Williams FJ44-1A
Service difficulty reports · 59
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 engine_model_key = 'FJ441A' 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 = 'FJ441A' 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 CA050711008Cable · failed(CAN) FOUND FWD AILERON CABLE TENSION AT ZERO. CROSSOVER CABLES FOUND TO BE LOOSE. REMOVED AILERON CROSSOVER CABLES FROM CNTRL COLUMNS WITHOUT DISTURBING HUMBUCKLE LOCKING. INSPECTED CABLES, CHAINS, SWAGES AND HUMBUCKLE. DETERMINED ONE OF CROSSOVER CABLE CHAISDR DJFA2005070Warning Light · illuminatedDURING CRUISING, APPROX 1 HR AFTER TAKING OFF WITH FULL FUEL, RT FUEL FILTER BY-PASS & MASTER CAUTIONS ILLUMINATED. RT BOOST PUMP TURNED ON. 10 MINS LATER, LT FUEL FILTER BY-PASS ILLUMINATED. LT BOOST PUMP TURNED ON & AN EMERGENCY DECLARED. DURING DESCENT,SDR DJFA2004043Carbon Seal · failedCREW REPORTED THAT 10 MINUTES AFTER TAKE OFF, DURING CLIMB TO ALTITUDE, THE RT ENGINE OIL PRESSURE LIGHT ILLUMINATED. THE OIL PRESSURE WAS READING APPROXIMATELY 50 PSI AND DECREASING. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO KBGM. MAINTENANCE INSTALLEDSDR CA040624009Coupling · failed(CAN)A/C HAD BEEN MODIFIED AT FACTORY TO REMOVE FLEX COUPLING AND TUBE ARRANGEMENT OF S/N 0001 THRU 0129 BLEED AIR SYSTEMS (REF. IPC36-10-00-01 SHEET 1 OF 4 DETAIL B) AND INSTALL FLEX COUPLING AND TUBE ARRANGEMENT OF S/N'S 0130 THRU 0184. THIS UPGRADED ARRANGSDR 2004FA0000421Precooler · splitPILOTS NOTICED SLIGHT TEMP RISE IN RT ENGINE, AND AN UNUSUAL VIBRATION ALL ENGINE INDICATIONS IN NORMAL RANGES POSTFLIGHT WALK AROUND NOTICED A SPLIT IN THE PRESSURIZATION (BLEED AIR) PRE-COOLER IN THE RT PYLON. PAINT DISCOLORATION WAS NOTED NO DAMAGE TO ADJASDR WI52003F00000Diffuser · rupturedUPON ENGINE DISSASSEMBLY THE DIFFUSER WAS FOUND TO EXHIBIT A SEPARATION OF THE AXIAL WELD OF THE PRESSURE CASE. THE FAILURE WAS INITIATED AS A FATIGUE CRACK WHICH RUPTURED AFTER REACHING A 3.00 INCH CRITICAL LENGTH. CAUSE IS ATTRIBUTED TO LOCAL MATERIAL THINSDR CA030626004Starter Gen · failed(CAN) LT GENERATOR WENT OFF LINE IN FLIGHT. AFTER LANDING WE TRIED TO START THE LT ENGINE AND NO RESPONSE,THE LT STARTER GENERATOR WAS CHANGE WITH AN OVERHAUL UNIT. THE LT GENERATOR WAS DUE FOR OVERHAUL AT 2049 HOURS.SDR 2003FA0000466Blade · damagedON TAKEOFF, NOTICE SMALL BIRD PASS OVER NOSE AND LEFT WINDSHIELD, TAKEOFF WAS NORMAL. DURING CLIMBOUT, 14,500 FEET, STARTED TO HEAR A LOUD WHINE AND VIBRATION COMING FROM LEFT ENGINE. DIVERTED AND BROUGHT LEFT ENGINE TO FLIGHT IDLE. DESCENT AND LANDING WAS SDR AUS20020500Valve · broken(AUS) LT ENGINE BLEED AIR SYSTEM CHECK VALVE BROKEN. INVESTIGATION FOUND CENTRE SUPPORT WELDS FAILED CAUSING AIRFLOW BLOCKAGE.
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