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Fairey Firefly




The Fairey Firefly was a World War II -era Carrier-borne Fighter Aircraft of the Fleet Air Arm . It was superior in performance and firepower to its predecessor, the Fairey Fulmar , but did not enter operational service until towards the end of the war. It remained a mainstay of the FAA until 1950.

The Firefly was designed by H.E. Chaplin at Fairey Aviation in 1940 and in June of that year the Admiralty ordered 200 of the aircraft to meet Specification N.5/40. The prototype of the Mk.I Firefly flew on December 22 , 1941 . Although it was two tons heavier than the Fulmar (due largely to its armament of two 20 mm cannon in each wing), the Firefly was 40 mph (64 km/h) faster due to improved Aerodynamics and a more powerful engine; the 1,730 hp (1290 kW) Rolls-Royce Griffon IIB. In March 1943 the first Firefly Mk.Is were delivered but they did not enter operational service until July 1944 when they equipped No. 1770 Squadron aboard HMS ''Indefatigable'' .

Fireflies provided air cover during the sinking of the German Battleship ''Tirpitz'' in 1944.

Two variants of the Mk.I Firefly were built; 429 "fighter" Firefly F Mk.Is, built by Fairey and General Aircraft Ltd , and 376 "fighter/ Reconnaissance " Firefly FR Mk.Is (which were fitted with the ASH detection Radar ). The last 334 Mk.Is built were upgraded with the 1,765 hp (1,316 kW) Griffon XII engine.

Only 37 Mk.II Fireflies were built, all of which were Night Fighter Firefly NF Mk.IIs. They had a slightly longer fuselage than the Mk.I and had modifications to house their airborne interception (AI) radar. They were superseded by the "night fighter" Firefly NF Mk.I variant. A Firefly '''Mk.III''' was proposed, based on the Griffon 61 engine, but never entered production. The Firefly '''Mk.IV''' was equipped with the 2,330 hp (1,740 kW) Griffon 72 engine and first flew in 1944, however it did not enter service until after the end of the war.


SPECIFICATIONS (MK.I)


  plane Or Copter plane
  jet Or Prop prop
  crew Two
  length Main 37 ft 7 in
  length Alt 1146 m
  span Main 44 ft 6 in
  span Alt 1356 m
  height Main 13 ft 7 in
  height Alt 414 m
  area Main ft&2
  area Alt m&2
  empty Weight Main lb
  empty Weight Alt kg
  loaded Weight Main lb
  loaded Weight Alt kg
  max Takeoff Weight Main 14,020 lb
  max Takeoff Weight Alt 6,359 kg
  engine (prop) Rolls-Royce Griffon IIB
  type Of Prop liquid-cooled V-12
  number Of Props 1
  power Main 1,730 hp
  power Alt 1,290 kW
  max Speed Main 316 mph at 14,000 ft
  max Speed Alt 509 km/h at 4,300 m
  range Main 1,070 miles with auxiliary tanks
  range Alt 1,722 km
  ceiling Main 28,000 ft
  ceiling Alt 8,530 m
  climb Rate Main ft/min
  climb Rate Alt m/s
  loading Main lb/ft&2
  loading Alt kg/m&2



OPERATORS

  • Australia, Canada, Denmark, Ethiopia, Netherlands, Sweden, Thailand, United Kingdom,



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