| Type | Aircraft | |
| Company | Société Aéronautique Française (Avions Dewoitine) | |
| Scheme | Monoplane Parasol | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
7.6
88.7
|
|
| Height (m) |
0.6
3
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
24.8
925
|
|
| Wingspan (Beam) (m) |
0.1
12.8
95
|
|
| Weights | ||
| Empty weight (kg) |
8
1,090
276,800
|
|
| Loaded weight (kg) |
5
1,580
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Capacity passengers (per.) |
1
1
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
270
28,165
|
|
| Сruise Speed (km/h) |
52
236
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
500
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
8,991.6
161,544
|
|
| Range (Ferry range) (km) |
4
400
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
600
36,000
|
|
| Combat | ||
| Guns (qt) |
1
4
18
|
2 × fuselage-mounted synchronised 7.7 mm (0.303 in) Vickers machine guns; 2 × wing-mounted 7.5 mm (0.295 in) Darne machine guns in the center section (optional) |
| Stat | ||
| Introduction | 1925 | |
| First flight | 1925 | |
