Airbus A310-304

Aircraft Data

The Airbus A310 is a twin engine, wide body medium/long range airliner, Derived from the A300, with shortened fuselage and new wings and flightdeck, Many have been converted to freighters or military tankers. Production ceased in 2007.

The -300 is the longer range development of the basic series 200, with extra fuel tankage in the tailplane. The -300 has winglets and is cleared for transoceanic flights to ETOPS standards .

Summary data for Airbus A310 300
Country of originFirst flightNo. builtNo. in serviceCrewPassengers
France19851701502210 - 280

Power

2 x CFM CFM56 (18500 - 34000 lbf), General Electric CF6 (41500 - 69800 lbf), Pratt & Whitney JT9D (45800 - 56000 lbf) or Pratt & Whitney PW4000 (52000 - 99040 lbf) turbofan engines.

Typical choices would be the CFM56-80C2A8 at 59000lb thrust, or the PW4156 at 56000lb.


Dimensions

Dimensions for Airbus A310 300
Length153 ft. 1 in.
Wing Span144 ft. 0 in.
Height51 ft. 0 in.
Empty Weight179,025 lbs.
Max Weight361,560 lbs. (Max take-off weight option)

Performance

Performance of Airbus A310 300
Max Speed484 kts
Cruise Speed430 kts
Ceiling40,000 ft.
Normal Range4,310nm
Max Range5,170nm (Range for high gross weight CFM56 version)

Updated 15th March 2009

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Airbus A310-304

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Date Taken:
9th July 2013
Image ID:
180339

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