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 = 'D55' 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 = 'D55' 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 2020FA0000518Strut · corrodedTHIS AIRCRAFT IS USED IN A PART 147 TRAINING FACILITY AND HAS NOT FLOWN SINCE 2012. CORROSION FOUND IN RT MLG STRUT TUBE BEHIND FELT WIPER. THE SAME IS SUSPECTED IN THE LT CYLINDER.SDR 2017FA0000376Engine · malfunctionedAFTER 12 - 15 MINUTES ON THE GROUND AND ENGINE RUN UP WITH NO INDICATIONS OF ANY PROBLEMS WITH ANY SYSTEMS, LEFT ENGINE HAD POWER LOSS WITHIN 1 - 2 SECONDS AFTER ROTATION WITH GEAR DOWN. RPM DOWN TO 1600 RPM, LEFT FUEL FLOW NEEDLE BOUNCING BACK AND FORTH FROSDR 2017FA0000346Engine · power lossAFTER 12 TO 15 MINUTES ON GROUND AND ENGINE RUN UP WITH NO INDICATIONS OF ANY PROBLEMS WITH ANY SYSTEMS, LEFT ENGINE HAD POWER LOSS WITHIN 1 TO 2 SECONDS AFTER ROTATION WITH GEAR DOWN. RPM DOWN TO 1600 RPM, LEFT FUEL FLOW NEEDLE BOUNCING BACK AND FORTH FROM TSDR 2011FA0000247Duct · chafedDURING ANNUAL INSP, FOUND THE RT ENGINE FUEL METERING UNIT BLAST DUCT CHAFING ON ENGINE MOUNT TUBE. FOUND THAT THE METAL WIRE IN THE BLAST DUCT HAD WORN THROUGH THE BLAST DUCT AND WORE INTO THE ENGINE MOUNT TUBE REQUIRING THE ENGINE MOUNT TO BE REMOVED FOR REPSDR XGN2011F00008Cylinder · crackedNR 1 CYLINDER ON LT ENGINE WAS CRACKED THRU THE HEAD ON THE TOP SIDE BETWEEN THE FINS ABOVE THE INTAKE VALVE. THIS IS ANOTHER DEFECTIVE REV NR 3 CYLINDER.SDR XGN2011F00007Cylinder Head · crackedNR 3 CYLINDER ON LT ENGINE HAD A COMPLETE HEAD SEPARATION CAUSED BY THE FAILURE OF THE AREA AROUND THE INTAKE VALVE. THIS AREA IS THE COMMON FAILURE FOR MFG REV NR 3 CYLINDERS DUE TO A MFG DEFECT/DESIGN IN THE HEAD CASTING. THE AREA THICKNESS WAS MFG TOO THSDR 2007FA0001029Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001023Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001022Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001021Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001020Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001019Cylinder Head · crackedCRACKED CYL HEAD BEHIND INJECTOR BETWEEN FIN NR 12, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001085Nose Rib · crackedAT ANNUAL INSPECTION, FOUND CRACKED FLAP ROD ATTACH POINT RIB. RT FLAP ONLY. (K)SDR XGN2007F00025Cylinder · crackedNR 6 CYLINDER WAS NEW, REV 3, E SERIES, CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH REV 3, E SERIES TO CRACK IN THE SAME LOCATION. (K)SDR XGN2007F00021Cylinder Head · crackedNR 6 CYLINDER WAS NEW ECI, REV 3, E SERIES, CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH ECI, REV 3, E SERIES, TO CRACK IN THE SAME LOCATION. (K)SDR 2007FA0000698Cylinder · crackedNR 6 CYLINDER WAS NEW ECI REV 3 E SERIES CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH ECI REV 3 E SERIES TO CARCK IN THE SAME LOCATION. (K)SDR