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 = 'F90' 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 = 'F90' 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 20010417CW013Skin · crackedDURING PHASE 2 INSPECTION, FOUND 6 INCH CRACK AT TOP AILERON SKIN. SKIN WAS CLOSE TO FAILURE.SDR 20001025SH002Gasket · splitGASKET SPLITTING AND FUEL LEAKING FROM NACELLE INTO ENGINE EXHAUST PATH. (X)SDR 20000629SH001Valve · leakingINTERNAL LEAK OF FUEL THROUGH GATE VALVE, WITH SHUT-OFF VALVE IN CLOSED POSITION. (I)SDR 20000516SH009Wire · chafedSEVERAL WIRES IN A WIRE BUNDLE WERE FOUND CHAFED THROUGH TO GROUND ON A LEADING EDGE RIB. WIRES GOING TO INTERMITTENT GROUND INCLUDE RT AUTOFEATHER WIRE, ELECTRIC HEAT WIRE, BATTERY CHARGE SHUNT-TO-MODULE WIRES. BUNDLE WAS INSULATED AND SECURED AWAY FROM RISDR 2000ZZZX156Ballast · failedDURING FLIGHT, THE PASSENGER IN THE LEFT AFT SEAT NOTED SMOKE COMING FROM BEHIND THE WINDOW SHADE. THE CREW SECURED THE LIGHTING SYSTEM BY SECURING THE CIRCUIT BREAKER. THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION, THE LIGHT BALLAST WAS FOUND MELTESDR RU3A9903Screw · shearedAT PROPELLER CHANGE RUN-UP, SAFETY SCREW WHICH HOLDS DOWN LINK PIN TO LINK ARM SHEARED OFF CAUSING THE BLADE TO MOVE INTO FEATHER. (X)SDR 99ZZZX2049Valve · failedAIR VALVE STUCK IN OPEN POSITION CAUSING FULL HOT AIR TO CABIN. SMOKE STARTED TO FLOW INTO CABIN AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE CLEANED VALVES AND OPS CHECKED OK. BOTH BYPASS VALVES WILL BE REPLACED.SDR 99ZZZX1581Valve · malfunctionedAIR VALVE STUCK IN OPEN POSITION CAUSING FULL HOT AIR TO CABIN. SMOKE STARTED TO FLOW INTO CABIN AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE CLEANED VALVES AND OPS CHECKED OK. BOTH BYPASS VALVES WILL BE REPLACED.SDR 98ZZZX3331Blade · failedENGINE RECEIVED FOR SUSPECTED COMPRESSOR TURBINE BLADE FAILURE. UPON INSPECTION, ONE OR MORE CT BLADES WERE FOUND TO HAVE FAILED. ENGINE TOTAL TIME 4,827.5 HOURS. TIME SINCE OVERHAUL 689 HOURS.SDR CA970807045Regulator · malfunctioned(CAN) CREW REPORTED ELECTRICAL BUS SEPARATION FOLLOWED BY AVIONICS CIRCUIT BREAKERS TRIPPING. LEFT GENERATOR DEEMED TO BE THE CAUSE AND WAS ISOLATED. MAINTENANCE FOUND THAT THE LEFT HAND GENERATOR CONTROL UNIT FAILED.SDR 97ZZZX4850Pump · failedLEFT ENGINE HIGH PRESSURE FUEL PUMP FAILED. DISASSEMBLY REVEALED DRIVE COUPLER SPLINES WORN OUT ON PUMP. OIL MISTING HOLE PLUGGED, SPLINES RUNNING DRY. THIS CONDITION CAN BE REVEALED BY PUSHING A PIPE CLEANER INTO PUMP DRAIN CAVITY. RUST DEPOSITS INDICATE SDR 97ZZZX3821Plate Assy · looseFUEL VENTING FROM RIGHT HEATED