Soviet Ultralight and Homebuilt Aircraft homebuilt aircraft assembly


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Type 2-seat conventional low wing aerobatic monoplane
Engine 140 hp
Propeller 2-blade metal 6,16 ft dia
Landing gear trigear
Length 21 ft
Wing Span 28,3 ft
Wing Area 122,2 sq.ft
Wing Aspect Ratio 6,6
Airfoil NACA 23015
Vertical Tail Area 12,3 sq.ft
Rudder Area 6,2 sq.ft
Horizontal Tail Area 22,2 sq.ft
Elevator Area 10 sq.ft
Empty Weight 1330 lb
Gross Weight 1845 lb
Wing Loading 15,1 lb / sq.ft
Power Loading 13,1 lb / hp
Fuel Capacity 13 gal
Top Speed 158 mph
Stall Speed 68 mph
Takeoff Roll n.a.
Rate of Climb n.a.
Bldg. Materials Wing: metal
Tail: metal
Fuselage: metal




3 view drawing




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