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Aist-123



Type 2-seat conventional low wing monoplane
Engine 140 hp
Propeller 2-blade metal 6,1 ft dia
Landing gear trigear
Length 23,6 ft
Wing Span 36 ft
Wing Area 185,5 sq.ft
Wing Aspect Ratio 7
Airfoil Clark-YH
Vertical Tail Area 15,1 sq.ft
Rudder Area n.a.
Horizontal Tail Area 27,6 sq.ft
Elevator Area n.a.
Empty Weight 1524 lb
Gross Weight 2037 lb
Wing Loading 10,98 lb / sq.ft
Power Loading 14,5 lb / hp
Fuel Capacity n.a.
Top Speed 143 mph
Stall Speed 50 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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