| Company | Blériot Aéronautique | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
8.3
88.7
|
|
| Wings | ||
| Wing area (m2) |
1.1
29
925
|
|
| Weights | ||
| Empty weight (kg) |
8
388.7
276,800
|
|
| Loaded weight (kg) |
5
598.7
242,500
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
94.8
28,165
|
|
| Stall Speed (km/h) |
40
64.4
257.7
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
90
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
70
60,000
|
1 powerplant |
| Performance | ||
| Range (Ferry range) (km) |
4
406
40,700
|
|
| Dynamic Performance | ||
| Time to altitude (min) |
0.6
4.3
105
|
|
| Stat | ||
| First flight | 01.02.1911 | |
