Soviet Ultralight and Homebuilt Aircraft homebuilt aircraft assembly


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Spilo



Type single-seat ultralight
Engine 35 hp
Propeller 2-blade wooden fixed 5 ft dia
Landing gear trigear
Length 17,6 ft
Wing Span 28,6 ft
Wing Area 122,2 sq.ft
Wing Aspect Ratio 6,7
Airfoil n.a.
Vertical Tail Area 18,9 sq.ft
Rudder Area 4,55 sq.ft
Horizontal Tail Area 23,3 sq.ft
Elevator Area 11,1 sq.ft
Empty Weight 389 lb
Gross Weight 589 lb
Wing Loading 4,82 lb / sq.ft
Power Loading 16,8 lb / hp
Fuel Capacity 5 gal
Top Speed 62 mph
Stall Speed 37 mph
Takeoff Roll 167 ft
Rate of Climb 600 fpm
Bldg. Materials Wing: tubing, fabric
Tail: tubing, fabric
Fuselage: tubing




3 view drawing




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