| Company | Société des avions Caudron | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
6.6
88.7
|
|
| Wings | ||
| Wing area (m2) |
1.1
7
925
|
|
| Wingspan (Beam) (m) |
0.1
6.8
95
|
|
| Wing loading (kg/m2) |
3.1
100
829
|
|
| Rotors | ||
| Rotor number (qt) |
1
2
8
|
|
| Weights | ||
| Empty weight (kg) |
8
405
276,800
|
|
| Loaded weight (kg) |
5
695
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
350
28,165
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
280
320,000
|
|
|
23
280
320,000
|
||
| Propellers | ||
| Prop blade number (qt) |
1
2
8
|
|
| Stat | ||
| Number built (qt) |
0
3
43,000
|
|
| First flight | 1933 | |
