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

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 34 kW (45 hp) Salmson 9ADb radial engine, first flew on 1 May 1950

Three examples of the type were current on the French Civil Aircraft Register in 2009, including an Aero 101C and two Aero 101s.^[1]

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 48 kW (65 hp) Continental A65.

Data from ^[2]

General characteristics

• Crew: 2
• Length: 5.6 m (18 ft 4 in)
• Wingspan: 7.6 m (24 ft 11 in)
• Height: 2.2 m (7 ft 3 in)
• Wing area: 14.0 m² (151 sq ft)
• Empty weight: 312 kg (688 lb)
• Gross weight: 505 kg (1,113 lb)
• Powerplant: 1 × Minié 4.DC.32 4-cyl. air-cooled horizontally-opposed piston engine, 56 kW (75 hp)

Performance

• Maximum speed: 178 km/h (111 mph, 96 kn)

• Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 534.
• Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. pp. 424–25.
• Partington, Dave (2009). European Registers Handbook 2009. Tonbridge, Kent: Air-Britain (Historians) Ltd. ISBN 978-0-85130-417-5.

• Aero 110