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 = '182D' 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 = '182D' 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 2015FA0000262Torque Tube · looseWHILE INSPECTING THE ACFT, NOTICED RIVETS LOOSE ON ELEVATOR TORQUE TUBE WHERE THE TORQUE TUBE ATTACHES TO THE PYLON ASSEMBLY.SDR FAA20140228000106Block · damagedBEARING BLOCK FOUND DAMAGED.SDR 2012FA0000270Contact · loosePILOT REPORTED A HIGH MAGNETO DROP. UPON INSPECTION THE LT MAGNETO WOULD NOT TIME CONSISTENTLY. REMOVED AND DISASSEMBLED THE MAGNETO AND FOUND 1 SIDE OF THE CONTACT POINT TO BE VERY LOOSE.SDR 2006FA0000816O-Ring · splitTHE RT FUEL TANK CAP O-RING SPLIT AND FUEL SIPHONED OUT OF THE RT TANK DURING FLIGHT.SDR AU510001443Skin · cracked(AUS) LH AND RH WING FLAP SKINS CRACKED. WHEN THE SKINS WERE REMOVED FOR REPLACEMENT, INTERNAL CORROSION WAS ALSO FOUND.(OTHER CAUSE: AGE ) (CASA# 510001443)SDR 2004FA0000321Cylinder · damagedCOULD NOT GET ENGINE TO RUN PROPERLY. COMPRESSION GOOD ON NR 6, FINALLY DETERMINED NR 6 WAS NOT OPERATING PROPERLY. REMOVED CYLINDER, SENT FOR OVERHAUL. FOUND HOLE IN EXHAUST VALVE PORT. (VOID IN THE CYLINDER CASTING) CYLINDER REJECTED AND RETURNED WITH LESDR 2002FA0000088Handle · strippedWHILE INVESTIGATING A COMPLAINT OF A DEFECTIVE DOOR LATCH IT WAS DISCOVERED THAT THE INTERNAL SPLINES OF THE DOOR HANDLE WERE STRIPPED.SDR 20000908SH011Rotor · overheatedMAGNETO DISASSEMBLED FOR 500-HOUR MAINTENANCE, BALL BEARINGS, PN 1081806 AND PN 2202, FROM ROTATING MAGNET ASSY WERE OBSERVED TO HAVE A SMOKY-BLUE CAST. ROTOR WAS RE-ASSEMBLED IN CASE HALVES TO FACILITATE SHAFT END PLAY CHECK WITH DIAL INDICATOR. PER SERVICESDR AU990754Screw · loose(AUS) CARBURETOR FLOAT TO BODY ATTACHMENT SCREWS LOOSE ALLOWING THE FLOAT TO CONTACT THE BODY AND PREVENT CLOSING OF THE NEEDLE AND SEAT. CARBURETOR FLOODING.SDR 98ZZZX3429O-Ring · failedO-RING SWELLED PREVENTING FUEL SELECTOR PORT FROM OPENING.SDR AU980489Guide · worn(AUS) DURING PERIODIC INSPECTION, NR 4 CYLINDER COMPRESSION WAS 20/80. THE EXHAUST VALVE P/N 646286 WAS REMOVED AND FOUND TO BE WORN 0.203 MM (0.008 INCH) JUST ABOVE STEM NECK. THE VALVE GUIDE P/N 643767 WAS WORN 0.457 MM (0.018 INCH) AT THE LOWER HALF AREA.SDR 98ZZZX489Bearing Block · corrodedUPON REMOVING BOTH WINGS TO INSTALL MONARCH PLASTIC FUEL TANKS, THE REAR SPAR INBOARD ATTACH BLOCKS, LEFT AND RIGHT, WERE FOUND TO HAVE INTERGRANULAR CORROSION IN THE INBOARD SLOT AREA ABOVE THE LARGE BOLT HOLES. CORROSION AREA ABOUT .50 INCH WIDE BY .1250 INSDR AU970265Spar · corroded(AUS) CENTRE SECTION REAR CARRY THROUGH SPAR CORRODED - SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970264Bulkhead · corroded(AUS) FORWARD CENTRE BULKHEAD LOCATED UNDER FLOOR SEVERELY CORRODED - SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970263Rudder · corroded(AUS) RUDDER CORRODED - SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970262Elevator · corroded(AUS) LH AND RH ELEVATORS CORRODED - SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970261Stringer · corroded(AUS) FUSELAGE STRINGERS CORRODED - SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970260Bulkhead · corroded(AUS) REAR FUSELAGE BULKHEAD CORRODED IN AREA OF DORSAL FIN ATTACHMENT- SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970259Skin · corroded(AUS) FUSELAGE SKINS CORRODED IN AREA OF ALL SKIN JOINTS IN BOTTOMS OF BOTH CABIN ENTRY DOORS AND DOOR HINGE ATTACHMENT AREAS, CABIN ROOF CORRODED - SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970258Aileron · corroded(AUS) LH AND RH AILERONS CORRODED - SEE MDR 97/0252 FOR ADDITIONALINFORMATIONSDR AU970257Flap · corroded(AUS) LH AND RH WING FLAPS CORRODED - SEE MDR 97/0252 FOR ADDITIONALINFORMATIONSDR AU970256Skin · corroded(AUS) LH AND RH WING TOP AND BOTTOM SKINS CORRODED - WING INSPECTION PANELS ALSO CORRODED - SOME RIVETS MISSING - SEE MDR 97/0252 FORADDITIONAL INFORMATIONSDR AU970255Rib · corroded(AUS) LH AND RH WINGS CORRODED IN AREA BETWEEN RIBS AND SKIN - SEE MDR97/0252 FOR ADDITIONAL INFORMATIONSDR AU970252Spar · corroded(AUS) LH WING FRONT MAIN SPAR CORRODED - SEE MDR 97/0255 TO MDR 97/0265 FOR ADDITIONAL DEFECTS REPORTED UNDER THE SAME MDR NUMBERSDR AU970251Bulkhead · cracked(AUS) FUSELAGE LH BULKHEAD CRACKEDSDR AU970249Spar · cracked(AUS) WING REAR SPAR CRACKED IN RADIUS OF WING ATTACHMENT WEBSDR 95ZZZX5883Lifter · failureINSPECTION FOR ENGINE MAKING METAL FOUND LIFTERS AND CAMSHAFT FAILURE. LIFTER P/N SA628488, P/N SA646277.
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