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Rogožarski SIM-XII-H : ウィキペディア英語版 | Rogožarski SIM-XII-H
The Rogožarski SIM-XII-H (Serbian Cyrillic:Рогожарски СИМ-XII-Х) was a Yugoslav trainer single-engine floatplane, with two floats designed in 1938. It was designed and built at the Rogožarski factory in Belgrade. ==Design and development==
The YRAF was unsuccessfully trying to choose the most appropriate seaplane for pilot training so they turned to the Rogožarski factory for help in 1937 and ordered the seaplane school project to be made that would fit in its characteristics to the school plane SIM-X. Since it was not possible to make a simple modification (adaptation of existing aircraft SIM-X) for installation of EDO floats, chief designed Sima Milutinović fitted the plane with a more powerful engine Walter Major 6 190 hp, leading to an increase in aircraft size. Thus, this new high-flying school plane with two floats represented an entirely new plane, designated SIM-XII-H. During 1937, the project went into realization stage, and as early as the end of the year the prototype was ready for testing.〔Станојевић, Драгољуб.; Чедомир Јанић (12/1982.). "Животни пут и дело једног великана нашег ваздухопловства - светао пример и узор нараштајима" (in (Serbian)). Машинство (YU-Београд: Савез инжењера и техничара Југославије) 31: 1867 - 1876.〕 The test flight was conducted on February 7, 1938, by test pilot Ivan Koroša in hydro-base Divulje. After the flight tests had achieved satisfactory results, the first batch of aircraft was ordered, which were delivered in mid-1939.〔http://airserbia.com/vvkj/index.php?str=avioni&av=75〕 Aircraft SIM-XII-H, a supported two-seat high-flying plane, with engine Walter Major 6 (190 hp), of predominantly wooden construction, with an elliptical cross-section of fuselage entirely made of wood and covered with plywood, wings as the supporting structure made of wood covered with fabric, with rounded ends. On each side, the wings are supported by a pair of inclined struts attached to the fuselage. The fuel tank was located in the central part between the wings, that is, at their junction. The first series of aircraft had two (a pair of) EDO floats installed (EDO Float Model 47).
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