Airbus Industrie A330-342

Service difficulty reports · 44

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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 = 'A330342'
  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 CA190809014Unknown · smoke(CAN) DURING CLIMB OUT OF CDG, THERE WAS SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO CDG. #1 OVEN FOUND BURNT. OVEN 5501 REMOVED FROM AICRAFT. ELECTRICAL INSPECTION C/O ON MID GALLEY AS PER AMM 24-00-00-200-801-A. NO DEFECTS FOUND. ALL MID GALLEY OVEN C/B Aug 9, 2019 · Airbus A330342 · Air Distribution SystemSDR CA190802004Tire · cracked(CAN) DURING THE FLIGHT CREW`S WALK AROUND, THE PILOT NOTICED A SERIES OF CRACKS GOING ALL AROUND THE TIRES CLOSE TO THE RIM (ONLY ON THE INSIDE WALLS OF BOTH TIRES). BOTH WHEELS WERE CHANGED. AIRCRAFT BACK TO SERVICE (TC# 20190802004)Jul 30, 2019 · Airbus A330342 · TireSDR CA190522023Bolt · broken(CAN) #3 MAIN WHEEL FOUND 3 TIE BOLTS BROKEN. DAMAGE TO RIM, BRAKE AND BRAKE FAN. ON ARRIVAL BRAKE FAN WAS MAKING NOISE, DURING INSPECTION FOUND 3 FINS BROKEN OFF AND NOTICED 3 TIE BOLTS BROKEN (TC# 20190522023)May 21, 2019 · Airbus A330342 · Wheel/Ski/FloatSDR HALA2016103100376Seat Track · corrodedSEAT TRACK SECTION -Y1959, C26 - C38 IS CORRODED. CORROSION REMOVED IAW SRM 55-74-00 REV 91. DAMAGE DIMENSIONS STA 29968 CROWN CENTRAL/LATERAL 13MM X 5MM DEPTH 1MM, STA 31578 CROWN CENTRAL/LATERAL 10MM X 5MM DEPTH 1MM, 3 STA 33188 CROWN SUPERIOR 40MM X 10MM Oct 31, 2016 · N382HA · Airbus A330342 · Fuselage, Seat/Cargo Attach FittingsSDR CA160321004O-Ring · leaking(CAN) DURING CLIMB, THE CREW HAD ECAM MSG G RSVR LEAK, GREEN SYS DEPLETED AND FREE FALL EXTENSION CARRIED OUT. AFTER LANDING ACFT TOWED TO THE GATE FOR DEPLANING.Mar 18, 2016 · Airbus A330342 · Hydraulic System, MainSDR CA160224003Hydraulic Line · leaking(CAN) ACFT WAS CLIMBING AFTER TAKING OFF AND THE MLG WOULD NOT RETRACT. ECAM MESSAGE LDG RETRACTION FAULT QRH PROCEDURE APPLIED AND NO RESET OF SYSTEM WORK. CREW DECIDED TO RETURN TO DEPARTURE AIRPORT. NORMAL LANDING PERFORMED.Feb 23, 2016 · Airbus A330342 · Hydraulic System, MainSDR CA140917014Oven · failed(CAN) A POPPING NOISE HAS BEEN HEARD AND SPARKS WERE SEEN COMING OUT FROM THE BACK OF THE MID GALLEY OVENS. TWO OVENS WERE SUSPECTED (1 ON POS 5502 AND THE OTHER ONE ON POS 5503). ALL 5 BREAKERS OF MID GALLEY OVENS WERE PULLED OFF FOR THE REMAINDER OF THE FLIGSep 11, 2014 · Airbus A330342 · Buffet/GalleysSDR CA130506003Manifold · leaking(CAN) DURING WALKAROUND MAINTENANCE FOUND HYD LEAK AT GREEN GROUND SERVICE MANIFOLD, 2 SCREW HEAD BROKEN. MACHINE SCREWS WERE REPLACED AND ACFT RETURNED TO SERVICE.May 2, 2013 · Airbus A330342 · Hydraulic System, MainSDR CA130417002Hose · failed(CAN) 1000 PRIOR TO LANDING CREW REPORTED HYDRAULIC FLUID LOSS ON GREEN SYS. QRH PROCEDURE APPLIED AND ACFT LANDED UNEVENTFULLY. ACFT HAD TO