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Fokker A.I
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The Fokker A.I (Fokker designation M.8) was an "A-class" unarmed two-seat monoplane observation aircraft of the 1914-15 era early in World War I, powered as the earlier Fokker M.5 was, by a 58.8 kW (80 PS) Oberursel U.0 seven cylinder rotary engine, or ''umlaufmotor'', a near-clone of the Gnome Lambda rotary engine of the same power output level — the same U.0 seven cylinder rotary engine version was used on all Fokker military monoplanes before the Fokker E.II ''Eindecker'' fighter's debut in 1915-16. The A.I aircraft resembled a substantially enlarged Fokker M.5, with a tall dorsal cabane structure to handle the triple sets of stationary flying and landing wires anchored to the wing panels' forward spar, each panel having fourteen wing ribs, and the similarly triple sets of wing warping cables attached to the rear spar. The earlier A.IIs were both built by Fokker and license-built by Halberstadt. The origins of the A.I, A.II and A.III were in a Morane-Saulnier Type H purchased from France. This led to the initial Fokker M.5 airframe designed by Martin Kreutzer, from which the larger A.I was derived. Fokker gave many aerobatic demonstrations in the M.5 on the eve of World War I. The M.8, was ordered as the A.I by the ''Fliegertruppe'' (Imperial German Army Air Service) and Fokker produced between 30 and 40 of them.
==Specifications==
Data from Scott, Josef (2012). Fokker Eindecker Compendium, Volume 1. Berkhampstead, Hertfordshire UK: Albatros Publications, Ltd. p. 18. ISBN 978-1-906798-22-2.
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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