Airbus A330-322

Service difficulty reports · 24

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 = 'A330322'
  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 CA040617006Relay · failedCOFFEEMAKER WAS REMOVED DUE TO TRIPPING CIRCUIT BREAKER. STRIP REPORT REVEALED THAT THE UNAPPROVED RELAY WAS FITTED TO THE COFFEEMAKER. CORRECT P/N KR-90693-1 P/N FOUND KR 14DGE24.Jun 8, 2004 · Airbus A330322 · Buffet/GalleysSDR CA030723006Web · torn(CAN) ON ARRIVAL, MAINTENANCE NOTICED APPROXIMATELY 18 INCHES OF METAL PROTRUDING INTO THE AIR STREAM OF NR 1 ENGINE INBOARD THRUST REVERSER, JUST FORWARD OF THE CASCA DE VANES. FURTHER INVESTIGATION REVEALEDTHE DAMAGE TO BE THAT THE TORQUE-BOX FLOW WEB PANELJul 20, 2003 · Airbus A330322 · Engine Thrust ReverserSDR CA030328006Slide · malfunctioned(CAN) DURING DEPLOYMENT OF SLIDE RAFT L1 AND L4, AUTOMATIC INFLATION DID NOT OCCUR. DOOR AND SLIDE BOTTLE PRESSURES WERE IN THE GREEN RANGE. DEPLOYMENT NORMAL UP TO POINT OF SPEED LACING NOT RELEASING. MANUAL INFLATION HANDLE PULLED AND REMAINING DEPLOYMENT WAMar 27, 2003 · Airbus A330322 · Emergency EquipmentSDR CA030304004Mount · burned(CAN) A/C ARRIVED YVR WITH APU INOP. INSPECTION OF THE 5000VE PANEL REVEALED THAT THE FUSE F/N 6KA1 WAS INFACT BLOWN. CLOSER INSPECTION ALSO FOUND THAT ONE STUD BOLT OF THE MOUNT P/N NSA931190-1 THAT THE FUSE SITS ON WAS HEAVILY DAMAGED BY EXTREME HEAT. NUT OMar 1, 2003 · Airbus A330322 · Electrical Power SystemSDR CA021223004Controller · malfunctioned(CAN) REJECTED TAKE-OFF AT APPROX. 50 KTS FOR ECAM WARNING: ENG-THRUST LOSS (AMBER) ABNORMAL WING A. ICE (AMBER)THRUST LEVERS, IDLE (BLUE) AIRCRAFT RETURNED TO GATE WHERE MAINTENANCE FOLLOWED TROUBLE SHOOTING TASK 71-00-00-810-934, REPLACED THE ZONE CONTROLLDec 21, 2002 · Airbus A330322 · Fuel Controlling SystemSDR CA011018006O-Ring · fretted(CAN) A/C EXPERIENCED LOSS OF YELLOW HYDRAULIC SYS, ECAM WARNING - HYD RSVR LO/HYD SYS LO PR, APPROX 1(ONE) HR INTO FLT. FLT CREW SECURED SYS AS PER THE AFM&DIVERTED FLT TO MAN. UPON ARRIVAL IN MAN, MAINT FOUND FLUID DRIPPING FROM NR 2 ENGINE THRUST REVEROct 2, 2001 · Airbus A330322 · Hydraulic Filter, AuxiliarySDR CA010726026Probe · blocked(CAN) A/C ARRIVED WITH CAPTS. AIRSPEED READING INCORRECTLY. MTCE SWAPPED ADIRU #1 INTO #3 POSITION TO DEFER WITH LEAST AMOUNT OF IMPACT. A/C DEPARTED AND REJECTED T/O. ADM WAS OBTAINED FROM AIR CANADA AND INSTALLED IN A/C SSV. AVIONICS WAS CALLED IN TO C/O PITJul 24, 2001 · Airbus A330322 · Pitot/Static SystemSDR CA010706001Engine · failed(CAN) DURING DEPARTURE