Antonov An-218

Antonov An-218

Role	Widebody airliner
Manufacturer	Antonov
Status	Project is abandoned
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.
The first flight was initially scheduled for 1994. Due to the severe economical conditions the project was abandoned. Only a full-scale wooden replica of An-218 was built, but eventually it was taken apart.^[1]

Specifications (An-218-100, as designed)

General characteristics

Crew: 2 (flight deck)
Capacity: 300/350/400 passengers
Length: 59.79 m (196 ft 2 in)
Wingspan: 50 m (164 ft 1 in)
Height: 15.7 m (51 ft 6 in)
Wing area: 270 m² (2,900 sq ft)
Empty weight: 90,000 kg (198,416 lb)
Max takeoff weight: 170,000 kg (374,786 lb)
Powerplant: 2 × Progress D-18T1 high bypass turbofan, 250 kN (57,000 lbf) thrust each

Performance

Maximum speed: 870 km/h (541 mph; 470 kn)
Range: 11,500 km (7,146 mi; 6,210 nmi)

References

↑ Sole few photos

External links

Wikimedia Commons has media related to Antonov An-218.

Antonov aircraft

Airliners	An-10 An-24 An-28 An-74 An-140 An-148 An-158 An-174 An-180 An-218

Transports	OKA-38 An-2 An-3 An-4 An-8 An-12 An-14 An-22 An-26 An-32 An-38 An-50 An-70 An-72 An-74 An-112 An-124 An-132 An-178 An-225

Reconnaissance and surveillance	An-6 An-30 An-71 An-88

Experimental	An-13 SKV An-188

Gliders	A-1 A-2 A-7 A-9 A-10 A-11 A-13 A-15 A-40

Microlights	T-2M

This article is issued from Wikipedia - version of the 10/16/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.

Antonov An-218

Specifications (An-218-100, as designed)

See also

References

External links