# Service difficulty reports: Airbus A330-322 A list on [Airbus A330-322](https://openairdocs.org/model/airbus-a330-322.md). Newest first. General aviation reporting is voluntary. - [SDR CA040617006](https://openairdocs.org/sdr/CA040617006.md): Relay · failed · Jun 8, 2004 · Airbus A330322 · Buffet/Galleys > COFFEEMAKER 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. - [SDR CA030723006](https://openairdocs.org/sdr/CA030723006.md): Web · torn · Jul 20, 2003 · Airbus A330322 · Engine Thrust Reverser > (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 PANEL - [SDR CA030328006](https://openairdocs.org/sdr/CA030328006.md): Slide · malfunctioned · Mar 27, 2003 · Airbus A330322 · Emergency Equipment > (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 WA - [SDR CA030304004](https://openairdocs.org/sdr/CA030304004.md): Mount · burned · Mar 1, 2003 · Airbus A330322 · Electrical Power System > (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 O - [SDR CA021223004](https://openairdocs.org/sdr/CA021223004.md): Controller · malfunctioned · Dec 21, 2002 · Airbus A330322 · Fuel Controlling System > (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 CONTROLL - [SDR CA011018006](https://openairdocs.org/sdr/CA011018006.md): O-Ring · fretted · Oct 2, 2001 · Airbus A330322 · Hydraulic Filter, Auxiliary > (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 REVER - [SDR CA010726026](https://openairdocs.org/sdr/CA010726026.md): Probe · blocked · Jul 24, 2001 · Airbus A330322 · Pitot/Static System > (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 PIT - [SDR CA010706001](https://openairdocs.org/sdr/CA010706001.md): Engine · failed · Apr 8, 2001 · Airbus A330322 · Engine (Turbine/Turboprop) > (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 DE - [SDR USAA010257](https://openairdocs.org/sdr/USAA010257.md): Nut · cracked · Mar 6, 2001 · N670UW · Airbus A330322 · Engine Mount Section > CLT - FOUND NUT CRACKED.5 INCH, FORWARD INBOARD BARREL NUT, AFT LEFT ENGINE MOUNT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EA 69252. (M) - [SDR USAA010256](https://openairdocs.org/sdr/USAA010256.md): Nut · cracked · Mar 6, 2001 · N670UW · Airbus A330322 · Engine Mount Section > CLT - FOUND NUT CRACKED.5 INCH, FORWARD LEFT BARREL NUT, AFT LEFT ENGINE MOUNT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EA 69252. (M) - [SDR CA010201016](https://openairdocs.org/sdr/CA010201016.md): Clamp · loose · Dec 20, 2000 · Airbus A330322 · Engine Bleed Air System > (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. - [SDR CA001207018](https://openairdocs.org/sdr/CA001207018.md): Flow Valve · faulty · Nov 25, 2000 · Airbus A330322 · Air Distribution System > (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. - [SDR CA001123013](https://openairdocs.org/sdr/CA001123013.md): O-Ring · deteriorated · Nov 20, 2000 · Airbus A330322 · Hydraulic System, Main > (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 FOU - [SDR USAABA00007](https://openairdocs.org/sdr/USAABA00007.md): Warning Light · activated · Nov 2, 2000 · N670UW · Airbus A330322 · Landing Gear Brake System > PIT - 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 B - [SDR CA000928043](https://openairdocs.org/sdr/CA000928043.md): O-Ring · ruptured · Sep 11, 2000 · Airbus A330322 · Hydraulic System, Main > (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 VAL - [SDR USAABA00002](https://openairdocs.org/sdr/USAABA00002.md): Fan · overheated · Aug 5, 2000 · N670UW · Airbus A330322 · Air Distribution Fan > PHL - FLT 3 - CREW NOTED ELECTRICAL SMELL IN FORWARD CABIN AREA. MAINTENANCE REPLACED THE RECIRCULATION FAN. (M) - [SDR CA000810013](https://openairdocs.org/sdr/CA000810013.md): Block · worn · Jul 28, 2000 · Airbus A330322 · Turbine Engine Compressor Section > (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 V - [SDR USAABA00001](https://openairdocs.org/sdr/USAABA00001.md): Adc · malfunctioned · Jun 20, 2000 · N670UW · Airbus A330322 · Air Data Computer > FLT 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 FU - [SDR CA000621041](https://openairdocs.org/sdr/CA000621041.md): Transmitter · failed · Jun 7, 2000 · Airbus A330322 · Engine Oil Pressure > (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. - [SDR CA001123012](https://openairdocs.org/sdr/CA001123012.md): Actuator · failed · Mar 16, 2000 · Airbus A330322 · AC Generation System > (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. - [SDR CA991116012](https://openairdocs.org/sdr/CA991116012.md): Blade · cracked · Nov 13, 1999 · Airbus A330322 · Hydraulic System, Auxiliary > (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. - [SDR CA991103045](https://openairdocs.org/sdr/CA991103045.md): O-Ring · cracked · Oct 23, 1999 · Airbus A330322 · Engine Thrust Reverser > (CAN) THRUST REVERSER HYDRAULIC FILTER ASSY O-RING WAS FOUND CUT AND EXTRUDED. - [SDR CA990907059](https://openairdocs.org/sdr/CA990907059.md): Ecam · false signal · Aug 12, 1999 · Airbus A330322 · Central Display > (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. - [SDR CA990728073](https://openairdocs.org/sdr/CA990728073.md): Flt Computer · malfunctioned · Jul 16, 1999 · Airbus A330322 · Flight Management Computing Hardware System > (CAN) DURING CLIMB, FLAPS AND SLATS SELECTED TO ZERO DEGREE POSITION, POSITION FAULT INDICATED ON ECAM. FLIGHT WARNING COMPUTER REPLACED, FAULT FIXED. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/model/airbus-a330-322/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.