The design was intended to be easily scalable to much larger aircraft.
It features a cantilever mid-wing, a two-seats-in-tandem enclosed cockpit under a glazed canopy, fixed tricycle landing gear with wheel pants and a single engine in pusher configuration.
[2] The aircraft is made from sheet aluminum, has an 18.0 ft (5.5 m) span wing and is powered by a 200 hp (149 kW) Lycoming IO-360-A1B6D engine.
With full fuel of 50 U.S. gallons (190 L; 42 imp gal) the payload is 300 lb (140 kg).
[2] The sole example built was registered in the United States with the Federal Aviation Administration in 1974, but its registration was cancelled in August 2013.