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Lioré et Olivier LeO 40

From Wikipedia, the free encyclopedia

LeO 40
Role Experimental biplane
National origin France
Manufacturer Lioré et Olivier
First flight 1932
Number built 1

The Lioré et Olivier LeO 40 was a French experimental biplane built by Lioré et Olivier.[1] The two-seat LeO 40 had full span slats fitted to both wings, it was powered by a 95 hp (71 kW) Argus engine in Pusher configuration.[1] Only one was built and the design was abandoned.[1]

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Transcription

Specifications

General characteristics

  • Capacity: 2

References

Notes

  1. ^ a b c Orbis 1985, p. 2332

Bibliography

  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.



This page was last edited on 24 December 2020, at 14:15
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