Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.
[1] The Sova was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations.
It features a paraglider-style wing, single-place accommodation and a single 16 hp (12 kW) Sova engine in pusher configuration with a 2.4:1 ratio reduction drive and a 123 cm (48 in) diameter two-bladed wooden propeller.
[1] As is the case with all paramotors, take-off and landing is accomplished by foot.
Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.