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The Sukhoi 26

The Sukhoi Su-26 is a single-seat aerobatic aircraft from the former Soviet Union. It is powered by a single 400 HP reciprocating radial engine. The Su-26 has mid-mounted straight wings and fixed landing gear. The main gear is mounted on a solid titanium arc. The Sukhoi Su-26 made its first flight in June 1984, the original four having a two-bladed prop. Production switched to the Su-26M, with refined tail surfaces and a 3-bladed propeller. Further refinements were made that resulted in the model winning both the men's and women's team competitions at the 1986 World aerobatics championships. Experts consider the Su-26 one of the best aerobatic aircraft in the world.

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DESCRIPTION
Length 23 ft 11 in
Height 9 ft 6 in
Wing span 26 ft 11 in
Wing area 127.0 sq ft
Construction Carbon fiber, steel, titanium
ENGINE
Type M14-PF, 9-cylinder 4-stroke, gasoline, air-cooled
Horse power 400 HP
Propeller MTV-9-260 3-blade composite
Fuel Gasoline 100LL
WEIGHTS
Empty Weight 1540 lbs
Maximum aerobatic weight 1785 lbs
Maximum take off weight 2116 lbs
PERFORMANCE DATA
Take-off run 410 ft.
Take-off over 50 ft obstacle 918 ft
Rate of climb 3453 ft / min
Cruise 137 mph
Roll rate 400 / sec
Load Factor +10g / -10g
Vne 280 mph
Service ceiling 12,120 ft
Landing distance over 50 ft obstacle 1247 ft
Touchdown speed 77 mph
Landing roll 918 ft
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