[1] With three-axis controls, the Avenger was intended to appeal to conventional light aircraft pilots and was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg).
It has a strut-braced high-wing, single-seat, open cockpit, single pusher engine configuration, and is equipped with tricycle landing gear using nosewheel steering.
The fuselage consists of a single aluminium keel tube that runs from the tail surfaces to the nose wheel.
The landing gear has notably high ground clearance for rough field operations and the engine, mounted on the wing trailing edge, drives a propeller that is protected by the low-mounted tailboom.
[1] Available as either a kit for home construction or as a complete aircraft,[2] the Avenger was introduced in the early 1980s when the market was becoming saturated with ultralight designs; as a result, the company quickly went out of business and production ended.