RU-8 SEMINOLE
Reconnaissance aircraft

	Specification:
	Year deployed Wing span, m Length, m Height, m Wings area, m2 Weight, kg - empty aircraft - maximum take-off Internal fuel, l Engine Power, hp Maximum speed, km/h Cruising speed, km/h Range, km Service ceiling, m Crew	- 1959 - 13.80 - 9.61 - 3.45 - 25.74 - 1860 - 2858 - 507+174 - 2 PE  Textron Lycoming GO-480-G2F6 - 2 У 295 - 345 - 327 - 2655 - 6950 - 1 + 2-3