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 jasc_code = '7324' 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 jasc_code = '7324' 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 CA001201024Valve · cracked(CAN) A/C INVOLVED IN HELI-LOGGING OPS 15 MILES SOUTH OF SQUAMISH&60 MINS INTO ITS 1ST CYCLE OF DAY. A/C HAD JUST DELIVERED ITS LOAD TO LOG LDG&ABOUT TO TRANSITION INTO A CLIMB BACK UP HILL WHEN YAW & SUBSEQUENT TORQUE SPLIT NOTICED. FURTHER INVEST. REVEALED SDR 20000802SH014Flow Divider · failedWHILE C/W TEXTRON-LYC SA 55-550 ENG RECALL, FUEL FOUND IN CRANKSCASE MIXED WITH OIL. TEXTRON CHECKED FUEL SYS, FOUND NO PROBLEMS. TECH REP INSPECTED INSTALL AND FOUND NO PROBLEMS WITH INSTALL, BUT NOTED FUEL DRIPPING FROM FUEL INJECTOR LINES WITH MIX AND THRSDR 20000405SH009Flow Divider · malfunctionedENGINE HAD MOMENTARY ROUGHNESS WHILE IN CRUISE FLIGHT. REPLACED FUEL FLOW DIVIDER, FUEL SERVO, AND ELECTRIC BOOST PUMP. (X)SDR AU000094Diaphragm · worn(AUS) LEFT ENGINE FUEL FLOW DIVIDER DIAPHRAGM FAILED DUE TO CHAFING ON THE VALVE PLATE.SDR CA991004003Flow Divider · leaking(CAN) FLOW DIVIDER AND DUMP VALVE PASSING EXCESS FUEL.SDR 99ZZZX2937Flow Divider · stickingFLOW DIVIDER STUCK AND WOULD NOT FULLY OPEN. THIS HAPPENED ON TAKEOFF WHICH RESULTED IN A 1,000 RPM LOSS FOR ABOUT 3-4 SECONDS.SDR 99ZZZX2936Flow Divider · stickingFLOW DIVIDER STUCK AND WOULD NOT FULLY OPEN. THIS HAPPENED ON TAKEOFF AT 700 - 800 FEET WHICH RESULTED IN A 1,100 - 1,200 RPM LOSS AND ENGINE SPUTTERED FOR ABOUT 10 SECONDS.SDR 99ZZZX2939Flow Divider · stickingFLOW DIVIDER STUCK AND WOULD NOT FULLY OPEN. THIS HAPPENED WHILE IN SLOW FLIGHT. ENGINE SHUT OFF FOR ABOUT 10 - 15 SECONDS.SDR 98ZZZX3197Flow Divider · scoredPILOT REPORTED ENGINE QUIT DURING RECOVERY FROM A STALL AT 3,000 FEET AGL. PILOT WAS ABLE TO RESTART ENGINE AND FLY ACFT BACK TO AIRPORT SAFELY. ENGINE WAS IDLING ROUGH. MAINTENANCE REMOVED COVER AND FOUND SCORING AND SMALL METAL FLAKES INSIDE OF THE FLOW DSDR CA980610014Diaphragm · failed(CAN) DURING THE ENGINE RUN-UP PREPARATORY TO THE ANNUAL INSPECTION, THE ENGINE WAS RUNNING VERY ROUGH WITH BLADE SMOKE COMING FROM THE EXHAUST. INSPECTION REVEALED THE RUBBER DIAPHRAGM IN THE FUEL FLOW DIVIDER HAD DRIED OUT, DISINTEGRATED AND PLUGGED THE FUESDR AU980206Flow Divider · faulty(AUS) RH ENGINE FUEL FLOW DIVIDER FAULTY.SDR 98ZZZX1125Line · failedFUEL REF LINE FROM FLOW DIVIDER TO BAFFLE BROKE CAUSING A ROUGH RUNNING ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT.SDR QXEA9700894Divider · malfunctionRETURNED TO GATE WITH NR 2 ENGINE FUEL PRESSURE WARNING. REPLACED NR 2 FUEL FLOW DIVIDER, OPERATIONAL