Airbus A330-343
Service difficulty reports · 136
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 = 'A330343' 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.
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 = 'A330343' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA150218006Unknown · odor(CAN) NOTICEABLE SOCK SMELL THROUGHOUT ACFT, MOST NOTICEABLE IN FLIGHT DECK & STRONG SMELL VICINITY ON TAKEOFF. RETURNING, SUGGESTED DIVERSION, CAPTAIN DECLINED IN FAVOR OF DIVERTING ELSEWHERE. RESOLUTION IAW TSM TASKS 21-00-81-810-805A & TSM TASK 71-00-81-8SDR CA150206003Controller · failed(CAN) ON TAKEOFF ROLL, A LOW POWER ECAM INDICATION PROMPTED A REJECTED TAKEOFF. SPEED AT REJECT WAS 105 KTS. IAW TSM71-00-00-810-941 & 21-63-00-810-913 REPLACED NR 2 FCV IAW 21-51-51 PB 401. ZONE CONTROLLER REPLACED IAW AMM 21-63-34 PB 401. PACK CONTROLLERSDR CA150122001Actuator · failed(CAN) AFTER TAKEOFF THE LANDING GEAR WOULD NOT LOCK IN THE UP POSITION AND THE GEAR DOORS WOULD NOT CLOSE. THE FLIGHT RETURNED. NO EMERGENCY WAS DECLARED BUT ERS MET THE FLIGHT ON ARRIVAL FOR A PRECAUTIONARY INSPECTION. RESOLUTION LT MLG UPLOCK ASSY REPLACED SDR CA141208002Engine · odor(CAN) INCIDENT DETAILS: SHORTLY AFTER TAKEOFF, WHEN THE AIR CONDITIONING WAS SELECTED ON A STRONG DIRTY SOCK ODOR WAS NOTED IN THE FLIGHT DECK AND CABIN. THE ODOR DISSIPATED BY THE TIME THE FLIGHT REACHED CRUISE ALTITUDE BUT CAME BACK WHEN THE FLIGHT BEGAN ITSSDR CA140910002Windshield · cracked(CAN) THE ACFT ENCOUNTERED A CRACKED FRONT LT OUTER PANEL WHILE ENROUTE. LT WINDSHIELD REPLACED IAW AMM 56-11-11.SDR CA140820001Drain Valve · damaged(CAN) INCIDENT DETAILS: DIVERTING DUE TO AFT GALLEY FLOODED. ENTIRE WATER SYSTEM SHUT-OFF IN ATTEMPTS TO STOP FLOODING. RESOLUTION FOUND COFFEE,CONGEALED MILK AND TISSUE CAUSING BLOCKAGE AT T PIECE IN AFT CARGO FLOOR JUST ABOVE AFT DRAIN MAST. BLOCKAGE REMOVSDR CA140818010Pump · failed(CAN) CREW ENCOUNTERED A NR 1 ENGINE ECAM MESSAGE LOW OIL PRECAUTIONARY MESSAGE. CREW PROCEEDED TO SHUT DOWN ENGINE 1 AND NOTIFIED DISPATCH OF INTENTION TO LAND AT NEAREST SUITABLE AIRPORT. HAVE CONFIRMED OIL PUMP SHEARED. ENGINE CHANGE NOT REQUIRED. NR 1 ENSDR CA140707011Line · failed(CAN) INCIDENT DETAILS: ON LONG FINAL, THE ACFT LOST 1 OF ITS HYDRAULIC SYSTEMS. THEY CONTINUED THE APPROACH AND LANDED WITHOUT FURTHER INCIDENT. AFTER STOPPING ON THE RWY THERE WAS SMOKE COMING OFF THE MLG. THE FIRE DEPARTMENT INSPECTED THE LANDING GEAR ANDSDR CA140627011Pump · failed(CAN) GREEN HYD FAILURE ENROUTE, CARRYING ON TO DESTINATION, DECLARING A PAN PAN ON ARRIVAL. FOUND NR 1 ENGINE GREEN HYD EDP DAMAGED ALSO CAUSING NR 2 ENG GREEN EDP TO BE OVERHEATED. BOTH PUMPS REPLACED TASK 29-00-00-280-092-AAND TASK 29-00-00-280-805-A CARSDR CA140611003Bottle · leaking(CAN) FLIGHT CREW ADVISED COMPLETE DEPLETION OF FLIGHT CREW OXYGEN WHILE ENROUTE/OVER ICELAND. IN CONSULTATION WITH THE DUTY PILOT/FLEET MANAGER AND FLIGHT DISPATCH THE FLIGHT WAS RECOMMENDED TO CONTINUE AS LONG AS THE ACFT PRESSURIZATION WAS NORMAL AND THE SSDR CA140417001Drain · leaking(CAN) FUEL LEAK AFTER ENGINE START, CRASH FIRE RESCUE CALLED FOR SUPPORT. APPROXIMATELY 2 LITERS FUEL COVERING APPROXIMATELY 6 SQ FT DRAINED