Airbus A310-304 Iran Air EP-IBL
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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
Typical choices would be the CFM56-80C2A8 at 59000lb thrust, or the PW4156 at 56000lb.
| Engine Count | 2 | ||||
| Engine Variations | |||||
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* 3 main variants available, with 94 inch, 100 inch and 112 inch fans, that deliver increasing thrusts. Many sub-variants available within these ranges.
Dimensions
| Length | 46.66 m. 153 ft. 1 in. |
| Wing Span | 43.89 m. 144 ft. 0 in. |
| Height | 15.54 m. 51 ft. 0 in. |
| Empty Weight | 81277 kg. 179025 lbs. |
| Max Weight |
164148 kg.
361560 lbs.
Max take-off weight option |
Performance
| Max Speed | 779 kph 484 mph |
| Cruise Speed | 692 kph 430 mph |
| Ceiling | 12192 m. 40000 ft. |
| Normal Range | 7982 4310 nm km. |
| Max Range |
9575
5170
nm
km.
Range for high gross weight CFM56 version |
Display data using: Metric Imperial
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