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 = 'R182' 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 = 'R182' 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 95ZZZX6445Hose · leakingHOSE USED AS COUPLING BETWEEN RIGID FUEL LINES MADE OF ALUMINUM TUBING, FOUND BADLY DETERIORATED AND LEAKING FUEL. THIS LINE IS LOCATED AT PILOT'S WINDSHIELD POST AND LINE IS ROUTED ALONG WITH ELECTRICAL WIRING. ANY SPARKS COULD RESULT IN A VERY SERIOUS CONDSDR 95ZZZX6429Fitting · crackedFAILED FITTING IS USED TO ATTACH THE RIGHT MAIN GEAR SPRING TUBE TO THE AXLE. ON ANNUAL INSPECTION, FOUND A ONE INCH CRACK PARALLEL TO TUBE STARTING ON THE BOTTOM OF THE MACHINED HOLE THAT THE SPRING TUBE GOES INTO. IT APPEARS THAT CRACK HAPPENED BECAUSE OF SDR 95ZZZX6928Capacitor · faultyENGINE EXPERIENCED EXTREME ROUGHNESS AND HIGH RPM DROP ON LEFT POSITION OF 1800 RPM MAG CHECK. NR 4 AND NR 5 CYLINDERS WENT COLD ON G.E.M. FOR 3 SUCCESSIVE CHECKS. PLUGS AND WIRES CHECKED OK TO BOTH CYLINDERS. MAG WAS REMOVED AND INSPECTED WITH NO OBVIOUS DSDR 95ZZZX4430Gear Assy · teeth brokenLEFT MAGNETO WAS REPORTED INOPERATIVE. FOUND APPROXIMATELY ONE-THIRD OF THE LEFT DISTRIBUTION GEAR TEETH MISSING. BROKEN TEETH WERE SCATTERED THROUGHOUT THE MAGNETO. COULD HAVE DAMAGED THE RT PORTION OF THE MAGNETO. CAUSE IS UNKNOWN. NO GEAR HOLDING DEVICSDR 95ZZZX4570Hose · failedOIL COOLER TO ENGINE HOSE RUPTURED APPROXIMATELY 6 INCHES FROM FITTING. SUSPECT SOME KIND OF ACID PENETRATED THE HOSE IN ONE SPOT APPROXIMATELY 3 INCHES TO 3.50 INCHES AND DETERIORATED THE METAL AWAY. HOSE LINING FAILED ON A REAL HOT DAY AND PUMPED ALL THE OSDR 95ZZZX4520Control Cable · chafedTHROTTLE CABLE HOUSING CHAFES LANDING GEAR RELAY AND HAS WORN DEEPLY INTO RELAY HOUSING. SPLIT 2 INCH LONG PIECE OF MIL-H-6000, .3125 INCH, HOSE. PLIOBOND GLUE AND TYE-WRAP HOSE IN PLACE. NOTE: PROBLEM FOUND DURING ANNUAL INSPECTION.SDR 95ZZZX3463Rib · crackedCRACK NOTED IN INBOARD RT FLAP TRACK RIB IN LOWER CORNER WHERE RIB SECURES TO REAR SPAR WITH FOUR .1875 INCH FASTENERS. UPON REMOVAL, DISCOVERED THE TWO .1875 FASTENERS WERE SHEARED WITH NO WAY OF DETECTING VISUALLY. FOUND .1250 INCH RIVET SECURING THE REINFSDR 95ZZZX3206Reinforcement · crackedACTT 3,957.8. OPERATOR DISCOVERD 1 INCH CRACK AT LEFT HORIZONTAL STABILIZER REAR SPAR ATTACH POINT REINFORCEMENT BRACKET, OUTBOARD HOLE IN BEND RADIUS (LOWER). DEFECT FOUND DURING PRE-FLIGHT. THIS IS THE SECOND OCCURRENCE AT 2202.1 TOTAL TIME. OPERATOR REPSDR 95ZZZX3229Motor · seizedDURING FLIGHT, LANDING GEAR WOULD NOT DOWN AND LOCK UNDER ITS OWN POWER. DOWN AND LOCK WAS ACCOMPLISHED BY EMERGENCY HAND PUMP EXTENSION. DISASSEMBLY AND INSPECTION OF POWERPACK ASSY