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. The aircraft is made from sheet
aluminum. Its span wing has an area of and
flaps. The wing is supported by V-struts and
jury struts. Standard engines available are the
Rotax 912UL and the
Rotax 912ULS four-stroke powerplants. ==Variants==