Английская Википедия:Indraéro Aéro 101

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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 Шаблон:Convert 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.[1]

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 Шаблон:Convert Continental A65.

Specifications (Aéro 101)

Шаблон:Aircraft specs Шаблон:Aircontent

References

Шаблон:Reflist

Bibliography

External links

Шаблон:Commons category

Шаблон:Indraero aircraft

  1. Partington, 2009, pp 183-224