Airbus A310

Service difficulty reports · 606

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 = 'A310'
  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 97FDEA00359Duct · failedACFT DEPARTED BDL HAD AN AIR TURNBACK, NR 1 ENG ECAM ADVISORY NACELLE TEMP ADVISORY OCCURRED AFTER T/O CK LIST. FLASHING GREEN 230C AND THEN CRC/ECAM FOR NR 1 ENG FIRE HANDLE RED HANDLE AND BOTH LOOP LT ON. ATS DISCONNECTED. # 1 THROTTLE PLACED TO IDLE, FIRJun 20, 1997 · N402FE · Airbus A310* · Pneumatic Distribution SystemSDR 97FDEA00265Out Flow Valve · failedDURING CLIMBOUT, CABIN PRESSURE EXCEEDED 10K FT SWITCH TO MANUAL CABIN CONTROL. BUT STILL UNABLE TO KEEP BELOW 10K FT, PERFORMED ECAM AND CHECKLIST ITEMS. NOTE ON ECAM PRESS PAGE NOTICED FWD AND AFT NUMBER TWO VALVE OPEN REGARDLESS OF MODE. CONFIRMED INOP May 8, 1997 · N419FE · Airbus A310* · Pressure Regulator/Outflow ValveSDR 97FDEA00262Compressor · stalledAFTER TOUCHDOWN DEPLOYED BOTH REVERSER WITH FULL THRUST. IMMEDIATELY THEREAFTER HEARD A LOUD REPORT AND SAW FLASH FROM NR 2 ENGINE AREA. NR 2 ENGINE SUBSEQUENTLY SHUT DOWN AND NEVER CAME OUT OF REVERSE. NO OTHER ABNORMAL COCKPIT OR ECAM WARNINGS. *S/D* REMay 2, 1997 · N422FE · Airbus A310* · Turbine Engine Compressor SectionSDR 97FDEA00190Depressure Valve · failedDURING CLIMB, COULD NOT PRESSURIZE THE AIRCRAFT. MANUAL DEPRESSURIZATION VALVE SHOWED OPEN ON ECAM. RETURNED TO MC. *S/D* REMOVED AND REPLACED VALVE 93 HM IAW M/M 21-31-15 AND PERFORMED TEST IAW M/M 21-31-00, NO DISCREPANCIES NOTED.Mar 21, 1997 · N405FE · Airbus A310* · Cabin Pressure Control SystemSDR 97FDEA00185Duct · separatedNR 2 ENG TEMP ADV IN CRUISE WITH NR 2 NAC TEMP = 270 DEGREES C, FOLLOWED BY NR 2 THROTTLE WOULD NOT MOVE, FOLLOWED BY NR 2 BLEED FAULT. SHUT DOWN ENG NR 2 TO LAND, ALL OTHER ENG PARAMETERS PRIOR TO SHUTDOWN NORMAL. NR 2 OIL PRESS WAS NOT OBSERVED PAST SHUTDOMar 19, 1997 · N417FE · Airbus A310* · Pneumatic Distribution SystemSDR 96ZZZX1638Motor · misassembledON 2-27-96, TWO HORIZ STAB ACTUATOR MOTORS, SN AH-57563 AND SN AH-57871, WERE RECEIVED FROM REPAIR STATION AFTER INSPECTION AND VERIFICATION IAW REF AD AND AIRBUS AOT REFERENCED THEREIN. THESE MOTORS WERE ASSEMBLED TO AN A310 TAILPLANE ACTUATOR, PN 47142-203,Feb 27, 1996 · Airbus A310* · Stabilizer Actuator
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