Suchoi / Sukhoi Su-26

Aerobatic Aircraft

Suchoi / Suchoj / Sukhoi Su-26M2, G-SIID, c/n 01-04 © John Allan
Photo ©: John Allan (Photos at
The Sukhoi Su-26 is a single-engine single-seat aerobatic aircraft developed by the Soviet Design Bureau Sukhoi, today Sukhoi JSC (Russia).
Propulsion1 Radial Engine
Engine ModelVedeneyev M-14P
Engine Power268 kW359 hp
max. Cruise Speed309 km/h167 kts
  192 mph
max. Speed (vne)450 km/h243 kts
  280 mph
Service Ceiling4.000 m13.123 ft
Range895 km483 NM
556 mi.
Empty Weight700 kg1.543 lbs
max. Takeoff Weight962 kg2.121 lbs
Wing Span7,80 m25 ft 7 in
Wing Area11,8 m127 ft
Length6,83 m22 ft 5 in
Height2,89 m9 ft 6 in
First Flight30.06.1984
Production Statusout of production
Total Production>50
Data for (Version)Sukhoi / Suchoi Su-26M
VariantsSu-26M, Su-26MKh, Su-26M2