Antonov An-180

From Wikipedia, the free encyclopedia
Jump to: navigation, search
Antonov An-180
Role Wide-body propfan airliner
Manufacturer Antonov
Status Cancelled
Number built None

The Antonov An-180 was a Ukrainian design for a twin-aisle medium-range propfan airliner. Although the design was completed by the Antonov Design Bureau in 1994, the type was not built.[1]


The An-180 was a conventionally designed low-wing cantilever monoplane with a conventional tail unit. The unusual feature was the mounting of a Ivenchko Progress D-27 propfan mounted at the end of each tailplane.[1] Each propfan was to have a coaxial contra-rotating tractor propeller, and the An-180 was also designed with a retractable landing gear with twin nosewheels, and tandem pairs of mainwheels.[1]

It was planned to have a number of variants with seating starting at 150–156 passengers, to a larger variant for 200 passengers, and it was also planned to build a combination passenger/freight and an all-freight variant.[1]


Data from Brassey's World Aircraft & Systems Directory[1]

General characteristics

  • Crew: two or three
  • Capacity: 163
  • Length: 40.9 m (134 ft 2 in)
  • Wingspan: 35.83 m (117 ft 7 in)
  • Height: 11.148 m (36 ft 7 in)
  • Max takeoff weight: 67,500 kg (148,812 lb)
  • Powerplant: 2 × Ivenchko Progress D-27 propfan, 10,305 kW (13,819 hp) each at take off


  • Cruise speed: 800 km/h (497 mph; 432 kn)
  • Range: 3,300 km (2,051 mi; 1,782 nmi) with full payload
  • Service ceiling: 10,100 m (33,100 ft) cruise



  1. ^ a b c d e Taylor 1996, pp. 255–256.


  • Taylor, Michael J. H. Brassey's World Aircraft & Systems Directory. London: Brassey's, 1996. ISBN 1-85753-198-1.

External links[edit]