Airbus A310-300

Service difficulty reports · 89

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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 = 'A310300'
  ORDER BY difficulty_date DESC"

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SDR FDEA202410231576Switch · failedPDIS 733 52-70 8386 23OCT24 05:16 MEM OPEN PASSING FL230, RECEIVED A FLASHING RED LIGHT AND ALARM FOR THE R ENTRY DOOR. ALARM AND LIGHT STOPPED BELOW FL190 ON DESCENT. NO ECAM INDICATION OR PRESSURIZATION ISSUES NOTED. FACT 31OCT24 20:47 MEOct 23, 2024 · N733FD · Airbus A310300 · Door Warning SystemSDR FDEA202409191329Fitting · corrodedCORROSION FOUND BETWEEN BUSHES 'D" AND "E" DURING RH RIB 5 INSPECTION COMPLIED WITH FED EX EA 6-571-T0316490 PT2 AND R57240425. MAJOR REPAIR. EA 6-5710- T0316490 WINGS - BASIC WING STRUCTURE - CORROSION REPAIR OF RIB 5 FWD LUG RH. MPN A57240810214.Sep 19, 2024 · N680FE · Airbus A310300 · Wing Main, Frame StructureSDR FDEA202409121332Seat Track · corrodedMAIN DECK SEAT TRACK A POINT GOT CORROSION AT FR15B Y953 REPLACED THE SEAT TRACK WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR, PER GMM 06-2-100. AT FR15A~19, Y953 NOTE: 5.(C), P/N TYPE ERROR, CREATED A NEW SDR NO:24-Sep 12, 2024 · N655FE · Airbus A310300 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202408111331Shear Tie · damagedCOMPLY WITH EO 6-5310-E0330747 D P12 REPAIRED THE FRAME FOOT CRACK AT FR45 RH SIDE AREA 2 COMPLIED WITH EO 6-5310-E0330747 D P12 REPAIRED THE FRAME FOOT CRACK AT FR45 RH SIDE AREA 2, TITLE: FUSELAGE - MAINFRAME - INSPECTION OF LOWER FRAME BASE FITTING BETAug 11, 2024 · N730FD · Airbus A310300 · Fuselage Internal Mounting StructureSDR CA190327021Switch · faulted(CAN) EN ROUTE ECAM YELLOW SERVO JAM. ECAM ACTIONS HAD ALREADY BEEN PERFORMED. YELLOW SERVO CTL SWITCHED OFF. SUSPECT AN INDICATION PROBLEM. CREW IS CHECKING THEIR ETOPS AND FUEL REQUIREMENTS. DUE TO FAULT AND RELATED INOP HYD SYSTEM FLIGHT UNABLE TO CONTINUE Mar 26, 2019 · Airbus A310300 · Elevator Control SystemSDR CA160223002Strut · faulty(CAN) ESTABLISHED ON FINAL FOR LANDING THE CREW SELECTED GEAR DOWN, THEY DID NOT GET A GREEN LIGHT FOR THE NOSE GEAR FROM EITHER SYS, RED LIGHTS ONLY FOR THE NOSE GEAR INDICATING AN UNSAFE GEAR SITUATION. THE CREW COMPLETED THEIR CHECKS IAW THE QRH. AN EMERGFeb 22, 2016 · Airbus A310300 · Nose/Tail Landing Gear Strut/AxleSDR CA160108004Wire · damaged(CAN) WIRES LOCATED IN THE WHEEL WELL NEAR A CANISTER. THE WIRE ROUTING WAS TOO SLACK AND WITH TIME THE LOOSE PROTECTED WIRES GOT WORN OUT.Jan 6, 2016 · Airbus A310300 · Electrical Power System WiringSDR CA151223004Water Heater · sparks(CAN) WATER HEATER WAS PRODUCING SPARKS WHEN F/A DID RESET THE UNIT IN FLIGHT.Dec 22, 2015 · Airbus A310300 · Wash Water SystemSDR CA151203006Valve · failed(CAN) ECAM YELLOW SYS LOW PRESSURE IN FLIGHT. 