The SO.95 Corse II was a light twin-engined transport, the prototype flying on 17 July 1947. The type was originally fitted with a tailwheel undercarriage, which was retained in the civil version, but the military variant featured a tricycle landing gear. The Corse II was used almost exclusively by the light transport units of the French Naval Air Arm; only two saw
regular airline service, operating with Air Services of India between Bombay, Bangalore and Delhi before being withdrawn in 1950.
| ENGINE||2 x 580hp Renault 12S-02-201 12-cylinder Vee-type engines|
| Take-off weight||5600 kg||12346 lb|
| Wingspan||18.00 m||59 ft 1 in|
| Length||12.32 m||40 ft 5 in|
| Height||4.30 m||14 ft 1 in|
| Max. speed||330 km/h||205 mph|
| Ceiling||7000 m||22950 ft|
| Range||1300 km||808 miles|
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