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 = '150M' 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 = '150M' 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 2002FA0000123Window · separatedPILOT SIDE WINDOW (LOCATED ON PILOT'S DOOR) DEPARTED AIRCRAFT DURING FLIGHT WHEN WINDOW WAS OPENED. FOLLOWING AN EXAMINATION OF THE DOOR ON THE AIRCRAFT, IT APPEARED THAT BOTH THE FORWARD AND REAR HINGE PINS SHEARED ALLOWING THE WINDOW AND WINDOW FRAME TO SEPASDR CA020103005Bolt · wrong part(CAN) WHILE REMOVING MCCAULEY PROP FOR 5 YEARS CORRISON INSPECTION IT WAS NOTED THAT PROP BOLTS WERE TO SHORT APPROX 4 THREADS ON ALL BOLTS WERE SECURING THE PROP. NEW BOLT KIT A2513-77 INSTALLED & LOCKED.SDR CA020130006Rectifier · worn(CAN) ALTERNATOR RECTIFIER FAILED CAUSING ELECTRICAL FAILURE DURING FLIGHT.SDR CA011130014Muffler · cracked(CAN) A NOISE WAS HEARD IN CRUISE. MUFFLER FOUND CRACKED BEFORE RISER.SDR CA011114014Mount · cracked(CAN) DURING A 50 HOUR INSPECTION THE ENGINE MOUNT WAS FOUND CRACKED. THE SUPPORT WAS REPLACED.SDR CA011005003Volt Regulator · inoperative(CAN) INCOMPATIBILITY BETWEEN PARTS.IT HAS BEEN DISCOVERED THAT SEVERAL SUPPLIERS HAVE BEEN INFORMED THAT VOLTAGE REGULATORS LAMAR DGR 6 & ELECTROSYS VR600A ARE COMPATIBLE & INTERCHANGEABLE. IN ACTUALFACT LAMAR DGR6 IS INTERCHANGEABLE WITH THE ELECTROSYS VR60SDR CA011102007Spring · broken(CAN) DURING A PRE-FLIGHT INSPECTION, THE PILOT SAW THE RUDDER TURNED WHILE THE FRONT WHEEL WAS STRAIGHT AND THE PEDALS WERE OFF-CENTERED. AN INSPECTION DETERMINED THE RIGHT SPRING WAS MISSING AND FOUND BELOW IN THE FUSELAGE.SDR AUS20011086Rib · cracked(AUS) HORIZONTAL STABILISER RIBS PNO 0432001-6 AND PNO 0432001-36 CRACKED FROM FORWARD ATTACHMENT POINT NUTPLATE RIVETS.SDR AU010122Rib · cracked(AUS) HORIZONTAL STABILISER FORWARD ATTACHMENT RIBS CRACKED.SDR AU010121Rib · cracked(AUS) HORIZONTAL STABILISER FORWARD ATTACHMENT RIBS CRACKED.SDR CA010206004Valve Guide · worn(CAN) ENGINE RAN VERY ROUGH AT START UP.CYLINDER NR 3 REMOVED DUE TO LOW COMPRESSION. EXHAUST GUID WORN CAUSING CARBON TO JAM VALVE IN OPEN POSITION. CYLINDER RELACED DUE TO ABOVE PROBLEM.SDR CA001106005Arm · bent(CAN) RUDDER HORN ARM FOUND BENT DURING INSPECTION OF RUDDER CONTROL SYSTEMSDR AU000927Filter · corroded(AUS) FUEL FILTER BOWL CONTAMINATED WITH ALUMINIUM HYDROXIDE. FILTER BOWL CORRODED. (X)SDR CA000907014Propeller · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. (X)SDR 20000811SH001Spinner · crackedSPINNER BACKING PLATE HAS CRACKS RADIATING FROM THE BOLT HOLE AREAS. AN UNAUTHORIZED REPAIR WAS MADE.THE REPAIR WAS MADE BY MAKING A CIRCULAR FLAT SHEET METAL SAME THICKNESS AS THE ORIGIANL MATERIAL,THEN RIVETED TO THE BACKING PLATE. BOLT HOLES WERE DRILLED SDR CA000824010Muffler · cracked(CAN) AFTER TAKEOFF AND IN CLIMB-OUT, PILOT EXPERIENCED POWER LOSS (90 PERCENT). PILOT RETURNED TO THE AIRPORT AND LANDED SAFELY. ON ROLL OUT, ENGINE STOPPED COMPLETELY AND COULD NOT BE RESTARTED. INVESTIGATION FOUND THE REAR SECTION OF THE LEFT HAND