[2] The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules and is noted for its robust design and ability to handle rough field operations.
It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, tricycle landing gear and a single engine in tractor configuration.
Its 9.5 m (31.2 ft) span wing is supported by V-struts and jury struts.
The standard engine available was the 80 hp (60 kW) Rotax 912UL four-stroke powerplant.
[1] Data from Bayerl[1]General characteristics Performance