| Type | Aircraft | |
| Company | Breguet Aviation | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
15.9
88.7
|
|
| Height (m) |
0.6
5.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
56.3
925
|
|
| Wingspan (Beam) (m) |
0.1
20.5
95
|
|
| Weights | ||
| Empty weight (kg) |
8
4,840
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
8,600
575,000
|
|
| Loaded weight (kg) |
5
8,200
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Capacity passengers (per.) |
1
12
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
385
28,165
|
at 1600 m |
| Сruise Speed (km/h) |
52
340
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
1,608
60,000
|
2 powerplants 804 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
6,000
161,544
|
|
| Range (Ferry range) (km) |
4
1,000
40,700
|
|
| Dynamic Performance | ||
| Time to altitude (min) |
0.6
7
105
|
to 1500 m |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1936 | |
| First flight | 05.03.1936 | |
