| Type | Aircraft | |
| Company | Société des avions Caudron | |
| Scheme | Parasol Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
6.2
88.7
|
|
| Height (m) |
0.6
2.3
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
20
925
|
|
| Wingspan (Beam) (m) |
0.1
11.5
95
|
|
| Weights | ||
| Empty weight (kg) |
8
328
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
572
575,000
|
|
| Loaded weight (kg) |
5
555
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
pilot |
| Capacity passengers (per.) |
1
1
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
126
28,165
|
|
| Сruise Speed (km/h) |
52
102
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
40
60,000
|
1 powerplant |
| Performance | ||
| Endurance (h) |
0.0
4
150
|
|
| Stat | ||
| Number built (qt) |
0
24
43,000
|
|
| Introduction | 1925 | |
| First flight | 01.05.1925 | |