FROM FUEL TANK SUMP DRAIN VALVE. LEAK WAS BROUGHT UNDER CONTROL BY MAINTENANCE. THE VALVE TO DRAIN WATER FROM TANK SDR CA140325004Video Display · malfunctioned(CAN) PASSENGER`S PERSONAL HEADSET SHORT CIRCUITED & BEGAN TO SMOKE. PAX WAS SEATED IN SEAT 42A. SPOKE WITH CORP SAFETY TO SEE IF CREW SHOULD KEEP THE HEADSET TO HAND IN UPON ARRIVAL. CORP SAFETY SAID IT WAS NOT REQUIRED & REQUESTED THAT THE CREW WRITE IT USDR CA140225006Engine · stalled(CAN) ON DEPARTURE PASSING 13,000 FT CREW HEARD A LOUD BANG FOLLOWED BY AN ENG 1 STALL ECAM. MOMENTARY FLAMES OBSERVED FROM AFT OF LT ENGINE ACCOMPANIED BY ACRID ODOR. ODOR DISSIPATED AFTER APPROXIMATELY 5 MINUTES. NR 1 ENG TROUBLESHOT IAW TV 142067, ALL PRSDR CA140204005O2 Generator · failed(CAN) DURING C-CHECK ON REPLACEMENT AND ACTIVATION OF THE OXYGEN GENERATORS TO BE DISCARDED, APPROACHING LIFE LIMIT, THE O2 GENERATORS FAILED TO ACTIVATE, NO CHEMICAL REACTION OR ANY HEAT GENERATED WHEN FIRING MECHANISM TRIGGERED.SDR CA140103012Display · failed(CAN) TWO DMCS FAIL PRIOR TO GOING OCEANIC AND UNABLE TO MAKE NON RVSM, NR 3 DMC REPLACED IAW AMM 31-62-34PB401. SATISFACTORY SUSPECT ND DU FAILED INTERMITTENTLY. SWAPPED CAPTAIN`S ND DU WITH LOWER ECAM DU FOR T/S.SDR CA131028007Indication Sys · failed(CAN) AFTER T/O THE CREW REPORTED AN UNSAFE R1 DOOR INDICATION. THE FLIGHT RETURNED AND LANDED OVERWEIGHT. RESOLUTION REATTACHED CONNECTOR FOR SENSOR 12MJ AT PSCU CONNECTOR BOX. DUMMY CONNECTOR BACK IN STOWAGE POSITION. GAP CHECKED OK IAW AMM TASK 52-71-11SDR CA130820007Controller · failed(CAN) AFTER 2 GATE RETURNS, FLIGHT WENT AIRBORNE AND HAD FURTHER MAINTENANCE ISSUES, NO ICE PROTECTION. RETURNED TO STATION AND LANDED OVERWEIGHT BY APPROXIMATELY 20 TONS. PFR SHOW ENGINE NR 2 PYLON LEAK AIR SWITCHED OFF BMC NR 2 TEST SHOWS BLEED LEAK. AFTESDR CA130722002Manifold · leaking(CAN) THE CREW REPORTED THE GREEN HYDRAULIC SYS WAS LOSING FLUID AND SHUTDOWN THE SYSTEM. THE FLIGHT WAS TOWED OFF THE RUNWAY AFTER LANDING. CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY, ATC ADVISED DISPATCH THAT NO MAYDAY OR PANPAN DECLARED FOUND ON GREEN HYSDR CA130516003Valve · dislodged(CAN) FUEL SPILL FROM ACFT WING SUMP VALVE JAMMED IN OPEN POSITION DURING FUELLING. APPROXIMATELY 1 LITER OF FUEL COVERING AREA 2 X 2.5 SQUARE METERS. SPILL CONTAINED AND ABSORBAL USED FOR CLEAN UP. FOUND DRAIN VALVE REQUIRED RESEATING, RESEATED DRAIN SUMP VASDR CA121217003O-Ring · leaking(CAN) WHILE BOARDING, FUEL WAS OBSERVED LEAKING FROM THE RT WING SUMP DRAIN. RESULTING SPILL WAS APPROXIMATELY 5 X 5. BOARDING SUSPENDED. CFR AND MAINTENANCE CALLED OUT TO GATE. HIGH POWER GROUND RUN CARRIED OUT FUEL WETNESS FOUND ON CLAMP CONNECTION REF ISDR CA121112003Coffeemaker · shorted(CAN) A F/A SUSTAINED A SHOCK FROM THE MID GALLEY COFFEEMAKER FOLLOWED BY THE BREAKER POPPING AND A FLASH. F/A IS EXPERIENCING SOME NUMBNESS IN THEIR FINGERS. IFS ADVISED AND WILL MEET THE FLIGHT. MAINTENCE CONTROL ADVISED. COFFEEMAKER REPLACED REF C 521867SDR CA120926001Acm · failed(CAN) SHORTLY AFTER TAKEOFF THERE WAS A STRONG ACRID ODOR IN THE COCKPIT AND THE PASSENGER CABIN. THE FLIGHT CREW REPORTED VERY THIN VISIBLE SMOKE AND A TEMPERATURE RISE IN THE COCKPIT AS WELL. THE