CHECK GOOD.SDR CA971216052Flow Divider · leaking fuel(CAN) AFTER TAKEOFF, PILOT NOTED FUMES IN THE COCKPIT AND SMOKE FROM INBOARD EXHAUST STACK ON NR 1 ENGINE. AFTER FLIGHT, MAINTENANCE SPOOLED THE ENGINE AND FOUND FUEL LEAKING FROM THE FLOW DIVIDER. IT IS THOUGHT WHEN THE ELBOW FITTINGS WERE TRANSFERRED TO THSDR RAIA971006Flow Divider · leakedMEM - FLT 7140 - ON SHORT FINAL, NR 2 ENGINE FIRE LIGHT ILLUMINATED CREW PERFORMED REQUIRED CHECK LIST, FIRE EXTINGUISHED. MAINTENANCE REPLACED RIGHT ENGINE FUEL FLOW DIVIDER, PERFORMED ENGINE FIRE INSPECTION. (M)SDR 97ZZZX1688Flow Divider · failedSTL - FLT 7542 - LEFT ENGINE WOULD NOT MAKE TORQUE. MAINTENANCE REPLACED LEFT ENGINE FUEL FLOW DIVIDER. (X)SDR CA960828007Flow Divider · faulty(CAN) ON APPROACH #1 ENGINE SUFFERED TORQUE FLUCTUATIONS BEFORE FLAMING OUT. THE FUEL FLOW DIVIDER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA960909017Flow Divider · inoperative(CAN) #2 ENGINE WOULD NOT START AFTER REFUELING STOP. DURING THE START SEQUENCE EXCESSIVE FUEL STARTED DRIPPING FROM THE EXHAUST PIPE. THIS FUEL IGNITED CAUSING SOME TORCHING AT THE EXHAUST STACKS. MAINTENANCE FOUND THE FLOW DIVIDER AND CHECK VALVE TO BE INCRESDR CA960703001Check Valve · stuck open(CAN) AFTER SHUTDOWN SMOKE WAS NOTICED COMING FROM THE INTAKE AND THE EXHAUST. TROUBLESHOOTING REVEALED A FAULTY CHECK VALVE BETWEEN THE FUEL BOOSTER PUMP AND THE ECOLOGY PUMP LETTING FUEL INTO THE BURNER CAN. THE CHECK VALVE WAS REPLACED, THE ENGINE INSPECTEDSDR RAIA960508Flow Divider · leakingSTL - FLT 7152 - NR 2 ENGINE POWER, EGT DROPPED OFF ON TAKEOFF. SECURED FUEL SUPPLY FITTING ON FLOW DIVIDER. (M)SDR CA960304007Fuel Divider · sticking(CAN) DURING TAKEOFF ROLL, ENGINE WOULD NOT DEVELOP TAKEOFF POWER. ONLY PRODUCED 2000 LBS TORQUE INSTEAD OF 3400 LBS. FOUND SECONDARY FUEL NOZZLES NOT COMING ON LINE. CHANGED FLOW DIVIDER-PURGE VALVE. TEST RUN & TEST FLOWN SATISFACTORY. VALVE HAD JUST HAD NEW SDR 96ZZZX938Line · brokeFUEL LINE FROM FLOW DIVIDER TO NR 6 NOZZLE BROKE AT B-NUT NOZZLE AND SPRAYED RAW FUEL ON ENGINE. ENGINE ROUGH, BUT NOT SHUT DOWN AND LANDED OK WITH NO FIRE. VERY LUCKY!SDR GLBA96024Flow Divider · leakingORD - CREW REPORTED AND EXCESSIVE FUEL FLOW INDICATION WITH LEFT ENGINE RUNNING AND FUEL LEAK AT LEFT ENGINE. MAINTENANCE REPLACED LEFT FLOW DIVIDER. LEAK CHECK AND OPS CHECK GOOD. (M)SDR 95ZZZX1117Flow Divider · defectivePILOT REPORTED LT ENGINE WOULD NOT MAKE A CLEAN SHUT DOWN. INVESTIGATION REVEALED FLOW DIVIDER CHECK VALVE WAS PASSING FUEL BELOW PRESET PRESSURE. FOUND RUBER DIAPHRAGM DRIED OUT DUE TO LACK OF USE.
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