EXHAUSTSDR 20000817SH025Cylinder · failedDURING A 100-HOUR INSPECTION, FOUND THE MILLININUM CYLINDER ASSY WHICH WAS INSTALLED IN THE NR 3 POSITION WOULD ONLY HOLD A COMPRESSION OF 32 PSI AFTER 200 HOURS OF SERVICE. POSSIBLE CAUSE UNKNOWN AT THIS TIME. (X)SDR AU000513Bolt · loose(AUS) AILERON PULLEY PN S378-4 TO CENTER CONSOLE ATTACHMENT BOLT HAD THE NUT MISSING AND THE INCORRECT WASHER SPACING UNDER THE PULLEY GUARDS. (X)SDR CA000606036Exhaust Valve · broken(CAN) IN-FLIGHT, THE ENGINE WAS RUNNING ROUGH. NR 3 CYLINDER SPARK PLUGS FOUND BROKEN. NR 3 CYLINDER MOVED AND REPLACED BY OVERHAULED ONE (EXHAUST VALVE FOUND BROKEN).SDR CA000530029Alternator · cracked(CAN) LOWER CASE HALF WEBS FOUND CRACKED.SDR 20000522SH003Bar · brokenUNABLE TO GET NORMAL NOSE WHEEL STEERING DUE TO BREAK IN TUBE ALLOWING PEDAL MOVEMENT WITHOUT MOVING LINKAGE TO STEERING OR RUDDER. (X)SDR AU000214Exhaust Valve · seized(AUS) NR 4 CYLINDER EXHAUST VALVE SEIZED.SDR CA000128043Arm · damaged(CAN) CARB HEAT BOX ACTUATOR ARM HAD BROKEN OFF AT RIVETS THAT SECURE SPRING STEEL STRIP TO ARM.SDR CA991230039Exhaust Valve · stuck(CAN) NR 3 CYLINDER LOW COMPRESSION THE EXHAUST VALVE WAS FOUND TO BE PARTIALLY STUCK AND BURNED.SDR AU000128043Arm · broken(AU) CARBURETOR HEAT BOX ACTUATOR ARM HAD BROKEN OFF AT RIVETS THAT SECURE SPRING STEEL STRIP TO ARM.SDR CA991112020Throttle · failed(CAN) THROTTLE CONTROL HAD NO EFFECT ON RPM. OPERATOR COULD NOT FIND FAULT ON GROUND.SDR CA991112013Field Rotor · sheared(CAN) DURING FLIGHT, THE CHARGING SYSTEM FAILED AND WOULD NOT RESET. AFTER LANDING, MAINTENANCE PERSONNEL DETERMINED THAT THE ALTERNATOR FIELD ROTOR HAD SHEARED AFT OF THE FORWARD (DRIVE END) BEARING.SDR 20000817SH030Muffler · erodedDURING CRUISE FLIGHT, SMOKE FROM UNDER INSTRUMENT PANEL NOTED. PILOT SECURED ELECTRICAL AND MAGNETO SWITCH AND EXECUTED A FORCED LANDING. HEAT DAMAGE TO ELECTRICAL WIRES NEAR THE BATTERY BOX. EXAMINATION OF THE RIGHT MUFFLER P/N 0450400-26, REVEALED THE AFSDR CA991028012Clutch · worn(CAN) STARTER SEIZED.SDR 99ZZZX3822Gasket · mismanufacturingDURING MAJOR OVERHAUL WHILE INSTALLING MUFFLERS WITH NEW SUPERIOR 'BLO PROOF' EXHAUST GASKETS, FOUND GASKET TO TOUCH INTAKE ON ADJACENT CYLINDERS 1 AND 3 AND WOULD NOT FIT FLUSH AT CYLINDERS 2 AND 4. THIS COULD LEAD TO EXHAUST BEING DIRECTLY PORTED ON INTAKE SDR AU990585Skin · corroded(AUS) VERTICAL STABILIZER SKIN CORRODED INTERNALLY.SDR 99ZZZX3495Crankshaft · crackedCRANKSHAFT REMOVED FROM REBUILT ENGINE DURING OVERHAUL WAS FOUND TO HAVE NUMEROUS HEAT CRACKS IN ALL FORWARD FILLETS OF CRANKPINS. FILLET RADII OF ALL CRANKPINS AND MAIN JOURNALS WERE FOUND BELOW TOLERANCES OF OVERHAUL MANUAL. CRANK WAS .010 INCH UNDERSIZE, SDR 99ZZZX2361Skin · crackedTHE WINDSHIELD HAD WORN THROUGH THE DECK SKIN IT RESTS ON AT THE 11: AND 1:00 O'CLOCK POSITIONS WHEN VIEWED FROM PILOT SEAT.SDR CA990330037Rod · broken(CAN) OIL PROBLEM IN-FLIGHT, AIRCRAFT RETURNED TO POINT OF DEPARTURE. POST-FLIGHT INSPECTION FOUND NO OIL IN THE ENGINE, BUT OIL WAS FOUND ON