Fisher Boomerang
Introduction 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  empty weight. The aircraft has a standard empty weight of .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  main wheels. Wings were available in several spans, from , the longer span being used for the two seat variant.The Boomerang is fitted with a  Kawasaki 340 engine as standard equipment or optionally a  Kawasaki 440A engine, both with a reduction drive system. The aircraft has an empty weight of  and a gross weight of , giving a useful load of .The aircraft was discontinued due to poor sales.
Specifications (Boomerang)
See also
References