| Type | Aircraft | |
| Company | Société des avions Caudron | |
| Scheme | Biplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
11.2
88.7
|
|
| Height (m) |
0.6
2.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
54.3
925
|
|
| Wingspan (Beam) (m) |
0.1
17.9
95
|
|
| Weights | ||
| Empty weight (kg) |
8
1,422
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
2,167
575,000
|
|
| Loaded weight (kg) |
5
2,167
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
183
28,165
|
|
| Сruise Speed (km/h) |
52
165
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
430
60,000
|
2 powerplants 215 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
5,950
161,544
|
|
| Endurance (h) |
0.0
3
150
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
250
36,000
|
|
| Combat | ||
| Guns (qt) |
1
5
18
|
7.7-mm (0.303-in) Lewis machine guns |
| Bombs weight (kg) |
2
120
39,000
|
|
| Stat | ||
| Number built (qt) |
0
370
43,000
|
|
| Introduction | 1917 | |
| First flight | 1917 | |
| Stop production | 01.07.1922 | |
