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
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Sukhoi Su-80 (Wikipedia)
Of Make
Source Sukhoi Su-80 (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Sukhoi Su-80 (Wikipedia)LeadQuote, Lead
is a Russian twin-turboprop, twin-boom STOL transport aircraft.
Originated In
Also in Geography Atlas: where this subject originated.
Source Sukhoi Su-80 (Wikipedia)LeadQuote, 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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