10 SECONDS AFTER, LOSS OF MOST OF THE YELLOW SYSTEM HYDRAULIC FLUID AND ASSOCIATED PITCH FEEL, SPOILER, YAW DAMPER 2 AFS.Nov 20, 2015 · Airbus A310300 · Landing Gear Brake SystemSDR CA150930003Cdu · cracked(CAN) CDU HOUSING CRACKED DURING TESTING OF THRUST REVERSER. OPERATED OK FOR 1 CYCLE AND THEN CRACKED AND SEPARATED ON CYCLE 2.Sep 25, 2015 · Airbus A310300 · Engine Thrust ReverserSDR CA150520002Duct · ruptured(CAN) DURING WALK AROUND, MAINTENANCE HEARD AN UNUSUAL NOISE COMING FROM NR NR 1 ENGINE. SOUND OF BLEED LEAK, RUSHING AIR. AFTER OPENING THE THRUST REVERSER COWLS, THE TECH FOUND A RUPTURED DUCT ON THE THRUST REVERSER PRESSURE REGULATING AND SHUTOFF VALVE, PMay 19, 2015 · Airbus A310300 · Engine Bleed Air SystemSDR CA150426001Indicator · overheated(CAN) APPROXIMATELY 5 MINUTES AFTER FULL ACFT ELECTRICAL POWER WAS APPLIED, THE RUDDER TRIM INDICATOR BEGAN EMMITING SMOKE AND PRODUCED A HEAVY ELECTRICAL BURNING ODOR.Apr 25, 2015 · Airbus A310300 · Independent InstrumentsSDR CA150318005Wire Harness · burned(CAN) DURING POWER ON OF ACFT, MULTIPLE WIRES BURN ON THE LT FWD AREA OF PANEL 800VU. PRELIMINARY OBSERVATION OF ROOT CAUSE IS WIRE CHAFING ON SHARP EDGE OF PANEL 800VU LH HINGE. IT IS OF INTEREST TO NOTE THAT THESE WIRES ARE STANDARD WIRES FOUND IN THE ESPM,Mar 18, 2015 · Airbus A310300 · Electrical Power System WiringSDR CA140812009Bolt · missing(CAN) A/C HAD INFLIGHT TURNBACK LT MLG DOOR NOT CLOSING. MAINTENANCE FOUND LH MLG UPLOCK (FIN 321212) ROD ASSY (REF A310 IPC 32-36-44-02 ITEM 100) ADRIFT FROM RETAINER BRACKET (REF A310 IPC 32-16-16-05 ITEM 100). THE RETAINER BOLT WAS MISSING. INSPECTION SHOWAug 10, 2014 · Airbus A310300 · Landing Gear Door Retract SectionSDR CA140124007Fairing · ruptured(CAN) DURING WALK AROUND INSPECTION, IT WAS FOUND THAT THE RT VERTICAL STABILIZER TO FUSELAGE FAIRING WAS DAMAGED, REFER IPC 53-19-69, ITEM 250. AFTER INSPECTION IT WAS NOTED THAT THE DAMAGE WAS DUE TO DELAMINATION OF THE PANEL. PANEL REPLACED AND INFORMED.Jan 23, 2014 · Airbus A310300 · Aerodynamic FairingsSDR CA140124006Wire · shorted(CAN) DURING FLIGHT LT INNER FUEL PUMP FAULT MESSAGE TRIGGERED. TROUBLESHOOTONG CARRIED OUT AND THE FOLLOWING FINDING WERE OBSERVED, GREEN HYD PUMP NR 2 WIRING AT SPECIFIED RAMP SUPPORT SHORTED TO GROUND, RESULTING IN 2 OF THE 3 PHASES TO SEVERE AND CAUSING OJan 22, 2014 · Airbus A310300 · Hydraulic Power System WiringSDR CA131219016Pin · cracked(CAN) PIN IS CRACKED. REPORTED TO MFG AND WAITING FOR MFG INSTRUCTIONS.Dec 14, 2013 · Airbus A310300 · Main Landing Gear Attach SectionSDR CA131213008Hinge Pin · cracked(CAN) DURING THE A-CHECK, WHILE PERFORMING LUBRICATION OF THE LT MLG, THE FWD ATTACHMENT PIN WAS FOUND WITH CRACKS AND A PORTION BROKEN OFF. THIS PIN IS PART OF THE GEAR AND IS REPLACED WITH THE GEAR ON OVERHAUL. THE GEAR WAS OVERHAULED IN OCT 2007 AND HAS ADec 12, 2013 · Airbus A310300 · Main Landing Gear Strut/Axle/TruckSDR CA130826003Line · cracked(CAN) DURING FLIGHT THE GREEN HYDRAULIC FLUID NOTICED TO BE DECREASING, FOLLOWED BY ECAM LOW LEVEL WARNING. LANDING MANUALLY EXTENDED FOR LANDING. ACFT HAD TO BE TOWED OFF RUNWAY DUE TO LOSS OF STEERING FROM GREEN HYDRAULIC SYSTEM FLUID LOSS. FOUND NR 2 ENGIAug 24, 2013 · Airbus A310300 · Hydraulic System, MainSDR CA130822012Manifold · leaking(CAN) O-RING FAILURE BETWEEN MANIFOLD ASSY FIN 291112, PN A2901150800000 AND BOSS FITTING MS21902-10. CAUSING ACFT TURN BACK DUE HYDRAULIC LOSS. IPC REF 24-24-03-04 050, O-RING REPLACED ON MANIFOLD ASSY FIN 291112. DEFECT ITEM NR 1100188.Aug 22, 2013 · Airbus A310300 · Hydraulic System, MainSDR CA130610006Eec · malfunctioned(CAN) AT THE TOP OF DESCENT, UPON THRUST REDUCTION TO FLIGHT IDLE, BOTH THRUST LEVERS WENT TO IDLE BUT THE NR 2 ENGINE N1 STAYED AT 70 PERCENT N1. STARTING AROUND 12,000 FT, TAT ABOVE FREEZING, THE N1 STARTED REDUCING TOWARDS IDLE. IT REACHED IDLE AT AROUND 8,Jun 4, 2013 · Airbus A310300 · Fuel Controlling SystemSDR CA130417001Cdu · damaged(CAN) NR 1 ENGINE THRUST REVERSER FAULT ON LANDING. FOUND OTBD REVERSER SLEEVE NOT FULLY STOWED. THRUST REVERSER WAS DEACTIVATED IAW MEL. ON DEPARTURE, THE NR 1 POWER LEVER WOULD NOT MOVE OUT OF IDLE POSITION. CENTER DRIVE UNIT (CDU) FEEDBACK MECHANISM FOUNApr 12, 2013 · Airbus A310300 · Engine ControlsSDR CA130318014Bearing · corroded(CAN) DURING INSPECTION UNABLE TO OPEN RT OVERWING EMERGENCY EXIT DOOR, FROM THE INSIDE NOR FROM THE OUTSIDE. DOOR HAD TO BE PRYED UP IN ORDER TO OPEN. FOUND SLIDING BEARING/BUSHING CORRODED ON LIFTING MECHANISM SHAFT, ITEM 220 OF IPC 52-23-11, FIG 14.Mar 11, 2013 · Airbus A310300 · Emergency ExitsSDR CA130318011Skin · cracked(CAN) DURING VISUAL INSPECTION, FOUND AFT CARGO DOOR ACTUATOR FITTING AT FRAME 61A AND INNER SKIN CRACKED BETWEEN LONGERON 1 AND 1A.Mar 11, 2013 · Airbus A310300 · Cargo/Baggage DoorsSDR CA130204003Actuator · failed(CAN) ON APPROACH THE CREW OBSERVED AN UNSAFE INDICATION OF THE NOSE GEAR UPON SELECTING GEAR DOWN FOR LANDING. THE CREW DECLARED AN EMERGENCY AND FOLLOWED THE APPLICABLE ABNORMAL CHECKLIST AND PERFORMED A GRAVITY GEAR EXTENSION WHICH RESULTED IN A SAFE GEAR IFeb 2, 2013 · Airbus A310300 · Landing Gear Door ActuatorSDR CA121203005Control Panel · overheated(CAN) IN CRUISE AT FL 370, VHF 2 CONTROL PANEL GREEN LIGHT WAS INTERMITTENT, THEN BECAME