BE TOWED OFF THE RUNWAY DUE TO LOSS OF STEERING CAPABILITY. AFTER INVESTIGATION, IT WAS FOUND THAT THE RT MLG DOOR UPLApr 16, 2013 · Airbus A330342 · Hydraulic System, MainSDR CA130121003Ballast · overheated(CAN) IN CRUISE, CREW REPORTED A RUBBER ORDER AT SEAT 29K. THE NEON BALLAST UNIT WAS FOUND WITH BURNED SPOTS AND ODOR. BALLAST WAS REPLACED IAW AMM AND TESTED SERVICEABLE.Jan 19, 2013 · Airbus A330342 · Passenger Compartment LightingSDR CA121015010Thermal Barrier · torn(CAN) CREW REPORTED VIA ACARS THAT NR 1 ENGINE EGT WAS LOWER THAN NR 2 ENGINE ALONG WITH AN INCREASE IN NACELLE TEMP. ON ARRIVAL, THE NR 1 ENGINE OTBD REVERSER HALF, C-DUCT, INNER FIX STRUCTURE, IFS WAS FOUND WITH DAMAGE. FURTHER INVESTIGATION SHOWED THE INOct 13, 2012 · Airbus A330342 · Engine Thrust ReverserSDR CA120111008Heat Exchanger · failed(CAN) DURING CRUISE ENGINE NR 1 ECAM ADVISORY FOR LOW QTY, OIL QTY AT 3.6. ACFT DIVERTED. FUEL OIL HEAT EXCHANGER AT FAULT. FOUND OIL IN HEAT EXCHANGER FUEL FILTER. THE FUEL OIL HEAT EXCHANGER HAS BEEN SENT FOR INVESTIGATION.Jan 4, 2012 · Airbus A330342 · Engine Oil CoolerSDR RYNA2011120800017Wire · reversedL2 DOOR EMERGENCY LIGHT EXIT SIGN ABOVE THE DOOR WILL NOT ILLUMINATE. TROUBLESHOT EXIT SIGN 23WL. FOUND POWER SUPPLY GOOD. FOUND WIRE 5183 AT PIN 3 AND WIRE 5182 PIN 1 REVERSED PER WDM 33-51-13. INSTALLED WIRE 5183 TO PIN 1 POSITION AND 5182 TO PIN 3 POSITDec 8, 2011 · N771RD · Airbus A330342 · Light System WiringSDR CA110719004Tire · failedATC ADVISED THAT A TIRE RECAP WAS FOUND ON RUNWAY. A FEW OF OUR ACFT WERE SUSPECTED TO BE THE OWNER FROM SCHEDULED DEPARTURES OFF THAT RUNWAY. UPON ARRIVAL, NR 1 TIRE WAS FOUND FLAT WITH RECAP MISSING. ALSO DAMAGE WAS FOUND ON LT MLG FIX FAIRING ALONG WITH Jul 16, 2011 · Airbus A330342 · TireSDR CA110708010Idg · failedDUE IDG FAILURE AND UNABLE TO CONFIRM IDG DISCONNECTED CREW ELECTED TO RETURN TO DEPARTUE FOR OVER WEIGHT LANDING APRX 210.0 KG. ELEC IDG 1 OIL SYS FAULT. OIL PRESSURE LOW , IDG OIL TEMP RISING COULD NOT ASCERTAIN WETHER IDG WAS DISCONNECTED AFTER IDG P/B PUJul 1, 2011 · Airbus A330342 · AC Generator-AlternatorSDR CA110117005Check Valve · failedENROUTE, THE FLIGHT EXPERIENCED A YELLOW HYD SYS FAILURE. QRH WAS FOLLOWED AND A PHONE PATCH WAS ESTABLISHED WITH MX CONTROL. THE FLIGHT IS CONTINUING. SN OF CHECK VALVE: 2525, MFG: SAMM..Jan 16, 2011 · Airbus A330342 · Hydraulic System, MainSDR CA110110007Blades · failedDURING THE INITIAL TAKEOFF ROLL THE NUMBER 1 ENGINE STALLED AND FAILED. THE CREW REJECTED THE TAKEOFF AT APPROX 5 KNOTS AND TAXIIED BACK TO THE GATE. NR 1 ENG BORO CARRIED OUT AS PER AMM 72-00-00-200-813 - HP 5TH STAGE HAD APPROX 30 BLADES WITH TIP CURL - INJan 7, 2011 · Airbus A330342 · Turbine SectionSDR CA101220002Brake · overheated(CAN) ON ARRIVAL BRAKE FIRE ASSOC. WITH HOT BRAKES/GREASE FIRE.CFR WERE CALLED,FIRE EXTINGUISHED BY RAMP CREW WITH