FLIGHT CREW APPLIED POWER TO START TO TAXI & NR 1 ENGINE FLAMED-OUT WITH AN ECAM WARNING OF STALL. DUE TO NO AUDIABLE STALL WAS OBSERVED, THE CREW RESTARTED THE ENGINE & ACCOMPLISHED A POWER RUN, NO FURTHER FAULT WAS OBSERVED AND THEY DEApr 8, 2001 · Airbus A330322 · Engine (Turbine/Turboprop)SDR USAA010257Nut · crackedCLT - FOUND NUT CRACKED .5 INCH, FORWARD INBOARD BARREL NUT, AFT LEFT ENGINE MOUNT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EA 69252. (M)Mar 6, 2001 · N670UW · Airbus A330322 · Engine Mount SectionSDR USAA010256Nut · crackedCLT - FOUND NUT CRACKED .5 INCH, FORWARD LEFT BARREL NUT, AFT LEFT ENGINE MOUNT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EA 69252. (M)Mar 6, 2001 · N670UW · Airbus A330322 · Engine Mount SectionSDR CA010201016Clamp · loose(CAN) NR 1 ENGINE PYLON BLEED AIR LEAK CAUTION ON THE ECAM WARNING. FOUND CLAMP LOOSE AND OUT OF PLACE IN THE NR 1 PYLON, CLAMP REINSTALLED AND RETIGHTEN, SURROUNDING AREA INSPECTED NO DAMAGE NOTED, SYSTEM TESTED SERVICEABLE AND AIRCRAFT DISPATCHED.Dec 20, 2000 · Airbus A330322 · Engine Bleed Air SystemSDR CA001207018Flow Valve · faulty(CAN) NR 1 AIR CONDITIONING PACK VALVE FAULTED DURING CRUISE. NR 2 AIR CONDITIONING PACK WAS AT THE TIME OF THE FAULT ON MEL 21-51-01. THE CAPTAIN, IN ACCORDANCE WITH HIS STANDARD OPERATING PROCEDURES RETURNED THE AIRCRAFT TO THE BASE OF DEPARTURE.Nov 25, 2000 · Airbus A330322 · Air Distribution SystemSDR CA001123013O-Ring · deteriorated(CAN) IN CRUISE ACTUAL LOSS OF BLUE SYSEM HYDRAULIC QUANTITY OCCURRED. THE FLUID LOSS WAS TRACED TO THE TRIMMABLE HORIZONTAL STABLILIZER ACTUATOR, BLUE SYSTEM VALVE BLOCK, HYDRAULIC PORT PLUG. THE PLUG WAS FOUND SECURE, BUT THE PLUG O-RING WAS UPON REMOVAL FOUNov 20, 2000 · Airbus A330322 · Hydraulic System, MainSDR USAABA00007Warning Light · activatedPIT - FLT 781, ON CLIMB-OUT FROM FRA, AT FL160, A HOT BRAKES CAUTION LIGHT ILLUMINATED. ECAM MESSAGE SHOWED ALL FOUR RT TRUCK BRAKES WARM, THE HOTTEST BEING THE RIGHT FRONT WHEEL NR 4 WHICH SHOWED 330 DEGREES CELSIUS. LANDING GEAR WAS EXTENDED IN FIGHT AND BNov 2, 2000 · N670UW · Airbus A330322 · Landing Gear Brake SystemSDR CA000928043O-Ring · ruptured(CAN) CREW OBSERVED ECAM MESSAGE BLUE HYDRAULIC SYSTEM LOW QUANTITY. THE CREW DEPRESSURIZED THE HYDRAULIC SYSTEM AS A PRECAUTION. THERE WAS NO LOSS OF HYDRAULIC PRESSURE PRIOR TO CREW ACTION. MAINTENANCE TROUBLE SHOOTING REVEALED THE O RING OF THE SAMPLING VALSep 11, 2000 · Airbus A330322 · Hydraulic System, MainSDR USAABA00002Fan · overheatedPHL - FLT 3 - CREW NOTED ELECTRICAL SMELL IN FORWARD CABIN AREA. MAINTENANCE REPLACED THE RECIRCULATION FAN. (M)Aug 5, 2000 · N670UW · Airbus A330322 · Air Distribution FanSDR CA000810013Block · worn(CAN) ECAM NR 1 ENGINE STALL WARNING DURING ENGINE SPOOL UP FOR TAKE-OFF ROLL, ABORTED TAKEOFF AND RETURNED TO GATE.CENTRALIZING BOLT HEADS AT THE NR 3, 5 & 6 POSITION VGV/IGV FOUND HARD RUBBING INTO THE RUBBING BLOCKS THAT GROVED AND OCCASIONALLY JAMMED THE VJul 28, 2000 · Airbus A330322 · Turbine Engine Compressor SectionSDR USAABA00001Adc · malfunctionedFLT 126 - EN ROUTE PHL-LGW, FL390, CRUISING AT 1.38 EPR, BOTH ENGINES INCREASED TO 1.61 EPR, THEN DOWN TO .95, THEN BACK TO 1.41. THIS FLUCTUATION OCCURRED OVER A TIME SPAR OF ABOUT A MINUTE AN A HALF. FLIGHT CONTINUED ON TO DESTINATION AND LANDED WITHOUT FUJun 20, 2000 · N670UW · Airbus A330322 · Air Data ComputerSDR CA000621041Transmitter · failed(CAN) AIRCRAFT RETURNED TO GATE WITH NR 1 ENGINE LOW OIL PRESSURE,AFTER BEING AIRBORNE FOR 20 MINUTES.LEFT HAND ENGINE OIL PRESSURE TRANSMITTER CHANGED, CONNECTOR PINS TENSION CHECKED SERVICEABLE, ENGINE GROUND RUN CARRIED OUT, LEAK CHECKED OK, SYSTEM NORMAL.Jun 7, 2000 · Airbus A330322 · Engine Oil PressureSDR CA001123012Actuator · failed(CAN) DURING 6C1 CHECK AT THE RAM AIR TURBINE (RAT) FAILED TO DEPLOY DURING AUTO AND MANUAL DEPLOYMENT TEST. TROUBLESHOOTING CARRIED OUT IN ACCORDANCE WITH TSM 29-24-00-810-802 DETERMINED RAT ACTUATOR FAULTY.Mar 16, 2000 · Airbus A330322 · AC Generation SystemSDR CA991116012Blade · cracked(CAN) DURING ROUTINE INSPECTION OF RAM AIR TURBINE, SCRATCH FOUND ON BLADE ROOT. FURTHER INVESTIGATION REVEALED A CRACK. THE SUBMITTER INDICATED THAT THERE IS NO SPECIFIC INSPECTION TASK CALLING UP THE INSPECTION OF THE RAM BLADES.Nov 13, 1999 · Airbus A330322 · Hydraulic System, AuxiliarySDR CA991103045O-Ring · cracked(CAN) THRUST REVERSER HYDRAULIC FILTER ASSY O-RING WAS FOUND CUT AND EXTRUDED.Oct 23, 1999 · Airbus A330322 · Engine Thrust ReverserSDR CA990907059Ecam · false signal(CAN) ECAM MESSAGE ON TAKEOFF INDICATED LOSS OF THRUST AND ENGINE ANTI-ICE FAULT WITH NO APPARENT FAULT. AIRBUS OIT 999.0106/96/SB AND TFU 73.25.000016.Aug 12, 1999 · Airbus A330322 · Central DisplaySDR CA990728073Flt Computer · malfunctioned(CAN) DURING CLIMB, FLAPS AND SLATS SELECTED TO ZERO DEGREE POSITION, POSITION FAULT INDICATED ON ECAM. FLIGHT WARNING COMPUTER REPLACED, FAULT FIXED.Jul 16, 1999 · Airbus A330322 · Flight Management Computing Hardware System
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