Antonov An-218

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)

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 D-18T1 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)

See also

Aircraft of comparable role, configuration and era

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

External links

• Aircraft facts (translated) (original page)
• An-218 airliner by Antonov ANTK