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 = 'GA8' 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 = 'GA8' 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 2025FA0000541Oil Filter · out of alignmentTEMPEST OIL FILTER FOUND DEFECTIVE AT INSPECTION. NEW OIL FILTER HAS A MANUFACTURING DEFECT. THE MOUNT THREADS ARE NOT TRUE TO CENTERLINE OF THE FILTER. THIS IS A SPIN ON OIL FILTER. WHEN INSTALLING IT IS EASY TO SEE THAT IT IS NOT TRUE SO IT WOBBLES WHILESDR 2025FA0000542Oil Filter · defectiveTEMPEST OIL FILTER PN AA48109 FOUND DEFECTIVE AT INSPECTION. NEW OIL FILTER HAS A MANUFACTURING DEFECT. THE MOUNT THREADS ARE NOT TRUE TO CENTERLINE OF THE FILTER. THIS IS A SPIN ON OIL FILTER. IT IS A PMA PART AND MFG. AND SOLD IN THE USA. WHEN INSTALLINSDR ENHA20241205001Cylinder · crackedDURING PREFLIGHT PILOT NOTICED THE ENGINE HAD AN OIL LEAK. MAINTENANCE INSPECTED AND DETERMINED THAT THE CRANKCASE NEAR NUMBER 6 CYLINDER WAS CRACKED NEAR THE FORWARD UPPER CYLINDER HOLD DOWN STUD.SDR ENHA202406130001Brake Assy · weakLEFT SIDE BRAKE SPONGY. MAINTENANCE BLED L/H BRAKE CALIPER. NO FURTHER DEFECTS STATED. GRANT LOG PAGE 248314SDR ENHA LP236232Latch · out of adjustCARGO DOOR OPENS DURING TAKEOFF. MECHANICS ADJUSTED CARGO DOOR LATCH AS REQUIRED. OPS CHECK SATISFACTORY. REF GA8 SM 52-40-00.SDR ENHA202305230001Latch · wornCARGO DOOR POP IN FLIGHT DURING TAKEOFF. MECHANICS REMOVED AN OBSTRUCTION, INSPECTED, CLEANED, AND REPLACED LATCH WITH SERVICEABLE UNIT REFERENCING SB GA8-2005-23. OPS CHECKED GOOD.SDR ENHA202208090052Brake Caliper · dryLEFT BRAKE COMPLETE FAILURE. MECHANICS BLED BRAKES AND FUNCTION RETURNED.SDR ENHA2021111100001Panel · bindingPILOT REPORTED THAT DURING TAKEOFF ROLL THE RUDDER PEDAL LOCKED UP RESULTING IN AN ABORTED TAKEOFF. MAINTENANCE INSPECTED AIRCRAFT AND DETERMINED THAT RUDDER BAR LOWER KICK PANEL PN: GA8-252025-021 WAS BINDING THE RUDDER/STEERING CONTROL. MAINTENANCE REPLACESDR 2020F00282Cylinder Head · crackedPILOT NOTICED BURNING SMELL AND A SPIKE IN OIL TEMPERATURE. PILOT LANDED AT NEAREST AIRPORT. MECHANIC FOUND CRACKED CYLINDER.SDR 2020FA0000239Nut · missingCREW BEGAN FLIGHT TRAINING TO GET RE QUALIFIED FOR GA8. AFTER COMPLETING PRACTICE MANEUVERS,CREW PROCEEDED TO AKIACHAK TO DO SPOT LANDING WITH CROSSWIND. AFTER THIRD LANDING EXECUTED A FULL STOP WITH TAXI BACK. AFTER A NORMAL DEMONSTRATED SOFT TAKEOFF, TRAINEESDR ENHA201911190001Float Valve · malfunctionedPILOT WAS DOING IOE, ON THE WAY BACK FROM CYF TO BET CREW NOTICE ONLY FUEL WAS ONLY COMING OUT OF R/H FUEL TANK.R/H FUEL TANK WENT FROM 1/2 TO 1/4 IN 10 MINUTES AT CRUISE. CREW DECIDED TO DO AN UNSCHEDULED LANDING AS THEY WERE 