IAE V2500-A1

Service difficulty reports · 306

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 = 'V2500A1'
  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.

SDR AWXA960224Bleed Valve · malfunctionedCMH - FLT 0266 - BOTH NR 1 AND NR 2 BLEED VALVES FAILED IN-FLIGHT. EMERGENCY DESCENT. ALL CABIN OXYGEN MASKS DROPPED. PERFORMED BLEED SYSTEM INSPECTION ON BOTH ENGINES PER SIL 36-034 AND RAN ENGINES. NO DEFECTS NOTED. REPLACED ALL OXYGEN MASKS EXCEPT ALL Apr 30, 1996 · N628AW · Airbus A320231 · Compressor Bleed ControlSDR AWXA960058Eec · failedPHX/SAN - FLT NR 860 - AIR TURN BACK, ENGINE 1 SENSOR FAULT, ECAM MESSAGE ENGINE SURGED AFTER TAKEOFF AND THEN STABILIZED. REMOVED AND REPLACED NR 1 ENGINE EEC PER CARD R9E73301. (M)Feb 8, 1996 · N637AW · Airbus A320231 · Fuel Control/Turbine EnginesSDR 96ZZZX489Bolt · failedENGINE WAS REMOVED FROM SERVICE DUE TO VIBRATION, DISASSEMBLY OF THE ENGINE REVEALED LPT GAS PATH DAMAGE. INVESTIGATION DETERMINED SEVEN OF THIRTY-SIX, 6TH TO 7TH STAGE DISK BOLTS HAD FAILED. PRELIMINARY ANALYSIS INDICATE THE BOLTS FAILED WITH THE CHARACTERIJan 17, 1996 · Turbine SectionSDR AWXA9500549Lock Pin · loosePHX-YVR - FLT NR 815 - AIR TURNBACK DUE TO NR 1 ENGINE BLEED FAULT. BLEED WENT TO OVERHEAT CONDITION TWO MINUTES AFTER SELECTED ON. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND SAFETY WIRE BROKEN AND LOCK PIN BACKED OUT OFAug 16, 1995 · N624AW · Airbus A320231 · Compressor Bleed ValveSDR JBXA950601Vsv Actuator · inoperativeBOS/RDU - FLT 16 - GOT ECAM MESSAGE, "NR 2 COMPRESSOR VANE MESSAGE". FOLLOWING MESSAGE, ENGINE SURGED. ENGINE WAS SHUT DOWN. LANDING WAS UNEVENTFUL. POST-FLIGHT REPORT REVEALED ENGINE HAD EXCEEDED ALLOWABLE EGT LIMITS. ENGINE WAS REMOVED AND REPLACED. (XJun 27, 1995 · N300ML · Airbus A320231 · Compressor Bleed ControlSDR AWXA9500071Eec · inoperativeLAS-PHL - FLT 1787 - EN ROUTE, AFTER TWO HOURS THE CREW OBSERVED ECAM 'ENGINE STALL ALERT' AND NOTED FLUCTUATION OF NR 2 ENGINE EPR. THIRTY MINUTES LATER CREW RECEIVED ECAM NR 2 'SENSOR FAULT AVOID RAPID THRUST CHANGES' MESSAGE. ACFT DIVERTED TO CMH WITHOUT Feb 1, 1995 · N626AW · Airbus A320231 · Fuel Control/Turbine Engines
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