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.
General characteristics Performance