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 = 'U206' 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 = 'U206' 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 CA111124003Scoop · failed(CAN) BOTTOM OF AIR SCOOP BEHIND AIR CLEANER BROKE OUT IN SMALL PIECES WHICH WERE INGESTED INTO THE ENGINE HOLDING VALVES WHICH CAUSED ENGINE TO QUIT. HEAVY MATERIAL WAS INSTALLED IN DEFECTED AREA. WILL MONITOR. ORIGINAL MATERIAL WAS SOFT AND WAS FLEXING CAUSDR CA090402003Screw · missing(CAN) THE PILOT NOTED HIS AILERON CONTROLS WERE SLUGGISH DURING FLIGHT AND THE CONTROL WHEEL WAS OFF CENTER DURING LEVEL FLIGHT. DURING ROUTINE INSP IT WAS FOUND THAT THE UPPER AILERON PULLEY BRACKET SCREW AND NUT WERE MISSING. THE PULLEY BRACKET WAS SLIGHTLY SDR CA070228003Control Arm · defective(CAN) THE SUBJECT AIRCRAFT WAS CLIMBING OUT AFTER TAKEOFF AND EXPERIENCED A SIGNIFICANT LOSS OF CLIMB POWER RELATED TO A DROP IN ENGINE RPM FROM 2700 RPM TO 1600 RPM. THE PILOT EXECUTED ALL APPROPRIATE EMERGENCY PROCEDURES/ACTIONS WITH NO IMPROVEMENT. THE PILSDR ENE2006F00000Cylinder Head · separatedBOTH CYLINDERS FAILED AT TAKEOFF POWER SETTING WITHIN 2 HOURS OF EACH OTHER. FAILURE CONSISTING OF COMPLETE SEPARATION OF THE HEAD FROM THE BARREL, CAUSING DAMAGE TO THE BAFFLING. EXHAUST COLLECTOR, AND SEVERING OF THE FUEL INJECTOR LINE.SDR 2004F00401Cylinder Head · separatedCYLINDER HEAD SEPARATED FROM BARREL IN CRUISE .SDR CA040709003Screw · worn(CAN) DURING ENGINE START, FIRST FLIGHT OF THE DAY, OIL PRESSURE WAS OBSERVED AS BEING TOO HIGH (75 PSI AT IDLE). SYSTEM BLOCKAGE WAS SUSPECTED, OIL FILTER INSPECTED (CLEAR), OIL DRAINED AND INSPECTED (CLEAR), PRESSURE CHECKED AT OTHER PRESSURE POINTS IAW MFGSDR MK92003F00000Bar · brokenFLANGE ON RUDDER BAR BROKEN. LT SIDE, LT BRAKE PEDAL ATTACHMENT. PILOT WAS LANDING AIRCRAFT WHEN IT BROKEN. LANDED AND TAXIED SAFETLY. CLOSE INSPECTION OF ALL FLANGES AND SPRAYING PENTRATING OIL DOWN RUDDER PEDAL BAR WOULD HELP PREVENT INTERIOR CORROSION WSDR AUS20030419Control Cable · separated(AUS) THROTTLE CABLE OUTER GUIDE SEPARATED FROM SWAGED SWIVEL JOINT ALLOWING CABLE TO FAIL IN COMPRESSION.SDR AUS20030345Bearing · worn(AUS) CONNECTING ROD BIG END BEARING WORN EXCESSIVELY.SDR AUS20010516Spring · failed(AUS) STARTER CLUTCH SPRING FAILED CAUSING DAMAGE TO THE CRANKSHAFT,CAMSHAFT GEAR AND ATTACHING HARDWARE. ROCKWELL HARDNESS TESTREVEALED INCONSISTANT HARDNESS.SDR AU000674Impulse Coupling · faulty(AUS) MAGNETO IMPULSE COUPLINGS (2OFF) HAD LOOSE RIVETS IN THE