Airbus A310-300

Service difficulty reports · 89

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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 = 'A310300'
  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 CA050610001Oven · sparks(CAN) CABIN CREW NOTICED SPARKS COMING FROM RT OVEN. OVEN WAS DEACTIVATED AND REPLACED AT THE NEXT MAINTENANCE STATION. OVEN ROUTED TO REPAIR SHOP FOR INVESTIGATION.Jun 2, 2005 · Airbus A310300 · Buffet/GalleysSDR CA050425009Push-Pull Cable · contaminated(CAN) WHILE IN CRUISE AT 340, AFTER 2.5 HRS IN FLIGHT, NR 2 ENGINE THROTTLE JAMMED. QRH APPLIED WING ANTI-ICE SELECTED. AFTER CRUISING AT 260, THROTTLE CONTROL RECOVERED AND NORMAL OPERATION UP TO FL 360 AND THE REMAINING OF THE FLIGHT. THROTTLE CONTROL VEApr 24, 2005 · Airbus A310300 · Power LeverSDR CA040413008Cdu · smoke(CAN) DURING TAXIING TO THE GATE, AIRCRAFT EXPERIENCED SMOKE IN THE FLIGHT DECK CAUSED BY NR 2 FMS CDU. NR 2 CDU WAS CONFIRMED FAULTY AFTER MAINTENANCE INVESTIGATION AND THE AIRCRAFT WAS DISPATCHED UNDER MEL. CDU WAS REPLACED ON RETURN FLIGHT AND ROUTED TO VApr 7, 2004 · Airbus A310300 · Flight Management Computing Hardware SystemSDR CA040413003Access Door · missing(CAN) THE AIRCRAFT ARRIVED AT THE STATION WITH THE MID LAVATORY SERVICING ACCESS DOOR MISSING. THE AIRCRAFT WAS DISPATCHED UNDER CDL AND A NEW DOOR WAS INSTALLED AT THE MAIN BASE. THE LAVATORY SYSTEM WAS CHECKED SERVICEABLE (NO LEAK). SUSPECT PANEL NOT PROPApr 7, 2004 · Airbus A310300 · Fluid Service DoorsSDR CA040405001Wire · malfunctioned(CAN) FLAP JAM OCCURRED AFTER TAKE OFF. AIRCRAFT RETURNED TO THE STATION FOR RECTIFICATION. FLAP SFCC COMPUTER WAS RESET BY MAINTENANCE. FLAP SYSTEM WAS INSPECTED AND OPERATED SEVERAL TIMES WITH NO FAULT FOUND. AIRCRAFT WAS DISPATCH WITH NO FURTHER PROBLEM. AIMar 28, 2004 · Airbus A310300 · Flight Control System WiringSDR CA040324009Rod End · sheared(CAN) DURING TROUBLE SHOOTING A DEFECT ON NR 2 ENGINE REVERSER, LT LOWER SLEEVE NOT STOWING PROPERLY, FOUND THE LOWER JACKSCREW ACTUATORROD END BROKEN. ACTUATOR ASSEMBLY REPLACED AND SYSTEM VERIFIED SERVICEABLE. THIS IS THE SECOND EVENT WITH THE SAME FAILURE WMar 24, 2004 · Airbus A310300 · Engine Thrust ReverserSDR CA040324008Switch · broken(CAN) AIRCRAFT ARRIVED WITH FLAP UNABLE TO RETRACT PAST THE INTERMEDIATE POSITION OF +-5 DEGREES.UPON INVESTIGATION FOUND THE LEFT HAND OUTBOARD VANE JAM DETECTOR UNIT SWITCH SHEARED AND INTERNALLY JAMMED AND BUFFER CRUSHED. THE BRACKET/SWITCH ASSEMBLY WAS REPMar 20, 2004 · Airbus A310300 · Trailing Edge Flap Control SystemSDR CA040324007Rod End · sheared(CAN) DURING ROUTINE INSPECTION, NR 1 ENGINETHRUST REVERSER RT TRANSLATING COWL