The Wibault 360 was a 1930s French five-passenger airliner designed and built by the Wibault company.[1]
The Wibault 360 was a low-wing monoplane powered by a 230 hp (172 kW) Salmson 9Ab radial engine and equipped with conventional landing gear.[1] The design was based on the earlier three-engined Wibault 283 but the 360 was smaller and had an enclosed cabin for a pilot and five passengers.[1] The prototype, designated the 360T5, first flew in August 1931.[1] A number of variants were built with different engines, the last of the series was the Wib.366 designed to compete in the 1934 London to Melbourne air race.[1]
Data from Air Transport: The Wibault Penhoet 360 T.5 Monoplane[2]
General characteristics
Performance
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