SU-26
Training aircraft

	Specification:
	Year deployed Wing span, m Length, m Height, m Wings area, m2 Weight, kg - empty aircraft - maximum take-off Fuel, l - Internal - AFT Engine Power, hp Maximum speed, km/h - dive - level Range, km Rate of climb, m/min Service ceiling, m Maximum overload Crew	- 1985 - 7.80 - 6.83 - 2.78 - 11.83 - 680 - 835 - 60 - 140 - 1 PE M-14P - 1 У 360 - 450 - 310 - 800 - 1080 - 4000 - 12 - 1