The prototype C.61 (F-ESAE) had a freight hold and cabin for six passengers. The conventional landing gear also included a wheel beneath the nose to prevent nose-overs on landing. For the production C.61s the cabin size was increased to accommodate eight passengers.
- In 1924 many C.61s were modified to take 194 kW (260 hp) Salmson CM.9 radial engines on the outboards, increasing the maximum loaded weight to 4834 kg (10657 lb).
- Crew: two
- Length: 14 m (45 ft 11.25 in)
- Wingspan: 24.14 m (79 ft 2.5 in)
- Wing area: 104 m2 (1119.48 ft2)
- Empty weight: 2200 kg (4850 lb)
- Gross weight: 3480 kg (7672 lb)
- Powerplant: 3 × Hispano-Suiza 8Ac inline piston, 134 kW (180 hp) each each
- Maximum speed: 160 km/h (99 mph)
- Range: 640 km (398 miles)
- Service ceiling: 4000 m (13125 ft)
- after 1923 (date unknown) - C.61 lost when it came down at sea
- July 3, 1926 - C.61 operated by Compagnie Internationale de Navigation Aérienne crashes in Czechoslovakia
- Donald, David, ed. (1997). The Encyclopedia of World Aircraft. Prospero Books. p. 236. ISBN 1-85605-375-X.
- "Accidents by Airline". Retrieved 2007-09-14.
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