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 Aero 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
Variants
- Aero 110
- Prototype of the Aero 101 with welded steel tube fuselage and Salmson 9ADb radial engine first flown on 1 May 1950, 1 built.
- Aero 101
- Production aircraft built with wooden structure and powered by Minié 4DC-32 engines, first flown on 27 July 1951
Specifications (Aéro 101)
Data from [1]
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 4DC-32 4-cyl. air-cooled horizontally-opposed piston engine, 56 kW (75 hp)
Performance
- Maximum speed: 178 km/h (111 mph; 96 kn)
References
- ↑ Parmentier, Bruno. "Indraéro Aéro 101". Retrieved 6 December 2013.
Bibliography
- 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.
External links
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