Antonov An-218

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Antonov An-218
Ан-218.jpg
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, but was never put into production.

Specifications (An-218-100, as designed)[edit]

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)

See also[edit]

Aircraft of comparable role, configuration and era

External links[edit]