[1][2][3][4] The wing was mounted high and was of fully cantilever design.
[1] Power was supplied by a tractor-mounted piston engine that drove a two-bladed propeller.
[4] 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Semaine de l'Aviation légère (light aviation week) held at Toussus-le-Noble from 22 April 1947 but was already somewhat outdated by the standards of the time.
[1] Data from Jane's All The World's Aircraft 1948General characteristics Performance