Technical data
Type F-3
Function Trainer
Year 1909
Crew 2
Engines 1*50hp Gnome
Length ~12m
Wingspan 10.5m/7.0m
Wing area 38.0m2
Empty weight 400kg
Loaded weight 580kg
Wing Load (kg/m2) 15
Power load (kg/hp) 11
Speed at 0m 65km/h

Farman-III, F-3, Farman

Differed from well known Farman-IV by tailfin/rudder shape, larger elevator area and longer rear sections of landing skis.

Few were delivered to Russia.



References:
  • "History of aircraft construction in the USSR", Vol.1 p.140;

  • Modified November 26, 1997 Back to
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