Indraéro Aéro 101
Indraéro · France · first flew 1951 · light aircraft
The Indraéro Aéro 101 was a light training biplane developed in France in the 1950s.
Recognition (WEFT)
| W — Wings | Mid-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 5.6 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Light two-seat training biplane
- Single tractor four-cylinder horizontally-opposed engine
- Short wingspan of 7.6 metres
A small two-seat biplane, 5.6 metres long with a 7.6 metre span and a maximum speed of 178 km/h.
Specifications
- The Indraéro Aéro 101 has a length of 5.6 m (18 ft).
- It has a wingspan of 7.6 m (25 ft).
- Its maximum speed is 178 km/h (111 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It was designed by Jean Chapeau and J. Blanchet and first flew on 27 July 1951. It was powered by a 75 hp Minié 4.DC.32 four-cylinder air-cooled horizontally-opposed engine.
Variants
The Aéro 110 prototype had a steel tube fuselage.
Where you'll see it
About 13 were built, and the Service de l'Aviation Légère et Sportive was the primary user. Three examples were still active in 2009.
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- Indraéro Aéro 20
- Indraéro Aéro 30
- AISA I-11
- Auster J/5 Aiglet Trainer
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- de Havilland Canada DHC-3 Otter
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