| Type | Aircraft | |
| Company | Blériot Aéronautique | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
14.7
88.7
|
|
| Height (m) |
0.6
3.4
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
88
925
|
|
| Wingspan (Beam) (m) |
0.1
23.2
95
|
|
| Weights | ||
| Empty weight (kg) |
8
3,750
276,800
|
|
| Loaded weight (kg) |
5
4,966
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
4
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
199
28,165
|
|
| Сruise Speed (km/h) |
52
168
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
1,100
60,000
|
2 powerplants |
| Performance | ||
| Service ceiling (m) |
0.6
7,450
161,544
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
321
36,000
|
|
| Combat | ||
| Guns (qt) |
1
4
18
|
2 × forward trainable Lewis guns in nose; 2 × rearward trainable Lewis guns in each of two engine nacelles |
| Bombs weight (kg) |
2
1,000
39,000
|
of bombs carried in internal bay |
| Stat | ||
| Number built (qt) |
0
44
43,000
|
|
| Introduction | 1926 | |
| First flight | 07.05.1926 | |
| Stop production | 1934 | |
