The SP-30 ultrashort takeoff and landing aircraft is a two-seat, very light aircraft, which is a sub-winged high-plane of the normal scheme with a tailplane and three-axis non-retractable landing gear with a steerable nose wheel.
The SP-30 ultrashort take-off and landing aircraft can be used for initial training in piloting techniques, and its additional equipment allows the aircraft to be used for aviation-chemical, patrol and forest protection operations in off-airfield conditions. The airframe is made of duralumin sheets of D16T alloy.
Riveted construction with a working skin provides the specified strength and rigidity at low weight of the aircraft.
The main technical characteristics of the aircraft ultra-short takeoff and landing SP-30:
Length, m - 6.28; Height, m - 3.13; Wingspan, m - 9.4.
Engine type - four-stroke, four-cylinder engine with opposition arrangement of cylinders, power 73.5 kW (100 hp).
Maximum take-off weight, kg - 495.
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