12 MINUTES OUT OF BET. THEY LANDESDR ENHA2019100400001Transfer Sys · malfunctionedPILOT STATED BEFORE LEEAVING, TOPPED OFF THE TANKS. DURING FLIGHT, NOTICED THE FUEL TANKS WERE FEEDING UNEVENLY. FURTHER INTO THE FLIGHT THE PROBLEM DID NOT CORRECT ITSELF AND THE IMBALANCE GOT WORSE. ON THE FINAL LEG THE LEFT TANK FUEL GAUGE WAS INDICATINSDR ENHA2019072500002Spark Plug · fouledLOSS OF RPM ON CLIMB. MX DETERMINED CAUSE WAS FOULED SPARK PLUG.SDR ENHA2019072500001Spark Plug · fouledLOSS OF RPM ON CLIMB. MX DETERMINED CAUSE WAS FOULED SPARK PLUG.SDR 2019FA0000182Latch · wornREAR PASSENGER DOOR OPENED DURING TAKEOFF.SDR ENHA2019F00167Brake · inadequateLEFT BRAKE LOSING PRESSURE AND EFFECTIVENESS. SERVICED BRAKE, OPS CHECK NORMAL.SDR ENHA2019F00166Brake · inadequateLEFT BRAKE LOSING PRESSURE AND EFFECTIVENESS. SERVICED BRAKE, OPS CHECK NORMAL.SDR 2019FA0000077Gasket · looseVALVE COVER GASKET LEAKING.SDR 2019F00111Hose · chafedFAILURE OF LH BRAKE DUE TO MLG FAIRING CHAFFING HOLE IN BRAKE FLEX HOSE.SDR CA151125006Skin · unsecure(CAN) SINCE THE OPERATION ON THE AIRCRAFT, ALL THE WING PANELS HAVE BEEN NOTICED TO BE COMING LOSE DURING ANY SCHEDULED MAINTENANCE PROCEDURE. ALL THE NUMBER 6 SCREWS THAT HOLD THE PANELS IN ARE ALL FOUND TO NOT TIGHTEN PROPERLY. A LARGER SCREW (NUMBER 8) IS NSDR N3N2016060700001Coil · failedMAGNETOS 6393 & 6350 AND SPARK PLUGS REM38E . THESE MAGNETOS ARE CONSISTENT AT FAILING. WE HAD TO KEEP 2 SPARES OF EACH MAGNETO ON THE SHELF AND SPAR INTERNAL REPLACEMENT PARTS JUST TO KEEP OPERATING. IT WAS NOT UNCOMMON TO HAVE TO REPLACE A BRAND NEW MAG ASDR 3WGR20140502001Magneto · contaminatedDURING 100 HOUR INSPECTION, FOUND BOTH MAGNETOS WERE CONTAMINATED WITH ENGINE OIL. LT MAGNETO TO ENGINE WAS SET AT 25 DEGREES BEFORE TOP DEAD CENTER (BTDC). IT SHOULD HAVE BEEN SET AT 20 DEGREES BTDC.SDR OVF2008F00001Brushes · wornAIRCRAFT EXPERIENCED AN ENGINE FAILURE. ATTEMPTS TO RESTART ENGINE FAILED AND SAFE LANDING WAS ACCOMPLISHED. CAUSE OF FAILURE REMAINS UNKNOWN AT THIS TIME. MAGNETOS FUEL PUMP, AND FUEL INJECTOR SERVO WERE SENT TO THE RESPECTIVE OEM`S. THE MAGNETOS WERE SENT SDR OVF2008F00000Brushes · wornTHIS IS AN UPDATE OF A SDR FILED 15 APRIL, 2008. MAGNETOS, FUEL PUMP, AND FUEL INJECTOR SERVO WERE SENT TO THE RESPECTIVE OEM`S. MAGNETOS WERE SENT TO MFG FOR ANALYSIS. THEY WERE SENT AS REMOVED TO PRECLUDE ANY FIELD CONTAMINATION. THEY WERE NOT PRODUCING SPASDR 2008F00016Engine · failedAIRCRAFT EXPERIENCED AN ENGINE FAILURE. ATTEMPTS TO RESTART ENGINE FAILED AND A SAFE LANDING WAS ACCOMPLISHED. CAUSE OF FAILURE REMAINS UNKNOWN AT THIS TIME. (K)SDR HN8R200700001Screen · contaminatedFOUND 2 PIECES OF METAL