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 = 'T310Q' 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 = 'T310Q' 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 2020FA0000451Tube · brokenIN PREPARATION FOR SLOW FLIGHT DURING A COMMERCIAL PILOT CHECK RIDE, LANDING GEAR EXTENSION WAS ACCOMPLISHED. AN UNUSUAL YAW WAS EXPERIENCED WITH UNUSUAL NOISE FROM THE LEFT MAIN LANDING GEAR. THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. GEAR WAS RESDR 2008FA0000411Rod End · brokenAFTER TAKEOFF, WHEN RETRACTING GEAR, PILOT HEARD LOUD CRACK. NOSE GEAR WOULD NOT RETRACT. AIRCRAFT LANDED WITH NOSE GEAR TRAILING AFT. NOSE GEAR COLLAPLSED ON LANDING. INSPECTION REVEALED ROD END UNDER PILOT`S FLOOR THAT CONNECTS NOSE GEAR RETRACT ROD TO BSDR 2007FA0000713Cylinder · leakingWHILE PERFORMING OTHER MAINTENANCE A FUEL STAIN WAS NOTICED BETWEEN THE SECOND AND THIRD COOLING FIN AFT OF THE FUEL INJECTOR ON THE NR 6 CYLINDER OF THE RT ENGINE. THIS CONDITION PROMPTED A CLOSER INSPECTION OF THE ENGINE RESULTING IN THE DISCOVERY OF SIMILASDR 2007FA0000625Bellcrank · failedFAILED DUE TO MECHANICAL OVERLOAD, NOSE GEAR JAMMED. (K)SDR 2006FA0001058Pitot Line · corrodedDURING A ROUTINE PITOT/STATIC TEST, FOUND THAT THE PITOT SYSTEM WAS LEAKING BEYOND LIMITS. THE LEAKAGE WAS DETERMINED TO BE IN THE TUBING FROM THE PITOT TUBE TO THE FORWARD CABIN BULKHEAD FITTING. UPON REMOVING THE TUBE (PN 0800106-379) SEVERE CORROSION WAS SDR HXR2004F00000Adc · malfunctionedADC AND ALTIMETER READING 2000 FT DIFFERENCE.SDR 2004FA0000853Rod End · brokenTHE AIRCRAFT DEPARTED. A LARGE NOISE WAS HEARD, COULD NOT EXTEND NOSE GEAR. LANDED WITH AN UNSAFE NOSE GEAR UP, NOSE GEAR COLLAPSED ON LANDING CAUSING DAMAGE. THE ROD END FAILED ON TUBE ASSY. NOTE: THIS IS A COMMON PROBLEM ON THE AK. (SW05200408481)SDR DYT2003F00000Bellcrank · brokenPILOT REPORTED BANG COMING FROM UNDER HIS FEET WHEN GEAR WAS RETRACTED. WHEN GEAR WAS EXTENDED THE NOSE GEAR DID NOT LOCK. AIRCRAFT LANDED AND NOSE GEAR COLLAPSED. INVESTIGATION FOUND THAT NOSE GEAR IDLER BELLCRANK, BROKEN.SDR 2003FA0000036Bellcrank · brokenTHE IDLER BELLCRANK FOR THE NOSE GEAR RETRACTION LINKAGE BROKE WHEN THE LANDING GEAR WAS SELECTED TO THE UP POSITION. PILOT WAS UNABLE TO EXTEND THE NOSE GEAR. UPON LANDING THE NOSE GEAR RETRACTED INTO THE WHEEL WELL. INSPECTION REVEALED THAT THE IDLER BELLSDR CA030211008Actuator · failed(CAN) CJ0701 ACTUATOR TAB IS A SMALL METAL TAB THAT FITS ON PORT GEAR DOWN SWITCH. TAB FAILED DUE TO METAL FATIGUE CAUSING INTERMITTENT GEAR SAFE LIGHT ON PORT SIDE.SDR 2002FA0001085Clamp · crackedTHIS CLAMP ATTACHES TAILPIPE TO TURBOCHARGER OUTLET. DURING COMPLIANCE WITH AD2000-1-16 FOUND CLAMP SPLIT AT THE APEX OF THE "V" AROUND 4.75" TO 5.0" OF CIRCUMFERENCE. PER AD2000-1-16 THIS CLAMP IS NOT LIFE-LIMITED.SDR 20010312CW010Bracket · crackedAC WAS IN THE HANGAR FOR 50 HOUR INSPECTION. STROBE LIGHTS WERE TURNED ON AND AN EXPLOSION DAMAGED THE LEFT WING TIP TANK. FWD FAIRING WAS BLOWN APART BY AN EXPLOSION. FOUND THE FWD TANK ACCESS PANEL SPOT WELDS FOR THE NAV/STROBE LIGHT BRACKETS WERE CRACKED,SDR 20000427SH031Hub · crackedPART CRACKED FROM GREASE FITTING HOLE ACROSS BACK OF HUB TO OPPOSITE SIDE. SENT TO HARTZEL PROPELLER FOR EVALUATION. (X)SDR 20000427SH030Hub · crackedRAM A/C ENGINE AND PROPELLER MODIFICATIONS PER STC NR SA 4011SW. (X)SDR 2000ZZZX225Fitting · unapproved partNOTE: FITTING WAS STEEL SUBMITTER STATED FITTING LOOKED HOMEMADE. INSTALLED FORGED NEW CORRECT CESSNA PART MADE FORM ALUMINUM. PART TOTAL TIME UNKNOWN.SDR 2000ZZZX224Deice System · inoperativeNOTED THAT DE-ICE FOR VERTICAL STABILIZER INOPERATIVE. FURTHER INVESTIGATION REVEALS HOSES TIED OFF. REPLACED HOSES, PATCHED BOOT. OPS CHECKED, WORKS FINE. TOATL TIME AT INSTALLATION UNKNOWN.SDR EY2R9600334Blade · corrodedBLADE, SN F45244YS, FOUND CORRODED.SDR EY2R9600333Blade · corrodedBLADE, SN F45225YS, FOUND CORRODED.SDR EY2R9600332Blade · corrodedBLADE, SN F45471YS, FOUND CORRODED.SDR EY2R9600331Hub · corrodedHUB FOUND CORRODED.SDR EY2R9600326Hub · corrodedHUB FOUND CORRODED.SDR EY2R9600322Ferrule · corrodedCORROSION FOUND ON FERRULE.SDR EY2R9600320Feather Cylinder · corrodedFEATHER CYLINDER FOUND WITH CORROSION.SDR EY2R9600317Retain Bearing · corrodedRETAIN BEARING FOUND CORRODED.SDR 95ZZZX3227Exhaust Riser · hole burnedDURING DEPARTURE CLIMB, THE EXHAUST RISER ON THE LEFT ENGINE NR 2 CYLINDER DEVELOPED A HOLE ON THE LOWER SIDE. PRIOR TO THE FAILURE OF THE PART IT APPEARED TO BE IN GOOD CONDITION. DURING THE PRECEDING FEW HOURS OF FLIGHT THE AIRCRAFT WAS USED FOR FLIGHT TRA
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