EXTINGUISHED. CREW NOTICED AN ELECTRICAL SPARK FOLLOWED IMMEDIATELY BY A LIGHT WHITE SMOKE COMING FROM UNIT AT THE ACTIVE GREEN LIGHT. THE CREW PULLED THE ASSOCIATED CIRNov 30, 2012 · Airbus A310300 · VHF Communications SystemSDR CA121127002Bolt · worn(CAN) ON APPROACH, THE SLATS EXTENDED NORMALLY BUT NO FURTHER MOVEMENT OF THE FLAP LEVER WAS POSSIBLE AFTERWARDS. THE SLAT/FLAP LEVER WAS STUCK IN THE UP POSITION PREVENTING THE MOVEMENT THROUGH THE POSITION DETENTS. THE CREW ADVISED ATC THAT A HIGHER APPROANov 23, 2012 · Airbus A310300 · Trailing Edge Flap Control SystemSDR CA120914010Duct · fractured(CAN) ACFT ARRIVED WITH 2 SNAGS RELATED TO AIR CONDITIONNING. CABIN TEMP HARD TO COOL DOWN AND LOW FLOW PLUS BOTH PACKS SURGING ON THE GROUND. REF W/O 1089584. DURING TROUBLESHOOTING, FOUND NR 1 PACK OUTLET DUCT RUPTURED. MISSING AREA APPROX 6" X 3". DUCT WSep 10, 2012 · Airbus A310300 · Air Distribution SystemSDR CA120224005Control Panel · smoke(CAN) FOUND SMOKE EMANATING FROM RUDDER AND AILERON TRIM CONTROL PANEL DURING COCKPIT PRE-DISPATCH CHECK. PART WAS REPLACED.Feb 7, 2012 · Airbus A310300 · Rudder Tab Control SystemSDR CA111026013Oven · burned(CAN) FWD GALLEY NR 2 OVEN BURNING ODOR. MEL 25-20, CAT D RAISED BY KLM IN AMS. UPON INVESTIGATION, FOUND FAN SEIZED. REPLACED OVEN IAW AMM 25-34-00. OPS CHECKED SERVICEABLE.Oct 25, 2011 · Airbus A310300 · Buffet/GalleysSDR 2011F00121Blade · brokenHPT STAGE 1 BLADE FOUND BROKEN AND MISSING DURING ROUTINE BSI, ON FOLLOWING CF6-80C2A8 ENGINES SN 659611, 659399, 659526, 659392, 659408, 659612, 659414. SECONDARY DAMAGE WAS ALSO OBSERVED ON NUMBER OF BLADES. ALL THE BLADES WAS NEW WHEN INSTALLED.Mar 6, 2010 · Airbus A310300 · Turbine SectionSDR CA091203003Duct · cracked(CAN) PIREP DEFECT 1037394 - FUEL MIGRATING FROM LT INNER TANK TO CTR TANK. MX FOUND THE APU BOOST PUMP CANNISTER DELIVERY DUCT CRACKED. REPLACED PER MM 49-32-14 AND SERVICEABLE. (TC NR 20091203003)Dec 2, 2009 · Airbus A310300 · APU Engine Fuel and ControlSDR CA090522001Hose · leaking(CAN) AFTER LANDING, DURING TAXI, THE GREEN HYD FLUID HAS BEEN LOST. THE ACFT HAS BEEN TOWED TO THE GATE. HOSE HAS BEEN REPLACED ON LT MLG DRAG BRACE. HYD SYS HAS BEEN BLED AND ACFT RETURNED TO SERVICE.May 16, 2009 · Airbus A310300 · Hydraulic System, MainSDR CA090514004Display · smoke(CAN) CREW DETECTED SMOKE IN FLIGHT DECK. DETERMINED IT WAS COMING FROM THE TCAS DISPLAY UNIT. ODOR DISSIPATED WHEN THE CIRCUIT BREAKER FOR TCAS MONITOR WAS PULLED. MONITOR LEFT DE-ACTIVATED UNDER MEL 34-35 WHILE PART ON ORDER.May 7, 2009 · Airbus A310300 · Central WarningSDR CA080801004Access Panel · missing(CAN) ON ARRIVAL, LEADING EDGE SLAT TRACK ACCESS PANEL 512HB FOUND MISSING. ADJACENT PANEL 512JB