FLYWEIGHT ASSEMBLIES. FOUND DURING INSPECTION IAW SLICK SB 1-86B. (X)SDR AU000620Cylinder · separated(AUS) NR 6 CYLINDER HEAD SEPARATED FROM BARREL. (X)SDR 20000908SH008Points · failedDURING PRE-INSPECTION RUN-UP BY MECHANIC, FOUND UNUSUAL MAG DROP ON RIGHT MAGNETO REMOVED FOR TROUBLESHOOTING. FOUND THE POINT ASSY CONTACT LOOSE AND FALLING OUT OF SPRING ARM. REPLACED CONTACT ASSY. OPS CHECKED GOOD. THIS MAG HAD 184 HOURS SINCE A TCM OVESDR 98ZZZX4656Condenser · failedCONDENSER FAILED 20.0 HOURS AFTER OVERHAUL. THIS CAUSED THE POINTS TO BURN RESULTING IN EXCESSIVE MAGNETO DROP. DATE CODE: 96-47.SDR 97ZZZX3810Bulkhead · crackedINSPECTION FOUND TAIL CONE BULKHEAD AT BS 230.187 CRACKED. REPLACED WITH P/N 1212130-2.SDR 97ZZZX3709Trim Tab · out of balancePARACHUTING FLIGHT - AFTER JUMP TRIMMED NOSE DOWN, IN DESCENT 150 MPH, ELEVATOR VIBRATION WHICH DISAPPEARED WHEN SPEED 130 MPH. TRIM TAB UNDERSIDE SKIN WAS DEFORMED UNDER BRACKET ASSEMBLY AND TRIM ACTUATOR WAS LOOSE FROM FASTENERS. ELEVATOR MASS BALANCE WASSDR 97ZZZX3708Trim Tab · core soakedPARACHUTING FLIGHT - FL 100, AFTER JUMP IN DESCENT SPEED 100 MPH ELEVATOR FLUTTER, FAST AND HEAVY MOVEMENTS 2-3 SECONDS, DISAPPEARED WHEN SPEED 80 MPH. TRIM ACTUATOR WAS LOOSE FROM BROKEN STABILIZER BRACKET, FREE MOVEMENT 2 INCHES. NEARBY RIB WAS ALSO BROKENSDR PNSA970301Engine · low powerAIRCRAFT DID NOT CLIMB WELL AFTER TAKEOFF. RETURNED TO BASE. NO DEFECTS NOTED WITH ENGINE, TEST FLIGHT OK.SDR EY2R9601269Retainers · corrodedRETAINERS FOUND CORRODED.SDR EY2R9601268Bearings · corrodedBEARINGS FOUND CORRODED.SDR EY2R9601267Hub · corrodedHUB CORRODED.SDR 96ZZZX3544Pulley · separatedDRIVE PULLEY FOUND SEPARATED FROM VENT FAN DURING UNSCHEDULED MAINTENANCE. ALTERNATOR, 386.7 HOURS SINCE OVERHAUL. PULLEY TIME UNKNOWN. CORROSION EVIDENT ON MATING SURFACES OF DETACHED PIECES.SDR EY2R9600644Dowel · corrodedDOWEL CORRODED.SDR 96ZZZX2299V-Channel · crackedV-CHANNEL CRACKED WHERE AILERON HINGE RIVETED TO IT. DIFFICULT TO SEE CRACK. SUSPECT DEFECTIVE IF MOVEMENT NOTICED WHEN PRESSURE APPLIED UPWARD TO FLAT OF AILERON LOWER SURFACE.SDR 96ZZZX2152Cylinder · crackedNR 3, NR 2, AND NR 5 CYLINDERS WERE FOUND CRACKED AT INTAKE SEAT.SDR 96ZZZX2151Cylinder · crackedNR 4 AND NR 1 CYLINDERS WERE FOUND CRACKED AT INTAKE SEAT.SDR 95ZZZX5038Lever · brokeTHROTTLE LEVER BROKE AT END OF LEVER WHERE THROTTLE ROD END ATTACHES ALLOWING THROTTLE TO DISCONNECT FROM ENGINE. AIRCRAFT LANDED WITHOUT DAMAGE OR INJURY.
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