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 = '401' 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 = '401' 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 2025FA0000406Bellcrank · crackedCONDUCTED A GEAR UP LANDING AT KGKY. PILOT STATED THAT THEY WERE CONDUCTING A MX FLT AFTER ACFT HAD NOT FLOWN IN OVER 20 YEARS. HAD PERFORMED MULTIPLE HIGH SPEED TAXIS WITH SUBSEQUENT ADJUSTMENTS MADE. DEPARTED & CONDUCTED AN INITIAL PATTERN WITH GEAR DOWN WSDR XGNA2020102600008Indication Sys · malfunctionedON TAKE OFF CLIMB OUT AT EDC THE PILOT OF FLIGHT GTX336 THOUGHT HE OBSERVED ERRONEOUS FUEL FLOW INDICATIONS ON THE RIGHT FUEL FLOW GAUGE. HE DID NOT DECLARE AN EMERGENCY, BUT REQUESTED RTB AS A PRECAUTION. HE STATED BOTH ENGINES WERE RUNNING. ONCE ON THE GRSDR CA140625006Fitting · cracked(CAN) WHEN COMPLETING THE SID INSPECTION PROGRAM THE LT ELEVATOR WAS REMOVED FOR INSPECTION. A TAPER PIN, PASSES THROUGH A FITTING. THE FITTING WAS FOUND CRACKED AT THE TAPER PIN HOLE.SDR XGN2012F00001Engine · damagedPILOT REPORTED LOSING OIL PRESSURE ON THE LEFT ENGINE IN CRUISE FLIGHT. THE ENGINE WAS SHUT DOWN IN FLIGHT TO PREVENT DAMAGE. REMOVAL OF THE OIL FILTER AND ITS INSPECTION SHOWED METAL CONTAMINATION IN THE FILTER. THE ENGINE WAS REMOVED FROM SERVICE.SDR CA120524012Cotter Pin · missing(CAN) IN LEVEL CRUISE FLGHT THE LT ALTERNATOR STOPPED PRODUCING POWER. AFTER LANDING OIL WAS DISCOVERED UNDER THE LT ENGINE. THE ALTERNATOR WAS REMOVED. THE ALTERNATOR ARMATURE WAS FOUND BROKEN OFF. THE COTTER PIN HOLDING THE DRIVE GEAR NUT WAS FOUND MISSINSDR XGN2011F00000Spring · brokenLANDING GEAR WOULD NOT RETRACT. FOUND SAFETY SWITCH SPRING BROKEN AND LEVER ACTUATOR TEETH WORN OUT.SDR 2010FA0001182Support · detached2 OF THE 3 BOLTS ATTACHING THE UPPER HALF OF THE LT MLG SIDE BRACE SUPPORT BRACKET WERE FOUND MISSING. THE STRESS IMPOSED ON THE REMAINING BOLT CAUSED IT TO BE PULLED THROUGH THE ATTACHING STRUCTURE. THE FAILURE OF THIS ATTACHMENT CAUSED THE GEAR TO NOT ACQUSDR CA101021004Fitting · crackedRT ELEVATOR END FITTING CRACKED AT TAPER PIN HOLE. FOUND DURING INSP.SDR CA080930006Wheel · cracked(CAN) RT MAIN WHEEL ASSY BEAD AREA FOUND CRACKED. WHEEL REPLACED WITH SERVICEABLE UNIT.SDR YJV2009F00000Connecting Rod · brokenENGINE VIBRATING, HIGH OIL TEMP AND LOW OIL PRESSURE. POST FLIGHT FOUND NR 2 CONNECTING ROD BROKEN. (K)SDR CA080314013Engine · making metal(CAN) ON FINAL APPROACH INTO AIRPORT THE RT ENGINE MANIFOLD PRESSURE STARTED CHANGING. THE PILOT THEN NOTICED THAT THE RT OIL PRESSURE HAD DROPPED TO THE RED LINE. THE RT PROP WAS FEATHERED AND THE ENGINE WAS SHUTDOWN. SMALL BITS OF METAL WERE FOUND UNDER THE SDR CA070126011Torque Link · failed(CAN) AIRCRAFT WAS DOING TOUCH AND GO`S ON THE 2ND LANDING PILOT REPORTED ABNORMAL LANDING AND NO GEAR UP INDICATION. GEAR CYCLED AND ONLY 2 OUT OF 3 INDICATOR LIGHTS ILUMINATED. RT MAIN, NO INDICATION. GEAR CYCLED AGAIN NO UP INDICATION AND NO RT GREEN DOWN SDR CA070115015Mount · loose(CAN) DURING SCHEDULED LANDING GEAR ROUTINE INSPECTION, LANDING GEAR ACTUATOR GEARBOX MOUNTING BOLTS (3) FOUND MISSING AND REMAINING (1) BOLT FOUND SHEARED. EMERGENCY GEAR OPERATION ATTEMPTED TO RELOCATE GEAR. EMERGENCY OPERATION INHIBITED DUE TO IMPROPER GEASDR CA061023005Case · cracked(CAN) THE ENGINE HAD A SMALL OIL LEAK. AFTER REMOVING THE DIP STICK ASSEMBLY, A CRACK WAS FOUND BETWEEN NR 2 AND NR 4 CYLINDERS. THE