THE ENGINE COMPARTMENT. TEMPERATURE PROBE NUT FOUND LOOSE AND THIS WAS DETERMINED TO BE THE CAUSE OF THE OIL LEAK. SDR CA990323026Ground Strap · corroded(CAN) AIRCRAFT FUEL GAUGES INOPERATIVE/MISREADING. INSPECTION CARRIED OUT AND GROUND WIRES FOUND CORRODED/BROKEN. PARTS REPLACED.SDR 99ZZZX1016Starter · failedSTARTER OVERHAULED IN APRIL, 1996. NO LOG BOOK ENTRIES FOUND. ENGINE WAS OVERHAULED 12-6-98. STARTER HOUSING FELL OFF THE ARMATURE. ESTIMATED TIME: 700 HOURS ON STARTER.SDR CA990226010Piston · worn(CAN) DURING INSPECTION THE COMPRESSION ON NR 1 CYLINDER WAS 67/80 AND THERE WERE NON-MAGNETIC PARTICLES IN THE OIL FILTER. CYLINDER NR 1 WAS REMOVED AND MANY PARTS OF THE PISTON HAD DISINTEGRATED AT THE TOP COMPRESSION RING. THE RING WAS BROKEN. THE TOLERASDR CA990119030Skin · cracked(CAN) DOOR SKIN FOUND CRACKED IN TWO PLACES AT THE TOP.SDR CA990119012Mount · cracked(CAN) LEFT TUBE MEMBER AT THE LOWER NOSE GEAR STRUT ATTACH POINT FOUND CRACKED. WHEN REPAIRING, THE TUBE WAS FOUND CORRODED.SDR CA990115029Valve · sticking(CAN) INTAKE VALVE STICKING OPEN CAUSING LOSS OF POWER.SDR 99ZZZX198Display · malfunctionedOUT OF BOX FAILURE. DISPLAY PRODUCES NOSIE IN NAV AUDIO. RETURNED UNIT TO NARCO FOR REPAIR.SDR 99ZZZX197Gears · brokenUNIT HAS APPROXIMATELY ONE HOUR OF OPERATION SINCE NEW CHANNELING GEARS BROKEN. RETURNED TO NARCO FOR REPAIRS.SDR CA981109024Floorboard · cracked(CAN) DURING ANNUAL INSPECTION, A CRACK WAS FOUND IN THE FLOOR PANEL UNDER THE COPILOT'S SEAT TRACK VERY AFT POSITION. CRACK WAS PARALLEL TO THE END OF THE SEAT TRACK AND THEN RUNS FORWARD ON BOTH SIDES. CRACK ALSO FOUND UNDER THE INBOARD SEAT TRACK POSITION.SDR 98ZZZX4331Switch · failedUNIT DOES NOT TURN OFF. SUBMITTER SUSPECTS DEFECTIVE ON/OFF SWITCH. UNIT HAS APPROXIMATELY ONE HOUR TOTAL TIME. RETURNED UNIT TO FACTORY FOR REPAIR.SDR CA980922012Piston Ring · cracked(CAN) DURING INSPECTION, METAL PARTICLES WERE FOUND IN THE OIL SCREEN AND FILTER. A COMPRESSION CHECK REVEALED LOW COMPRESSION ON NR 1 CYLINDER. FURTHER INVESTIGATION FOUND A CRACKED PISTON RING, DAMAGED PISTON AND A SCORED CYLINDER WALL.SDR 99ZZZX104Magneto · misinstalledMAGNETO INTERNALLY TIMED 180 DEGREES OUT.SDR 99ZZZX103Magneto · misinstalledMAGNETO INTERNALLY TIMED 180 DEGREES OUT.SDR CA980825006Mount · cracked(CAN) DURING INSPECTION THE ENGINE MOUNT WHICH RUNS FROM THE LOWER RIGHT HAND FIREWALL PICKUP TO THE NOSE GEAR COLLAR WAS FOUND CRACKED AT THE WELD. THE SUBMITTER REPORTS THAT 1337.9 HOURS EARLIER, A SIMILAR CRACK WAS FOUND AND REPAIRED ON THE LEFT HAND SIDE SDR 98ZZZX3809Cylinder · failedCYLINDER SEPARATED THREE-FOURTHS THE WAY AROUND AT MID-BARREL. SUBSEQUENT OIL RING FAILURE.SDR 98ZZZX3272Control Cable · failedDURING A ROUTINE PRE-FLIGHT INSPECTION, PILOT REPORTED THE TRIM (ELEVATOR) DID NOT WORK. AFTER ACCESS WAS GAINED IN THE TAIL SECTION, IT WAS APPARENT THE CABLE BROKE INTO TWO PARTS DUE TO EXTREME RUST. THE AREA IN WHICH THIS OCCURRED IS VERY DIFFICULT TO ACC
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