[<< wikipedia] SECAT RG-75
The SECAT RG-75 (sometimes designated  SECAT 75T) was a light utility monoplane built in France shortly after World War II. It was a conventional cabin monoplane with two seats side-by-side. 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Semaine de l'Aviation légère (light aviation week) held at Toussus-le-Noble from 22 April 1947 but was already somewhat outdated by the standards of the time.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.


== Specifications ==
Data from Jane's All The World's Aircraft 1948General characteristics
Crew: one pilot
Capacity: one passenger
Length: 7.00 m (23 ft 0 in)
Wingspan: 10.00 m (32 ft 10 in)
Height: 1.90 m (6 ft 3 in)
Wing area: 14.0 m2 (151 sq ft)
Empty weight: 280 kg (617 lb)
Gross weight: 500 kg (1,100 lb)
Powerplant: 1 × Régnier 4D2 , 52 kW (70 hp)Performance

Maximum speed: 180 km/h (112 mph, 97 kn)
Cruise speed: 170 km/h (106 mph, 92 kn)
Range: 800 km (500 mi, 430 nmi)
Service ceiling: 5,000 m (16,400 ft)
Rate of climb: 3.5 m/s (639 ft/min)


== Notes ==


== References ==
Bridgeman, Leonard (1948). Jane's All the World's Aircraft 1948. London: Sampson Low Marston. pp. 153c.
Gaillard, Pierre (2002). "Les avions de la SECAT". Les Cahiers du RSA. Paris: Le Réseau du Sport de l'Air (239): 40–41.
The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing. p. 2839.
Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 797.