SECAT RG-75

RG-75
Role Light utility aircraft
National origin France
Manufacturer SECAT
Designer Rémy Gaucher[1]
Number built 2[1]


The SECAT RG-75 (sometimes designated SECAT 75T[1]) was a light utility monoplane built in France shortly after World War II.[1][2] It was a conventional cabin monoplane with two seats side-by-side.[1][2][3][4] The wing was mounted high and was of fully cantilever design.[1][4] The conventional undercarriage consisted of two fixed, divided main units plus a fixed tailskid.[1] Power was supplied by a tractor-mounted piston engine that drove a two-bladed propeller.[1][4] Construction was of wood throughout, covered in plywood.[4]

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Semaine de l'Aviation légère (light aviation week) held at Toussus-le-Noble from 22 April 1947 but was already somewhat outdated by the standards of the time.[1] SECAT produced no further examples.[1]


Specifications

Data from Jane's All The World's Aircraft 1948

General characteristics

Performance


Notes

  1. 1 2 3 4 5 6 7 8 9 10 Gaillard, p.41
  2. 1 2 The Illustrated Encyclopedia of Aircraft, p.2839
  3. Taylor, p.797
  4. 1 2 3 4 Jane's All The World's Aircraft 1948, p.153c

References


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