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 = 'Z242L' 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 = 'Z242L' 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 CA111004002Magneto · failed(CAN) DURING PERFORMANCE OF MAGNETO 500 HOUR INSPECTION, THE ELECTRODE FINGER OF THE DISTRIBUTOR BLOCK WAS OBSERVED LOOSE WITH THE ABILITY TO MIGRATE UP AND DOWN THE SHAFT OF THE DISTRIBUTOR GEAR. THE DISTRIBUTOR CAP WAS OBSERVED WITH GROOVES AND PITTING. PRSDR CA110331025Distributor Blk · loose(CAN) WHILE INVESTIGATING A ROUGH RUNNING ENG, DISCOVERED THE DISTRIBUTOR FINGER ON THE DISTRIBUTOR GEAR LOOSE.SDR CA101019011Nut · splitTHE PROP NUT SPLIT DURING THE RE-TORQUING SEQUENCE FOLLOWING PROP REMOVAL FOR SCHEDULED DE-SLUDGING. THE TORQUE VALUES WERE WITHIN LIMITS.SDR CA101004003Impulse Coupling · looseA LOOSE RIVET WAS FOUND ON THE IMPULSE COUPLING DURING SCHEDULED MX.SDR CA100909003Control Cable · frayedFLAP CENTER CABLE FOUND FRAYED DURING 100 HR.SDR 2010FA0000463Control Cable · frayedFOUND FLAP CABLE STRANDS BROKEN.SDR 2010FA0000462Control Cable · frayedFOUND FLAP CABLE STRANDS BROKEN.SDR 2010FA0000461Control Cable · frayedFOUND FLAP CABLE STRANDS BROKEN.SDR CA100212001Strut · broken(CAN) WHILE A 50HR INSP WAS BEING CARRIED OUT ON THE ACFT, IT WAS DISCOVERED THAT THE EXHAUST STRUT WAS BROKEN IN HALF APPX MID SECTION OF THE SHAFT. IT WAS OBSERVED THAT THERE WERE NO SIGNS OF CORROSION, BENDING, OR OBVIOUS DAMAGE TO THE PART TO CAUSE IT TO FSDR CA100120002Tube Frame · cracked(CAN) A CRACK WAS DISCOVERED IN THE AIRFRAME TUBING STRUCTURE FWD OF THE LT RUDDER PEDAL TORQUE TUBE SUPPORT LOCATION. THE CRACK WAS NOTED DURING A 100 HOUR INSP. THE CRACK APPEARED TO HAVE DEVELOPED QUICKLY WITHIN THE LAST 50 HOURS OF OPERATION. THE CRACK EXSDR CA100105002Impulse Coupling · broken(CAN) THE MECHANIC CONDUCTING A SCHEDULED 50 HOUR INSP NOTICED THAT THE IMPULSE COUPLING DID NOT HAVE THE USUAL "SNAP" WHILE ROTATING THE PROP. A PAWL SPRING WAS FOUND BROKEN AND THE REMAINING SPRING FELT VERY WEAK.SDR CA091210007Cable · frayed(CAN) THE RT STEERING CABLE WAS OBSERVED TO BE FRAYED DURING 500 HOUR INSP.SDR CA091127001Line · broken(CAN) THE LEFT BRAKE LINE WAS OBSERVED TO BE BROKEN AT A FLARE END. (TC NR 20091127001)SDR CA091112003Spring · broken(CAN) THE RT STEERING SPRING BROKE DURING TAXI FOLLOWING A FLIGHT.SDR CA091028006Wheel · cracked(CAN) A CRACK WAS IDENTIFIED ON THE OUTER EDGE OF THE WHEEL RIM RUNNING CIRCUMFERENTIALLY APPROX. 