FUEL VENT. FOUND FUEL LEAKING PAST AUXILIARY TANK FLAPPER VALVE. LOOSE/WORN RIVETS ALLOWED VALVE TO UNSEAT AND FUEL LEAKED BY GRAVITY FEED. REPLACED RIVETS THAT HOLD HINGE HALF TO PLATE.SDR CA970731021Itt Harness · separated(CAN) DURING NORMAL OPERATIONS THE CREW NOTICED THE NR2 ENGINE ITT DROPPED TO ZERO. THE ITT HARNESS WAS REPLACED AND THE ENGINE TESTED SERVICEABLE. INSPECTION OF THE HARNESS FOUND THE CHROMEL CONNECTION ON THE CRIMPED END WAS SEPARATED AND THE GLASS CERAMIC MSDR 97ZZZX1951Angle · crackedLANDING GEAR SUPPORT BRACKET PART CRACKED VARIOUS PLACES. PART REPLACED AT INSPECTION AND PROBLEM OCCURRED SAME PART 500 HOURS LATER IN SAME LOCATION. EXACT PART LOCATION, LEFT AND RIGHT GEAR ANGLES.SDR CA970115001Drag Leg · cracked(CAN) AIRCRAFT LANDED ON ICY RUNWAY WITH FROZEN BRAKES AND CAME TO A JARRING STOP WHEN CLEAR RUNWAY WAS ENCOUNTERED. INSPECTION FOUND THE RADII OF THE LEFT HAND DRAG LEG CRACKED.SDR 96ZZZX5833Window · fracturedNOV. 1, 1996: CRUISE FLIGHT @ FL 230, OUTER LAMINATION OF PILOT WINDSHIELD FRACTURED 2-3 INCHES INBOARD OF CENTER POST. FRACTURE WAS VERTICAL THE ENTIRE HEIGHT OF WINDSHIELD. INNER LAMINATION NOT AFFECTED. PRECAUTIONARY LANDING MADE WITHOUT INCIDENT. WINSDR 96ZZZX4707Fuel Cell · mismanufacturedFUEL CELL PROBE MOUNTING PORTS WERE .75 INCH TOO CLOSE TOGETHER. FUEL CELL SUPPOSEDLY NEW FROM MANUFACTURER.SDR 96ZZZX2413Oxygen Mask · fail deployDURING ROUTINE MAINTENANCE, THE OXYGEN AUTO-DEPLOY SYSTEM WAS ACTIVATED. ALL MASKS FAILED TO DEPLOY. THE CAUSE WAS THE NEW HEADLINER MATERIAL THICKNESS WHICH PREVENTED THE ACTUATOR PLUNGER FROM CONTACTING THE STRIKER PLATE ON THE MASK CONTAINER. THIS IS THESDR 95ZZZX4210Wheel Assy · wrong tie boltWHILE PERFORMING TIRE REPLACEMENT, NOTICED THE WHEEL TIE BOLTS AND NUTS WERE INCORRECT STANDARD 'AN' STEEL BOLTS - AN6-31 BOLTS, AN960-6 WASHERS, AND MS21042-6 NUTS AND AN363-624 NUTS. INSTALLED CORRECT HARDWARE IAW CLEVELAND WHEEL AND BRAKE INSTALLATION MANUSDR 95ZZZX2838Trim Tab Sys · out of rigPILOT REPORTS RUDDER TRIM TAB BECOMES STUCK WHEN TRIMMED FULL RIGHT. (REPORTED ON RETURN FROM LOCAL AREA TRAINING FLIGHT AT 14:00). T/S RUDDER TRIM TAB ACTUATOR, FOUND PEDESTAL KNOB/INDICATOR OUT OF RIG AS WELL AS RUDDER TRIM TAB ACTUATOR/ROD ENDS, AND CABLESDR 95ZZZX2276Intercostal · crackedCABIN DOOR INTERCOSTAL FOUND CRACKED. THIS PART SUPPORTS CABIN DOOR HANDRAIL ASSY TO DOOR. SUGGEST HEAVIER GAUGE METAL IN MANUFACTURING OR ADDITIONAL STIFFNESS NEEDED. IN SINGLE SUPPORT CABLE APPLICATION, INSPECTION SHOULD BE AT EVERY 150-HOUR INSPECTION AN
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