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Caudron airplanes in Russian service

The Caudron G.4 was designed as a twin engined development of the G.3 tractor biplane.
While the G.4 had a similar pod and boom layout to the G.3, it has two engines mounted on struts between the wings instead of a single similar engine at the front of the crew (pilot and observer-gunner) nacelle, while wingspan was increased and the tailplane had four rudders instead of two. This biplane could to carry a bombload of 100 kg and was armed with a turreted machinegun.

Length: 7.2 m    Wingspan: 17.2    Height: 2.6 m 
     Wing area: 39 sq.m 
     Powerplant:    2 x 80 (100) hp
     Service ceiling: 4000 (4500) m 
     Empty weight:     733 (848) kg
  Max takeoff weight: 1180 (1347) kg 
     Maximum speed:    124 (132) km/h
     Endurance:        3,5 (4) hours

Russian Caudron G.4 airplane

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