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 engine_model_key = 'CF680A' 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 engine_model_key = 'CF680A' 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 AU971615Fuel Heater · cracked(AUS) LH ENGINE FUEL/OIL HEAT EXCHANGER CRACKED AND LEAKING AT FORWARD END HEADER. CRACK LENGTH 25.4MM (1IN).SDR AU971617Engine · defective(AUS) RT ENGINE VIBRATING. SUSPECT HIGH PRESSURE COMPRESSOR ROTOR SLIGHTLY OUT OF BALANCE. ENGINE HAS A HISTORY OF VIBRATIONS.SDR AU970911Bearing · cracked(AUS) LH ENGINE AFT ENGINE MOUNT LINK BEARING INNER RACE CRACKED IN TWO PLACES. LOWER FITTING ASSEMBLY BEARING INNER RACE CRACKED IN ONEPLACE.SDR AU971069Seal · leaking(AUS) RAM AIR TURBINE (RAT) HYDRAULIC PUMP HOUSING SEALS LEAKING.SDR AU970698Cylinder · corroded(AUS) LH MAIN LANDING GEAR OUTER CYLINDER FORWARD TRUNNION CONTAINEDSEVERAL AREAS OF CORROSIONSDR AU970792Valve · worn(AUS) RH BLEED AIR VALVE FAULTY. WORKSHOP INSPECTION FOUND VALVE SHAFT WORN AT CONVEX SEALING RING.SDR DL76S970526Engine · failedLT ENG FAILED ON T/O WITH LOAD BANG AND SHUT ITSELT DOWN.SDR AU970481Hydraulic Fuse · faulty(AUS) RH MAIN LANDING GEAR TRUCK POSITIONER `UP' LINE HYDRAULIC FUSE FAULTYSDR AU971595Spring · fractured(AUS) HYDRAULIC SYSTEM RH FUSE PNO V2-4360-2 SPRING PNO 33582 FAILED. SPLIT RING PNO 33581 DAMAGED AND RESET PISTON PNO 33589 JAMMED INSIDE ADAPTER PNO 33590.SDR AU970455Fuselage · corroded(AUS) FUSELAGE CONTAINED LEVEL 2 CORROSION - FOUND DURING INSPECTIONSDR AALA970087Bleed Valve · defectiveORD - FLT T2353 - LATE IN THE TAKEOFF ROLL AT ORD, RT ENGINE HIGH STAGE LIGHT AND EICAS MESSAGE CAME ON FOLLOWED BY HOT ODOR NOTED IN COCKPIT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED RT HIGH STAGE VALVE. ACCOMPLISHED LEAK CHECK WITH NSDR AU960892Fcu · faulty(AUS) LH ENGINE FUEL CONTROL UNIT FAULTYSDR AU961098Combustor · cracked(AUS) ENGINE COMBUSTOR OUTER COWL CRACKED AND BROKENSDR DL76S961254Engine · malfunctionedRT ENG FLAME-OUT JUST AFTER ROTATION. ALL INDICATIONS NORMAL AT LIFTOFF, THEN FLAME-OUT OCCURRED. REPLACED LEAKING FUEL MANIFOLD LINE AND LEAKING FUEL NOZZLE, LEAK CHECK AND ENGINE RUN OK.SDR AU960897Cylinder · cracked(AUS) RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNION CRACKED AND CORRODED IN AREA OF FILLET SEALSDR AU960898Cylinder · cracked(AUS) RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNION CRACKED AND CORRODED IN AREA OF FILLET SEALSDR AU960570Trunnion · corroded(AUS) LH AND RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNIONS CONTAINED UNACCEPTABLE CORROSION DURING ULTRASONIC AND EDDY CURRENT INSPECTIONS IAW ER B76-32-10-24 - RH OUTER CYLINDER CORRODED IN AREA OF JOURNAL CHAMFER AT THE 2 O'CLOCK POSITION -LH TRUNNION CSDR AU960264Controller · seized(AUS) LH ENGINE MAIN ENGINE CONTROL (MEC) POWER LEVER SEIZED - STRIP INSPECTION OF MEC COULD FIND NO FAULTSSDR DL767960423Press Syst · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE ON CLIMBOUT. INSPECTED AIRCRAFT ON ARRIVAL, NO DOORS OR SERVICE DOORS OPEN. FOUND EQUIPMENT COOLING VALVES OPEN, RESEQUENCED EQUIPMENT COOLING VALVES AND LOCKED OUT PER MEL 21-58-06. AIRCRAFT PRESSURIZED NORMALLY.SDR AU960111Coupling · failed(AUS) NO2 ENGINE CONTAINED A MASSIVE OIL LEAK IN THE INTAKE AREA - INSPECTION OF THE OIL SCAVENGE PUMP FOUND THE PUMP CONTAMINATEDWITH BRAIDED SEAL MATERIAL - HP TURBINE COUPLING NUT PRESSURE TUBE RUPTURED AT THE TUBE TO AFT FLANGE WELDED JOINT - A CIRCUMFERSDR AU960210Pin · cracked(AUS) LH ENGINE PYLON MID SPAR FITTING FUSE PIN CRACKED ON INNER BORE APPROXIMATELY 23MM (0.90IN) IN FROM THE HEAD OF THE PIN - CRACK LENGTH APPROXIMATELY 12MM (0.47IN) - FOUND DURING EDDY CURRENT INSPECTION IAW B76-54-40-4D - CRACK CONFIRMED BY MAGNETICPARTISDR 95ZZZX6796Fuel Filter · cloggedSAL/LAX - FLT 510 - DURING TAKEOFF, ENGINE NR 1 DID NOT REACH N1 REQUIRED FOR TAKEOFF AT THE RUNWAY HEADING. DUE TO THIS SITUATION, THE AIRCRAFT RETURNED TO GATE. THE NR 1 ENGINE WAS INSPECTED, AND FOUND WITH A CLOGGED FUEL FILTER WHICH WAS REPLACED. AFTER
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