[1] The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules.
It features a strut-braced high-wing, a two seats in side-by-side configuration enclosed cockpit, tricycle landing gear or conventional landing gear and a single engine in tractor configuration.
Its 9.04 m (29.7 ft) span wing employs dual parallel struts.
[1] Originally produced by Sauper/ALMS, the design was later manufactured by Aero Synergie.
[2] Popular in Europe and Africa as a trainer, it also found use as a personal aircraft due to its simple construction and ease of handling.