
Airbus A310-304
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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 .
Country of origin | First flight | No. built | No. in service | Crew | Passengers |
---|---|---|---|---|---|
France | 1985 | 170 | 150 | 2 | 210 - 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
Length | 153 ft. 1 in. |
---|---|
Wing Span | 144 ft. 0 in. |
Height | 51 ft. 0 in. |
Empty Weight | 179,025 lbs. |
Max Weight | 361,560 lbs. (Max take-off weight option) |
Performance
Max Speed | 484 kts |
---|---|
Cruise Speed | 430 kts |
Ceiling | 40,000 ft. |
Normal Range | 4,310nm |
Max Range | 5,170nm (Range for high gross weight CFM56 version) |
Updated 15th March 2009
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- Airbus A310
- CFM CFM56
- General Electric CF6
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- Pratt & Whitney JT9D
- Pratt & Whitney PW4000
- turbofan
- twin engine
- twin jet
- wide body
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