELSDR CA001005010Downlock · misaligned(CAN) - RIGHT GEAR COLLAPSED AFTER LANDING. DOWNLOCK FOUND MISADJUSTED (TOO SHORT). DOWNLOCK BELLCRANK, SIDE BRACE LINK REPLACED. DOWNLOCK READJUSTED. (X)SDR CA990318038Window · separated(CAN) AFTER T/F EMERGENCY WINDOW DEPARTED AIRCRAFT. UPON FURTHER INVESTIGATION, THE WINDOW SEPARATED FROM THE FRONT AND PROCEEDED TO PEEL BACKWARDS. THE EMERGENCY CABLE WAS NOT PULLED. THE REAR LOCKING PINS WERE BENT AND THE WINDOW TABS WERE RIPPED FROM THESDR 98ZZZX983Idler Gear · failedIDLER IN NOSE GEAR RETRACT LINKAGE BROKE DURING RETRACTION DUE TO INTERFERENCE OF NOSE GEAR AND WHEELWELL DOORS. NOSE GEAR FAILED TO EXTEND DUE TO LOSS OF NITROGEN CHARGE IN STRUT. STRUT HAD BEEN OVERSERVICED WITH HYDRAULIC FLUID. WITH THE STRUT BEING OVERSSDR EY2R9600168Hub · crackedPROP HUB ASSY CRACKED IN THREAD AREASDR EY2R9600064Hub · crackedPROP ASSY HUB CRACKEDSDR AU960503Exhaust Valve · leaking(AUS) ENGINE COMPRESSION LEAKAGE FROM EXHAUST VALVES ON ALL 6 CYLINDERS- FOUND DURING COMPRESSION CHECK IAW AD/ENG/4 AMDT 5 - ENGINECALENDER TIME SINCE OVERHAUL WAS 19 YEARSSDR 95ZZZX568Mount · damagedNEW OWNER BROUGHT AIRCRAFT IN FOR PITOT HEAT PROBLEM. NOTICED LT ENGINE WAS SAGGING RELATIVE TO THE COWLING. FURTHER INSPECTION REVEALED THE FORWARD MOUNTS TO HAVE UNSEATED AND DROPPED IN THE SUPPORT STRUCTURE. THE RT ENGINE WAS CHECKED AND FOUND TO HAVE TH
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