TheBailey Solo is a Britishparamotor that was designed and produced byBailey Aviation ofBassingbourn,Royston forpowered paragliding. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.^[1]

The Solo was designed to comply with the USFAR 103 Ultralight Vehicles rules as well as European regulations. It features aparaglider-style wing, single-place accommodation and a single 14 hp (10 kW)Solo 210 engine inpusher configuration with areduction drive and a 110 cm (43 in) diameter three-bladed compositeGermanHelix-Carbon propeller. The fuel tank capacity is 10 litres (2.2 imp gal; 2.6 US gal). The aircraft backpack chassis is built so that it can be quickly disassembled into five parts for ground transport and storage.^[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: 22 kg (49 lb)
• Fuel capacity: 10 litres (2.2 imp gal; 2.6 US gal)
• Powerplant: 1 ×Solo 210 single cylinder,two-stroke, air-cooledaircraft engine, with areduction drive, 10 kW (14 hp)
• Propellers: 3-bladedHelix-Carbon, 1.10 m (3 ft 7 in) diameter

• Bailey aircraft
• 2000s British ultralight aircraft
• Single-engined pusher aircraft
• Paramotors

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