[1][2][3] The aircraft 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 20.5 hp (15 kW) Bailey V5 engine in pusher configuration with a 3.2:1 ratio belt reduction drive and a 130 cm (51 in) diameter Helix Carbon GmbH two-bladed carbon fibre propeller.
The aircraft is built from TIG welded aluminium tubing, with the propeller safety cage made from a single hoop and is a four-piece split type design.
The pilot harness was designed by Bailey Aviation and Sup’Air of France.
Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.