Airbus A340-313

Service difficulty reports · 74

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 = 'A340313'
  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 CA991008014Pump · faulty(CAN) GREEN SYSTEM HYDRAULIC LOSS OF PRESSURE AND QUANTITY.Sep 21, 1999 · Airbus A340313 · Hydraulic Pump (Electric/Engine), MainSDR CA991008013Fire Loop · malfunctioned(CAN) ON CLIMB-OUT, NR 2 ENGINE FIRE DETECT SYSTEM FAULT. NR 2 ENG FIRE LOOP B REPLACED.Sep 16, 1999 · Airbus A340313 · Detection SystemSDR CA991008012Ecu · faulty(CAN) UNSTABLE ENGINE POWER CAUSED BY ECU CHANNEL B FAULT, LOW PRESSURE TURBINE CLEARANCE VALVE AND T12 SENSOR ALSO CHANGED.Sep 13, 1999 · Airbus A340313 · Fuel Control/Reciprocating EnginesSDR CA990614088Brake · failed(CAN) WHEEL NR 5 BRAKE TEMPERATURE AT SHUT DOWN 635 DEGREES CELSIUS. REPLACED NR 5 MAIN WHEEL ASSY AND INSPECTED BRAKE UNIT. NO FAULT FOUND WITH BRAKE UNIT.May 26, 1999 · Airbus A340313 · BrakeSDR CA990308035Door · not secured(CAN) FUEL PANEL DOOR OPEN LIGHT ON TAKEOFF ABORTED, NR 4 AND NR 8 BRAKES OVERHEATED. LATCHES ON FUEL PANEL DOOR ADJUSTED.Jan 11, 1999 · Airbus A340313 · Service DoorsSDR CA981030011Extract Fan · malfunctioned(CAN) WHEN ESTABLISHING EXTERNAL POWER VENT EXTRACT FAULT MESSAGE CAME ON ELECTRONIC CENTRALIZED AIRCRAFT SYSTEM FOLLOWED BY ACRID SMELL. EXTRACT FAN OVERHEAT RESET, OPERATION NORMAL, OVERBOARD VALVE RETURNED TO NORMAL. REPLACED EXTRACT FAN ASSEMBLY AND OPEROct 16, 1998 · Airbus A340313 · Air Distribution FanSDR CA981030012Skin · damaged(CAN) ON TOUCH-DOWN, CABIN CREW REPORTED SCRAPING. MAINTENANCE INSPECTION REVEALED SKIN SCRAPED BETWEEN STN FR 68 AND FR 73 AT STR 53R/53L, DAMAGE AREA WAS APPROXIMATELY 3 FEET WIDE BY 7 FEET LONG. REPAIRED PER SRM.Oct 2, 1998 · Airbus A340313 · Fuselage Main, Plate/SkinSDR CA980928028Bolt · loose(CAN) 1.5 HOURS AFTER LANDING, SMOKE WAS SEEN COMING FROM THE AUXILIARY POWER UNIT. THE APU WAS SELECTED OFF FROM THE COCKPIT. INSPECTION FOUND FUEL IN THE APU OIL TANK AND EVIDENCE OF BURNING AT THE EXHAUST MUFFLER. FURTHER INSPECTION FOUND A FCU BOLT HAD Aug 26, 1998 · Airbus A340313 · APU Engine Fuel and ControlSDR CA990203012Ecu · failed(CAN) NR 2 ENGINE FLAMED OUT AT 70 KNOTS ON TAKEOFF. TAKEOFF REJECTED. POWER LOSS AND TURBINE TEMPERATURE IN EXCESS OF 1000 DEGREES CELSIUS. TROUBLESHOOTING FOUND INTERMITTENT FAULT CONFUSED FULL DIGITAL CONTROL; CHANNEL A VARIABLE STATOR VANE FEED BACK ACTAug 21, 1998 · Airbus A340313 · Fuel Controlling SystemSDR CA980827020Radome · bird strike(CAN) MULTIPLE BIRD STRIKES ON RADOME. MAINTENANCE CONFIRMED EVIDENCE OF MULTIPLE BIRD STRIKES ON RADOME. AIRCRAFT CHECKED FOR OTHER DAMAGE AND NONE FOUND. AIRCRAFT DECLARED SERVICEABLE.Jul 17, 1998 · Airbus A340313 · Aerodynamic FairingsSDR CA980814012Radome · bird strike(CAN) MUTIPLE BIRD STRIKES ON RADOME. MAINTENANCE INSPECTION OF RADOME CONFIRMED BIRD STRIKES, NO DAMAGE TO RADOME, ENGINES/VANES OR PITOT STATIC SYSTEM.Jul 17, 1998 · Airbus A340313 · Aerodynamic FairingsSDR CA980608025Oven · contaminated(CAN) FIRE OCCURRED IN MIDDLE GALLEY OVEN. FIRE EXTINGUISHED BY CREW. IT WAS DETERMINED FIRE WAS CAUSED BY FOOD PAPER WRAPPING. OVEN CHECKED OKAY, NO FAULT FOUND.May 14, 1998 · Airbus A340313 · Buffet/GalleysSDR CA980512020Relief Valve · leaking(CAN) NACELLE TEMPERATURE ADVISORY AND FLASHING NR 1 NACELLE ON TAKE-OFF THRU 1500 FEET. TEMPERATURE ABOVE 240 DEGREES. MAINTENANCE REVEALED OVERPRESSURE RELIEF VALVE LEAKING AT SHAFT. VALVE REPLACED, BANJO FITTING REPAIRED, AND LEAK CHECK CARRIED OUT SERVIApr 14, 1998 · Airbus A340313 · Cabin