ALSO FOUND DAMAGED. LOST IN FLIGHT. PANEL 512HB REPLACED AND PANEL 512JB REPAIRED IAW SRM.Jul 23, 2008 · Airbus A310300 · Leading Edge DevicesSDR CA080728005Circuit Breaker · burned(CAN) DURING TROUBLESHOOTING OF THE INOPERATIVE LT OUTER TANK FUEL PUMP (DEACTIVATED IAW MEL) THE CIRCUIT BREAKER 3QA WAS FOUND BURNED, BODY CRACKED AND ONE LEG MISSING. CIRCUIT BREAKER WAS REPLACED AND SYS TESTED SERVICEABLE. A DETAILED VISUAL INSPECTION CAMPJul 21, 2008 · Airbus A310300 · Fuel System WiringSDR CA080617004Shaft · sheared(CAN) ACFT ARRIVED AT GATE WITH CAPTAINS’ WINDSHIELD WIPER ASSEMBLY MISSING. FURTHER INVESTIGATION FOUND THAT CONVERTER SPLINED SHAFT HAD SHEARED OFF CAUSING THE WIPER ASSY TO DEPART ACFT WHILE TAXIING IN FROM LANDING TO APRON. WIPER ASSY WAS FOUND IN TAXIWAY.Jun 16, 2008 · Airbus A310300 · Windshield/Door Rain/Ice RemovalSDR CA080409003Outflow Valve · malfunctionedAFTER 30 MIN IN CRUISE, CAB PRESSURE REG NR 2 FAULT, FOLLOWED BY CAB PRESSURE REG NR 1 FAULT. UNABLE TO CONTROL IN MANUAL. EMERGENCY DESCENT AND QAR PROCEDURES FOLLOWED. PAX MASK SYSTEM ACTIVATED IN AUTO. FLIGHT RETURNED TO STATION AT FL 10,000 FT. ACFT WApr 7, 2008 · Airbus A310300 · Pressure Regulator/Outflow ValveSDR CA080314016Switch · contaminated(CAN) DURING CLIMB, ECAM WARNING "FLAP KRUEGER NOT RETRACTED LIGHT" CAME ON. FLIGHT RETURNED TO THE STATION. SFCC INDICATED FAULT COMING FROM THE LT KRUEGER RETRACT SWITCH. MAINT FOUND THE SWITCH BACK SHELL CONTAMINATED WITH WATER. CONNECTOR AND SWITCH CLEANEMar 9, 2008 · Airbus A310300 · Trailing Flap Position Indicating SystemSDR CA071127002Coffeemaker · sparks(CAN) DURING FLIGHT, THE F/A REPORTED THE FWD COFFEE MAKER/WATER BOILER OVERHEATING AND NOTICED SOME SPARK COMING FROM THE UNIT. THE UNIT WAS DEACTIVATED. THE UNIT WAS REPLACED BY MAINTENANCE AND ROUTED TO THE REPAIR SHOP FOR INVESTIGATION. (TC NR 20071127002)Nov 21, 2007 · Airbus A310300 · Buffet/GalleysSDR CA070731001Seal · leaking(CAN) DURING TAXI-IN AT THE GATE, A LARGE FUEL LEAKAGE WAS OBSERVED COMING FROM THE HMU FUEL DRAIN BELOW NR 2 ENGINE. ENGINE WAS SHUTDOWN, BUT LEAKAGE CONTINUED. NR 2 ENGINE FIRE HANDLE WAS PULLED AND LEAKAGE STOPPED. FOUND LEAKAGE WAS FOM THE MEC SHAFT SEAJul 27, 2007 · Airbus A310300 · Fuel Controlling SystemSDR CA070313003Power Supply · overheated(CAN) DURING CRUISE, FLIGHT CREW OBSERVED WHAT APPEARED TO BE WHITE SMOKE EMANATING FROM READING LIGHT (PSU) PANEL ASSEMBLY ABOVE SEAT 30 AB. CREW SWITCHED OFF READING LIGHTS AND SMOKE STOPPED. ON ARRIVAL TO THE STATION, MAINTENANCE FOUND ONE TRANSFORMER PRINTMar 12, 2007 · Airbus A310300 · Passenger Compartment LightingSDR CA061227001Wire · burned(CAN) ON ARRIVAL, FLIGHT CREW REPORTED TCAS AND RA FAILURE