IN THE OIL SUMP SUCTION SCREEN DURING ANNUAL INSPECTION. ONE PIECE LOOKS LIKE A DRILLED OUT HELI COIL .5 INCH LONG X .25 WIDE AND THE OTHER LOOKS LIKE A PIECE OF CASTING .2 LONG X .125 WIDE. THE ENGINE WILL BE REMOVED AND SENT OUT FORSDR HN8R200600001Servo · defectiveNOSE DOWN AUTO TRIM INOP WAS REPORTED BY PILOT. TROUBLESHOOTING REVEALED THE AUTOPILOT COMPUTER WAS NOT RECEIVING INPUT CALLING FOR NOSE DOWN TRIM FROM THIS PITCH SERVO.SDR CA061026004Indicator · burned(CAN) PILOT REPORTED MALFUNCTION OF PITOT HEAT BREAKER SWITCH, UPON INSPECTION, CIRCUIT BOARD ATTACHED TO BACK OF SWITCH WAS FOUND BADLY BURNT AND END OF WIRE CONNECTION FROM THE PITOT TO THE POWER SWITCH WAS FOUND OVERHEATED. MAIN PITOT WAS REPAIRED. THE CISDR AU510002133Trim System · faulty(AUS) RUNAWAY ELEVATOR TRIM SYSTEM. AIRCRAFT IS FOREIGN REGISTERED. (CASA NR 510002133)SDR AU510002073Crankshaft · faulty(AUS) CRANKSHAFT REMOVED AND REPLACED DUE TO APPLICABILITY WITH AD AND SB 566. (AD/SB DESC: SB 566 AND AD/LYC/112 ) (CASA NR 510002073)SDR AU510001788Pump · failed(AUS) AUXILIARY FUEL PUMP DRIVE SHEARED. PUMP IS LOCATED BENEATH COPILOT SEAT.(OTHER CAUSE: MATERIAL ) (CASA NR 510001788)SDR AU510001789Pump · failed(AUS) ENGINE DRIVEN FUEL PUMP FAILED. (CASA NR 510001789)SDR CA051117005Control Cable · broken(CAN) AC DEPARTED, WHEN STAB TRIM STARTED TO RUN AWAY TO NOSE UP POSITION. PILOT HAD TO HOLD WHEEL TO KEEP IN POSITION ON CLIMB. AC LANDED AT MAINT BASE TO GET CHECKED OUT. CABLE TENSION WAS BROUGHT UP TO MAX TENSION IAW MM. WHEN TENSION WAS CHECKED ON 17THSDR AU510001483Blade · failed(AUS) PROPELLER BLADE TIP SEPARATED IN FLIGHT. APPROXIMATELY 228.6 (9IN) OF BLADE SEPARATED. SEVERE VIBRATION CAUSED ENGINE TO SEIZE DURING EMERGENCY LANDING. AIRCRAFT IS REGISTERED AND OPERATING IN CANADA. (CASA# 510001483)SDR CA050630005Blade · broken(CAN) AC WAS IN CRUISE AT 3500 FEET. PILOT HEARD A LOUD BANG, AC STARTED TO SHAKE VIOLENTLY. PILOT WAS ABLE TO MAINTAIN ALTITUDE AND TURNBACK. EMERGENCY CALL WAS MADE. ENGINE STARTED TO SURGE ON SHORT FINAL, OIL LIGHT CAME ON, ENGINE QUIT. MADE A SAFE LANDSDR AUS20040295Bushing · galled(AUS) CONTROL WHEEL SHAFT BUSHING GALLED AGAINST WELD PENETRATION ON INNER FACE OF CONTROL COLUMN SLEEVE.SDR AUS20030793Bolt · sheared(AUS) HORIZONTAL STABILISER RT REAR PIVOT ATTACHMENT BOLT SHEARED.SDR AUS20030063Screw · loose(AUS) ENGINE OIL PUMP BODY 'ALLEN' SCREW LOOSE. FOUND DURING INSPECTION IAW LYCOMING SB/555.SDR AUS20021007Structure · cracked(AUS) HORIZONTAL STABILIZER CRACKED.SDR AUS20011077Bracket · sheared(AUS) RT HORIZONTAL STABILISER ATTACHMENT BRACKET RIVETS SHEARED.
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