Farman F.211

Day-Night Four-Engined Heavy Bomber Prototype [ 1932 ]

The Farman F.211 was a French interwar heavy bomber product that did not see serial production.

Authored By: Staff Writer | Last Edited: 08/07/2018 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

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In 1929, the French Air Ministry detailed a new specification calling for a four-seat night bomber with inherent daytime capabilities. The Farman F.211 was developed by Farman Aviation Works in response and took to the air for the first time in early 1932. The large aircraft was powered by four engines arranged in a unique "push-pull" configuration (detailed below). The design was not adopted by the French Air Force and remained in prototype status for the duration of its flying life. Attention was then moved to the dimensionally larger F.220 which also brought along with it more power from its engines and this model found considerably more success.

The F.211 was very much a product of the time - it held an ungainly appearance seen in many of the interwar bombers put forth by various companies of the world. The nose section was largely glazed over to provide meaningful vision "out-of-the-cockpit" for its multi-person crew. A "tail-dragger", wheeled undercarriage was used but fixed in place during flight. The high-wing mounting of the mainplanes was a step in the right aerodynamic direction but the quadruple engine configuration was set in two nacelles (one to either side of the fuselage) and arranged with one ahead of the other - one engine "pulling" and the other "pushing". The nacelles were further mounted on wingstubs fitted along the lower sides of the fuselage and had to be braced to the underside of the wing mainplanes by struts.

Power to the bomber came from 4 x Gnome-Rhone "Titan" 7Kcrs 7-cylinder radial piston engines developing 300 horsepower each. Maximum speed for the aircraft was 140 miles per hour with a range out to 620 miles and a service ceiling up to 16,405 feet.

Overall dimensions of the aircraft included a length of 15.9 meters, a wingspan of 23 meters and a height of 4.2 meters. Empty weight was 11,135 lb against a Maximum Take-Off Weight of 16,315 lb. Internally, the bomber could carry a war load of 2,315 lb. Defense was through 1 x 7.7mm twin machine guns at the nose, another station held dorsally, and a single 7.7mm machine gun at a ventral station.

With French authority disinterest in the F.211 model, Farman pursued the F.212, an improved form now fitting Gnome-Rhone 7Kds radial piston engines of 350 horsepower each. The war load was also increased to 3,085 lb. This version appeared in 1934 but also only ever managed to reach a prototyping stage before the end.

The F.215 was a proposed passenger airliner variant intended to seat twelve in comfort and based on the F.211/F.212 design. This model was not furthered into a physical form. The dimensionally larger F.220 model series of 1935 found more success - it was produced in eighty examples into 1938 and encompassed a variety of models based on the F.220 lineage including the F.222 which became France's largest bomber of the Inter-war period.©MilitaryFactory.com

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Specifications

Service Year

1932

Origin

France

Status

CANCELLED
Development Ended.

Crew

4

Production

1
UNITS

Farman Aviation Works - France

(View other Aviaton-Related Manufacturers)

France (cancelled)

(OPERATORS list includes past, present, and future operators when applicable)

✓ Ground Attack (Bombing, Strafing)
Ability to conduct aerial bombing of ground targets by way of (but not limited to) guns, bombs, missiles, rockets, and the like.

✓ X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.

Length

52.5 ft
(16.00 m)

Width/Span

75.5 ft
(23.00 m)

Height

13.8 ft
(4.20 m)

Empty Wgt

11,133 lb
(5,050 kg)

MTOW

16,314 lb
(7,400 kg)

Wgt Diff

+5,181 lb
(+2,350 kg)

(Showcased structural values pertain to the base Farman F.211 production variant)

Installed: 4 x Gnome-Rhone 7Kcrs "Titan" 7-cylinder radial piston engine developing 300 horsepower each.

Max Speed

137 mph
(220 kph | 119 kts)

Ceiling

16,404 ft
(5,000 m | 3 mi)

Range

621 mi
(1,000 km | 1,852 nm)

♦ MACH Regime (Sonic)

Sub

Trans

Super

Hyper

HiHyper

ReEntry

♦

(Showcased performance specifications pertain to the base Farman F.211 production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)

STANDARD:
2 x 7.7mm machine guns in nose position (twin-gunned mount).
2 x 7.7mm machine guns in dorsal position (twin-gunned mount).
1 x 7.7mm machine gun in ventral position (single-gunned mount).

OPTIONAL:
Up to 2,315 pounds of conventional drop ordnance.

Supported Types

Graphical image of an aircraft medium machine gun

Graphical image of an aircraft conventional drop bomb munition

(Not all ordnance types may be represented in the showcase above)

Hardpoint Mountings: 0

F.211 - Base Series Designation; Gnome-Rhone 7Kcrs "Titan" engines of 300 horsepower.

F.212 - Improved variant; fitted with Gnome-Rhone 7Kds radial piston engines of 350 horsepower; bombload of 3,085 pounds.

F.215 - Proposed passenger hauler with seating for twelve.

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