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SECAT RG-75 __NOTOC__
The SECAT RG-75 (sometimes designated SECAT 75T〔) was a light utility monoplane built in France shortly after World War II.〔〔''The Illustrated Encyclopedia of Aircraft'', p.2839〕 It was a conventional cabin monoplane with two seats side-by-side.〔〔〔Taylor, p.797〕〔''Jane's All The World's Aircraft 1948'', p.153c〕 The wing was mounted high and was of fully cantilever design.〔〔 The conventional undercarriage consisted of two fixed, divided main units plus a fixed tailskid.〔 Power was supplied by a tractor-mounted piston engine that drove a two-bladed propeller.〔〔 Construction was of wood throughout, covered in plywood.〔 ==History== Two prototypes, registered ''F-WBBX'' and ''F-WBBT'' were tested at the CEV at Brétigny-sur-Orge in 1947 by pilots Marcel Joannès and Guy Buteau. Shortly afterwards, ''F-WBBT'' was displayed together with other SECAT designs at the ''Semaine de l'Aviation légère'' (light aviation week) held at Toussus-le-Noble from 22 April 1947 but was already somewhat outdated by the standards of the time.〔 SECAT produced no further examples.〔
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