By 1998 the kit and plans were being offered by Winners Circle Engineering Inc. of Monrovia, Indiana.
The aircraft was designed to comply with the US Experimental - Amateur-built aircraft rules. It features a single main rotor, a single-seat enclosed cockpit with a windshield, tricycle landing gear with wheel pants, hydraulic disk brakes and a self-aligning nosewheel, plus a tail caster. The acceptable power range is 47to and the standard engine used is a twin cylinder, air-cooled, two-stroke, single-ignition 500NaN0 Rotax 503 engine in pusher configuration. The cabin width is 220NaN0.
The aircraft fuselage structure is made from bolted-together aluminum tubing has a full aerodynamic, bullet-shaped, composite cockpit fairing that adds 12lb to the aircraft's empty weight. Its two-bladed rotor has a diameter of 251NaN1 and an optional pre-rotator. The aircraft has a typical empty weight of 380lb and a gross weight of 630lb, giving a useful load of 250lb. With full fuel of the payload for the pilot and baggage is 220lb.
The standard day, sea level, no wind, take off with a 500NaN0 engine is 5000NaN0 and the landing roll is 100NaN0.
The manufacturer estimated the construction time from the supplied kit as 150 hours.
By 1998 the company reported that 100 plans and kits had been sold and three aircraft were completed and flying.
In April 2015 one example was registered in the United States with the Federal Aviation Administration to the designer.[2]