LOWER JACKSCREW ACTUATOR ROD END FOUND SHEARED IN THREADPORTION OF ROD END. JACKSCREW ACTUATOR ASSEMBLY REPLACED AND SYSTEM VERIFIED SERVICEABLE.Mar 2, 2004 · Airbus A310300 · Engine Thrust ReverserSDR CA031021006Transformer · burned(CAN) DURING FLIGHT, THE CABIN CREW REPORTED AN ELECTRICAL BURNING ODOR IN CABIN AT ROW 13. THE LIGHTS WERE EXTINGUISHED AND THE ODOR DISAPPEARED AFTER 15 MINUTES. MAINTENANCE FOUND THE TRANSFORMER AT ROW 14 ABC SMELLED BURNED. THE PASSENGER SERVICE MODULE Oct 14, 2003 · Airbus A310300 · Equipment/Furnishings WiringSDR CA030930002Odor · detected(CAN) FLIGHT CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE CABIN ON APPROACH WITH GEAR SELECTED DOWN.DURING GROUND TEST , THE PROBLEM WAS TRACED TO THE RT AIR CONDITIONING PACK .THE HEAT EXCHANGER HAD BEEN REPLACED ON THE PREVIOUS FLIGHT AND WAS FRESHLY O/H Sep 29, 2003 · Airbus A310300 · Cabin Cooling SystemSDR CA030911001Servo · jammed(CAN) DURING TAXI ,THE ECAM MESSAGE AILERON BLUE SYSTEM JAM CAME ON UPON THE FLIGHT CONTROL CHECK BY THE FLIGHT CREW. PROCEDURE PERFORMED AS PER CHECK LIST AND THE AIRCRAFT RETURNED TO THE GATE DUE TO HARD DEFLECTION OF CONTROL WHEEL AND UNABLE TO DETERMINE MSep 10, 2003 · Airbus A310300 · Aileron Control SystemSDR CA030819001Servo · malfunctioned(CAN) DURING TAKE-OFF ROLL, OUT OF EXETER AND A COUPLE OF TIMES IN FLT, CREW REPORTED RUDDER KICKED, FOLLOWED BY A BANK OF 10 DEGREES. THE YAW AUTOPILOT ACTUATOR WAS REPLACED AND THE SYSTEM WAS CONFIRMED SERVICEABLE AFTER A VERIFICATION FLT.Aug 13, 2003 · Airbus A310300 · Autopilot SystemSDR CA030522002Access Door · broken(CAN) AIRCRAFT ARRIVED AT THE STATION WITH THE RT ENGINE OIL TANK ACCESS DOOR HALF PORTION BROKEN OFF ANDMISSING. NEW DOOR WAS INSTALLED. FAN COWL WAS SLIGHTLY DAMAGED BY THE DOOR STRIKING. DAMAGE WAS CONSIDERED ACCEPTABLE AS PER AMM. SUSPECT THAT OIL TANK ACCMay 20, 2003 · Airbus A310300 · Service DoorsSDR CA030403001Hose · damaged(CAN) AIRCRAFT LOST GREEN HYDRAULIC FLUID DURING FLIGHT . DURING TROUBLE SHOOTING , THE RT MLG TRUCK POSITION ACTUATOR FLEX HOSE WAS FOUND PERFORATED UNDER THE BRADED SURFACE . THE HOSE ASSY WAS REPLACED AND THE SYSTEM WAS TESTED SERVICEABLE.Apr 2, 2003 · Airbus A310300 · Hydraulic System, MainSDR CA030321002Tube · damaged(CAN) DURING FLIGHT HYDRAULIC RESERVOIR LOW LEVEL APPEARED ON GREEN SYSTEM. AFTER INVESTIGATION A PIN HOLE WAS FOUND ON THE LT WING SPOILER PRESSURE TUBE. TUBE ASSY WAS REPLACED AS M/M AND SYSTEM SERVICED AIRCRAFT WAS RETURNED TO SERVICE. CAUSE OF FAILURE ISMar 20, 2003 · Airbus A310300 · Hydraulic System, MainSDR CA030214009Bolt · loose(CAN) DURING THE A-01 CHECK, RT MAIN LANDING GEAR, EMERGENCY BRAKE