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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.
[edit] Specifications (An-218-100, as designed)
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
[edit] References
[edit] See also
Comparable aircraft
An-400
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