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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)

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[edit] 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

[edit] Performance

• Maximum speed: 870 km/h (470 kt, 540 mph)
• Range: 11,500 km (6,200 nm, 7,200 mi)

[edit] References

• Aircraft facts (translated) (original page)

[edit] Related content

[edit] Comparable aircraft

• Airbus A330
• Boeing 767
• Ilyushin Il-96
• Tupolev Tu-304

[edit] Designation sequence

• An-174 - An-180 - An-204 - An-218 - An-225 - An-400

[edit] Related lists

• List of airliners
• List of civil aircraft

[edit] See also

Template:Antonov aircraft

ja:An-218 (航空機)

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