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Fokker A.I

Fokker · Fixed Wing / Reconnaissance / Trainer · Netherlands · Pioneer Age (pre-1919)

Fokker A.I — Fixed Wing / Reconnaissance / Trainer
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The Fokker A.I 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 A.I and 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 and between Fokker and Halberstadt, about 63 were produced.

Specifications

Category
Fixed Wing
Sub-Category
Reconnaissance
Domain
Defence
Era
Pioneer Age (pre-1919)
Country
Netherlands
Manufacturer
Fokker
Operator
German Air Service
Primary Role
Fixed Wing / Reconnaissance / Trainer
Status
Retired
Service Entry
1916
Produced
20
Engine
1x Oberursel U.I rotary
Thrust / Power
100 hp
Launch
Ground
Length (ft)
22
Wingspan (ft)
37.7
Empty Weight (lb)
1100
MTOW (lb)
1675
Service Ceiling (ft)
13000
Range (mi)
150
Max Speed (mph)
87
Armament
nil (intended to be unarmed)