To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.

From Wikipedia, the free encyclopedia

Farman F.211
Farman F.211 photo L'Aerophile April 1934.jpg
Role Four-seat day/night bomber
National origin France
Manufacturer Farman Aviation Works
First flight 1932

The Farman F.211 was a French four-seat day or night bomber designed and built by the Farman Aviation Works for the French Air Force.[1]


Designed as a day/night bomber the F.211 was similar but smaller than the F.220.[1] The F.211 was a high-wing braced monoplane with engines mounted on stub-wings with each stub wing having a pair of Gnome-Rhône Titan 7Kcrs radial engines, one tractor and one pusher.[1] The type did not enter production.[1]


Four-seat day or night bomber with four 300hp (224kW) Gnome-Rhône Titan 7Kcrs radial engines.[1]
Improved design with more powerful 350hp (261kW) Gnome-Rhône 7Kds radial engines, an increased bomb load of 1400kg (3086lb) and other detail changes.[1]
Proposed airliner version with two crew and 12 passengers, not built.[1]

Specifications (F.211)

Farman F.211 3-view drawing from L'Aerophile April 1934
Farman F.211 3-view drawing from L'Aerophile April 1934

Data from Orbis[1]

General characteristics

  • Crew: 4
  • Length: 15.90 m (52 ft 2 in)
  • Wingspan: 23.00 m (75 ft 6 in)
  • Height: 4.22 m (13 ft 10 in)
  • Wing area: 109 m2 (1,170 sq ft)
  • Empty weight: 5,050 kg (11,133 lb) equipped
  • Max takeoff weight: 7,400 kg (16,314 lb)
  • Powerplant: 4 × Gnome-Rhône Titan 7Kcrs 7-cylinder radial piston engine, 220 kW (300 hp) each


  • Maximum speed: 220 km/h (140 mph, 120 kn)
  • Range: 1,000 km (620 mi, 540 nmi)
  • Service ceiling: 5,000 m (16,000 ft)


  • Guns: 2 × twin 7.7mm (0.303in) machine-gun in nose and dorsal position and one single 7.7mm (0.303in) machine-gun in ventral position.
  • Bombs: up to 1050kg (2315lb)


  1. ^ a b c d e f g h Orbis 1985, p. 1755
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing.
This page was last edited on 2 July 2019, at 18:47
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.