The aircraft is supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.

[2][3][4][5] The Zephyr was designed to comply with the Fédération Aéronautique Internationale microlight rules.

It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear, a T-tail and a single engine in tractor configuration.

The semi-tapered 9.6 m (31.5 ft) span wing is made from plywood with composite spars and leading edges and employs a UA-2 airfoil.

The standard engine factory-supplied was the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant.