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Antonov An-218
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| Antonov An-218 | |
|---|---|
| Type | Widebody airliner |
| Manufacturer | Antonov |
| Status | Cancelled |
| Number built | 0 |
The Antonov An-218 was a proposal by the Antonov Design Bureau for a widebody commercial airliner. A twin-engined design, it was intended to carry approximately 350 passengers, but was never put into production.
Specifications (An-218-100, as designed)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: 2
- Capacity: 300/350/400 passengers (depending on chair spacing)
- Length: 59.79 m (196 ft 1 in)
- Wingspan: 50.0 m (164 ft)
- Height: 15.7 m (51 ft 6 in)
- Wing area: 270 m² (2,900 ft²)
- Empty weight: 90,000-91,000 kg (20,000 lb)
- Max takeoff weight: 170,000 kg (370,000 lb)
- Powerplant: 2× Progress D18T1 turbofans, 255 kN (57,000 lbf) each
Performance
- Maximum speed: 870 km/h (470 kt, 540 mph)
- Range: 11,500 km (6,200 nm, 7,200 mi)
References
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See also
Template:Antonov aircraft
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de:Antonow An-218 ja:An-218 (航空機)
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