| Company | Breguet Aviation | |
| Scheme | Monoplane Midwing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
9
88.7
|
|
| Wings | ||
| Wing area (m2) |
1.1
20
925
|
|
| Wingspan (Beam) (m) |
0.1
20.0
95
|
|
| Wing loading (kg/m2) |
3.1
34.5
829
|
|
| Aspect ratio |
1.7
20
25.6
|
|
| Weights | ||
| Empty weight (kg) |
8
340
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
690
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Speeds | ||
| Stall Speed (km/h) |
40
62
257.7
|
|
| Never exceed speed (km/h) |
108.0
220
1,050
|
|
| Performance | ||
| Maximum glide ratio |
7
35
43
|
|
| Dynamic Performance | ||
| Rate of sink (m/min) |
36
42
55.8
|
|
| Stat | ||
| Number built (qt) |
0
18
43,000
|
|
| First flight | 26.05.1956 | |
