| Type | Aircraft | |
| Company | Société Aéronautique Française (Avions Dewoitine) | |
| Scheme | Parasol Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
7.5
88.7
|
|
| Height (m) |
0.6
2.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
20
925
|
|
| Wingspan (Beam) (m) |
0.1
11.5
95
|
|
| Weights | ||
| Empty weight (kg) |
8
820
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
1,240
575,000
|
|
| Loaded weight (kg) |
5
1,240
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
255
28,165
|
|
| Сruise Speed (km/h) |
52
225
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
300
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
8,000
161,544
|
|
| Range (Ferry range) (km) |
4
400
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
450
36,000
|
|
| Combat | ||
| Guns (qt) |
1
2
18
|
fuselage-mounted synchronised 7.7 mm (0.303 in) Vickers machine guns |
| Stat | ||
| Number built (qt) |
0
500
43,000
|
|
| Introduction | 1922 | |
| First flight | 18.11.1922 | |