FLIGHT RETURNED AND LANDED. NR 1 AIR CYCLE MACHINE REPLACESDR CA120914007A/C Pack · failed(CAN) OVERWEIGHT LANDING ON ACCOUNT OF AIRBORNE RETURN DUE TO NR 1 PACK FAILURE, APPROXIMATE LANDING WEIGHT 212,000 KGS. PFR SHOWS NO FAULT. PACK 1 OPERATED ON GROUND NO EXHAUST AIR OBSERVED-PACK 1 OVHT WARNING WAS ON AFTER 2 MINUTES. ECS GROUND REPORT SHOWSDR CA120913001Receptacle · failed(CAN) THE PTV UNIT AT SEAT 9K EMANATED SOME SMOKE. ISOLATED THE PROBLEM TO THE USB PORT WHICH WAS THEN DISCONNECTED. REPLACED DAMAGED USB PORT HARNESS ON CONTOUR SEAT SUITE 9K. REPLACED DAMAGED USB HARNESS. FOUND COVER DAMAGED, S/M TEMP REPAIRED, FOUND ISDR CA120712005Computer · failed(CAN) APPROXIMATELY 30MINUTES AFTER DEPARTURE THE CREW REPORTED AN ENGINE 2 BLEED LEAK INDICATION AND ELECTED TO RETURN TO STATION. LANDING WEIGHT WAS 15000KG OVER MAXIMUM. PANPAN WAS DECLARED WITH ATC. MAINTENANCE RESOLUTION: DUCT/PYLON LEAK INSPECTION CARRISDR RYNA201204100018Smoke Detector · false activationR3 LAVATORY SMOKE DETECTOR FAULT. PERFORMED MCDU TEST, FAULT CLEARED IAW 26-17-710.SDR RYNA201203270017Smoke Detector · faultySMOKE LAV DETECTOR FAULT LOCATION 38. PLACED ON MEL 26-17-01A. REPLACED SMOKE DETECTOR, OPS NORMAL IAW AMM 26-17-15-400-801-A. THIS CLEARS DMI 2225 PLACARDS REMOVED.SDR RYNA201203150014Smoke Warning · false activationPOST FLIGHT FAULT MESSAGE SMOKE DETECTOR LAVATORY 38. PERFORMED TEST AMM 26-17-00-PB-501, OPS CHECK NORMAL. PLACARD REMOVED.SDR CA120301006Oil System · leaking(CAN) FLIGHT CREW REPORTED A NR 2 ENGINE OIL LEAK. FLIGHT RETURNED TO DEPARTURE AIRPORT.SDR CA120119008Servo Valve · failed(CAN) IMMEDIATELY AFTER PARKING AT THE GATE, THE ACFT HAD A MINOR BRAKE FIRE ON THE LT MAIN GEAR SIDE. EMS WAS CALLED AS A PRECAUTION, HOWEVER THE FIRE WAS QUICKLY EXTINGUISHED. REPORTED BY FLIGHT CREW MAX BRAKE TEMP. 640C, 540C OBSERVED, BRAKE INSPECTED IAW SDR RYNA201201160003Lens · brokenFPEEPMS (FLOOR PROXIMITY EMERGENCY ESCAPE MARKING SYSTEM) LENS AT LAV 36 LOCK TAB BROKEN. REPLACED FPEEPMS LENS IAW AMM 33-51-13-400-801-A.SDR CA120103010Controller · failed(CAN) AFTER TAKEOFF APPROXIMATELY 60 MILES EAST THE FLIGHT CREW WAS ADVISED OF SMOKE AND A BURNING ELECTRICAL SMELL IN THE AFT GALLEY. THE CREW DECLARED AN, EMERGENCY EMERGENCY, AND RETURNED TO LAND OVERWEIGHT APPROXIMATELY 13000K. THE ACFT WAS MET BY EMERGENSDR CA111219018Idg · failed(CAN) THE CREW REPORTED WHILE IN CRUISE JUST PRIOR TO DESCENT THAT THE NR 2 GENERATOR FAILED AND SHOOK THE WHOLE ACFT. NR 2 IDG REPLACED IAW AMM 24-21-51.SDR RYNA201112080001Wire · mislocatedDOOR L2 EMERGENCY LIGHT EXIT SIGN ABOVE 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 POSITION SDR CA111221002Control Valve · fractured(CAN) FAILURE OF FLANGE ON FLOW CONTROL VALVE TROUBLESHOOTING IAW 36-11-00-720-806 CARRIED OUT. RT PACK FLOW CONTROL VALVE CHARGED & SYSTEM OPS CHECKED. SERVICEABLE.SDR CA110203008Monitor · smoke(CAN) 49A MONITOR STARTED TO SMOKE THEN TV WENT OUT AND EAR PIECE MELTED, SYSTEM WAS SHUTDOWN ASAP. REPORTED TO FLIGHT OPS: ENTERTAINMENT AT SEATS 49AC DE-ACTIVATED. UNDERSEAT ELECTRICAL CONNECTORS AT 48AC CAPPED & STOWED. REF: PP A330-23-42838. SVDU & AUDI
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