| Company | Société des avions Caudron | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
6
88.7
|
|
| Height (m) |
0.6
2
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
10
925
|
|
| Wingspan (Beam) (m) |
0.1
8
95
|
|
| Rotors | ||
| Rotor number (qt) |
1
2
8
|
|
| Weights | ||
| Empty weight (kg) |
8
175
276,800
|
|
| Loaded weight (kg) |
5
300
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
125
28,165
|
|
| Propellers | ||
| Prop diameter (m) |
1.8
2.0
5.8
|
|
| Prop blade number (qt) |
1
2
8
|
|
| Stat | ||
| Number built (qt) |
0
4
43,000
|
|
| First flight | 01.12.1911 | |
