Indraéro Aéro 101

The Indraéro Aéro 101 was a light training biplane developed in France in the 1950s.

Design and service
It was a conventional design with single-bay staggered wings braced with an I-strut, and fixed tailskid undercarriage with divided main units. The pilot and instructor sat in tandem, open cockpits. A small batch of aircraft were ordered by SALS for aeroclub use.

The prototype, known as the Aéro 110, differing from the later production Aero 101s by having a welded steel tube fuselage and a 45 hp Salmson 9ADb radial engine, first flew on 1 May 1950

Operational history
Three examples of the type were current on the French Civil Aircraft Register in 2009, including an Aero 101C and two Aero 101s.

Variants

 * Aéro 110:Prototype of the Aero 101 with welded steel tube fuselage and Salmson 9ADb radial engine first flown on 1 May 1950, 1 built.
 * Aéro 101: Ten production aircraft built with wooden structure and powered by Minié 4.DC.32 engines, first flown on 27 July 1951.
 * Aéro 101C: At least one aircraft fitted with a 65 hp Continental A65.