The aircraft is supplied in complete, ready-to-fly form.
[1][2] The aircraft was derived from the Airsport Sonata motor glider and designed to comply with the Fédération Aéronautique Internationale microlight rules.
It features a cantilever low-wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.
It requires an engine of about 65 hp (48 kW) and no more than 60 kg (132 lb).
[1][2][3] Data from Bayerl and Tacke[1][2]General characteristics Performance