Developed by the Societe Indraero and first flown in 1953, the Aero 101 was designed by MM. Chapeau and Blanchet as a light tandem two-seat training biplane for the Service de l’Aviation Legre et Sportive (S.A.L.S.), and an initial production batch of thirteen was built.
Derived from the Aero 110, it differs by being all-wood construction, a tail wheel and brakes. Powered by a 75 hp Minie 4 DC-32 engine, the tandem open cockpits are fitted with dual controls.
Engine: 75 hp Minie 4 DC-32
Wing span: 24 ft 11 in
Length: 18 ft 4 in
Max speed: 108.6 mph
Cruise: 93 mph
ROC: 630 fpm
All Aero 