MANIFOLD WAS SUSPECTED TO BE LEAKING. INSPECTION FOUND THE ALTERNATE BRAKE RETURN ACCUMULATOR LOOSE ON THE MANIFOLD, DUE TO THE FACT THAT THE BOLTS INSTALLED TO SECURE THE ACCUMULATOR WERE NOT Feb 10, 2003 · Airbus A310300 · FastenersSDR CA030122009Bolt · stripped(CAN) DURING A CHECK ROUTING INSPECTION THE FOUR BOLTS (AN6-17) AT THE ATTACHMENT OF THE SHOCK ABSORBER OFTHE UPPER PART OF THE BARREL HAVE BEEN FOUND STRIPPED AND THE NUTS LOOSE. INSTALLATION OF THE BOLTS HAS TO BE CARRIED OUT IAW INSTRUCTIONS GIVEN IN THE MEJan 14, 2003 · Airbus A310300 · Nose/Tail Landing GearSDR CA030115009Panel · missingUPON A/C ARRIVAL FROM FLIGHT, FOUND ON WALK AROUND 3 MISSING PANELS (PANELS 134ER; P/N A5247007020600, 134CR; P/N A5247007020200, 134DR; P/N A5247007020400). HOLDING BRACKETS THOSE PANELS WERE ALSO FOUND TO BE DAMAGED. NEW HOLDING BRACKETS WERE FABRICATED IADec 9, 2002 · Airbus A310300 · Service DoorsSDR CA030112004Transmitter · reads low(CAN) THE YELLOW HYDRAULIC TRANSMITTER READING LOW ON ARRIVAL. DURING SERVICING OF THE YELLOW HYDRAULIC SYSTEM, FLUID EMERGED FROM THE AIR DEPRESSURIZATION RELIEF VALVE. THE ERRONEOUS READING (FROM THE DEFECTIVE 'HYDRAULIC TRANSMITTER,CAUSED MTCE TO OVERFILL TDec 1, 2002 · Airbus A310300 · Hydraulic Quantity IndicatorSDR CA030112002Clamp · broken(CAN) UPON A/C ARRIVAL, DURING WALK AROUND, MTCE NOTED THAT THE NR 5 MLG WHEEL BRAKE COOLING FAN SHROUD ATTACHMENT CLAMP WAS BROKEN. MTCE REPLACED THE CLAMP IAW AMM 12-37-32.Nov 28, 2002 · Airbus A310300 · Landing Gear Brake SystemSDR CA021117002Duct · cracked(CAN) BLEED DUCT ON AIRFRAME SIDE OF ENGINE BLEED VALVE ON TAKE TO REVERSER AIR MOTOR OF NR 1 ENGINE WAS FOUND CRACKED AND SEVERELY LEAKING. DUCT WAS REPLACED AND A LEAK CHECK WAS CARRIED OUT AND NONE WERE FOUND.Nov 10, 2002 · Airbus A310300 · Engine Bleed Air SystemSDR CA030106020Plate · bent(CAN) A/C WAS COMING OUT OF AC CHECK AND DURING FERRY FLT CREW REPORTED THAT THEY WERE UNABLE TO OBTAIN FULL REVERSE THRUST ON EITHER ENGINE ON LANDING. PILOT WAS UNABLE TO MOVE THRUST LEVERS TO FULL REVERSE POSITION AND MAXIMUN REVERSE THRUST ACHIEVED WAS 40 Nov 1, 2002 · Airbus A310300 · Engine Thrust ReverserSDR CA021110001Light · burned out(CAN) IN CRUISE AT39 000 FT. COCKPIT CREW NOTICED A BURNING ODOR COMING FROM THE OVERHEAD PANEL. NOTHING CAME OUT OF THE SNIFFER FAN (THE ODOR WAS NOTICED INTERMITTENTLY FOR 30 MINS. AND THEN STOPPED.). THE ODOR WAS NOTICED EQUALLY AT ROW 2 AND 15. TROUBLE SHOct 9, 2002 · Airbus A310300 · Passenger Compartment LightingSDR CA020920001Liner · missing(CAN) DURING THE WALK AROUND OF AIRCRAFT, FOUND THE LOWER FWD LINING ASSY, AT AFT CARGO COMPARTMENT DOOR FRAME, WAS