FLAGS ON BOTH IVSI’S DURING FLIGHT. WHILE TROUBLESHOOTING TCAS FAILURE, SEVERAL BURNED WIRES WERE DISCOVERED IN A BUNDLE LOCATED BEHIND THE ATC1 AND TCA RACK (500VU). THE WIRE SUSPECTED OF CAUSING THE Dec 19, 2006 · Airbus A310300 · Navigation System WiringSDR CA061011005Access Panel · missing(CAN) UPON AIRCRAFT ARRIVAL, DURING WALK AROUND INSPECTION, FOUND THE FWD CARGO DOOR LOWER FWD ACCESS PANEL, FIN811AR, MISSING. MOUNTING HARDWARE, FASTENERS AND LANYARDS WERE STILL ATTACHED TO THE CARGO DOOR. DOOR WAS INSPECTED AND NO FURTHER DAMAGE WAS NOTICESep 29, 2006 · Airbus A310300 · Fuselage Structure (General)SDR CA060728005Control Panel · smoke(CAN) DURING FLIGHT, LIGHT SMOKE CAME FROM THE NR 1 VHF CONTROL PANEL. THE CIRCUIT BREAKER WAS PULLED AND THE FLIGHT PROCEEDED WITHOUT ANY FURTHER PROBLEM. THE PANEL WAS REPLACED AT THE ARRIVAL STATION AND WAS SYSTEM CHECKED SERVICEABLE. PANEL WAS ROUTED TO THJul 21, 2006 · Airbus A310300 · VHF Communications SystemSDR CA060314001Cover · missingTHE AIRCRAFT ARRIVED FROM FLIGHT WITH ONE OF THE FORWARD CARGO DOOR ACCESS PANEL LATCH COVER MISSING. DURING INVESTIGATION FOUND THE PANEL ATTACHMENT AREAS HAD ELONGATED, WHICH ALLOWED THE ATTACHMENT SCREWS TO PASS THROUGH THE ACCESS PANEL. NEW PANEL ASSY WAMar 9, 2006 · Airbus A310300 · Cargo/Baggage DoorsSDR CA060228003Pickup · contaminatedAIRCRAFT LANDED WITH FULL SLATS AND NO FLAPS. UNABLE TO EXTEND FLAPS ON LANDING. SYSTEM TORQUE LIMITERS AND SCREW JACKS LIMITER INSPECTED AND NO FAULT FOUND. DURING TROUBLESHOOTING, THE LT AND RT POWER PICK UP UNITS WERE FOUND CONTAMINATED WITH SKYDROL AND Feb 26, 2006 · Airbus A310300 · Trailing Edge Flap Control SystemSDR CA050809001Switch · shorted(CAN) DURING STATION TURN AROUND, MAINTENANCE NOTICED SMALL SPARK COMING OUT OF THE ANTI-COLLISION CONTROL SWITCH (2LV). CIRCUIT BREAKER (5LV) OF THE LOWER BEACON WAS POPPED. FOUND THE ANTI-COLLISION SWITCH CONTACTS 1B AND 2B SHORTED TOGETHER, REGARDLESS OF Aug 4, 2005 · Airbus A310300 · Exterior LightingSDR CA050722003Circuit Breaker · burnedFLIGHT CREW REPORTED, RT OUTER TANK FUEL PUMP NR 1, LOW PRESSURE FAULT. DURING TROUBLESHOOTING, FOUND CIRCUIT BREAKER FIN 4QA TRIPPED AND EMITTING BURNT SMELL. CIRCUIT BREAKER WAS REPLACED AND SYSTEM OPS CHECKED SERVICEABLE.Jul 16, 2005 · Airbus A310300 · Engine Fuel System WiringSDR CA050707001Wheel · crackedDURING TRANSIT CHECK ONE OF THE MAIN WHEEL TIRE WAS FOUND WITH LOW PRESSURE. MAIN WHEEL ASSEMBLY WAS REMOVED AND SENT TO THE REPAIR SHOP FOR INVESTIGATION. DURING INSPECTION, THE OUTBOARD WHEEL HALVE WAS FOUND CRACKED APPROX ONE INCH LONG ON LOWER WHEEL WEB Jun 8, 2005 · Airbus A310300 · Wheel/Ski/Float
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