5 CM (TC 20091028006)SDR CA091001001Control Cable · frayed(CAN) THE FWD ELEVATOR TRIM CABLE WAS OBSERVED FRAYED DURING A 500 HOUR INSPECTION.SDR CA091001002Control Cable · frayed(CAN) BOTH RUDDER CABLES WERE OBSERVED FRAYED DURING A 500 HR INSP. BOTH CABLES WERE FRAYED IN AN AREA AROUND A PULLEY.SDR CA090922002Distributor Gear · loose(CAN) THE DISTRIBUTOR BLOCK GEAR FINGER WAS FOUND LOOSE DURING MX ON THE MAGNETO.SDR CA090916006Camshaft · making metal(CAN) DURING THE ANNUAL INSPECTION DEBRIS WAS FOUND IN THE ENGINE OIL SCREEN. FURTHER INVESTIGATION FOUND ADDITIONAL DEBRIS IN THE OIL FILTER. #3 CYLINDER WAS REMOVED AND INTERNAL COMPONENTS OF THE ENGINE INSPECTED. DEBRIS SOURCE WAS IDENTIFIED TO BE A CAM SHASDR CA090807001Control Cable · frayedTHE RT RUDDER CABLE WAS OBSERVED TO HAVE BROKEN STRANDS IN THE AREA AROUND A PULLEY DURING A 500 HOUR INSP. THE STRANDS WERE NOT OBSERVED AS BROKEN UNTIL THE CABLE TENSION WAS RELEASED AND THE CABLE DISASSEMBLED FROM THE AIRFRAME.SDR CA090626002Control Cable · frayed(CAN) BOTH LT AND RT RUDDER CABLES WERE DISCOVERED FRAYED DURING SCHEDULED MX.SDR CA090626001Control Cable · frayed(CAN) THE FLAP CONTROL CTR CABLE WAS DISCOVERED FRAYED DURING SCHEDULED MX.SDR CA090629004Tube · worn(CAN) THE ACFT RT TIRE WENT FLAT DURING REFUELING OPERATIONS. TIRE WAS REINFLATED IN ORDER TO BE PUSHED INTO THE HANGAR WHERE IT WENT FLAT AGAIN SHORTLY AFTERWARDS. TIRE AND TUBE WERE DISASSEMBLED. TUBE WAS WORN THROUGH BY DAMAGE TO THE INSIDE WALL OF THE TSDR CA090608004Control Cable · sheared(CAN) THE LT TRIM CABLE WAS THREADED THROUGH THE THE WASHER ON THE CABLE STOP AT MFG. TIGHTENING OF THE STOP NUT PERFORMS A SHEARING ACTION ON THE CABLE. THIS DEFECT HAS BEEN NOTED PREVIOUSLY.SDR CA090605001Control Cable · frayed(CAN) THE FWD ELEVATOR TRIM CABLE WAS DISCOVERED FRAYED DURING SCHEDULED MX.SDR CA090611005Crankcase · cracked(CAN) A 4-6 CM VERTICAL CRACK WAS NOTED BETWEEN NR 2 AND NR 4 CYL IN THE CRANKCASE DURING A 100 HR INSP. CRACK WAS SEEPING OIL.SDR CA090508002Control Cable · frayed(CAN) THE FWD ELEVATOR TRIM CABLE WAS DISCOVERED FRAYED DURING A SCHEDULED 500 HOUR INSP.SDR CA090430002Mount · cracked(CAN) THE ENGINE MOUNT WAS FOUND CRACKED IN THE UPPER RT MOUNT TO ENGINE ATTACH AREA.SDR CA090427004Stop Pin · worn(CAN) THE IMPULSE COUPLING STOP PIN WAS FOUND WORN BEYOND MFG LIMITS. IMPULSE COUPLING TSN 499.9 HOURS.SDR CA090421004Stop Fitting · misinstalled(CAN) THE TRIM STOP WAS OBSERVED TO BE ASSEMBLED INCORRECTLY ON THE CABLE. SUBSEQUENT TIGHTENING OF THE STOP NUT WOULD HAVE SHEARED THE CABLE AND LED TO IMMINENT FAILURE.SDR CA090421003Control Cable · frayed(CAN) THE AFT ELEVATOR TRIM CABLE WAS DISCOVERED WITH BROKEN STRANDS DURING SCHEDULED MX.SDR CA090324005Gear · inoperative(CAN) THE STARTER GEAR FAILED TO ENGAGE DURING OPS CHECK WHILE UNDERGOING SCHEDULED MX.SDR CA090324001Impulse Coupling · worn(CAN) THE IMPULSE COUPLING PAWLS AND STOP PIN WERE FOUND WORN BEYOND MFG TOLERANCES.SDR CA090310004Distributor Gear · loose(CAN) THE ELECTRODE FINGER ON THE DISTRIBUTOR GEAR WAS DISCOVERED LOOSE IN THE PERFORMANCE OF UNISON SB 3-08A DURING SCHEDULED MX. THE DISTRIBUTOR BLOCK ASSY HAD BEEN REPLACED JUST OVER 200 HOURS AGO.SDR