[1] The Model A was designed as a very low-cost aircraft to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg).

It features a strut-braced parasol-wing, a single-seat, open cockpit, conventional landing gear and a single engine in pusher configuration.

The powerplant, specified as a 22 hp (16 kW) single cylinder, two stroke, carburetted Zenoah G-25 aircraft engine, is mounted behind the pilot and behind the wing, above the fuselage.

The wings and tailplane can be removed in 20 minutes by two people to permit ground transportation by trailer or for storage.

[1] The controls are conventional, but limited in pitch and roll authority, bringing a recommendation by reviewer Andre Cliche not to fly the Model A in windy or turbulent conditions.