# Service difficulty reports: Airbus A330-202 A list on [Airbus A330-202](https://openairdocs.org/model/airbus-a330-202.md). Newest first. General aviation reporting is voluntary. - [SDR 2011F00020](https://openairdocs.org/sdr/2011F00020.md): Restraint · sheared · Jan 5, 2011 · Airbus A330202 · Escape Slide > L4 DOOR SLIDE NOT FULLY DEPLOYED DURING ROUTINE CHECK (OPS CHECK - CABIN ESCAPE FACILITIES DEPLOYMENT) ON A6 CHECK, MX REPLACED THE SLIDE. PRELIMINARY FINDING IS THE 410 LB RESTRAINT HAS NOT BEEN SHEARED WHICH CAUSED THE SLIDE NOT DEPLOYED AT LAST STAGE. - [SDR 0401863354](https://openairdocs.org/sdr/0401863354.md): Bolt · missing · Oct 4, 2004 · N854NW · Airbus A330202 · Fasteners > DURING CLIMB THE CREW OBSERVED DECREASING OIL QUANTITY AND PRESSURE ON THE NR 2 ENGINE. WHEN OIL PRESSURE DECREASED BELOW 70 PSI THE ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO NRT. AFTER LANDING HEAVY, A BRAKE FIRE OCCURRED ON THE LEFT MAIN LANDING GEAR - [SDR AUS20031159](https://openairdocs.org/sdr/AUS20031159.md): Actuator · incorrect · Nov 16, 2003 · Airbus A330202 · Stabilizer Actuator > (AUS) INCORRECT GREASE USED ON TRIM ABLE HORIZONTAL STABILIZER ACTUATOR (THSA). AEROSHELL 22 USED INSTEAD OF CORRECT AEROSHELL 33. USE OF INCORRECT GREASE MAKES AIRCRAFT NON COMPLIANT WITH AD/330/7.UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR. - [SDR AUS20030438](https://openairdocs.org/sdr/AUS20030438.md): Pump · failed · Apr 21, 2003 · Airbus A330202 · APU Engine Fuel and Control > (AUS) APU FUEL PUMP FAILED. AFT PUMP HAD THE COVER BLOWN OFF AND FUEL IN THE ELECTRICAL WINDINGS. - [SDR AUS20030578](https://openairdocs.org/sdr/AUS20030578.md): Motor · failed · Apr 17, 2003 · Airbus A330202 · Engine Starter > (AUS) ENGINE STARTER MOTOR FAILED. DAMAGE CAUSED TO ENGINE. - [SDR AUS20030437](https://openairdocs.org/sdr/AUS20030437.md): Motor · failed · Apr 17, 2003 · Airbus A330202 · Engine Starter > (AUS) ENGINE STARTER MOTOR FAILED. EXTERNAL DAMAGE TO ENGINE. - [SDR USAASA01047](https://openairdocs.org/sdr/USAASA01047.md): Wire · broken · Aug 29, 2001 · N112US · Airbus A330202 · Light System Wiring > LGA - THE FORWARD CLOSET EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES IN THE WIRE HARNESS ASSEMBLY FOR THE FORWARD CLOSET. OPERATIONALLY CHECKED OK. (M) - [SDR USAASA01041](https://openairdocs.org/sdr/USAASA01041.md): Windshield · cracked · Aug 4, 2001 · N102UW · Airbus A330202 · Window/Windshield System > DCA - FLT 6875 - EN ROUTE LGA-DCA, WHILE CLIMBING THROUGH FL180, THE CAPTAINS WINDSHIELD OUTER PANEL SHATTERED, ACCOMPANIED WITH BRIEF ARCING. QRH PROCEDURES WERE FOLLOWED. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE C - [SDR USAASA01030](https://openairdocs.org/sdr/USAASA01030.md): Unknown · odor · Jun 28, 2001 · N105UW · Airbus A330202 · Air Distribution System > DCA-LGA - FLT 6848 - THE AFT LAVATORY SMOKE DETECTOR SMOKE WARNING ILLUMINATED ON CLIMB-OUT OF DCA. SMOKE ODOR WAS ALSO CONFIRMED BY A FLIGHT ATTENDANT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LAVATORIES AND THE AIR C - [SDR USAASA01023](https://openairdocs.org/sdr/USAASA01023.md): Power Supply · discharged · Jun 7, 2001 · N108UW · Airbus A330202 · Emergency Lighting > CLT - FOUND THE EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE, AT THE LEFT OVERWING EXIT AND OVERHEAD AISLE, WITH THE NO SMOKING LIGHTS SELECTED ON. THE LIGHTS CAME ON WHEN THE EMERGENCY LIGHTS WERE SWITCHED ON. