IAE V2533-A5

Service difficulty reports · 506

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 = 'V2533A5'
  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 GTIA200600069Metering Unit · failedENG NR 2 AUTO SHUTDOWN AFTER START AND STABILIZED. ECAM MSG ENG 2 FAIL AND ECAM MSG ENG 2 FADEC ALT OVERSPEED PROTECTION LOST. REMOVED AND REPLACED NR 2 FMU.Jun 11, 2006 · N588NK · Airbus A321211 · Fuel Control/Reciprocating EnginesSDR GTIA200600020Engine · shutdownNR 2 ENGINE AUTO SHUTDOWN. RESTARTED OK. NO DEFECTS FOUND.May 22, 2006 · N588NK · Airbus A320* · Engine (Turbine/Turboprop)SDR GTIA050272Sleeve · crackedFOUND NR 4 MAIN TIRE WORN TO LIMITS, WHEN TIRE WAS REMOVED FOUND NR4 MLG AXLE SLEEVE CRACKED. DAMAGED LENGTH MEASUREMENT IS NOT BEYOND .238 INCH, ACCOMPLISHED NDT INSPECTION OF NR4 AXLE SLEEVE, NO CRACK PROPAGATION BEYOND VISIBLE MEASUREMENT OF .238 INCH. (KNov 19, 2005 · N587NK · Airbus A320321 · Main Landing Gear Strut/Axle/TruckSDR GTIA050267Structure · ground damagePERFORMED HARD LANDING/ OVERWEIGHT LANDING INSPECTION, FOUND DAMAGE AT LOWER TAIL SECTION BETWEEN FR67-FR68 IAW AMM, NO ADDITIONAL DAMAGE NOTED. INSTALLED INTERM REPAIR IAW EA AND DWG, AIRCRAFT FERRIED FOR REPAIR. PERMANENT REPAIR ACCOMPLISHED, AIRCRAFT OK FSep 19, 2005 · N583NK · Airbus A320321 · Fuselage Main, Plate/SkinSDR GTIA040829Compressor · stalledLP NR 2907041; SHUTDOWN RT ENGINE, AIR RETURN. RT ENGINE COMPRESSOR STALL ON T/O AFTER V1, PULLED THROTTLE TO IDLE. TRIED ADVANCING POWER AGAIN ANOTER COMPRESSOR STALL AT ABOUT 1.3 EPR, FLEW SINGLE ENGINE APPROACH AND LANDING. REMOVED AND REPLACED RT ENGINENov 1, 2004 · N584NK · Airbus A321211 · Turbine Engine Compressor SectionSDR RYN2004F00028Compressor · damagedDURING CLIMB OUT, NR 2 ENGINE STALLED. APPROPRIATE PROCEDURES WERE FOLLOWED. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT INCIDENT. REMOVED AND REPACED NR 2 ENGINE.Feb 13, 2004 · Airbus A321211 · Turbine Engine Compressor Section
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