AU510002160Cable · failedLH ENGINE THROTTLE CABLE FAILED IN AREA UNDER SHEATH.SDR XGN2004F00001Camshaft · brokenAIRCRAFT WAS ENROUTE, PIC NOTICED THE AIRCRAFT YAWING WAY TO THE RIGHT. THERE WAS NOT ANY LOSS OF OIL OR FUEL PRESSURE NOR ANY VIBRATION. THE PILOT SHUT THE ENGINE DOWN AND LANDED. THE OIL PAN WAS REMOVED AND FOUND THE CAMSHAFT WAS BROKEN. HAVE NO IDEA WHASDR AUS20030813Hub · cracked(AUS) PROPELLER HUB CRACKED IN BLADE RETENTION THREADS. FOUND DURING INSPECTION IAW AD/PMC/47 AMDT1.SDR CDM2002F00000Line · brokenPILOT DECLARED AN EMERGENCY. NOTICED OIL STREAMING FROM RIGHT ENGINE. MADE A SAFE LANDING. THE MECHANIC DISCOVERED THE HARD-LINE FROM THE PROPELLER UNFEATHERING ACCUMULATOR HAD BROKEN AT THE FLARED END WHICH ATTACHED TO THE PROPELLER GOVERNOR. THE SINGLE FSDR CA020510020Clamp · cracked(CAN) COUNTERWEIGHT CLAMP FOUND TO BE CRACKED IN THE MIDDLE MID-WAY BETWEEN THE CLAMP RETAINING BOLTS.SDR XGN2002F00000Crankcase · crackedHALF CIRCLE CRACKED AT NR 6 CYLINDER PAD. CRACK RUNS FROM UPPER PART OF CRANKCASE FROM CYLINDER BASE STUD AT 2 OCLOCK POSITION TO CYLINDER BASE STUD AT 10 OCLOCK POSITION. WITH SEVERAL CRACK RADIATING FROM THE HALF CIRCLE CAUSING A SMALL TRIANGULAR PIECE TOSDR AUS20010647Pump · failed(AUS) LH ENGINE DRIVEN VACUUM PUMP ROTOR SEIZED AND DRIVESHAFT SHEARED.SDR 20010411CW007Counterweight · separatedCOUNTERWEIGHT DEPARTED LEFT PROP ON TAKEOFF ROLL. SPINNER AND BACKING PLATE WERE DESTROYED. PROP HUB WAS CRACKED IN TWO PLACES. NO OTHER DAMAGE TO AIRCRAFT OR ENGINE. ROTOR COUNTERWEIGHT WAS NOT FOUND.SDR 20010328CW005Motor · defectiveSQUAKED FLAP C/B TRIPS WHEN FLAPS ACTUATED. ISOLATED FLAP MOTOR WITH REMOTE C/B & EXT POWER. FOUND BAD FLAP MOTOR. LOCATED NEW MOTOR. INST MOTOR WORKED ON GROUND, TRIPPED C/B IN FLIGHT. ISOLATED MOTOR, DETERMINED BAD MOTOR. LOCATED ANOTHER MTR, WHEN REC''SDR AU000875Rod End · seized(AUS) NOSE LANDING GEAR REAR ACTUATING ROD ROD END SEIZED AND FAILED ALLOWING NLG TO COLLAPSE ON LANDING. (X)SDR 20000531SH016Counterweight · crackedCRACK INDICATION BETWEEN BOLT ATTACHING HOLES. (X)SDR 20000531SH015Hub · crackedRELEVANT ET INDICATION, CRACK OUTER MOST THREAD, BOTH SIDES. (X)SDR AU990852Bracket · corroded(AUS) CENTER RUDDER SUPPORT BRACKET CONTAINED SEVERE EXFOLIATION CORROSION. TWO RIVETS MISSING. MAIN FUEL CELLS ALSO LEAKING.SDR 99ZZZX3105Bearing · failedNR 2 AND NR 3 CYLINDERS AND CONNECTING RODS REMOVED FROM BOTH ENGINES FOR C/W TCM CSB99-3. UPON REMOVAL OF THE CONNECTING RODS, THE ROD BEARINGS (SUPERIOR PN SA630826) WERE FOUND TO HAVE LOST SIGNIFICANT AMOUNT OF BABBITT MATERIAL. THE REMAINING CYLS AND CONSDR 99ZZZX2800Cylinder · brokenDURING CRUISE FLIGHT, LEFT ENGINE BEGAN TO RUN ROUGH. PILOT FEATHERED ENGINE. A NORMAL SINGLE ENGINE LANDING WAS MADE. FOUND NR 3 CYLINDER BROKEN HALF WAY BETWEEN FLANGE AND BOTTOM OF HEAD. PISTON CAME OUT AND BROKE. CASE BROKE