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Start | Airbus | A310-200



Airbus A310-200


General information


ManufacturerAirbus
ModelA310-200
ModificationA310-200
CountryFrance
Years1982
TypePassenger aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan43.90 m
Length46.66 m
Height15.81 m
Wing area219.00 m2
Zero fuel weight80600 kg
Empty weight-
Maximum takeoff weight142000 kg
Normal takeoff weight-
Flight duration-
Engine2 General Electric CF6-80C2A8 (Pratt Whitney PW4156)
Power-
Thrust2 x 25420 (26780) kN
Maximum speed940 km/h
Cruising speed895 km/h
Rate of climb-
Practical range4070-6670 km
Service ceiling11300 m
Hovering ceiling-
Crew2
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