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Kieger AK3
The Kieger AK3 is conventionally laid out single engine, tractor configuration, low wing two seat light aircraft built in France from 2006. At least two have flown.
==Design and development==
The AK3 is the third two seat, single engine, low wing design from André Kieger. It is produced by Junkers Profly France and is alternatively known as the Junkers Profly Junka UL. The wing has a single spar with a plywood leading edge and a false spar for the mounting of ailerons and flaps. Production aircraft have small winglets. Each wing is fixed to the fuselage with a pair of sailplane style pins for rapid demounting. The fuselage is built around four longerons, giving it a square lower section; the upper fuselage is rounded and merges into the line of the large perspex canopy over the side-by-side seating. The tailplane is mounted on top of the fuselage and the fin is swept; both are plywood structures. There are horn balances on elevators and rudder.〔
The AK3 is powered by a 58.8 kW (78.9 hp) Rotax 912 UL four cylinder horizontally opposed engine, housed in the nose under a carbon fibre cowling and driving a three blade propeller. It has a tricycle undercarriage, with glass/carcon fibre laminate cantilever spring main legs mounted onto the fuselage and a trailing link nose wheel on a forward angled cantilever leg. The mainwheels have hydraulic brakes and all wheels are faired.〔
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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