Caudron G.3
1913
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Caudron G.3

Developed from the G.II of 1913, the G.III was a two-seat sesquiplane powered by a 59.6kW Le Rhone, Gnome or Anzani engine mounted in the nose of the short crew nacelle. Originally operated by French squadrons as reconnaissance aircraft over the Western Front and then in less dangerous theatres of war, the G.III subsequently became a trainer, serving also with the British, Belgian, Italian and American forces.

Caudron G.3


Specification 
 CREW2
 ENGINE1 x Le Rhone, 59kW
 WEIGHTS
    Take-off weight734 kg1618 lb
    Empty weight445 kg981 lb
 DIMENSIONS
    Wingspan13.4 m43 ft 12 in
    Length6.4 m20 ft 12 in
    Height2.6 m8 ft 6 in
    Wing area27.0 m2290.63 sq ft
 PERFORMANCE
    Max. speed106 km/h66 mph
    Ceiling3000 m9850 ft
    Range w/max.fuel300 km186 miles

Caudron G.3

Comments 
JOSE VELASCO ADAME, eduardis(@)hotmail.com, 30.09.2007

LISTO CUENTEN CON MIGO TENGO PLANOS,HERRAMIENTAS,FOTOS, TIEMPO LIBRE,EXPERIENCIA DE CONSTRUCCION DE DOS AVIONES CAUDRON G 3 PARA LA FUERZA AEREA COLOMBIANA, EN LA CUAL TRABAJE MAS DE 20 AŅOS.

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