MISSING. MAINTENANCE REPLACED THE LINING ASSY IAW AMM 53-17-88.Sep 15, 2002 · Airbus A310300 · Fuselage Miscellaneous StructureSDR CA020912003Light · burned out(CAN) TEMPORARY SMOKE ODOR DURING CLIMB OUT. ONE GALLEY LIGHT BURNED OUT AT THE SAME TIME. NO ECAM WARNING. MAINTENANCE REPLACED THE GALLEY LIGHTS AT L1 DOOR AND CHECKED SERVICEABLE PER THE AMM 33-24-11. NO SIGNS OF OVERHEAT DAMAGE ON BALLASTS.Sep 8, 2002 · Airbus A310300 · Flight Compartment LightingSDR CA020829014Shutoff Valve · failed(CAN) IN YQB, HAD TO SHUT NR 1 ENGINE DOWN WITH FIRE HANDLE SINCE MOVING THE HP FUEL LEVER NR 1 TO THE OFF POSITION. CLOSE THE HP FUEL VALVE. MAINTENANCE IN YQB, CHECKED THE FUEL SYSTEM FOR PROPER FUNCTION, IN ACCORDANCE WITH THE AMM 71-00-00, P.534 AND CHEAug 26, 2002 · Airbus A310300 · Fuel Selector/Shut-Off ValveSDR CA020722003Connector · burned(CAN) DURING PREDEPARTURE CHECK, IT WAS NOTICED THAT THE NR 2 ENGINE GREEN HYDRAULIC PUMP LOW PRESSURE LIGHT ON THE OVERHEAD PANEL, WAS NOT ON. IT WAS FOUND THAT NR 2 GREEN HYDRAULIC PUMP CONNECTOR FIN DV213 WAS BADLY BURNED AND THAT THE PINS WERE HEAVILY CORJul 21, 2002 · Airbus A310300 · Hydraulic Power System WiringSDR CA020718006Transmitter · failed(CAN) ON TAKE OFF ROLL A "TAKE-OFF CONFIGURATION WARNING" WAS TRIGGERED. AIRCRAFT SPEED WAS BELOW 80 KTS, CREW PROCEEDED WITH AN ABORTED TAKE OFF.TROUBLESHOOTING REVEALLED A DISCREPANCY BETWEEN THE THS POSITION INDICATION ON ECAM AND THE PITCH TRIM WHEEL INDEXJul 11, 2002 · Airbus A310300 · Stabilizer Position IndicatingSDR CA020712005Control Valve · leaking(CAN) DURING AN A-CHECK A HYDRAULIC OIL PUDDLE WAS FOUND IN FRONT OF NOSE GEAR. AFTER INVESTIGATION A PIN HOLE WAS FOUND ON THE RIGHT NLG DOOR ACTUATOR CONTOL VALVE. THE ACTUATOR, CONTOL VALVE ASSEMBLY WAS REPLACED AND A LEAK CHECK WAS CARRIED OUT WITH NO FUTHJul 11, 2002 · Airbus A310300 · Landing Gear Retraction/Extension SystemSDR CA020705003Panel · damaged(CAN) DURING WEEKLY CHECK, NR 2 RT SLAT ACTUATOR PANEL ASSY. FOUND DAMAGED. PART OF THE COMPOSITE PANEL WAS MISSING. AIRCRAFT WAS AOG. THE PANEL WAS FLOWN IN. MAINTENANCE REPLACED THE PANEL I.A.W. AMM 57-40-00.Jul 2, 2002 · Airbus A310300 · Leading Edge DevicesSDR CA020708009Water Heater · failed(CAN) DURING THE C-08 CHECK, IT WAS DISCOVERED DURING THE OPERATIONAL TEST, THAT THE POTABLE WATER HEATERS, IN LAVATORY F, WERE MAKING THE C/B TRIP. THE 3 UNITS WERE REMOVED AND SENT TO THE AVIONICS SHOP. WHEN REMOVING THE TOP COVER OF ONE UNIT, WE FOUND A SOJun 13, 2002 · Airbus A310300 · LavatoriesSDR CA020604007Isolation Valve · failed(CAN) AFT TRIM TANK MESSAGE AFTER ISO VALVE STARTED TO FLASH (VALVE IN TRANSIT). MAINTENANCE REPLACED THE AFT TRIM