| Type | Aircraft | |
| Company | Société des avions Caudron | |
| Scheme | High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
8.2
88.7
|
|
| Height (m) |
0.6
2.1
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
20
925
|
|
| Wingspan (Beam) (m) |
0.1
11.9
95
|
|
| Weights | ||
| Empty weight (kg) |
8
600
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
1,050
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Capacity passengers (per.) |
1
2
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
210
28,165
|
|
| Сruise Speed (km/h) |
52
185
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
140
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
4,500
161,544
|
|
| Range (Ferry range) (km) |
4
850
40,700
|
|
| Stat | ||
| Number built (qt) |
0
27
43,000
|
|
| Introduction | 1934 | |
| First flight | 1935 | |
