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THK-5 __NOTOC__
The THK-5 was a twin-engine aircraft developed in Turkey in 1945 as an air ambulance.〔Taylor 1989, 683〕〔"The Turkish Air League", 351〕 It was a conventional, low-wing cantilever monoplane of wooden construction throughout. The main units of the tailwheel undercarriage retracted into the wing-mounted engine nacelles and the THK-5 could carry two stretcher cases plus a medical attendant. This was followed in production by a six-seat utility transport version designated THK-5A〔 and three examples of an improved version of the 5A designated THK-10.〔Deniz 2004〕 A single example of the type was exported, sold to Denmark. When THK was taken over by MKEK, this was one of the designs selected for further work. However, although the designation MKEK-5 was allocated,〔 nothing further came of this.〔
==Specifications (THK-5)==
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「THK-5」の詳細全文を読む
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