|Role||Two-seat general purpose monoplane|
|Primary user||French Air Force|
Design and development edit
The Bo.11 was mid-wing monoplane from 1911 with wire-braced wings and lateral control by wing warping. It was powered by a 52 kW (70 hp) Gnome rotary piston engine. The Bo.11 served with the Aéronautique Militaire at military air training schools and at a civil flying school at Buc. The aircraft could be fitted with twin floats.
- Crew: 2
- Length: 6.70 m (21 ft 11.75 in)
- Wingspan: 9.60 m (31 ft 6 in)
- Height: 2.50 m (8 ft 2.5 in)
- Powerplant: 1 × Gnome rotary piston engine , 52 kW (70 hp)
- Maximum speed: 90 km/h (56 mph, 49 kn)
- Cruise speed: 70 km/h (43 mph, 37 kn)
See also edit
Aircraft of comparable role, configuration, and era
- Orbis 1985, p. 820
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.