Pressure Control SystemSDR CA980417015Actuator · inoperative(CAN) LOUD BANGING NOISE HEARD FROM NOSE AREA DURING TAKEOFF. THIRD TIME REPEAT. A/C RETURNED TO BASE. MAINTENANCE REPLACED NOSE LANDING GEAR UPLATCH AND ACTUATOR.Mar 30, 1998 · Airbus A340313 · Landing Gear ActuatorSDR CA971021017Flight Computer · failed(CAN) IMMEDIATELY AFTER TAKEOFF AUTO THROTTLE FLIGHT MESSAGE. ALSO LOST AUTO PILOT, AUTO THROTTLE, FLIGHT DIRECTOR, AUTO PILOT NOT AVAILABLE, NO SPEED TARGET, FLIGHT MODE ANNUNCIATOR BLANK, AIRCRAFT RETURNED TO BASE. MAINTENANCE ACTION INVOLVED REPACKING FLIGHOct 8, 1997 · Airbus A340313 · Autopilot ComputerSDR CA970922026Wheel Assembly · failed(CAN) CENTRE LINE LANDING GEAR SEPARATED ON TAKEOFF. MAINTENANCE ACTION INVOLVED REPLACING CENTRE LINE GEAR AND TWO CENTRE WHEELS. FINAL ANALYSIS OF FAILURE WILL CLOSE THIS SDR.Sep 1, 1997 · Airbus A340313 · Main Landing GearSDR CA970905008Pump · failed(CAN) LOW HYDRAULIC PRESSURE GREEN SYSTEM LIGHT ILLUMINATED. SYSTEM FLUID LEVEL REMAINED JUST ABOVE LOW LEVEL WARNING AFTER ECAM COMPUTER ACTIONS. MAINTENANCE ACTION INVOLVED REPLACING NR1 AND NR4 ENGINE HYDRAULIC PUMPS. LANDING GEAR SYSTEM RESET AND GREEN HYDAug 22, 1997 · Airbus A340313 · Hydraulic Pump (Electric/Engine), MainSDR CA970903019Wing Tip Brakes · tripping(CAN) FLAPS LOCK OUT AFTER EXTENSION FOR LANDING. WING TIP BRAKES FOUND TO BE TRIPPING ON NR2 FLAP/SLAT CONTROL COMPUTER. SYSTEM RESET AND FLAPS OPERATED NORMALLY.Aug 19, 1997 · Airbus A340313 · Leading Edge Slat Control SystemSDR CA970722042Fuselage · damaged area(CAN) DURING LOADING OF FORWARD CARGO HOLD, IT WAS FOUND THAT A PALLET IN POSITION 21P HAD BEEN INSTALLED INCORRECTLY. ON LANDING IT HAD SHIFTED FORWARD AND CAME LOOSE FROM THE STRAPPING. PALLET REMOVED REVEALING DAMAGE TO LEFT HAND AND RIGHT HAND SIDEWALL PANJul 10, 1997 · Airbus A340313 · Fuselage Miscellaneous StructureSDR CA970505031Fuselage · lightning strike(CAN) LIGHTNING STRIKE RH SIDE OF FUSELAGE NOSE SECTION. NOSE AREA INSPECTED AS PER A.M.M. 05-51-18. NO DAMAGE FOUND.Apr 24, 1997 · Airbus A340313 · Fuselage Main, StructureSDR CA970505030Smoke Detector · activated(CAN) ON CLIMB OUT AT APPROXIMATELY FL280 ECAM MESSAGE, FROWARD CARGO SMOKE INDICATION. BOTH FIRE BOTTLES (P/N 472931-2 AND 472930-2) ACTIVATED. FLIGHT CREW CHECKED FORWARD CARGO HOLD FOR FIRE IN FLIGHT. NO EVIDENCE OF FIRE FOUND. MAINTENANCE ACTION INVOLVED CApr 23, 1997 · Airbus A340313 · Smoke DetectionSDR CA970428007Cabin Projector · electrical short(CAN) PRIOR TO DEPARTURE "J" CLASS CABIN FORWARD PROJECTOR STARTED SMOKING. THE PROBLEM IS RESTRICTED TO MODIFICATION DOT 5 PROJECTORS INCORPORATING MOD. -012 POWER SUPPLIES INTERNALLY. THE PROJECTOR POWER SUPPLY CAPACITORS OVERHEAT AND LEAK FLUID ONTO PRINTEDMar 28, 1997 · Airbus A340313 · Entertainment SystemSDR CA970318026Trim Air Valve · failed(CAN) AIRCRAFT OPERATING WITH #1 AIR CONDITIONING PACK ON DEVIATION DUE TO OVERHEAT. UNABLE TO CONTROL CABIN PRESSURIZATION, TRIED TO RESTART #1 PACK, NO SUCCESS. INITIATED EMERGENCY DESCENT TO 10,000 FEET. MAINTENANCE TROUBLE SHOOTING REVEALED TRIM AIR PRESSUFeb 13, 1997 · Airbus A340313 · Cabin Pressure Control SystemSDR CA970226066Smoke Detector · activated(CAN) AFTER PUSH BACK, LOWER CREW REST ALARM SOUNDED ONLY IN LOWER CREW REST. LOWER CREW REST AREA AND AFT CARGO AREA VISUALLY INSPECTED. NO FAULT FOUND. CREW REST DISCONNECTED FROM AIRCRAFT. ON FIRST ENTRY OF CREW REST UNIT, FAINT ODOR OF A PLASTIC BURNINFeb 13, 1997 · Airbus A340313 · Smoke Detection
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