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Supermarine Seagull (1921)

 

Supermarine Seagull (1921)

Seagull
Australian Seagull III at RAAF Base Richmond circa. 1928
Role Reconnaissance flying boat
Manufacturer Supermarine
First flight May 1921
Primary users Fleet Air Arm
Royal Australian Air Force
Number built 34
Developed from Supermarine Seal

The Supermarine Seagull was a British amphibian biplane flying boat developed from the Supermarine Seal by the Supermarine company. The Seagull was constructed of wood. The lower wing was set in the shoulder position and had two bays. The engine was mounted in a nacelle slung from the upper wing and powered a four-blade propeller in tractor configuration. The fuselage had an oval cross-section and had a planing bottom with two steps.

Contents

  • Design and development 1
  • Operational history 2
  • Operators 3
  • Surviving aircraft 4
  • Specifications (Seagull II) 5
  • Specifications (Seagull II) 6
  • See also 7
  • References 8
  • Bibliography 9
  • External links 10

Design and development

The prototype, which became known as the Seagull Mk I, was modified from an existing Supermarine Seal II in 1921. Only one aircraft was built. A Napier Lion II engine was fitted and there were modifications made to the nacelle.

Produced from 1922, the production aircraft, the Seagull Mk II, had a Napier Lion III engine, and these were supplied to the Air Ministry and Royal Navy. A total of 25 were built, although some of these were later modified.

The Seagull Mk III was the Australian version, built in 1925. These were similar to the Seagull II but with a Napier Lion V engine and radiators modified for tropical use. Six of these were supplied to the Royal Australian Air Force, and one other Seagull III was built for Japan.

One Seagull II was rebuilt and fitted with Handley-Page leading edge slots and twin fins and rudders in 1928. This was considered to be the Mark IV, although Supermarine never designated it as such. Three ex-service aircraft were later placed on the British Civil Register.

In 1930 work was started on a flying boat of similar size and layout but with a predominantly metal airframe, powered by a Bristol Jupiter IX engine in pusher configuration. First flown in 1933 This became known as the Seagull V and later as the Walrus.

Operational history

The type was used operationally as a fleet spotter by 440 (Fleet Reconnaissance) Flight, operating from HMS Eagle. They were superseded in 1925 by the Fairey IIId. The Seagull II was the first British aircraft to be catapult launched in 1925. The crew was normally three (Pilot, Observer, and Radio-Operator). The sole armament was a .303 in (7.7 mm) Lewis gun.

Nine Seagulls were bought by the Royal Australian Airforce in 1926 and 1927. These were used to carry out a photographic survey of the Great Barrier Reef.[1]

Operators

 Australia
 Japan
 United Kingdom

Surviving aircraft

  • The Fleet Air Arm Museum owns the front hull of an unknown Seagull. It was in use until 1974 as a garden shed, and presented to the museum in exchange for a new shed. It is currently on long-term loan to Solent Sky, an air museum in Southampton.[2]
  • The Royal Air Force Museum London has a Seagull V on display in their Battle of Britain hall. [3]

Specifications (Seagull II)

Data from Supermarine Aircraft since 1914 [4]

General characteristics
  • Crew: Three (pilot, wireless operator & observer)
  • Length: 34 ft 6 in (10.51 m)
  • Wingspan: 45 ft 11 in (13.99 m)
  • Height: 13 ft 6 in (4.11 m)
  • Wing area: 605 ft² (56.2 m²)
  • Empty weight: 3,691 lb (1,674 kg)
  • Loaded weight: 5,462 lb (2,477 kg)
  • Powerplant: 1 × Napier Lion II 12-cylinder water-cooled W-block piston engine, 480 hp (358 kW)

Performance

  • Maximum speed: 80 mph at sea level (70 knots, 129 km/h)
  • Service ceiling: 9,000 ft (2,743 m)
  • Endurance: 3½ hours
  • climb to 3,000 ft (915 m): 6.8 min
Armament

Specifications (Seagull II)

Data from Thetford 1982, p.319

General characteristics
  • Crew: Three (pilot, wireless operator and gunner)
  • Length: 37 ft (11.28 m)
  • Wingspan: 46 ft (14.02 m)
  • Height: 14 ft (4.26 m)
  • Wing area: 593 ft² (55.11 m²)
  • Empty weight: 3,897 lb (1,768 kg)
  • Loaded weight: 5,668 lb (2, 571 kg)
  • Powerplant: 1 × Napier Lion III 12-cylinder water-cooled W-block piston engine, 450 hp (337 kW)

Performance

Armament

See also

Related development
Related lists

References

  1. ^ Brown 1972, p.27.
  2. ^ "Supermarine Seagull". Solent Sky. Retrieved December 15, 2012. 
  3. ^ "Supermarine Seagull V". Royal Air Force Museum. Retrieved October 30, 2015. 
  4. ^ Andrews and Morgan 1987, p.81.

Bibliography

  • Andrews, C.F.; Morgan E.B. (1987). Supermarine Aircraft since 1914. London: Putnam.  
  • Brown, David. "Supermarine Walrus I & Seagull V Variants". Aircraft in Profile, Volume 11. Windsor, Berkshire, UK: Profile Publications Ltd., 1972.
  • Kightly, James and Wallsgrove, Roger. Supermarine Walrus & Stranraer. Sandomierz, Poland/Redbourn, UK: Mushroom Model Publications, 2004. ISBN 83-917178-9-5.
  • Shelton, John (2008). Schneider Trophy to Spitfire - The Design Career of R.J. Mitchell (Hardback). Sparkford: Hayes Publishing.  
  • Thetford, Owen. British Naval Aircraft Since 1912. London: Putnam, 1982 (5th ed.) ISBN 0 370 30021 1

External links

  • British Aircraft Directory

Media related to at Wikimedia Commons

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