By 2014 the company website was listed as "under construction", then was taken down and the company went out of business.[3]
Designed and first flown in the early 1980s, the Skin complies with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 4500NaN0. The Skin has a maximum gross weight of 3600NaN0. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with an optional cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.
The aircraft is made from steel and bolted-together aluminum tubing, with its double surface wing covered in Dacron sailcloth. Its 10.61NaN1 span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, air-cooled, two-stroke, dual-ignition 500NaN0 Rotax 503 or the liquid-cooled 640NaN0 Rotax 582 engine. With the Rotax 503 powerplant the aircraft has an empty weight of 1550NaN0 and a gross weight of 3600NaN0, giving a useful load of 2050NaN0. With full fuel of the payload is 1620NaN0.
A number of different wings can be fitted to the basic carriage, including the Gryps 14, Gyps 16, Gyps 19 and the Ares 21.