Fisher Boomerang

The Fisher Boomerang is a single-seat conventional landing gear, high-winged monoplane ultralight aircraft designed by Michael Fisher and introduced in mid-1982.

Development
The Boomerang was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb empty weight. The aircraft has a standard empty weight of 190 lb.

The aircraft is a single-seat ultralight with a high wing and a conventional three-axis type with ailerons, elevators and rudder. The airframe structure is of 6061T6 and 2024T3 aluminum tube, covered with Stits Polyfibre aircraft fabric. The landing gear is of a fixed taildragger configuration without suspension on the 20 in main wheels. Wings were available in several spans, from 28 to 32 ft, the longer span being used for the two seat variant.

The Boomerang is fitted with a 30 hp Kawasaki 340 engine as standard equipment or optionally a 40 hp Kawasaki 440A engine, both with a reduction drive system. The aircraft has an empty weight of 190 lb and a gross weight of 470 lb, giving a useful load of 280 lb.

The aircraft was discontinued due to poor sales.