The design goal of the Solution was to produce a legal US FAR 103 Ultralight Vehicles regulations compliant single seat ultralight that could be easily converted to a two-seater with the addition of a second seat and a larger engine. FAR Part 103 specifies a maximum empty weight of 2540NaN0 and the Solution has a standard empty weight of 2460NaN0. It features a cable-braced high-wing, a single-seat, open cockpit, conventional landing gear and a single engine in pusher configuration.
The aircraft is made from bolted-together aluminium tubing, with the flying surfaces covered in Dacron sailcloth. Its 331NaN1 span wing has a wing area of 183square feet, which is large enough to support a second person. The second seat would be installed behind the first, in tandem, and could be optionally equipped with dual controls.
The pilot is accommodated on an open seat and has conventional three-axis controls in the form of a centre stick and rudder pedals. The standard engine provided for single seat flying was the single cylinder two-stroke Rotax 277 of 280NaN0, while larger engines could be installed for two-seat operations.
V-STOL Aircraft had the design on the market for only a short period before the company went out of business. Assembly time from the kit is estimated at 50 hours.