The aircraft was designed to be a US homebuilt aircraft as its empty weight exceeds the US FAR 103 Ultralight Vehicles rules, which imposes a category maximum empty weight of 2540NaN0. The LiteWing has a standard empty weight of 2800NaN0. It features a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat, open cockpit with a three-piece fiberglass cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.
The aircraft is made from welded and bolted 6061-T6 aluminum tubing, with its NorthWing 157 wing covered in Dacron sailcloth. Its 321NaN1 span wing is supported by a single tube-type kingpost and uses an "A" frame control bar. The engine factory supplied was the 400NaN0 Rotax 447 twin cylinder, two-stroke, air-cooled aircraft engine. The aircraft can accept engines of 40to. Brakes on the main wheels are standard equipment.
Twenty examples had been completed and flown by February 2000.