Airbus A330-202

Service difficulty reports · 23

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 = 'A330202'
  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 2011F00020Restraint · shearedL4 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.Jan 5, 2011 · Airbus A330202 · Escape SlideSDR 0401863354Bolt · missingDURING 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 GEAROct 4, 2004 · N854NW · Airbus A330202 · FastenersSDR AUS20031159Actuator · incorrect(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.Nov 16, 2003 · Airbus A330202 · Stabilizer ActuatorSDR AUS20030438Pump · failed(AUS) APU FUEL PUMP FAILED. AFT PUMP HAD THE COVER BLOWN OFF AND FUEL IN THE ELECTRICAL WINDINGS.Apr 21, 2003 · Airbus A330202 · APU Engine Fuel and ControlSDR AUS20030578Motor · failed(AUS) ENGINE STARTER MOTOR FAILED. DAMAGE CAUSED TO ENGINE.Apr 17, 2003 · Airbus A330202 · Engine StarterSDR AUS20030437Motor · failed(AUS) ENGINE STARTER MOTOR FAILED. EXTERNAL DAMAGE TO ENGINE.Apr 17, 2003 · Airbus A330202 · Engine StarterSDR USAASA01047Wire · brokenLGA - THE FORWARD CLOSET EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES IN THE WIRE HARNESS ASSEMBLY FOR THE FORWARD CLOSET. OPERATIONALLY CHECKED OK. (M)Aug 29, 2001 · N112US · Airbus A330202 · Light System WiringSDR USAASA01041Windshield · crackedDCA - 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 CAug 4, 2001 · N102UW · Airbus A330202 · Window/Windshield SystemSDR USAASA01030Unknown · odorDCA-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 CJun 28, 2001 · N105UW · Airbus A330202 · Air Distribution SystemSDR USAASA01023Power Supply · dischargedCLT - 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 UJun 7, 2001 · N108UW · Airbus A330202 · Emergency LightingSDR CA010628027Controller · malfunctioned(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 May 22, 2001 · Airbus A330202 · SpoilersSDR CA000329024Cowl Door · separated(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.Mar 18, 2000 · Airbus A330202 · Engine Cowling SystemSDR CA000215020Connector · damaged(CAN) FLIGHT ATTENDANT REPORTED SMOKE IN AFT GALLEY. THROUGH INVESTIGATION REVEALED DAMAGED PINS IN THE CONNECTOR FOR THE TRASH COMPACTOR. CONNECTOR REPAIRED.Feb 9, 2000 · Airbus A330202 · Buffet/GalleysSDR CA000201018Engine · stalled(CAN) NR 1 ENG STALL, ECAM WARNING ON SPOOL UP. REPORT TO FOLLOW. NO FAULT FOUND. ENGINE RETURNED TO SERVICE.Jan 22, 2000 · Airbus A330202 · Engine (Turbine/Turboprop)SDR CA000128051Light · overheated(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 SEJan 9, 2000 · Airbus A330202 · Passenger Compartment LightingSDR AU000128051Light · overheated(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 Jan 9, 2000 · Airbus A330202 · Passenger Compartment LightingSDR CA991028019Valve · leaking(CAN) COMPLETE LOSS OF YELLOW SYSTEM HYDRAULIC FLUID. INVESTIGATION REVEALED A FAULTY O-RING ON CHECK VALVE 5316JM301.Oct 11, 1999 · Airbus A330202 · Hydraulic System, MainSDR CA991028018Rudder Pedal · jammed(CAN) CREW REPORTED LIMITED RUDDER TRAVEL. MAINTENANCE REMOVED CELL PHONE FROM CAPTAIN'S PEDALS.........SYSTEM OPERATED NORMAL!Oct 1, 1999 · Airbus A330202 · Rudder Control SystemSDR CA990915076Valve · failed(CAN) REJECTED TAKEOFF DUE TO ECAM ENGINE THRUST LOSS MESSAGE. ANTI-ICE VALVE REPLACED.Sep 6, 1999 · Airbus A330202 · Air Intake Anti/De-Ice SystemSDR CA990614069Pdu · failed(CAN) CARGO PDU FOUND SMOKING. UNIT REPLACED. UNITS ARE MADE BY TELAIRE. SEE TELAI RE SIL 25-100. SEE AIRBUS SB A330-25-3108.May 24, 1999 · Airbus A330202 · Cargo CompartmentsSDR CA990330035Pdu · malfunctioned(CAN) PDU UNITS FOUND RUNNING CONTINUOUSLY WITH BURNING SMELL AND SPARKING. PDU DISCONNECTED.Mar 7, 1999 · Airbus A330202 · AC Power Distribution SystemSDR CA990318059Idg · failed(CAN) ECAM MSG IDG OVERHEAT, INVESTIGATION REVEALED A LOOSE CANNON CONNECTOR AT UPPER RT PYLON.Mar 5, 1999 · Airbus A330202 · Alternator-Generator DriveSDR CA990330036Pdu · failed(CAN) PDU UNIT FOUND SMOKING, ELECTRICAL CONNECTOR DISCONNECTED, AIRCRAFT FLOWN TO MAINTENANCE BASE UNDER MEL.Feb 18, 1999 · Airbus A330202 · AC Power Distribution System
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