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 = 'A36TC' 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 = 'A36TC' 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 2016FA0000083Motor · failedBRUSH BROKE LOOSE AND LODGED IN MOTOR. MOTOR SHORTED AND SMOKE ENTERED THE COCKPIT.SDR 2013FA0000569Nipple · failedFUEL CELL WAS INSTALLED 8-15-12. MAIN FUEL NIPPLE FAILED, DEBONDED FROM INSIDE OF TANK. ACFT HAD FULL TANKS AND DUMPED ALL FUEL IN RT TANK IN FLIGHT.SDR 2011FA0000405Rotor · openALTERNATOR ROTOR OHM CHECK INFINITE.SDR 2004FA0000750Bolt · incorrectAFT UPPER LT WING ATTACH BOLT FOUND INSTALLED AND PRESUMABLY TORQUED WITHOUT CHAMFERED WASHER UNDER HEAD. DAMAGE TO BATHTUB FITTING UNKNOWN AT THIS TIME.SDR FTU2004F00005Seal · damagedAC ENGINE WAS DRIPPING OIL. ALL CYLINDERS LOOKED LIKE THEY HAVE BEEN REPLACED RECENTLY. FURTHER INVESTIGATION REVEALED MOST OF PUSH ROD HOUSING SEALS AT CYLINDER HEAD ATTACH POINT WERE DAMAGED OR NOT PROPERLY INSTALLED. IT HAS ALSO BEEN NOTICED THAT ECI PUSSDR BWV2004F00000Housing · crackedWHILE AIRCRAFT WAS UNDERGOING AN ANNUAL/PREBUY INSPECTION, IT WAS NOTED UPON EXAMINATION OF THE TURBOCHARGER OUTLET THAT A CRACK WAS FOUND RADIATING AROUND THE V-BAND CLAMP AREA. A SMALL AMOUNT OF MATERIAL REMAINED ATTACHING THE TAILPIPE TO TURBOCHARGER. LOSSDR S5M2004F00000Pump · failedTHE PILOT WAS FLYING IN CLEAR WEATHER. SUDDENLY HE LOST ALL INSTRUMENT AIR PRESSURE. THIS IS A DUAL PUMP AND BOTH PUMPS FAILED AT THE SAME TIME. WHEN PUMP WAS REMOVED, THE DRIVE SHAFT COULD BE PULLED OUT OF THE PUMP ABOUT 2 INCHES. WHEN SPOKE WITH THE MFG SDR 3739Spacer · missingTHESE BUSHINGS ARE LOCATED BETWEEN THE CONTROL COLUMN TORQUE KNEES, LOCATED BEHIND THE INSTRUMENT PANEL. THE SPACERS WERE FOUND MISSING WHILE INVESTIGATING EXCESSIVE PLAY IN THE TORQUE KNEES.SDR 2002FA0000455Shaft · oversizedTHE ORIGINAL LANDING GEAR ACTUATOR GEARBOX WAS BEING REMOVED AND DISASSSMBLED FOR A ROUTINE OVERHAUL. DIFFICULTY WAS ENCOUNTER WHEN TRYING TO REMOVE THE ACTUATOR SHAFT FROM THE GEARBOX HOUSING. IT WAS NOTED THAT THE FORCE REQUIRED TO SLIDE THE SHAFT OUT WAS SDR HP62002F00000Valve · brokenFLAPPER ASSEMBLY, HAS BROKEN AWAY FROM HINGE SHAFT AND WAS EJECTED OUT EXHAUST STACK. CAUSE IS THOUGHT TO BE VIBRATION (METAL FATIGUE).SDR 20000412SH009Battery · shortedWHILE PILOT WAS COMPLETING THE BEFORE TAKEOFF CHECK LIST, A COMPLETE ELECTRICAL SYSTEM FAILURE WAS EXPERIENCED. INITIAL INVESTIGATION REVEALED NO CIRCUIT BREAKERS, FUSES, OR CURRENT LIMITERS HAD FAILED TO OPEN. THE BATTERY WAS FOUND SMOKING. UPON REMOVING TSDR 97ZZZX813Switch · failedON PRE-INSPECTION RUN UP, IT WAS NOTED THAT THE ENGINE WAS NOT PRODUCING ACCEPTABLE POWER. DISCOVERED IGNITION SWITCH WAS STILL IN THE 'START' POSITION. WHEN PHYSICALLY SWITCHING BACK TO THE 'BOTH' POSITION, THE ENGINE RESUMED NORMAL POWER. TRYING SWITCH SESDR 96ZZZX4067Wye Pipe · crackedCRACKED IN FRONT OF ASSY NEAR CENTER SUPPORT BOSS. SUBMITTER STATES VERY HARD TO SEE DUE TO LOCATION AND BLACK COATING OF PART. SUGGEST DIFFERENT COLOR AND REDESIGNED PART MADE OUT OF THICKER MATERIAL.SDR 96ZZZX4066Bar · crackedDUE TO LOCATION OF ENGINE STABILIZER BAR, CRACK COULD NOT BE SEEN AT FIRST INSPECTION, ONLY FOUND UPON REMOVAL. LAST PART INSPECTION AT LAST ENGINE OVERHAUL, 387 HOURS.SDR 95ZZZX6751Rib · crackedINSPECTION FOUND CRACKED FLAP RIB AT ACTUATOR ATTACH POINT.SDR 95ZZZX3678Pump · gear failedSCAVAGE PUMP DRIVE GEAR FRACTURED IN 4 LOCATIONS FOLLOWING HEAVY WEAR OF TOOTH PROFILE. TOTAL ENGINE FAILURE FOLLOWED. AD 89-24-01R1 AND SB M90-6 PERTAIN TO THIS PUMP, BUT WERE NOT DUE YET.SDR 95ZZZX4359Regulator · failedUPON GEAR RETRACTION DURING A 'GO-AROUND', THE CHARGING SYSTEM WENT INTO A HIGH-VOLTAGE RUNAWAY. THE OVERVOLTAGE RELAY DID NOT TRIP TO PROTECT THE SYSTEM. THE BATTERY MASTER RELAY BURNED OUT. WITHOUT THE BATTERY IN THE CIRCUIT, THE VOLTAGE WENT VERY HIGH ANSDR 95ZZZX1148Cylinders · excess wornFACTORY NEW CYLINDERS TT 581.4 HOURS. INSTALLED 2-1-91, LOW COMPRESSION ALL CYLINDERS. CYLINDERS ARE WORN BEYOND SERVICEABLE LIMITS AND HAVE SEVERE RING WEAR. ROCKER SHAFTS ARE SEVERELLY WORN AND UNAIRWORTHY.
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