FIRE EXTINGUISHER. MAINTENANCE ADVISED. NR 7 BRAKE FIRE REPORTED BY LEAD AND EXTINGUISHED. MAINTENANCE TO INSPECT NR 7 TIRE AND BRAKE INSP. NODec 18, 2010 · Airbus A330342 · Landing Gear Brake SystemSDR CA101208003Blades · damaged(CAN) FLIGHT CALLED FLIGHT DISPATCH VIA THE SAT PHONE FOR A PATCH TO MOC DUE TO AN ENGINE VIBRATION DURING THE CLIMB. CREW ADVISED MOC THAT THEY WERE UNABLE TO ATTAIN CLIMB POWER DUE TO A HIGH ENGINE VIBRATION. IT WAS DECIDED TO RETURN BACK TO POINT OF DEPARTUDec 6, 2010 · Airbus A330342 · Turbine Engine Compressor SectionSDR CA101110011Connector · broken(CAN) FUEL LOW PRESSURE SWITCH CONNECTOR 4075KS-B FOUND WITH BROKEN BACKSHELL AND PINS NOT ENGAGING.Nov 10, 2010 · Airbus A330342 · Engine Fuel System WiringSDR CA101101003Line · leaking(CAN) UPON ARRIVAL AT THE GATE MAINTENANCE CAME ONBOARD AND NOTIFIED THAT A FUEL LEAK WAS NOTICED ON ENG NR 2. FIRE HANDLE WAS PULLED AND CFR CALLED. CLOSER INSPECTION REVEALED THAT A CLAMP WAS FOUND CHAFING ON THE FUEL FEED LINE FROM THE HEAT EXCHANGER TO FAug 21, 2010 · Airbus A330342 · Engine Fuel DistributionSDR CA100118004Windshield · arced(CAN) F CREW- ON DESCENT, PASSING THROUGH 7000FT, THE CAPTS MAIN FWD WINDSCREEN CRACKED WITH SOME ARCING OCCURING. NORMAL APPROACH CARRIED OUT. MX- WINDSHIELD CHANGE RECORDS SHOW THE WINDSHIELD HAD BEEN INSTALLED FOR 32907 HOURS.Jan 14, 2010 · Airbus A330342 · Flight Compartment WindowsSDR CA090924003Blade · damaged(CAN) COMPRESSOR STALL OF RT ENG DURING CRUISE. HIGH VIBS OF N3 UP TO 9.0 UNITS. OPERATED AT REDUCED PWR DURING DIVERSION FOUND HPC DAMAGED. STAGE NR 1 BLADES SEVERLY DAMAGED. MANY NICKS, TEARS AND DENTS AND MISSING MATERIAL ON ALL BLADES. ONE BLADE BROKEN OFSep 15, 2009 · Airbus A330342 · Turbine Engine Compressor SectionSDR CA090709007Pump · leaking(CAN) NR 2 ENG EDP LEAKING AT CASING WHERE PRESSURE LINE CONNECTED. PUMP REPLACED.Jun 23, 2009 · Airbus A330342 · Hydraulic Pump (Electric/Engine), MainSDR CA080804002Controller · malfunctioned(CAN) CREW DID AN EMERGENCY DESCENT DUE ECAM WARNING EXCESSIVE CABIN ALTITUDE WITH CPC NR 1 FAULT. THE EMERGENCY DESCENT STARTED FROM FL320 TO FL090. THE CABIN ALTITUDE REACHED 12000 FT. DURING THE DESCENT THEY GOT MESSAGE "CABIN PR SAFETY VALVE OPEN". DURINGAug 1, 2008 · Airbus A330342 · Cabin Pressure ControllerSDR CA051111001Engine · bird ingestion(CAN) EVIDENCE OF BIRD STRIKE AT FAN BLADES. NO SIGNS OF BIRD REMAINS OR DAMAGE ON CORE OF ENG FAN BLADES, LP/IP SPLITTER FAIRING, OGV'S AOHE AIR INLET IDG OIL COOLER INLET INSPECTED. (A) DUE TO ENG SURGE OUT OF AIRPORT ON 01/09/2005. BOROSCOPE INSPECTION CARRNov 11, 2005 · Airbus A330342 · Turbine Engine Compressor SectionSDR CA051104018Actuator · faulty(CAN) AFTER A MAIN LANDING GEAR ACTUATOR REPLACEMENT, THE NOSE LANDING GEAR WOULD NOT FREE FALL ON SYSTEM NR1 DURING TEST PROCEDURE. SYSTEM WAS OK ON SYSTEM NR2. THE FREE