Top speed 354 km/h Length 6.25 m | Wingspan 7.32 m | |
The Bede BD-7 was a light aircraft constructed in the United States in 1976. It shared the Bede BD-5's pusher propeller configuration but was considerably larger. The fuselage was all-metal, and the wings used the unique "panel-rib" wing construction pioneered on the Bede BD-4. Some sources state that the prototype (registration N7BD) flew in December 1976, but most suggest that it was never actually completed, much less flown.
Specifications (prototype)
General characteristics
Performance
References
Bede BD-7 Wikipedia(Text) CC BY-SA