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Sukhoi Su-80

General Aviation and Light Aircraft

The Sukhoi Su-80, formerly the Sukhoi S-80, is a Russian twin-turboprop, twin-boom STOL transport aircraft, meant to replace the An-24/26, An-28 and Yak-40 and to compete with the Antonov An-38. Lack of funds delayed the programme from the late 1990s, and the prototype first flew on 4 September 2001 with Igor Wotinzew at the controls. In early 2006 the type entered production at the KnAAPO factory in Komsomolsk-on-Amur. The layout, with three lift-generating surfaces, resembles the Scaled Composites ATTT and the Rockwell OV-10, and the fuselage has space for 30 passengers and a beaver-tail cargo ramp at the rear. Several airlines and air forces signed preliminary agreements or expressed interest, but no aircraft performed active service.

Facts
Year
2001 1
Engine Class
Turboprop 1
Maximum Mass (kg)
13,500 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Sukhoi Su-80 (Wikipedia)

Of Make

Source Sukhoi Su-80 (Wikipedia)
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Source Sukhoi Su-80 (Wikipedia)Lead
Quote, Lead
is a Russian twin-turboprop, twin-boom STOL transport aircraft.

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Source Sukhoi Su-80 (Wikipedia)Lead
Quote, Lead
is a Russian twin-turboprop, twin-boom STOL transport aircraft.
Sources
1. Sukhoi Su-80 (Wikipedia)
  • Design and development
    On 4 September 2001, Igor Wotinzew started with the prototype, 82911, on his first flight.
  • Specifications
    Powerplant: 2 × General Electric CT7-9B turboprop engines, 1,305 kW (1,750 hp) each
  • Lead
    is a Russian twin-turboprop, twin-boom STOL transport aircraft.
  • Specifications, maximum takeoff weight
    Max takeoff weight: 13,500 kg (29,762 lb)
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