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 = '182F' 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 = '182F' 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 2025FA0000683Torque Link · brokenNOSE GEAR UPPER TORQUE LINK BROKE CAUSING GEAR TO COLLAPSE UPON TOUCHDOWN.SDR 2021FA0000418Selector Valve · bypassingTHE FUEL SELECTOR VALVE WOULD NOT STOP THE FLOW OF FUEL IN ANY OF THE FOUR DETENTS (OFF-LEFT-BOTH-RIGHT) AT THE FIREWALL FUEL GASCOLATOR DURING AN ANNUAL INSPECTION. THE AIRPLANE HAD SAT IDLE FOR APPROXIMATELY 8 YEARS WITH THE FUEL TANKS FULL. AS I WAS ABOUTSDR 2011FA0000417Spring Assy · brokenLEFT MAIN GEAR SPRING BROKE ON TAXI TO TAKEOFF. CRACK WAS LOCATED INSIDE THE SADDLE AREA WHICH PREVENTED ABILITY TO SEE CRACK THROUGH THE ACCESS PANNELS. THE ONLY WAY TO INSPECT THIS SPRING STRUT IS TO REMOVE THE GEAR STRUT FROM THE ACFT AND VISUALLY OR NDT SDR 2011FA0000143Muffler · obstructedTHE STARBOARD MUFFLER BAFFLE CONE BROKE LOOSE FROM THE MUFFLER HOUSING AND OBSTRUCTED THE EXHAUST PIPE, CREATING BACK PRESSURE IN THE EXHAUST SYSTEM WHICH CAUSED THE ENGINE TO LOSE POWER. THE SUBSEQUENT FORCED LANDING ACCIDENT SUBSTANTUALLY DAMAGED THE AIRCRAFSDR AU510001998Rocker · deterioratedROCKER ARMS (2OFF) HAD HARD FACING FAILURE. FOUND DURING INSPECTION IAW AD/ENG/4 AMDT9.SDR AUS20040446Spar · corroded(AUS) RT WING MAIN SPAR ANGLE CONTAINED EXFOLIATION CORROSION IN AREA OF WING ATTACHMENT ANGLE.SDR CA040622003Crankcase · cracked(CAN) CRANKCASE WAS DISCOVERED CRACKED NEAR OIL CAP LOCATION. CRANKCASE REPLACED.SDR AUS20030651Angle · corroded(AUS) LT WING FRONT SPAR CAP ANGLE CORRODED.SDR AUS20030650Plate · corroded(AUS) LT WING FRONT SPAR CAP DOUBLER PLATE CONTAINED INTERGRANULAR CORROSION.SDR N3571YControl Wheel · strippedON ROUTINE SKYDIVING FLIGHT, THE APPROPRIATELY RATED AND QUALIFIED PILOT ENTERED A CROSS CONTROL MANEUVER TO CLOSE CABIN DOOR. UPON RETURNING TO NORMAL FLIGHT THE PIC EXPERIENCED LOSS OF AILERON CONTROL EXHIBITED BY CONTROL WHEEL ROTATING 360 DEGREES WITH NO SDR AUS20021071Seat Track · cracked(AUS) LT FRONT SEAT OUTBOARD SEAT TRACK CONTAINED NUMEROUS CRACKS.SDR AUS20021070Bulkhead · cracked(AUS) REAR BULKHEAD LOCATED AT STA 309.187 CRACKED.SDR FGQ2001F00000Fitting · corrodedINSPECTION OF LEFT WING ASSEMBLY REVEALED SEVERE EXFOLIATION CORROSION OF WING ATTACH FITTING (FWD) EXTENDING, APPROXIMATELY 18 INCHES OUTBOARD WING SKIN WAS LIFTED UP FROM SPAR.SDR CA001205020Tire · failed(CAN) SMALL HUMP IN TREAD AT ONE SPOT IN CIRCUMFERENCE OF TIRE. DEFECT WAS NOTED WHEN MOVING AIRCRAFT BY HAND AND TREAD GROOVES APPEARED TO SPREAD APART AT THIS SPOT. SUSPECT PARTIAL FAILURE OF REINFORCING PLIES BENEATH THE SURFACE. THERE IS NO VISIBLE TRAUMSDR 20000821SH003Bulkhead · crackedDURING ANNUAL INSPECTION, CRACK FOUND UPPER PORTION OF LEFT RUDDER CABLE CUT OUT ON TAIL BULKHEAD. AD 72-07-09 CRACKS AND LOOSE BOLTS RUDDER/FIN LAST C/W 4/94 AT ACFT TOTAL TIME 3,845 HOURS BY DYE PENETRANT AND VISUAL INSPECTION. NO DEFECTS WERE NOTED AT THASDR AU990751Angle · corroded(AUS) RIGHT WING SPAR CAP TOP ANGLE CONTAINED INTERGRANNULAR CORROSION IN THE AREA FROM WS 76 TO WS 118.SDR 98ZZZX1660T-Fitting · crackedINSPECTION FOR AN OIL LEAK FOUND THE T-FITTING THAT FEEDS OIL PRESSURE TO BOTH TURBOS WAS CRACKED. THE FITTING IS LOCATED JUST AFT OF THE LEFT TURBO. IF THE LEAK HAD GONE UNNOTICED, THERE IS A SUBSTANTIAL POSSIBILITY OF AN ENGINE FIRE. RECOMMEND USING BRASSSDR 98ZZZX1467Yoke · failedCONTROL YOKE FAILURE ON LANDING. CONTROL YOKE BROKE, FAILED IN UPPER LEFT SIDE. AIRCRAFT MANUFACTURED IN 1963. SUSPECT CAUSE EXTREME AGE OF PLASTIC PART. AIRCRAFT AND CONTROL YOKE TT 2,800 HOURS.SDR CA970603012Piston · worn(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PISTON FOUND WORN, PISTON REPLACED.SDR 98ZZZX550Yoke · failedWHILE CHECKING ELEVATOR TRAVEL, YOKE BROKE WHEN BROUGHT UP AGAINST ELEVATOR STOP LEAVING BROKEN PART IN HAND. RECOMMEND PULL TEST.SDR EY2R9601208Bearing · corrodedBALL BEARING CORRODED.SDR AU961145Seat Belt · wrong part(AUS) BOTH REAR SEATS FITTED WITH AUTOMOTIVE SEAT BELTS - UNAPPROVED PART - PERSONNEL/MAINTENANCE ERRORSDR AU961035Balance Tube · separated(AUS) ENGINE INDUCTION SYSTEM BALANCE TUBE SEPARATED AT ONE END - MOUNT ALSO BROKEN AWAY FROM TUBESDR 95ZZZX605Valve · excess wearCONTINENTAL O470F ENGINE WITH ONLY 165 HOURS SINCE FACTORY REMANUFACTURE. EXHAUST VALVE STEMS SHOW EXTREME WEAR. FOUND VALVE GUIDES TO BE NITRALLOY.
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