FOUND MOTOR SEIZED. DISASSEMBLY AND INSPECTION OF MOTOR FOUND CARBON BRUSHSDR 95ZZZX3007Casting · creepTHE END SHAKES ON ALL 3 OF THE CRITICAL MECHANISM SHAFTS WERE UNDER THE O/H MANUAL TOLERANCE. THEY MEASURED .0002 INCH, .0009 INCH, AND .0009 INCH. THE .0002 INCH END SHAKE WAS ON THE WHEEL ASSY SHAFT.SDR 95ZZZX2891Control Cable · frayedFLAP INDICATOR CABLE HAS A RECURRING PROBLEM WITH THIS CABLE. FIRST ONE LASTED 1550 HRS, NR 2 1949 HRS, NR 3 APPROXIMATELY 1600 HRS. IT APPEARS CABLE RUBS ON HOUSING WHERE CABLE EXITS AND ATTACHES TO FLAP CABLE BECAUSE OF ANGLE. SUGGEST: TAPER WASHERS TO ASDR 95ZZZX1109Rib · brokenDURING ANNUAL, FOUND LEADING EDGE OF HORIZONTAL STABILIZER HAD SAME MOVEMENT AS 200 SERIES CESSNAS WITH BROKEN RIBS. DISASSEMBLY SHOWED THAT 3 RIBS ON RIGHT AND 4 RIBS ON LEFT SIDE WERE BROKEN. REPLACED RIBS AND SKINS.SDR 95ZZZX1108Rib · brokenDURING ANNUAL, FOUND LEADING EDGE OF HORIZONTAL STABILIZER HAD SAME MOVEMENT AS 200 SERIES CESSNAS WITH BROKEN RIBS. DISASSEMBLY SHOWED THAT 3 RIBS ON RIGHT AND 4 RIBS ON LEFT SIDE WERE BROKEN. REPLACED RIBS AND SKINS.SDR 95ZZZX1107Rib · brokenDURING ANNUAL, FOUND LEADING EDGE OF HORIZONTAL STABILIZER HAD SAME MOVEMENT AS 200 SERIES CESSNAS WITH BROKEN RIBS. DISASSEMBLY SHOWED THAT 3 RIBS ON RIGHT AND 4 RIBS ON LEFT SIDE WERE BROKEN. REPLACED RIBS AND SKINS.SDR 95ZZZX1106Rib · brokenDURING ANNUAL, FOUND LEADING EDGE OF HORIZONTAL STABILIZER HAD SAME MOVEMENT AS 200 SERIES CESSNAS WITH BROKEN RIBS. DISASSEMBLY SHOWED THAT 3 RIBS ON RIGHT AND 4 RIBS ON LEFT SIDE WERE BROKEN. REPLACED RIBS AND SKINS.SDR 95ZZZX790Impulse Coupling · failedAIRCRAFT WOULD NOT START. FLYWEIGHTS WORE OUT PER INSPECTION REQUIRED IN AD 78-09-07. THIS WAS THE NEW SNAP-ON TYPE COUPLING ALSO.SDR 95ZZZX1101Distributor Gear · teeth strippedACFT WAS FLOWN ON THE PREVIOUS EVENING. NO PROBLEMS NOTED. NEXT MORNING, ACFT WOULD NOT START. AFTER TROUBLESHOOTING ACFT, FOUND MAGNETO PROBLEMS UPON DISASSEMBLY OF MAG. BOTH DISTRIBUTOR GEARS WERE SEVERELY DAMAGED (TEETH WERE STRIPPED FROM BOTH GEARS). SDR 95ZZZX962Carburetor · pump bindingCARBURETOR ACCELERATOR PUMP STICKING OR BINDING CAUSING EXTREMELY DIFFICULT THROTTLE OPERATION. THIS WAS A FACTORY REMANUFACTURED ENGINE WITH A NEW CARBURETOR. TIME IN SERVICE IS 23.0 HOURS. THIS HAS OCCURRED ONCE BEFORE ON THE SAME MODEL CARBURETOR, ON A DSDR 96ZZZX4741Pivot · defectiveAIRCRAFT REPORTED COMPLETE LOSS OF RT BRAKE. DETERMINED PIVOT CRACKED PER SEB 90-1, REV 2. THIS WAS NEW STYLE PIVOT. WHILE FITTING NEW PIVOT, DETERMINED LOAD OF AIRCRAFT WAS BEING CARRIED BY BUSHING 2241120-1 BECAUSE OF CLOSER FIT. THE MAIN SUPPORT BUSHINGS
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