| Type | Aircraft | |
| Company | Société Aéronautique Française (Avions Dewoitine) | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
19.0
88.7
|
|
| Height (m) |
0.6
5.4
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
80
925
|
|
| Wingspan (Beam) (m) |
0.1
29
95
|
|
| Weights | ||
| Empty weight (kg) |
8
5,280
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
9,350
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
4
112
|
two pilots, radio operator and a mechanic |
| Capacity passengers (per.) |
1
8
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
300
28,165
|
|
| Сruise Speed (km/h) |
52
250
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
1,725
60,000
|
3 powerplants 575 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
6,300
161,544
|
|
| Range (Ferry range) (km) |
4
2,000
40,700
|
|
| Stat | ||
| Number built (qt) |
0
4
43,000
|
|
| Introduction | 1933 | |
| First flight | 11.07.1933 | |
