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Fairey Fleetwing

Two-Seat Carrierborne Reconnaissance Biplane Prototype

The Fairey Fleetwing failed to out-duel the Hawker Osprey in trials for the Fleet Air Arm service of Britain.
Authored By: Staff Writer | Edited: 9/11/2018
National Flag Graphic


Year: 1929
Status: Cancelled
Manufacturer(s): Fairey Aviation Company - UK
Production: 1
Capabilities: Fighter; Ground Attack; Navy/Maritime; Reconnaissance (RECCE); X-Plane;
Crew: 2
Length: 29.36 ft (8.95 m)
Width: 37.01 ft (11.28 m)
Height: 11.42 ft (3.48 m)
Weight (Empty): 3,307 lb (1,500 kg)
Weight (MTOW): 4,740 lb (2,150 kg)
Power: 1 x Rolls-Royce Kestrel IIMS V-12 water-cooled supercharged inline engine developing 600 horsepower and driving a two-bladed propeller at the nose.
Speed: 169 mph (272 kph; 147 kts)
Ceiling: 25,000 feet (7,620 m; 4.73 miles)
Range: 500 miles (805 km; 435 nm)
Rate-of-Climb: 1,190 ft/min (363 m/min)
Operators: United Kingdom (cancelled)
In the mid-1920s, the British Air Ministry, on behalf of the Fleet Air Arm (FAA), drew up a new requirement in "Specification 22/26" calling for a twin-seat, carrier-based reconnaissance aircraft. Fairey Aviation Company was one of the respondents with what became their Fairey "Fleetwing" biplane product. The aircraft competed unsuccessfully against the Hawker "Osprey" for the specification and this resulted in just one aircraft being completed.

Design of the Fleetwing is attributed to Marcel Lobelle.

The Fleetwing utilized a traditional biplane wing arrangement but its upper element was considerably larger than the lower. "N-style" struts were used to connect the two planes outboard of the fuselage. The crew of two was seated in tandem in separate cockpits with the pilot located aft / under the upper wing section. The engine was set within a streamlined nose section and the tail utilized a traditional arrangement. The undercarriage was fixed and only the two main legs were wheeled. Dimensions included a length of 29.3 feet, a height of 11.4 feet and a wingspan of 37 feet. Gross weight was 4,740lb. Power was from a single Rolls-Royce F.XI "Kestrel I" series water-cooled inline engine outputting 480 horsepower. This drove a two-bladed propeller at the nose.

A product of its time, construction of the aircraft was mixed, involving wood, canvas and metal. Other consistent qualities were its "tail-dragger", fixed undercarriage and open-air cockpits.

Proposed armament was a 7.7mm Vickers machine gun in a fixed, forward-firing fuselage position (portside, synchronized to fire through the spinning propeller blades) along with a 7.7mm Lewis Machine Gun on a specialized mounting in the rear cockpit. 4 x 20lb bombs could be carried under the portside wing for light bombing duties.

The prototype Fleetwing went airborne for the first time on May 16th, 1929. The following month, the FAA conducted its deck trials leading to the Fleetwing being fitted with all-metal wing mainplanes as well as the Rolls-Royce "Kestrel IIMS" water-cooled supercharged series engine of 600 horsepower. Additional trials were held in October of 1929 which led to the Hawker product (a navalized version of the Hawker Hart) being selected ahead of the Fleetwing.

As built, the Fleetwing recorded a maximum speed of 169 miles-per-hour and held a rate-of-climb of 1,190 feet-per-minute.


1 x 7.7mm Vickers machine gun in portside fuselage mounting synchronized to fire through the spinning propeller blade.
1 x 7.7mm Lewis Machine Gun on trainable mounting in rear cockpit.

4 x 20lb conventional drop bombs held under portside wing.

Graphical image of an aircraft medium machine gun
Graphical image of an aircraft conventional drop bomb munition

Variants / Models

• Fleetwing - Base Project Name; single flyable example completed.
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