# Service difficulty reports: Airbus Industrie A330-342

A list on [Airbus Industrie A330-342](https://openairdocs.org/model/airbus-industrie-a330-342.md).

Newest first. General aviation reporting is voluntary.

- [SDR CA190809014](https://openairdocs.org/sdr/CA190809014.md): Unknown · smoke · Aug 9, 2019 · Airbus A330342 · Air Distribution System
  > (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
- [SDR CA190802004](https://openairdocs.org/sdr/CA190802004.md): Tire · cracked · Jul 30, 2019 · Airbus A330342 · Tire
  > (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)
- [SDR CA190522023](https://openairdocs.org/sdr/CA190522023.md): Bolt · broken · May 21, 2019 · Airbus A330342 · Wheel/Ski/Float
  > (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)
- [SDR HALA2016103100376](https://openairdocs.org/sdr/HALA2016103100376.md): Seat Track · corroded · Oct 31, 2016 · N382HA · Airbus A330342 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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
- [SDR CA160321004](https://openairdocs.org/sdr/CA160321004.md): O-Ring · leaking · Mar 18, 2016 · Airbus A330342 · Hydraulic System, Main
  > (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.
- [SDR CA160224003](https://openairdocs.org/sdr/CA160224003.md): Hydraulic Line · leaking · Feb 23, 2016 · Airbus A330342 · Hydraulic System, Main
  > (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.
- [SDR CA140917014](https://openairdocs.org/sdr/CA140917014.md): Oven · failed · Sep 11, 2014 · Airbus A330342 · Buffet/Galleys
  > (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 FLIG
- [SDR CA130506003](https://openairdocs.org/sdr/CA130506003.md): Manifold · leaking · May 2, 2013 · Airbus A330342 · Hydraulic System, Main
  > (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.
- [SDR CA130417002](https://openairdocs.org/sdr/CA130417002.md): Hose · failed · Apr 16, 2013 · Airbus A330342 · Hydraulic System, Main
  > (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 UPL
- [SDR CA130121003](https://openairdocs.org/sdr/CA130121003.md): Ballast · overheated · Jan 19, 2013 · Airbus A330342 · Passenger Compartment Lighting
  > (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.
- [SDR CA121015010](https://openairdocs.org/sdr/CA121015010.md): Thermal Barrier · torn · Oct 13, 2012 · Airbus A330342 · Engine Thrust Reverser
  > (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 IN
- [SDR CA120111008](https://openairdocs.org/sdr/CA120111008.md): Heat Exchanger · failed · Jan 4, 2012 · Airbus A330342 · Engine Oil Cooler
  > (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.
- [SDR RYNA2011120800017](https://openairdocs.org/sdr/RYNA2011120800017.md): Wire · reversed · Dec 8, 2011 · N771RD · Airbus A330342 · Light System Wiring
  > L2 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 POSIT
- [SDR CA110719004](https://openairdocs.org/sdr/CA110719004.md): Tire · failed · Jul 16, 2011 · Airbus A330342 · Tire
  > ATC 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
- [SDR CA110708010](https://openairdocs.org/sdr/CA110708010.md): Idg · failed · Jul 1, 2011 · Airbus A330342 · AC Generator-Alternator
  > DUE 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 PU
- [SDR CA110117005](https://openairdocs.org/sdr/CA110117005.md): Check Valve · failed · Jan 16, 2011 · Airbus A330342 · Hydraulic System, Main
  > ENROUTE, 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..
- [SDR CA110110007](https://openairdocs.org/sdr/CA110110007.md): Blades · failed · Jan 7, 2011 · Airbus A330342 · Turbine Section
  > DURING 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 - IN
- [SDR CA101220002](https://openairdocs.org/sdr/CA101220002.md): Brake · overheated · Dec 18, 2010 · Airbus A330342 · Landing Gear Brake System
  > (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. NO
- [SDR CA101208003](https://openairdocs.org/sdr/CA101208003.md): Blades · damaged · Dec 6, 2010 · Airbus A330342 · Turbine Engine Compressor Section
  > (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 DEPARTU
- [SDR CA101110011](https://openairdocs.org/sdr/CA101110011.md): Connector · broken · Nov 10, 2010 · Airbus A330342 · Engine Fuel System Wiring
  > (CAN) FUEL LOW PRESSURE SWITCH CONNECTOR 4075KS-B FOUND WITH BROKEN BACKSHELL AND PINS NOT ENGAGING.
- [SDR CA101101003](https://openairdocs.org/sdr/CA101101003.md): Line · leaking · Aug 21, 2010 · Airbus A330342 · Engine Fuel Distribution
  > (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 F
- [SDR CA100118004](https://openairdocs.org/sdr/CA100118004.md): Windshield · arced · Jan 14, 2010 · Airbus A330342 · Flight Compartment Windows
  > (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.
