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Large four-engined transport with a deep fuselage. The first prototype crashed during its first flight on 20 July 1948 killing the pilot Bertrand and his crew. Despite the second prototype flew succesfully on 9 April 1949, the aircraft did not enter production and the project was cancelled.
| ENGINE | 4 x 1600hp SNECMA 14R piston engines |
| WEIGHTS |
| Take-off weight | 40000 kg | 88185 lb |
| Empty weight | 21000 kg | 46297 lb |
| DIMENSIONS |
| Wingspan | 44.00 m | 144 ft 4 in |
| Length | 30.50 m | 100 ft 1 in |
| Height | 10.10 m | 33 ft 2 in |
| Wing area | 200.00 m2 | 2152.78 sq ft |
| PERFORMANCE |
| Max. speed | 410 km/h | 255 mph |
| Cruise speed | 320 km/h | 199 mph |
| Ceiling | 9000 m | 29550 ft |
| Range | 2000 km | 1243 miles |
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