| Type | Aircraft | |
| Company | Société Aéronautique Française (Avions Dewoitine) | |
| Scheme | Parasol Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
7.4
88.7
|
|
| Height (m) |
0.6
3.2
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
17.8
925
|
|
| Wingspan (Beam) (m) |
0.1
11.8
95
|
|
| Weights | ||
| Empty weight (kg) |
8
1,295
276,800
|
|
| Loaded weight (kg) |
5
1,730
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
400
28,165
|
at 4500 m |
| Сruise Speed (km/h) |
52
376
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
800.3
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
11,003.3
161,544
|
|
| Range (Ferry range) (km) |
4
1,150
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
895
36,000
|
|
| Propellers | ||
| Propellers (qt) |
1
1
8
|
|
| Combat | ||
| Guns (qt) |
1
2
18
|
Machine guns |
| Stat | ||
| Introduction | 1932 | |
| First flight | 01.08.1932 | |
