|
|
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.
| CREW | 2 |
| ENGINE | 1 x Le Rhone, 59kW |
| WEIGHTS |
| Take-off weight | 734 kg | 1618 lb |
| Empty weight | 445 kg | 981 lb |
| DIMENSIONS |
| Wingspan | 13.4 m | 43 ft 12 in |
| Length | 6.4 m | 20 ft 12 in |
| Height | 2.6 m | 8 ft 6 in |
| Wing area | 27.0 m2 | 290.63 sq ft |
| PERFORMANCE |
| Max. speed | 106 km/h | 66 mph |
| Ceiling | 3000 m | 9850 ft |
| Range w/max.fuel | 300 km | 186 miles |
| 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. |
|
Do you have any comments about this aircraft ?
|
| |