| Company | Breguet Aviation | |
| Scheme | Monoplane Midwing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
6.5
88.7
|
|
| Wings | ||
| Wing area (m2) |
1.1
12.9
925
|
|
| Wingspan (Beam) (m) |
0.1
14.4
95
|
|
| Wing loading (kg/m2) |
3.1
23.8
829
|
|
| Aspect ratio |
1.7
15.9
25.6
|
|
| Weights | ||
| Empty weight (kg) |
8
211
276,800
|
|
| Loaded weight (kg) |
5
306
242,500
|
|
| Capacity | ||
| Capacity passengers (per.) |
1
1
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
180
28,165
|
|
| Stall Speed (km/h) |
40
40
257.7
|
with 30° flaps |
| Performance | ||
| Maximum glide ratio |
7
27
43
|
at 78 km/h |
| Dynamic Performance | ||
| Rate of sink (m/min) |
36
45
55.8
|
at 78 km/h |
| Stat | ||
| Number built (qt) |
0
8
43,000
|
|
| First flight | 17.06.1948 | |