CA090313001Control Cable · frayed(CAN) THE FWD ELEVATOR TRIM CABLE WAS DISCOVERED WITH BROKEN STRANDS DURING INSPECTION.SDR CA090310003Impulse Coupling · loose(CAN) ONE OF THE IMPULSE COUPLING PAWL RIVETS WAS DISCOVERED LOOSE IN THE PERFORMANCE OF SB 1-86C DURING SCHEDULED MX. THE IMPULSE COUPLING WAS THE ORIGINAL FOR THIS MAG.SDR CA090219002Control Cable · frayed(CAN) THE FLAP CENTER CABLE WAS DISCOVERED FRAYED DURING SCHEDULED MAINTENANCE.SDR CA090219001Control Cable · frayed(CAN) THE AFT TRIM CABLE WAS DISCOVERED FRAYED DURING SCHEDULED MAINTENANCE.SDR CA090305009Seal · leaking(CAN) THE PILOT HAD TO MAKE A PRECAUTIONARY LANDING ON A FROZEN LAKE. THE PILOT DETECTED SOMETHING BURNING AND NOTICED OIL SPLATTER ON THE RT SIDE OF THE CANOPY GLASS. WHILE REVIEWING HIS PRECAUTIONARY LANDING INFO IN THE FLIGHT MANUAL HE OBSERVED THE ENG OIL SDR CA090305006Oil System · low pressure(CAN) THE ACFT WAS ON A CROSS COUNTRY FLIGHT WHEN IT HAD TO MAKE A PRECAUTIONARY LANDING. THE PILOT OBSERVED THAT THE LOW OIL PRESSURE WARNING LIGHT HAD ILLUMINATED AND THAT THE ENGINE OIL PRESSURE HAD DROPPED INTO THE YELLOW RANGE, CONTINUING TO DROP INTO THESDR CA090119001Spring · broken(CAN) THE PILOT DISCOVERED THE STEERING SPRING BROKEN AFTER ENCOUNTERING ABNORMAL STEERING FUNCTION DURING TAXI.SDR CA080908005Spring · broken(CAN) FLAP SPRING LOCK WAS DISCOVERED CRACKED DURING SCHEDULED MX. SPRING BROKE COMPLETELY DURING REMOVAL.SDR CA080723005Control Cable · frayed(CAN) CABLE WAS DISCOVERED FRAYED DURING REGULARY SCHEDULED MAINT.SDR CA080616005Control Cable · frayed(CAN) AFT ELEVATOR TRIM CABLE WAS DISCOVERED FRAYED DURING REGULARLY SCHEDULED MAINT. IT WAS SURMISED THAT FURTHER OPERATION OF THE TRIM SYS WOULD HAVE LED TO SYS FAILURE BEFORE THE NEXT SCHEDULED INSPECTION.SDR ECP2008F00000Block · crackedFOUND PILOT`S OUTBOARD BUSH BLOCK ON RUDDER CONTROL CRACKED.SDR CA080415004Control Cable · frayedFLAP CENTER CABLE WAS FOUND FRAYED DURING REGULARLY SCHEDULED MAINTENANCE.SDR CA080305008Alternator · failed(CAN) PILOT EXPERIENCED A COMPLETE ELECTRICAL FAILURE. SUBSEQUENT INVESTIGATION REVEALED A MELTED INSULATOR ON THE (BATT) TERMINAL OF THE ALTERNATOR. THE (BATT) WIRE TERMINAL END WAS MELTED AND BROKEN WITH THE FREE END CONTACTING THE ALTERNATOR CASE. THE FREE SDR CA080121004Baffle · cracked(CAN) INTERNAL BAFFLE ATTACH WELD WAS FOUND CRACKED DURING A 100 HOUR INSPECTION. (TC NR 20080121004)SDR CA071211002Control Cable · frayed(CAN) THE FLAP CENTER CABLE WAS FOUND FRAYED DURING REGULARLY SCHEDULED MAINTENANCE. (TC NR 20071211002)SDR CA071109003Baffle · cracked(CAN) DURING A 100 HOUR INSPECTION, ONE INTERNAL BAFFLE OF THE PRIMARY EXHAUST SILENCER WAS FOUND TO BE CRACKED 25 PERCENT OF THE ATTACHING WELD. SILENCER WAS SUBSEQUENTLY REPLACED. (TC NR 20071109003)
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