FALL ACTUATOR ASSEMBLY WAS REPLACED AND SYSTEM FOUND SERVICEABLE. THE FREE FALL ACTUATOR Nov 3, 2005 · Airbus A330342 · Landing Gear ActuatorSDR CA050516002Tire · deflatedPREMATURE FAILURE OF NR 5 TIRE OF A/C 934, ON LANDING IN LHR MAY 02,2005 FROM FLIGHT 850 FROM YYC. NR 5 WHEEL WAS FOUND DEFLATED. NR 5 MAIN WHEEL REPLACED ON A/C 934 AS PER AMM 32-45-01.May 16, 2005 · Airbus A330342 · TireSDR CA050502002Windshield · failedDURING CRUISE, AT FL 380, CAPTAIN WINDSHIELD CRACKED. QRH PERFORMED AND AIRCRAFT LANDED AT NEXT SUITABLE AIRPORT. WINDSHIELD INSPECTED AS PER AMM AND FOUND OUTER PANE SHATTERED. WINDSHIELD REPLACED.Apr 25, 2005 · Airbus A330342 · Flight Compartment WindowsSDR CA040405AAADuct · ruptured(CAN) FLIGHT CREW REPORTED A RUMBLE NOISE HEARD FROM COCKPIT AND CABIN CONTINUOUSLY WITH BLEED AIR / AIR CONDITIONING. UNABLE TO ISOLATE WITH AIR CONDITIONING PACKS. DURING INVESTIGATION, MAINTENANCE FOUND THE GROUND AIR CONDITIONING DUCT ( COMPOSITE ) RUPTUREApr 2, 2004 · Airbus A330342 · Pneumatic Distribution SystemSDR CA040326005Slide · leaking(CAN) FOLLOWING A SLIDE RAFT DEPLOYMENT TEST, FOUND SLIDE RAFT DEFLATING AT SLOW RATE BY A PIN HOLE. PIN HOLE LOCATE ON FORWARD TUBULAR SECTION AT APPROXIMATELY 4 FEET FROM GROUND. DEFECT IS UNDER INVESTIGATION WITH ENGINEERING AND VENDOR.Mar 25, 2004 · Airbus A330342 · Escape SlideSDR CA031106001Actuator · malfunctioned(CAN) ON APPROACH ECAM FLAP FAULT, FLAPS WOULD NOT EXTEND. CARRIED OUT FLAPLESS LANDING. WITH SLATS AT 2 FOUND WATER IN NR 2 RT FLAP INPUT GEARBOX ROTARY ACTUATOR. DRAINED ACTUATOR AND REPLACED FLUID, ALL CKS NORMAL. MPD TASK TO CHANGE FLUID IS CALLED FOR ANov 5, 2003 · Airbus A330342 · Trailing Edge Flap ActuatorSDR CA030106003Isolation Valve · failed(CAN) LANDING GEAR DID NOT LOWER ON APPROACH. CREW RECYCLED TWICE WITH NO SUCCESS.ALTERNATE EXTENSION (FREE FALL) CARRIED OUT AND UNEVENTFUL LANDING ACCOMPLISHED. L/G ISOLATION SAFETY VALVE REPLACED AS PER AMM 32-31-17 AND OPERATION CHECK CARRIED OUT AS PER AMJan 4, 2003 · Airbus A330342 · Landing Gear Retraction/Extension SystemSDR CA021218001Brake Assy · fire(CAN) NR 3 WHEEL OBSERVED SMOKING AS AIRCRAFT TAXIED TO GATE. THEN FLAMES WERE OBSERVED COMMING FROM BETWEEN WHEEL HUB SPOKES. CREW LOG REPORT STATED MEDIUM BRAKING AND IDLE REVERSE SELECTED FOR LANDING. DUE INOPERATIVE REVERSER NR 2. AFTER AIRCRAFT STOPPED ATDec 13, 2002 · Airbus A330342 · BrakeSDR CA021227002Coffeemaker · odor(CAN) A/C ARRIVED ON A TURN AROUND AT YYZ. CREW INFORMED MTCE THAT THEY SMELLED SOMETHING BURNING IN THE AFT GALLEY. MTCE ISOLATED THE ODOR TO THE AFT LT GALLEY UNIT, NR 1 & 2 COFFEEMAKERS. THE COFFEEMAKERS WERE REMOVED FOR INSPECTION. MTCE FOUND THAT THE SHELDec 12, 2002 · Airbus A330342 · Buffet/GalleysSDR CA030116005Shaft · chafed(CAN) UPON A/C ARRIVAL IN YVR, NR 2 ENGINE HAD AN OIL LEAK. EXTERNAL GEARBOX DRIVE SHAFT SHROUD FOUND