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Falconar F9A : ウィキペディア英語版
Falconar F9A

The Falconar F9A and F10A are a family of Canadian amateur-built aircraft, designed by Chris Falconar and produced by Falconar Avia. The F9A design was introduced in 1965 and both the F9A and F10A are supplied as kits or as plans for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook'', page 157. BAI Communications. ISBN 0-9636409-4-1〕
==Design and development==
The F9 is a variant of the Jodel D9. Falconar indicates that it incorporates a larger cockpit, simplified fittings, shoulder harnesses and aerodynamic improvements to improve stall characteristics.
Hans Teijgeler of Jodel.com says that the F9A varies from the D9 by using a new wing design, with new simplified spar and rib design and the dihedral point moved inboard, allowing the outer portion to fold for ground transport or storage, but at the cost of added weight. He describes the wing as "less efficient". Teijgeler says of the Falconar F9A, "the Falconar 'Jodel' should not be looked upon as a Jodel, but as a Falconar. This is ()either good or bad. Just a fact to take into account"
The F9A features a cantilever low-wing, a single seat enclosed cockpit that is wide, fixed conventional landing gear and a single engine in tractor configuration.〔
The F9A and F10A are made from wood, with the flying surfaces covered in doped aircraft fabric. Its span wing has an area of . Construction time from the supplied kit is estimated as 700 hours.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Falconar F9A」の詳細全文を読む



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