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The Schleicher Ka 6 is a single-seat glider designed by Rudolf Kaiser, built by Alexander Schleicher GmbH & Co, Germany and is constructed of Spruce and plywood with fabric covering. The design initially featured a conventional tailplane and elevator which was later replaced by an all-moving tailplane in the -Pe and Ka 6E variants. Variants built before the -CR and -BR used a main skid as the principal undercarriage, with later variants including the Ka 6E using a wheel as the main undercarriage with no nose skid. Other modifications for the Ka 6E include a more aerodynamic fuselage with glassfibre nose and wingroot fairings, longer canopy, and modified aluminium airbrakes. ==Variants== Dates of initial airworthiness approval in brackets: * Ka 6 - Initial version; span , (30 October 1956). * Ka 6B (27 September 1957) * Ka 6B-Pe - The Ka 6B with all-flying tailplane, (20 May 1960). * Ka 6BR - The Ka 6B with the main skid removed and a relocated mainwheel, (27 September 1957). * Ka 6CR - The Ka 6C with the main skid removed and a relocated mainwheel, (24 February 1959). * Ka 6CR-Pe - The Ka 6CR with all-flying tailplane, (20 May 1960). * Ka 6E The ultimate Ka-6, with all-flying tailplane, (29 July 1965) 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「Schleicher Ka 6」の詳細全文を読む スポンサード リンク
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