CHAFED THROUGH BY THE FUEL DRAIN TUBE. MTCE REPLACED THE DRIVESHAFT IAW AMM 72-62-11. ENGINEERING INITIATED A FLEET CAMPAIGN REVISING AN SI 5-72-004 REV 01. TNov 26, 2002 · Airbus A330342 · Turbine Engine Accessory DriveSDR CA021108005Bolt · loose(CAN) AT C02 CHECK FOUND THIS MAIN HINGE FITTING Y-BOLT O/B BEARING MIGRATED BY .0130 INCH AT REAR SPAR ATTACHMENT BOLT REPLACED BY NEW BOLT AT AC 11,599 HRS, 2,322 CYCLNov 6, 2002 · Airbus A330342 · Fuselage, Stabilizer Attach FittingsSDR CA020919002Eec · failed(CAN) ON APPROACH, ENGINE NR 2 FADEC FAULT. ECAM ACTION FOLLOWED ENGINE NR 2 SHUTDOWN FOR LANDING. POST FLIGHT REPORT INDICATED ENGINE NR 2 FADAC FAULT SOURCE DMC3 IDENT EIVMU, AFS, FWS. NR 2 ENGINE EEC REPLACED AND ENGINE GROUND RUN CARRIED OUT AND CHECKED Sep 18, 2002 · Airbus A330342 · Fuel Control/Turbine EnginesSDR CA020807004Monitor · failed(CAN) DURING FLIGHT THE LCD MONITOR AT L2 DOOR STOPPED WORKING AND EMITTED A BURNING SMELL. ON ARRIVAL IN CDG, MAINTENANCE INSPECTED THE MONITOR AND ITS ASSOCIATED WIRING AND FOUND NO DAMAGE. THE SYSTEM WAS DEACTIVATED (CONNECTOR REMOVED AND THE C/B PULLED) ANJul 30, 2002 · Airbus A330342 · Cabin Equipment/FurnishingsSDR CA020501015Line · damaged(CAN) WHILE THE AIRCRAFT WAS IN FOR AN ENGINE CHANGE , FOUND ON NR 1 ENGINE , THAT THE FUEL TUBE ASSY LINE DISCONNECT TO HP PUMP WAS DENTED. ONCE REMOVED, FOR REPLACEMENT , NOTICED THAT THE FERRULE, THE FERRULE SEAL CARRIERS WERE WORN AND PITTED AND ALSO THE CApr 19, 2002 · Airbus A330342 · Engine Fuel DistributionSDR CA020307016Pump · loose(CAN) DURING FINAL APPROACH INTO YVR, ECAM INDICATION OF GREEN SYSTEM RESERVOIR "UNDERFULL" WAS TRIGGERED, CREW CARRIED OUT PROCEDURES AS DETAILED ON ECAM WHICH INCLUDED DEPRESSURISING BOTH GREEN SYSTEM ENGINE DRIVEN PUMPS. AS A RESULT ON LANDING, AFTER ROLL-OMar 5, 2002 · Airbus A330342 · Hydraulic Pump (Electric/Engine), MainSDR CA020124008Control Unit · failed(CAN) ON THE PRE-DEPARTURE CHECK THE SMU (SYSTEM MANAGEMENT UNIT) CAUGHT ON FIRE NO EXTERNAL FLAME BUT FLAME AND WITHIN THE UNIT AND SMOKE COMING OUT OF THE UNIT.THE UNIT WILL HAVE A STRIP REPORT DONE AT THE MANUFACTURER FOR ANALYSIS. UNIT REPLACED.Jan 18, 2002 · Airbus A330342 · Entertainment SystemSDR CA011209002Solenoid Valve · broken(CAN) DURING DEACTIVATION OF THE NOSE LANDING GEAR STEERING SYSTEM, THE NOSE WHEELS TURNED 90 DEGREES RIGHT WITHOUT ANY STEERING INPUT WHEN STEERING / ANTI-SKID SWITCH WAS TURNED OFF. AT THAT MOMENT THE THE AIRCRAFT CONDITION WAS:-STEERING BY-PASS PIN INSTALLENov 29, 2001 · Airbus A330342 · Steering UnitSDR CA011207004Selector Valve · cracked(CAN) THE AIRCRAFT ARRIVED TO YYZ, WITH THE "YELLOW" HYDRAULIC SYSTEM EMPTY. FOUND RT ELEVATOR, OUTBOARD SERVO (F.I.N.3CS2) SELECTOR VALVE HOUSING CRACKED.Oct 22, 2001 · Airbus A330342 · Hydraulic System, Auxiliary
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