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FMA IA 50 Guaraní II
The I.A. 50 Guaraní II was an Argentine utility aircraft designed at the DINFIA (successor to the "Instituto Aerotecnico" - AeroTechnical Institute) in the early 1960s.
==History==
In the early 1960s, the Argentine state aviation conglomerate, DINFIA, realised that its IA 35 Huanquero twin-piston engined light transport was becoming outdated, and it was decided to develop a turboprop-engined derivative. While of similar layout to the Huanquero, with both aircraft being twin-engined low-wing monoplane of all metal construction with a twin tail, the new aircraft, the Guaraní, shared only 20% of the structure of the Huanquero. It was powered by two Turbomeca Bastan III engines each rated at .〔Magnusson 2010, p. 5.〕〔Taylor 1962, pp. 4–5.〕 It first flew on 6 February 1962.〔Taylor 1965, p.3.〕
The aircraft was further developed as the Guaruani II; the main difference being a single swept fin and a shortened rear fuselage. It also used more powerful () Bastan VIA]] engines. The fuselage was semi-monocoque with a squared cross-section, having unswept wings and swept tailplanes. The prototype Guaraní was rebuilt to this standard and flew in this form on 26 April 1963.〔〔Magnusson 2010, p. 6.〕
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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