- [SDR CA090924003](https://openairdocs.org/sdr/CA090924003.md): Blade · damaged · Sep 15, 2009 · Airbus A330342 · Turbine Engine Compressor Section
  > (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 OF
- [SDR CA090709007](https://openairdocs.org/sdr/CA090709007.md): Pump · leaking · Jun 23, 2009 · Airbus A330342 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) NR 2 ENG EDP LEAKING AT CASING WHERE PRESSURE LINE CONNECTED. PUMP REPLACED.
- [SDR CA080804002](https://openairdocs.org/sdr/CA080804002.md): Controller · malfunctioned · Aug 1, 2008 · Airbus A330342 · Cabin Pressure Controller
  > (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". DURING
- [SDR CA051111001](https://openairdocs.org/sdr/CA051111001.md): Engine · bird ingestion · Nov 11, 2005 · Airbus A330342 · Turbine Engine Compressor Section
  > (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 CARR
- [SDR CA051104018](https://openairdocs.org/sdr/CA051104018.md): Actuator · faulty · Nov 3, 2005 · Airbus A330342 · Landing Gear Actuator
  > (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
- [SDR CA050516002](https://openairdocs.org/sdr/CA050516002.md): Tire · deflated · May 16, 2005 · Airbus A330342 · Tire
  > PREMATURE 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.
- [SDR CA050502002](https://openairdocs.org/sdr/CA050502002.md): Windshield · failed · Apr 25, 2005 · Airbus A330342 · Flight Compartment Windows
  > DURING 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.
- [SDR CA040405AAA](https://openairdocs.org/sdr/CA040405AAA.md): Duct · ruptured · Apr 2, 2004 · Airbus A330342 · Pneumatic Distribution System
  > (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) RUPTURE
- [SDR CA040326005](https://openairdocs.org/sdr/CA040326005.md): Slide · leaking · Mar 25, 2004 · Airbus A330342 · Escape Slide
  > (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.
- [SDR CA031106001](https://openairdocs.org/sdr/CA031106001.md): Actuator · malfunctioned · Nov 5, 2003 · Airbus A330342 · Trailing Edge Flap Actuator
  > (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 A
- [SDR CA030106003](https://openairdocs.org/sdr/CA030106003.md): Isolation Valve · failed · Jan 4, 2003 · Airbus A330342 · Landing Gear Retraction/Extension System
  > (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 AM
- [SDR CA021218001](https://openairdocs.org/sdr/CA021218001.md): Brake Assy · fire · Dec 13, 2002 · Airbus A330342 · Brake
  > (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 AT
- [SDR CA021227002](https://openairdocs.org/sdr/CA021227002.md): Coffeemaker · odor · Dec 12, 2002 · Airbus A330342 · Buffet/Galleys
  > (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 SHEL
- [SDR CA030116005](https://openairdocs.org/sdr/CA030116005.md): Shaft · chafed · Nov 26, 2002 · Airbus A330342 · Turbine Engine Accessory Drive
  > (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. T
- [SDR CA021108005](https://openairdocs.org/sdr/CA021108005.md): Bolt · loose · Nov 6, 2002 · Airbus A330342 · Fuselage, Stabilizer Attach Fittings
  > (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 CYCL
- [SDR CA020919002](https://openairdocs.org/sdr/CA020919002.md): Eec · failed · Sep 18, 2002 · Airbus A330342 · Fuel Control/Turbine Engines
  > (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
- [SDR CA020807004](https://openairdocs.org/sdr/CA020807004.md): Monitor · failed · Jul 30, 2002 · Airbus A330342 · Cabin Equipment/Furnishings
  > (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) AN
- [SDR CA020501015](https://openairdocs.org/sdr/CA020501015.md): Line · damaged · Apr 19, 2002 · Airbus A330342 · Engine Fuel Distribution
  > (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 C
- [SDR CA020307016](https://openairdocs.org/sdr/CA020307016.md): Pump · loose · Mar 5, 2002 · Airbus A330342 · Hydraulic Pump (Electric/Engine), Main
  > (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-O
- [SDR CA020124008](https://openairdocs.org/sdr/CA020124008.md): Control Unit · failed · Jan 18, 2002 · Airbus A330342 · Entertainment System
  > (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.
- [SDR CA011209002](https://openairdocs.org/sdr/CA011209002.md): Solenoid Valve · broken · Nov 29, 2001 · Airbus A330342 · Steering Unit
  > (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 INSTALLE
- [SDR CA011207004](https://openairdocs.org/sdr/CA011207004.md): Selector Valve · cracked · Oct 22, 2001 · Airbus A330342 · Hydraulic System, Auxiliary
  > (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.

## 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 = 'A330342'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-industrie-a330-342/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.