| Type | Aircraft | |
| Company | Blériot Aéronautique | |
| Scheme | Biplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
14.8
88.7
|
|
| Height (m) |
0.6
4.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
119.1
925
|
|
| Wingspan (Beam) (m) |
0.1
23
95
|
|
| Weights | ||
| Empty weight (kg) |
8
2,919
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
5,600
575,000
|
|
| Loaded weight (kg) |
5
5,600
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
|
| Capacity passengers (per.) |
1
16
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
185
28,165
|
|
| Сruise Speed (km/h) |
52
158
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
1,680
60,000
|
4 powerplants 420 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
4,000
161,544
|
|
| Range (Ferry range) (km) |
4
525
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
132
36,000
|
|
| Stat | ||
| Number built (qt) |
0
2
43,000
|
|
| Introduction | 1926 | |
| First flight | 27.10.1926 | |