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY U - [SDR CA010628027](https://openairdocs.org/sdr/CA010628027.md): Controller · malfunctioned · May 22, 2001 · Airbus A330202 · Spoilers > (CAN) ON APPROACH AT 400 FT AND WHEN AUTOPILOT DISCONNECTED THE AIRCRAFT EXPERIENCED A SIGNIFICANT LEFT ROLL WHICH REQUIRED COMPENSATING SIDE STICK INPUT FOR THE FLARE. ON TAXI IN, MAINTENANCE NOTED THE L/H SPOILER 5 DEPLOYED AND OPERATIONAL CHECK OF SPOILERS - [SDR CA000329024](https://openairdocs.org/sdr/CA000329024.md): Cowl Door · separated · Mar 18, 2000 · Airbus A330202 · Engine Cowling System > (CAN) SHORTLY AFTER ROTATION LEFT ENGINE OUTBOARD FAN COWL DOOR ASSY DEPARTED. COWL APPEARS TO HAVE COME UNLATCHED AT THE LOWER EDGE CAUSING IT TO ROTATE UPWARDS AND BREAK OFF APPROX 24 INCHES FROM THE UPPER EDGE. INCIDENT UNDER INVESTIGATION BY SAFTEY BOARD. - [SDR CA000215020](https://openairdocs.org/sdr/CA000215020.md): Connector · damaged · Feb 9, 2000 · Airbus A330202 · Buffet/Galleys > (CAN) FLIGHT ATTENDANT REPORTED SMOKE IN AFT GALLEY. THROUGH INVESTIGATION REVEALED DAMAGED PINS IN THE CONNECTOR FOR THE TRASH COMPACTOR. CONNECTOR REPAIRED. - [SDR CA000201018](https://openairdocs.org/sdr/CA000201018.md): Engine · stalled · Jan 22, 2000 · Airbus A330202 · Engine (Turbine/Turboprop) > (CAN) NR 1 ENG STALL, ECAM WARNING ON SPOOL UP. REPORT TO FOLLOW. NO FAULT FOUND. ENGINE RETURNED TO SERVICE. - [SDR CA000128051](https://openairdocs.org/sdr/CA000128051.md): Light · overheated · Jan 9, 2000 · Airbus A330202 · Passenger Compartment Lighting > (CAN) CABIN CREW REPORTED UNSERVICEABLE READING LIGHT MOUNTED IN THE IR DOOR. INVESTIGATION REVEALED SIGNS OF OVERHEATING IN THE AREA OF THE POWER SUPPLY. A FLEET CHECK TURNED UP NO SUBSEQUENT FINDINGS, WATER INGRESS IS SUSPECTED AS CAUSING THE FAULT. PARTS SE - [SDR AU000128051](https://openairdocs.org/sdr/AU000128051.md): Light · overheated · Jan 9, 2000 · Airbus A330202 · Passenger Compartment Lighting > (AU) CABIN CREW REPORTED UNSERVICEABLE READING LIGHT MOUNTED IN THE IR DOOR. INVESTIGATION REVEALED SIGNS OF OVERHEATING IN THE AREA OF THE POWER SUPPLY. A FLEET CHECK TURNED UP NO SUBSEQUENT FINDINGS, WATER INGRESS IS SUSPECTED AS CAUSING THE FAULT. PARTS - [SDR CA991028019](https://openairdocs.org/sdr/CA991028019.md): Valve · leaking · Oct 11, 1999 · Airbus A330202 · Hydraulic System, Main > (CAN) COMPLETE LOSS OF YELLOW SYSTEM HYDRAULIC FLUID. INVESTIGATION REVEALED A FAULTY O-RING ON CHECK VALVE 5316JM301. - [SDR CA991028018](https://openairdocs.org/sdr/CA991028018.md): Rudder Pedal · jammed · Oct 1, 1999 · Airbus A330202 · Rudder Control System > (CAN) CREW REPORTED LIMITED RUDDER TRAVEL. MAINTENANCE REMOVED CELL PHONE FROM CAPTAIN'S PEDALS.........SYSTEM OPERATED NORMAL! - [SDR CA990915076](https://openairdocs.org/sdr/CA990915076.md): Valve · failed · Sep 6, 1999 · Airbus A330202 · Air Intake Anti/De-Ice System > (CAN) REJECTED TAKEOFF DUE TO ECAM ENGINE THRUST LOSS MESSAGE. ANTI-ICE VALVE REPLACED. - [SDR CA990614069](https://openairdocs.org/sdr/CA990614069.md): Pdu · failed · May 24, 1999 · Airbus A330202 · Cargo Compartments > (CAN) CARGO PDU FOUND SMOKING. UNIT REPLACED. UNITS ARE MADE BY TELAIRE. SEE TELAI RE SIL 25-100. SEE AIRBUS SB A330-25-3108. - [SDR CA990330035](https://openairdocs.org/sdr/CA990330035.md): Pdu · malfunctioned · Mar 7, 1999 · Airbus A330202 · AC Power Distribution System > (CAN) PDU UNITS FOUND RUNNING CONTINUOUSLY WITH BURNING SMELL AND SPARKING. PDU DISCONNECTED. - [SDR CA990318059](https://openairdocs.org/sdr/CA990318059.md): Idg · failed · Mar 5, 1999 · Airbus A330202 · Alternator-Generator Drive > (CAN) ECAM MSG IDG OVERHEAT, INVESTIGATION REVEALED A LOOSE CANNON CONNECTOR AT UPPER RT PYLON. - [SDR CA990330036](https://openairdocs.org/sdr/CA990330036.md): Pdu · failed · Feb 18, 1999 · Airbus A330202 · AC Power Distribution System > (CAN) PDU UNIT FOUND SMOKING, ELECTRICAL CONNECTOR DISCONNECTED, AIRCRAFT FLOWN TO MAINTENANCE BASE UNDER MEL. ## 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 = 'A330202' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/airbus-a330-202/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.