The Gurí was designed as a simple, low cost aircraft to comply with the
Fédération Aéronautique Internationale microlight rules. It features a
strut-braced high-wing, a two-seats-in-
side-by-side configuration semi-enclosed cockpit, fixed
conventional landing gear and a single engine in
tractor configuration. The aircraft is made from a mix of
aluminum tubing and
fiberglass, with its flying surfaces covered in
Dacron sailcloth. Its span wing employs V-struts and
jury struts. Standard engines used are the
Rotax 503, the
Rotax 582 two-stroke engine, the
Rotax 912UL and the
HKS 700E four-stroke powerplant. ==Specifications (Gurí) ==