ALSO, STEEL CYLINDER.SDR AU990479Spar · corroded(AUS) RIGHT WING TOP SPAR CAP CONTAINED EXFOLIATION CORROSION IN THREE AREAS.SDR AU980483Vent · blocked(AUS) DURING APPROACH, THE LT ENGINE LOST POWER. THE MAIN FUEL GAUGE READ HALF FULL AND THE LT MAIN TANK SHOWED EMPTY. INVESTIGATION FOUND THAT THE INBOARD FUEL VENT WAS BLOCKED CAUSING THE TANK FUEL BLADDER CELL TO COLLAPSE (SUCKED UP) AND PREVENTING THE FUSDR AU980304Relay · faulty(AUS) LANDING GEAR RELAY FAULTY. SUSPECT CAUSED BY INGRESS OF FOREIGN MATTER.SDR AU980238Fuel Cell · deteriorated(AUS) LT FUEL CELL DETERIORATED. DRAIN FITTING TORN. INTERNAL BAFFLE LOOSE.SDR 98ZZZX609Skin · crackedDURING RAMP INSPECTION, FOUND CRACK IN TOP SKIN JUST OUTBOARD OF OUTBOARD HINGE POINT. CRACK ALIGNED WITH CRACK IN SKIN P/N 96-610006-3. SUB-SURFACE STRUCTURE SHOWED NO DAMAGE, BUT CRACKED PAINT IN BALANCE WEIGHT ATTACH AREA INDICATES PREVIOUS STRESS. AIRCRSDR 98ZZZX608Skin · crackedDURING RAMP INSPECTION, FOUND CRACK IN TOP SKIN JUST OUTBOARD OF OUTBOARD HINGE POINT. CRACK ALIGNED WITH CRACK IN SKIN P/N 96-61006-49. SUB-SURFACE STRUCTURE SHOWED NO DAMAGE, BUT CRACKED PAINT IN BALANCE WEIGHT ATTACH AREA INDICATES PREVIOUS STRESS. AIRCRSDR 97ZZZX3700Bulkhead · crackedTHIS SPINNER BULKHEAD WAS A NEW PART THAT HAD ONLY 57 HOURS WHEN IT CRACKED. THE CRACK WAS LOCATED IN THE FRONT PLATE UNDER THE SCREW HEADS THAT HOLD THE PLATES THAT MOUNT THE BULKHEAD TO THE CRANKSHAFT. THE SPINNER WAS INSTALLED WITH THE PROPER AMOUNT OF SHSDR AU970170Battery · discharged(AUS) BATTERY VOLTAGE LOW - SUSPECT CAUSED BY ALTERNATOR SWITCHES BEING IN THE `OFF' POSITIONSDR AU970075Fitting · corroded(AUS) REAR SPAR RH WING FITTING CORRODED - WING BOLT, NUT AND WASHER ALSO CORRODED - FOUND DURING INSPECTION IAW AD/BEECH55/79SDR 96ZZZX4393Reservoir · av gas filledANNUAL INSPECTION FOUND PROPELLER AND WINDSHIELD ALCOHOL RESERVOIRS FILLED WITH 100LL AV GAS. SUSPSECT TANK MISTAKEN FOR HEATER FUEL TANK. FIRE HAZARD IF SYSTEM USED WITH ENGINES RUNNING. TANK IS PROPERLY MARKED FOR DE-ICER FLUID.SDR 96ZZZX4392Brake Disc · chafe scissorsFOUND RIGHT BRAKE DISC RUBBING GEAR SCISSORS. SUSPECT DISC ORDERED UNDER WRONG SERIAL NUMBERED AIRCRAFT. BRAKE DISC OFFSET .1250 INCH FROM PROPER P/N 164-27 DISC. AXLE SPACER AND SHIMS NOT PROPERLY INSTALLED TO MAKE UP CLEARANCE. FOUND DURING ANNUAL INSPECSDR EY2R9601570Hub · damagedPROP HUB OUTSIDE DAMAGESDR EY2R9600854Blade · corrodedBLADE, SN F12557YS, FOUND CORRODED.SDR EY2R9600853Blade · corrodedBLADE, SN F11710YS, FOUND CORRODED.SDR EY2R9600852Dowel · corrodedDOWEL CORRODED.SDR EY2R9600851Cylinder Pin · corrodedCYLINDER PIN FOUND CORRODED.SDR EY2R9600850Blade · corrodedBLADE, SN F14967YS, FOUND CORRODED.SDR EY2R9600849Dowel · corrodedDOWEL FOUND WITH CORROSION.SDR EY2R9600848Cylinder Pin · corrodedCYLINDER PIN CORRODED.
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