ENGINE WAS REMOVED FOR OVERHAUL. (TC NR 20061023005)SDR XGN2006F00014Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00013Cylinder · crackedCYLINDER HEAD CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00025Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00024Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00015Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00023Cylinder · crackedCYLINDR HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00022Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2005F00007Cylinder · crackedTHIS CYLINDER WAS IN THE NR 6 POSITION AND IS A TYPE (A) HEAD. THIS CRACKED CYLINDER HEAD WAS FOUND AT THE 50 HOUR INSPECTION. WE ARE FINDING SIGNS OF AIR LEAKAGE ON THE EXHAUST SIDE OF THE CYLINDER HEAD WHEN DOING A COMPRESSION CHECK. WE ARE SPRAYING SOAPYSDR TZR2005F00025Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS. RT ENGINE, NR 3 CYL. (SW05200509364) (K)SDR XGN2006F00021Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00020Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00019Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00062Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00061Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00018Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00017Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00059Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR TZR2005F00019Cylinder · crackedCYLINDER CRACKED FROM EXHAUST VALVE TO TOP SPARK PLUG PORT. ECI CYLINDER. (SW05200507952) (K)SDR TZR2005F00018Cylinder · crackedCRACKED FROM INJECTOR TOWARD SPARK PLUG, ECI CYLINDER. (SW05200507951) (K)SDR XGN2006F00060Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00066Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00065Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00016Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR TZR2005F00005Cylinder · crackedCYLINDER CRACK FROM EXHAUST VALVE. (K)SDR TZR2005F00004Cylinder · crackedCYLINDER CRACKED FROM EXHAUST VALVE TO TOP SPARK PLUG HOLE. (K)SDR XGN2006F00064Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR XGN2006F00063Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR TZR2005F00009Cylinder · crackedCYLINDER CRACKED VALVE TO VALVE. (K)SDR TZR2005F00006Cylinder Head · crackedCYLINDER CRACKED AT HEAD. (K)SDR TZR2005F00007Cylinder · crackedCYLINDER CRACKED FROM EXHAUST VALVE. (K)SDR TZR2005F00008Cylinder · crackedCYLINDER CRACKED AT SPARK PLUG HOLE. (K)SDR TZR2005F00013Cylinder · damagedCYLINDER COMPRESSION BELOW MINIMUMS. (K)SDR TZR2005F00003Cylinder · crackedCYLINDER CRACK FROM EXHAUST VALVE TO SPARK PLUG. (K)SDR TZR2005F00002Cylinder · crackedCYLINDER CRACKED FROM EXHAUST VALVE TO SPARK PLUG HOLE. (K)SDR TZR2004F00005Turbocharger · failedPILOT REPORTED LOSS OF TURBO BOOST AND OIL PRESSURE, SHUT DOWN ENGINE AND FEATHERED PROPELLER IN FLIGHT. LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. DURING POST FLIGHT INSPECTION OF TURBO OIL WAS OBSERVED IN THE EXHAUST OVERBOARD PIPE INDICATING SEAL FAILURE. SDR TZR2004F00000Bearing · failedAFTER INSTALLATION OF RT ENGINE, WHILE PERFORMING ENGINE FUEL SET-UP AND ADJUSTMENT OF MANIFOLD PRESSURE, THERE WAS A DECREASE IN MANIFOLD PRESSURE AND A NOTICEABLE NOISE AND VIBRATION FROM THE RT ENGINE. UPON FURTHER INVESTIGATION IT WAS NOTED THAT THE TURBO
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