The Sukhoi Su-26 is a single-seat aerobatic aircraft from the former Soviet Union, powered by a single radial piston engine. It has mid-mounted straight wings and fixed landing gear, with the main legs mounted on a solid titanium arc. The type made its first flight in June 1984 with a two-bladed propeller, and production then switched to the Su-26M, with refined tail surfaces and a German-made three-blade composite propeller. It won both the men's and women's team prizes at the 1986 World Aerobatics Championships, and the Su-26M3 with a new 320 kilowatt M9F engine dominated the 2003 and 2005 world championships and the 2004 European championships. Its instruments are fully metric apart from the altimeter.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Sukhoi Su-26 (Wikipedia)
Of Make
Source Sukhoi Su-26 (Wikipedia)
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Manufactured By
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Source Sukhoi Su-26 (Wikipedia)Lead, body styleQuote, Lead, body style
is a single-seater aerobatic aircraft from the former Soviet Union, powered by a single radial reciprocating engine.
Originated In
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Source Sukhoi Su-26 (Wikipedia)Lead, body styleQuote, Lead, body style
is a single-seater aerobatic aircraft from the former Soviet Union, powered by a single radial reciprocating engine.
Sources
1. Sukhoi Su-26 (Wikipedia)
Lead
The Su-26 made its first flight in June 1984
Specifications
Powerplant: 1 × Vedeneyev M14P 9-cylinder air-cooled radial piston engine, 270 kW (360 hp)
Lead, body style
is a single-seater aerobatic aircraft from the former Soviet Union, powered by a single radial reciprocating engine.
Specifications, maximum speed
Maximum speed: 450 km/h (280 mph, 240 kn)
Specifications, empty weight
Empty weight: 700 kg (1,543 lb)
Specifications, maximum takeoff weight
Max takeoff weight: 962 kg (2,121 lb)
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