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Noorduyn Norseman : ウィキペディア英語版
Noorduyn Norseman

The Noorduyn Norseman is a Canadian single-engine bush plane designed to operate from unimproved surfaces. Distinctive stubby landing gear protrusions from the lower fuselage make it easily recognizable.
Originally introduced in 1935, the Norseman remained in production for almost 25 years with over 900 produced. A number of examples remain in commercial and private use to this day. Norseman aircraft are known to have been registered and/or operated in 68 countries throughout the world and also have been based and flown in the Arctic and Antarctic regions.
==Design and development==

Designed by Robert B.C. Noorduyn, the Noorduyn Norseman was produced from 1935 to 1959, originally by Noorduyn Aircraft Ltd. and later by the Canada Car and Foundry company.
With the experience of working on many ground-breaking designs at Fokker, Bellanca and Pitcairn-Cierva, Noorduyn decided to create his own design in 1934, the Noorduyn Norseman. Along with his colleague, Walter Clayton, Noorduyn created his original company, Noorduyn Aircraft Limited in early 1933 at Montreal while a successor company bearing the name, Noorduyn Aviation, was established in 1935.
Noorduyn's vision of an ideal bush plane began with a high-wing monoplane airframe to facilitate loading and unloading passengers and cargo at seaplane docks and airports; next, a Canadian operator utilizing existing talents, equipment and facilities should be able to make money using it; last, it should all-around superior to those already in use there.
From the outset, Noorduyn designed his transport to have interchangeable wheel, ski or twin-float landing gear. Unlike most aircraft designs, the Norseman was first fitted with floats, then skis and, finally, fixed landing gear.
The final design looked much like Noorduyn's earlier Fokker designs, a high-wing braced monoplane with an all-welded steel tubing fuselage. Attached wood stringers carried a fabric skin. Its wing was all fabric covered wood, except for steel tubing flaps and ailerons. The divided landing gear were fitted to fuselage stubs; legs were secured with two bolts each to allow the alternate arrangement of floats or skis. The tail wheel strut could be fitted with a wheel or tail skid.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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