| Technical data | |
|---|---|
| Type | Farman F-XX |
| Function | Observation, Trainer |
| Year | 1913 |
| Crew | 2 |
| Engines | 1*80hp Gnome |
| Length | 8.06m |
| Wingspan | 13.76m 7.58m |
| Wing area | 35.0m2 |
| Empty weight | 416kg |
| Loaded weight | 675kg |
| Wing Load (kg/m2) | 19.1 |
| Power load (kg/hp) | 8.4 |
| Speed at 0m | 95km/h |
| Landing Speed | 55km/h |
| Range | 315km |
| Flight Endurance | 3h30min |
| Ceiling | 2500m |
| Climb | |
| 500m | 8.0min |
| 1000m | 20.0min |
| 2000m | 55min |
| Payload | |
| Fuel | 82+27kg |
Farman F-XX
 |
Similar to Farman-XVI, with refined design. Some construction elements were made lighter, other - strengthened. Some F-XX had dual controls. Aircraft was built at Anatra and Schetinin factories. Anatra continued production until 1922.
Last Farman F-XX was serving at Sevastopol aviator school in 1923.
 |
12k drawing from the Virtual Aircraft Museum |
| Predecessors | Modifications |
|---|---|
 Farman-XVI |
 Farman-XXII |
| References | Links |
|---|---|
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