Английская Википедия:Fisher Boomerang

Материал из Онлайн справочника
Перейти к навигацииПерейти к поиску

Шаблон:Short description Шаблон:Use mdy dates Шаблон:Use American English Шаблон:About

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 Шаблон:Convert empty weight. The aircraft has a standard empty weight of Шаблон: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 Шаблон:Convert main wheels. Wings were available in several spans, from Шаблон:Convert, the longer span being used for the two seat variant.[1][2]

The Boomerang is fitted with a Шаблон:Convert Kawasaki 340 engine as standard equipment or optionally a Шаблон:Convert Kawasaki 440A engine, both with a reduction drive system. The aircraft has an empty weight of Шаблон:Convert and a gross weight of Шаблон:Convert, giving a useful load of Шаблон:Convert.[1][2]

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

Specifications (Boomerang)

Шаблон:Aircraft specs

See also

Шаблон:Aircontent

References

Шаблон:Reflist


Шаблон:Fisher Flying Products

  1. 1,0 1,1 1,2 Taylor, John WR: Janes All the Worlds Aircraft 1983-84, Janes Publishing Company, 1983, p.660.
  2. 2,0 2,1 2,2 2,3 2,4 Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-7. Cybair Limited Publishing, 2001. Шаблон:ISBN