Development
The Courlis was an all-metal high-wing cantilever monoplane with twin booms supporting a tail unit. It was powered by a 190 hp (142 kW) Mathis G8R piston engine mounted in the rear fuselage in a pusher configuration. It had a fixed tricycle landing gear and had four seats in the enclosed cabin. The prototype, registered ''F-WBBF'', first flew on 9 May 1946. Production was started and a total of 144 aircraft were completed with a number being exported to South America. Problems with the engine (insufficient power, cooling)Pegase n°58, ''La formule des appareils bipoutres à moteur propulsif'', Jacques Noetinger resulted in the withdrawal of the engine's type certificate and some airframes were never fitted with an engine and scrapped. The company did test fit the aircraft with a 220 hp (164 kW) Mathis engine but production was ended. The aircraft flew for some years, owned by French private pilots, but by the mid-1950s, most had been withdrawn from service, with many being stored atVariants
;SUC-10 Courlis :Production variant with a 190hpAircraft on display
One aircraft is held by the Musée de l'Air et de l'Espace, Le Bourget, Paris, France, but is not currently (2007) on public display.Specifications (SUC-10 Courlis)
See also
References
Notes
Bibliography
*Donald, David, ed. ''The Complete Encyclopedia of World Aircraft''. London: Orbis, 1997. p. 796. . * * * {{refend 1940s French civil utility aircraft High-wing aircraft Single-engined pusher aircraft Twin-boom aircraft Aircraft first flown in 1946