The aircraft was designed to comply with the
Fédération Aéronautique Internationale microlight category and the US
light-sport aircraft category. It features a
cable-braced or
strut-braced hang glider-style
high-wing, weight-shift controls, a two-seats-in-
tandem, open cockpit,
tricycle landing gear with
wheel pants and a single engine in
pusher configuration. The aircraft is made from bolted-together
aluminum tubing, with its double surface wing covered in
Dacron sailcloth. The aircraft uses an "A" frame weight-shift control bar. The powerplant options include the twin cylinder, liquid-cooled,
two-stroke,
dual-ignition Rotax 582 engine, the four cylinder, air and liquid-cooled,
four-stroke,
dual-ignition Rotax 912 or
Rotax 912S engine. In its AS-III model the aircraft has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload is . A number of different wings can be fitted to the basic carriage, including the cable-braced
Aeros Profi, the strut-braced
Aeros Profi TL and the
Apollo Reflex 11 or 13. ==Variants==