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From Wikipedia, the free encyclopedia

Role Reconnaissance aircraft
Manufacturer Farman
Designer Henri Farman
First flight 1912
Number built 2

The Farman HF.10 was a reconnaissance aircraft built in France shortly before the First World War.


The HF.10 was developed in 1911 for the military aircraft competition (Concours Militaire), held in Reims. The HF.10 had a Gnome Rhone engine, but the subsequent HF.10bis had a slightly more powerful Gnome Gamma engine with a power of 70 hp.[1]


Data from [2]

General characteristics

  • Crew: 3
  • Length: 10.20 m (33 ft 6 in)
  • Wingspan: 16.00 m (52 ft 6 in)
  • Height: 2.70 m (8 ft 10 in)
  • Wing area: 72 m2 (780 sq ft)
  • Empty weight: 350 kg (772 lb)
  • Max takeoff weight: 550 kg (1,213 lb)
  • Powerplant: 1 × Gnome Omega 7-cylinder air-cooled rotary piston engine, 37 kW (50 hp)
  • Propellers: 2-bladed fixed-pitch wooden pusher propeller


  • Maximum speed: 80 km/h (50 mph, 43 kn)
  • Range: 315 km (196 mi, 170 nmi)


This page was last edited on 31 May 2019, at 21:12
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