Paraavis Sova

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. The fuel tank capacity is 8 litres (1.8 imp gal; 2.1 US gal).^[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.^[1]

Data from Bertrand^[1]

General characteristics

• Crew: one
• Empty weight: 27 kg (60 lb)
• Fuel capacity: 8 litres (1.8 imp gal; 2.1 US gal)
• Powerplant: 1 × Sova single cylinder, two-stroke, air-cooled aircraft engine, with a 2.4:1 reduction drive, 12 kW (16 hp)
• Propellers: 2-bladed wooden, fixed pitch, 1.23 m (4 ft 0 in) diameter