Willfong Jay E FALCON
Service difficulty reports · 215
Newest first. General aviation reporting is voluntary.
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 = 'FALCON' 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 = 'FALCON' 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 Y2PA96023Turbo Compressor · smokingYIP - FLT 14035 - ON TAKEOFF WHEN AIRCRAFT STARTED TO PRESSURIZE, FUEL FUMES AND SMOKE ENTERED THE COCKPIT FROM THE FIRST OFFICER'S FLOOR VENT. THE CREW RETURNED TO POINT OF DEPARTURE. NO EMERGENCY PRODCEDURES WERE REQUIRED. THE PROBLEM WAS DETERMINED TO BESDR Y2PA96018Valve · contaminatedELP - FLT 13608 - CABIN WOULD NOT PRESSURIZE PAST 2.5 PSI DURING CLIMB OUT. THE CABIN CONTINUED TO CLIMB DURING ASCENT PHASE OF FLIGHT AND CREW ELECTED TO RETURN TO POINT OF DEPARTURE AT EL PASO, TEXAS. NO EMERGENCY PROCEDURES WERE REQUIRED AND AIRCRAFT LANDSDR 96ZZZM874Gearbox · stripped fittingWHILE PERFORMING A PREFLIGHT INSPECTION, OIL WAS NOTICED TO BE EXCESSIVELY LEAKING AT OIL SCAVENGE LINE FITTING ATTACHING SCAVENGER LINE TO ACCESSORY GEARBOX. FITTING WAS FOUND TO BE LOOSE. UPON FURTHER INVESTIGATION FITTING WAS FOUND TO BE STRIPPED. ACCESSSDR 96ZZZX3640Door Frame · crackedTHREE SMALL CRACKS IN CARGO DOOR FRAME NOTES DURING SSIP X-RAY INSPECTION. (AD 92-17-05 REQUIREMENT).SDR 96ZZZX3639Latch Bracket · crackedTWO CARGO DOOR ROTATING LATCH BRACKETS FOUND CRACKED DURING SSIP DYE-PENETRANT INSPECTION. (AD 92-17-05 REQUIREMENT).SDR YIEA96008Engine · flamed outYIP - RIGHT ENGINE FLAMED OUT DURING MAX ALTITUDE ACCELERATION TEST AT 35,000 FT. AIRCRAFT DESCENDED AND ENGINE RESTART WAS ATTEMPTED AT 24,000 FEET WITHOUT SUCCESS AND THEN AT 21,000 FEET WHERE ENGINE RELIT. AIRCRAFT RETURNED TO YIP AND MADE A NORMAL TWO ENSDR YIEA96007Low Press Filter · crushedYIP - LEFT ENGINE FLAMED OUT DURING STEADY STATE CLIMB AT 36,000 FEET. AIRCRAFT DESCENDED AND THE ENGINE WAS AIRSTARTED PER THE CHECK LIST. AIRCRAFT RETURNED TO YIP AND MADE A NORMAL TWO ENGINE LANDING. LEFT ENGINE WAS INSPECTED FOR FOD IN THE INLET, EXHAUSSDR 96ZZZM308Fuel Pump Filter · crushedYIP - LEFT ENGINE FLAMED OUT DURING STEADY STATE CLIMB AT 36,000 FEET. AIRCRAFT DESCENDED AND THE ENGINE WAS AIRSTARTED PER THE CHECK LIST. AIRCRAFT RETURNED TO YIP AND MADE A NORMAL TWO ENGINE LANDING. LEFT ENGINE WAS INSPECTED FOR FOD IN THE INLET, EXHAUSSDR YIEA96002Engine · flame outPILOT REPORTED WHILE IN A STEADY STATE CLIMB-OUT OF FL 310, LT ENG FLAMED OUT AT 31,400 FEET. ACFT FLYING AT .68 MACH. THERE WERE NO CLOUDS AND NO TURBULENCE. CREW DESCENDED AND TRIED RESTARTS AT FL 290, FL 250, AND FL 150 WITHOUT SUCCESS. ENG RELIGHT FINASDR 96ZZZX908Connector · looseYIP - GEAR WOULD NOT RETRACT AFTER TAKEOFF. YIP FOUND CANNON PLUG TO 9G NOT COMPLETELY SECURE - SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 95ZZZM691Engine · flamed outWHILE LEVEL AT FL410 IN CRUISE, A MINOR THROTTLE ADJUSTMENT WAS MADE AND THE NR 1 ENGINE FLAMED OUT. THE CREW DESCENDED TO FL 270 AND PERFORMED A NORMAL AIRSTART. ENGINE PARAMETERS AFTER AIRSTART WERE NORMAL. A PRECAUTIONARY LANDING WAS MADE AT SPI. MAINTESDR YIEA00395Engine · flamed outA/C WAS LVL AT CRUISE OF 35,000 FT, AIRSPEED WAS 200 KTS, OPERATING IN VICINITY OF LIGHT TO MODERATE PRECIP WITH THE ENG ANTI-ICE ON. A/C WAS DIRECTED TO CHANGE HEADING FROM 180 TO 240 DEGREES, WHEN LIGHT TO MODERATE TURBULENCE WAS ENCOUNTERED, AIRSPEED DECRESDR YIEA00295Rivets · wornDURING INSPECTION, THE AIRCRAFT WAS FOUND TO HAVE SEVERAL RIVETS LOOSE IN THE AREA OF THE SKIN DOUBLER, INSTALLED AS PART OF THE CABIN DOOR, STC SA2490S0. FURTHER INSPECTION REVEALED DEFECTIVE 'UPSET' HEADS ON MANY OF THE RIVETS INSTALLED DURING THIS MODIFICASDR YIEA00195Engine · flamed outPILOT REPORTED WHILE ACFT LEVEL AT CRUISE ALTITUDE 27,000 FEET AND AIRSPEED MACH. .70, RT ENGINE FLAMED OUT AFTER LIGHTNING FLASH ON RT SIDE OF ACFT. ACFT DESCENDED TO 20,000 FEET AND ENGINE SUCCESSFULLY RESTARTED. ENG OPERATION NORMAL AFTER THAT. ACFT/ENG SDR 95ZZZX734Valve · defectivePILOT REPORTED PRESSURIZATION FAILED IN-FLIGHT. PILOT SET EMERGENCY PRESSURIZATION. TROUBLESHOT SYSTEM, FOUND A/C VALVE FAILED. REPLACED A/C VALVE, SYSTEM CHECKS GOOD. THIS UNIT REQUIRES INSPECTION EVERY 600 HOURS. OPERATOR AAIP HAS THIS VALVE ON CONDITIO
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