| Type | Aircraft | |
| Company | Société des avions Caudron | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
7.8
88.7
|
|
| Height (m) |
0.6
2.6
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
9
925
|
|
| Wingspan (Beam) (m) |
0.1
7.7
95
|
|
| Weights | ||
| Empty weight (kg) |
8
672
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
1,050
575,000
|
|
| Loaded weight (kg) |
5
1,050
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
pilot |
| Speeds | ||
| Max. Speed (km/h) |
25
370
28,165
|
|
| Сruise Speed (km/h) |
52
340
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
220
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
9,700
161,544
|
|
| Range (Ferry range) (km) |
4
1,100
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
660
36,000
|
|
| Stat | ||
| Number built (qt) |
0
19
43,000
|
|
| Introduction | 1936 | |
| First flight | 18.02.1936 | |
