Top speed 450 km/h Range 1,100 km Weight 700 kg Engine type Vedeneyev M14P | Length 6.83 m Wingspan 7.8 m Cruise speed 330 km/h | |
![]() | ||
The Sukhoi Su-31 is a Russian single-engined aerobatic aircraft designed by Sukhoi as a lighter and more powerful version of the Sukhoi Su-29.
Contents

Design and development

The design of the aircraft started in 1991 as a single-seat development of the earlier Sukhoi Su-29 with a more powerful Vedeneyev M-14PF engine and new landing gear. The low-wing cantilever monoplane first flew in June 1992 as the Su-29T and the first production aircraft flying in 1994.
Variants

Specifications
Data from Su-26, 29, 31 Specifications
General characteristics

Performance

References
Sukhoi Su-31 Wikipedia(Text) CC BY-SA