Liore-Olivier LeO 9
1922
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Liore-Olivier LeO 9

Derived from a 1917 project designated LeO 3, the LeO 9 single-seat cantilever monoplane fighter was of metal construction and of advanced aerodynamic concept. Powered by a 300hp Hispano-Suiza 8Fb eight-cylinder water-cooled engine, the LeO 9 was exhibited, prior to first flight at the Paris Salon in 1921. Flight testing was initiated in the following year, but, on 24 September 1923, the wing folded during a very sharp turn and the aircraft crashed at Villacoublay with the death of the pilot, Gaston Martin. Further development of the LeO 9 was then discontinued.


Specification 
 WEIGHTS
    Empty weight1175 kg2590 lb
 DIMENSIONS
    Wingspan10.94 m36 ft 11 in
    Length6.59 m22 ft 7 in
    Height2.18 m7 ft 2 in
    Wing area17.20 m2185.14 sq ft

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