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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regular airline service, operating with Air Services of India between Bombay, Bangalore and Delhi before being withdrawn in 1950.
| CREW | 2 |
| PASSENGERS | 10-13 |
| ENGINE | 2 x 580hp Renault 12S-02-201 12-cylinder Vee-type engines |
| WEIGHTS |
| Take-off weight | 5600 kg | 12346 lb |
| DIMENSIONS |
| Wingspan | 18.00 m | 59 ft 1 in |
| Length | 12.32 m | 40 ft 5 in |
| Height | 4.30 m | 14 ft 1 in |
| PERFORMANCE |
| Max. speed | 330 km/h | 205 mph |
| Ceiling | 7000 m | 22950 ft |
| Range | 1300 km | 808 miles |
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