| Type | Aircraft | |
| Company | Breguet Aviation | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
24.4
88.7
|
|
| Height (m) |
0.6
8.6
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
173.1
925
|
|
| Wingspan (Beam) (m) |
0.1
40.4
95
|
|
| Wing loading (kg/m2) |
3.1
165
829
|
|
| Weights | ||
| Empty weight (kg) |
8
16,134
276,800
|
|
| Loaded weight (kg) |
5
28,660
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
10
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
330
28,165
|
|
| Сruise Speed (km/h) |
52
230
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
4,480
60,000
|
4 powerplants 1120 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
6,000
161,544
|
|
| Range (Ferry range) (km) |
4
6,923
40,700
|
|
| Endurance (h) |
0.0
0.5
150
|
|
| Dynamic Performance | ||
| Time to altitude (min) |
0.6
9
105
|
to 3000 m |
| Stat | ||
| Number built (qt) |
0
5
43,000
|
|
| Introduction | 1938 | |
| First flight | 04.04.1938 | |
| Stop production | 1954 | |
