Fisher Boomerang

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The Fisher Boomerang is a single-seat conventional landing gear, high-winged monoplane ultralight aircraft designed by Michael Fisher and introduced in mid-1982.[1][2]

Development

The Boomerang was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum Script error: No such module "convert". empty weight. The aircraft has a standard empty weight of Script error: No such module "convert"..[2]

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 Script error: No such module "convert". main wheels. Wings were available in several spans, from Script error: No such module "convert"., the longer span being used for the two seat variant.[1][2]

The Boomerang is fitted with a Script error: No such module "convert". Kawasaki 340 engine as standard equipment or optionally a Script error: No such module "convert". Kawasaki 440A engine, both with a reduction drive system. The aircraft has an empty weight of Script error: No such module "convert". and a gross weight of Script error: No such module "convert"., giving a useful load of Script error: No such module "convert"..[1][2]

The aircraft was discontinued due to poor sales.[2]

Specifications (Boomerang)

Data from Janes All the Worlds Aircraft 1983-84[1]

General characteristics

See also

Aircraft of comparable role, configuration, and era

References

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  1. ↑ a b c d Taylor, John WR: Janes All the Worlds Aircraft 1983-84, Janes Publishing Company, 1983, p.660.
  2. ↑ a b c d e Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-7. Cybair Limited Publishing, 2001. Template:ISBN

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