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, fixed tricycle landing gear and a single engine in tractor configuration.[2]
The aircraft fuselage is made from welded steel tubing, with the wing made from aluminum tubing, all covered in heat-shrunk Dacron aircraft fabric. Its 8.51NaN1 span wing has an area of 13.5m2 and is supported by V-struts with jury struts. The standard engine available is the 640NaN0 Rotax 582 two-stroke, which gives a cruising speed of 1300NaN0, with the 800NaN0 Rotax 912UL four-stroke powerplant optional, which gives a cruising speed of 1600NaN0.[2]