Airplane built by the Stebbins-Geynet Aeroplane Company of Norwich, Connecticut (William H. Stebbins of the USA and Louis Geynet of France), possibly the model A of 1909, which was equipped with a Cameron 25-30 hp four-cylinder, air-cooled engine. As a tri-bi-plane it had a detachable middle wing, which once removed converted the machine from a triplane into a biplane. Positive control was secured by use of the Stebbins-Geynet “auto-control” system. A pull or push movement operated the elevating rudders, while the balancing was done by means of side movements or slight turns. The rear vertical rudder was manipulated by means of a foot lever. It featured a single-place, open cockpit.
The Model B followed in 1910, same as the Model A, but with a seven-cylinder Holmes-modified Gnôme rotary, and 6sqft rudder instead of 10sqft.
Model A
Engine: 35-40hp Cameron pusher
Wingspan: 24’0″
Seats: 1
Model B
Engine: Gnôme
Wingspan: 24’0″
Seats: 1
All Aero 