[1][2] The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules.
It features a cantilever low-wing, a single-seat, enclosed cockpit with a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration.
Its 7.48 m (24.5 ft) span wing employs an SM701 airfoil and slotted flaps.
Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke and the 80 hp (60 kW) Rotax 912UL four-stroke powerplant.
[1][2] Data from Bayerl[1][2]General characteristics Performance