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Indraero Aero 110
 The Aero 110 fuselage has a fabric covered steel-tube framework and powered by a 45 hp Salmson 9ADB radial air-cooled engine.
A Single-bay staggered biplane, upper and lower wings are of equal span and chord. A hinged panel in the upper wing provides access to the front cockpit. Full dual controls are fitted.
Produced by the Societe Indraero and flown for the first time on 1 May 1950, the Aero 110 was produced for the Service de l’Aviation Legre et Sportive (S.A.L.S.).
Engine: 45 hp Salmson 9ADB
Wing span: 24 ft 11 in
Length: 18 ft 4 in
Empty weight: 594 lb
Loaded weight: 1000 lb
Max speed: 81 mph
Cruise: 71.4 mph
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