| 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
|
|
| Rotors | ||
| Rotor number (qt) |
1
2
8
|
|
| Weights | ||
| Empty weight (kg) |
8
1,182
276,800
|
|
| Loaded weight (kg) |
5
1,750
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
222
28,165
|
at 1000 m |
| Performance | ||
| Endurance (h) |
0.0
2
150
|
|
| Propellers | ||
| Prop blade number (qt) |
1
2
8
|
|
| Combat | ||
| Guns (qt) |
1
4
18
|
2 × fixed 7.9 mm (0.311 in) synchronised Madsen machine gun firing through propeller arc and 2 × similar guns on mounting in rear cockpit |
| Stat | ||
| Number built (qt) |
0
5
43,000
|
|
| First flight | 1926 | |
