Fairey Firefly IIM

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Firefly IIM
Belgian Fairey Firefly Y-17 from 3/II/2 Aé (Red Cocottes) Squadron near its home base at Nivelles. Fairey c/n F-1505 was delivered from Fairey Hayes (UK) on 21 August 1931.
Role Fighter
Manufacturer
Fairey Aviation Company Limited
Designer Marcel Lobelle
First flight 5 February 1929
Introduction 1931
Primary users Belgium
USSR
Number built 91

The Fairey Firefly IIM was a British fighter of the 1930s. It was a single-seat, single-engine

Belgian Air Force throughout the 1930s until the outbreak of World War II
.

Design and development

The Firefly was a private-venture design, penned by

Specification F.20/27 for a single-seat interceptor. It first flew on 5 February 1929.[1]

The Firefly II competed for the

RAF contract against the Hawker Fury, showing superior speed but was criticised for having heavier controls.[1]
Crucially, it retained a mainly wooden structure despite the Air Ministry's demands for metal structures. This led to the Fury being selected. Afterwards, the prototype was rebuilt and renamed Firefly IIM, the "M" denoting the all-metal construction of the rebuilt machine.

A revised prototype with longer-span wings, the Firefly III was built to

trainer by the RAF's High Speed Flight preparing for the 1931 Schneider Trophy race.[4]

Operational history

A contract was won for 25 IIM aircraft for Belgium's

Aviation Militaire, followed by a contract for a further 62 to be constructed by Avions Fairey, Fairey's Belgian subsidiary. The Belgian aircraft served briefly in the Second World War
from May to June 1940.

Two of the Belgian aircraft were converted to Firefly IV, with 785 hp (585 kW) Hispano-Suiza 12Xbrs engines but the improvement was not deemed sufficient to warrant development. One was restored to its original form, while the other passed to Fairey for trials. One aircraft was supplied to the Soviet Union.

Operators

 Belgium
  • Belgian Air Force
 United Kingdom
 Soviet Union
  • Soviet Air Force
    – One Firefly Mk IIM, used for tests and trials.

Variants

Fairey Firefly II
Single-seat fighter prototype, powered by a 480 hp (360 kW) Rolls-Royce Kestrel piston engine. One built.
Fairey Firefly IIM
Single-seat single-engine fighter aircraft, of all-metal construction, equipped with resigned tail surfaces and revised engine cooling system.
Fairey Firefly III
Single-seat shipboard fighter prototype. One built.
Fairey Firefly IIIM
The Fairey Firefly III was rebuilt with all-metal construction and redesignated Firefly IIIM.
Fairey Firefly IV
Two Belgian Firefly IIs were converted, and fitted with the 785 hp (585 kW) Hispano-Suiza 12Xbrs engine.

Specifications (Firefly IIM)

Data from The Complete Book of Fighters[5]

General characteristics

  • Crew: 1
  • Length: 24 ft 8 in (7.52 m)
  • Wingspan: 31 ft 6 in (9.60 m)
  • Height: 9 ft 4 in (2.84 m)
  • Wing area: 236.8 sq ft (22.00 m2)
  • Empty weight: 2,387 lb (1,083 kg) equipped
  • Gross weight: 3,285 lb (1,490 kg)
  • Max takeoff weight: 3,404 lb (1,544 kg) [6]
  • Powerplant: 1 ×
    Rolls-Royce F.XIS
    V-12 liquid-cooled piston engine, 480 hp (360 kW)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 175 mph (282 km/h, 152 kn) at sea level, 223 mph (194 kn; 359 km/h) at 13,125 ft (4,000 m)
  • Range: 240 mi (390 km, 210 nmi) [4] (Firefly II)
  • Service ceiling: 30,800 ft (9,400 m) [7]
  • Time to altitude: 10 minutes 55 seconds to 20,000 ft (6,000 m)

Armament

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Notes

  1. ^ a b c Mason 1992, p. 212.
  2. ^ Willis Aeroplane August 2020, p. 92.
  3. ^ Taylor 1988, pp. 175–176.
  4. ^ a b Mason 1992, p. 213.
  5. ^ Green and Swanborough 1994, p.198.
  6. ^ Taylor and Alexander 1969, p. 47.
  7. ^ Taylor 1988, p. 179.

Bibliography

External links