TANK ISO VALVE I.A.W. THE AMM 28-22-54 AND AIRCRAFT RETURNED TO SERVICE.May 28, 2002 · Airbus A310300 · Aircraft Fuel Distribution SystemSDR CA020315011Ballast · failed(CAN) ON PUSH BACK THE FLIGHT ATTENDANT NOTICED A STRONG ELECTRICAL BURNING SMELL , NO SMOKE , IN THE FORWARD CABIN LT SIDE . THE AIRCRAFT RETURNED TO THE GATE FOR INVESTIGATION . THE FORWARD CABIN CEILING AREA WAS INSPECTED FOR SIGNS OF A BURNED WIRE OR DISCOMar 14, 2002 · Airbus A310300 · Flight Compartment LightingSDR CA020221012Adc · out of adjust(CAN) AIRCRAFT RETURNED AFTER TAKEOFF WITH MULTIPLE FLIGHT ENVELOPE AND SPEED PROTECTION FAULTS. MAINTENANCE FOUND LOADED FLIGHT PLAN DATA NOT IN AGREEMENT . IRS(INERTIAL REFERENCE SYSTEM) WERE REALIGNED , FLIGHT PLAN DATA REINSERTED AND ALL FMS (FLIGHT MANAGEFeb 2, 2002 · Airbus A310300 · Flight Management Computing Hardware SystemSDR CA020110019Mec · failed(CAN) DURING TAKE OFF NR 2 ENGINE SPEED UP WAS SLOW ON APPROACH NR 2 ENGINE WAS 15 TO 20 PERCENT LOWER THAN NR 1 ENGINE AND THROTTLE LEVERS WERE EVEN. MAIN ENGINE CONTROL REPLACED. LEAK CHECK CARRIED OUT AND IDLE RUN CARRIED OUT, ALL PARAMETERS CHECKED WITJan 7, 2002 · Airbus A310300 · Fuel Control/Turbine EnginesSDR CA020118001Control Unit · malfunctioned(CAN) MANY INDICATIONS (DEFECTS REPORTED) OF SLATS / FLAPS SYSTEM NR 1 & 2 FAULTS HAVE BEEN REPORTED ON AIRCRAFT, HAVING SEVERAL MAINTENANCE ACTION C/OUT FROM 2001-11-25 TO 2001-12-20 AND THE FINAL RECTIFICATION BEING THE REPLACEMENT OF THE LAT FLAP CONTROL Dec 20, 2001 · Airbus A310300 · Leading Edge Slat Control SystemSDR CA020628004Blade · damaged(CAN) COMPRESSOR STALL ON TAKE OFF IN LRM, ON ENGINE NR 2 , MTCE FOUND AFTER VISUAL INSPECTION, 2 BLADES DAMAGED. FURTHER INSPECTION C/OUT IN ACCORDANCE WITH AMM 72-00-00 P.600, REVEALED DAMAGE ON HIGH PRESSURE COMPRESSOR. NUMEROUS BLADES NICKED, CURLED, TORN Aug 5, 2001 · Airbus A310300 · Engine (Turbine/Turboprop)SDR CA960712103Transponder · malfunction(CAN) WHILE VMC AT FL350 IN LEVEL FLIGHT NEAR THE AUTUN VOR, AIRCRAFT EXPERIENCED AT FULL TCAS ADVISORY & RESOLUTION. FIRST A TARGET DISPLAYED ON THE IVSI AT THE 2-3 O'CLOCK POSITION AT 2-3 NM RANGE AT THE SAME ALTITUDE, ACCOMPANIED BY AN AURAL WARNING. APPROXJul 2, 1996 · Airbus A310300 · Air Collision Avoidance SystemSDR 96ZZZX3410Lanyard · fail testOXYGEN MASK LANYARDS FOR ACTIVATING PASSENGER OXYGEN SYSTEMS FAILED THE PULL TEST. INSPECTION OF ALL LANYARDS WITH THIS PART NUMBER BOX RESULTED IN IDENTIFYING 100 PERCENT DEFECTIVE, I.E., BAD CRIMPS AND CRIMPS SLIPPING. PURITAN BENNETT HAS BEEN NOTIFIED ANDJun 14, 1996 · Airbus A310300 · Passenger Oxygen System
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