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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.
| WEIGHTS |
| Empty weight | 1175 kg | 2590 lb |
| DIMENSIONS |
| Wingspan | 10.94 m | 36 ft 11 in |
| Length | 6.59 m | 22 ft 7 in |
| Height | 2.18 m | 7 ft 2 in |
| Wing area | 17.20 m2 | 185.14 sq ft |
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