The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever single-strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cabin with doors, fixed tricycle landing gear and a single engine in tractor configuration.
The aircraft is made from welded steel tubing with its wings made from aluminum sheet. Its 8.51NaN1 span wing has an area of 12.75m2 and flaps. The standard engine used is the 1000NaN0 Rotax 912ULS four-stroke powerplant.
Reviewer Marino Boric described the design of the welded steel tube fuselage in a 2015 review as assuring "good protection for the crew".[1]