Fairey Firefly ![]() Firefly FR .Mk4
A natural development of the Fulmar two-seat fighter, the Firefly was designed by a team led by H E Chaplin to meet specification N.5/40, an amalgamation of earlier requirements which had called for a carrier-based fighter with a turret. However, the turret was dropped, and when chief test pilot Chris Staniland flew the first Firefly I on December 22, 1941, it was a clean tandem-seater with manually-folding wings containing four 20-mm (0.79-in) cannon and retractable Youngman area-increasing flaps. At first there was no requirement for the type to be able to carry bombs or rockets. Full production started in August 1942.
Conversions included the NF.I, with American 3-cm AI radar (usually APS-6) in a ventral pod, with other changes including shrouded exhausts, and the FR.IA which was a Mk.I rebuilt almost to FR.1 standard. From the 471st aircraft the engine was the 1990-hp Griffon XII.
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A natural development of the Fulmar two‑seat fighter, the Firefly was designed by a team led by H E Chaplin to meet specification N.5/40, an amalgamation of the earlier requirements of N.8/39 and N.9/39 which had called for a carrier‑based fighter with a turret. However, the turret was dropped, and when chief test pilot Chris Staniland flew the first Firefly I on December 22, 1941, it was a clean tandem-seater with manually‑folding wings containing four 20‑mm (0.79‑in) cannon and retractable Youngman area‑increasing flaps. At first there was no requirement for the type to be able to carry bombs or rockets.
It was a stressed skin monoplane with folding elliptical wings housing four cannon and with the trailing edge with Youngman flaps which could be recessed into the wing.
Full production started in August 1942 with the first production F.I flying on 26 August 1942. Indian Air Force Firefly Mk.1 target tug
The Royal Canadian Navy employed 65 Fireflies of the Mk AS5 variety on board its own aircraft carriers between 1946 and 1954. The letters 'AS' stand for anti-submarine, which was the intended primary role of the RCN's Fireflies.
![]() Firefly AS.5
![]() Firefly U.9
The remaining 160 Mk 7s were all Firefly T.Mk 7 trainers. Firefly production eventually terminated in March 1956 with the delivery of the last of 24 new-build Firefly U.Mk 8 target drones, but 54 Mk 5s were also con-verted to this mission, these being known as Firefly U.Mk 9 aircraft. The U.8, U.9 and U.10 were all radio-controlled drones or targets. The Fairey Firefly 8 (Rolls-Royce Griffon 59) had four cameras in each wing-tip fairing to photograph missiles which are directed to its vicinity. For test purposes and other duties it may be flown by a crew of two-pilot and observer. Unlike the Firefly 7, from which it was developed, has an arrester hook fitted in the aperture under the fuselage. This is for arrested landings on aerodromes while under radio control. It has an 86-gallon fuel tank between the cockpits. The U.9 was the standard target for development and training with the Seaslug ship-to-air missile, while the U.10 was a similar rebuild of the AS.7.
![]() Firefly 9
All targets had large multi-angle high-speed camera pods on the wingtips.
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Firefly F.I
c/n 1-470 Engine: Rolls-Royce Griffon IIB, 1730 hp
Wingspan: 44 ft 6 in / 13.56 m
Wing area: 327.979 sq.ft / 30.47 sq.m
Length: 37 ft 7 in / 11.4 m
Height: 13 ft 7 in / 4.15 m
Empty weight: 9750 lb / 4422 kg
Loaded weight: 14,020 lb / 6359 kg
Wing loading: 42.85 lb/sq.ft / 209.0 kg/sq.m
Max speed: 316 mph / 509 kph / 275 kts
ROC: 1700 fpm / 518 m/min
Service ceiling: 28,000 ft / 8534 m
Range internal fuel: 580 mi / 933 km
Range w/max.fuel: 1720 km / 1069 miles
Armament: 4 x 20mm Hispano cannon
Bombload: 2000 lb / 906 kg
Crew: 2
Firefly I
c/n 471-
Engine: Rolls-Royce Griffon XII, 1990 hp
Wingspan: 44 ft 6 in / 13.56 m
Length: 37 ft 7 in / 11.4 m
Height: 13 ft 7 in / 4.15 m
Empty weight: 9750 lb / 4422 kg
Loaded weight: 14,020 lb / 6359 kg
Max speed: 316 mph / 509 kph
ROC: 1700 fpm / 518 m/min
Service ceiling: 28,000 ft / 8534 m
Range internal fuel: 580 mi / 933 km
Armament: 4 x 20mm Hispano cannon
Bombload: 2000 lb / 906 kg
Firefly II
Wingspan: 44 ft 6 in / 13.56 m
Length: 37 ft 7 in / 11.4 m
Height: 13 ft 7 in / 4.15 m
Firefly III
Wingspan: 44 ft 6 in / 13.56 m
Length: 37 ft 7 in / 11.4 m
Height: 13 ft 7 in / 4.15 m
Firefly FR.Mk 4
Engine:one 2,245-hp (1674-kW) Rolls-Royce Griffon 74
Wingspan 12.55 m (41 ft 2 in)
Wing area 30.66sq.m (330 sq ft)
Length 11.58 m (38 ft 0 in)
Height 4.24 m (l3ft 11 in)
Empty weight: 4388 kg (9,674 lb)
Loaded weight clean: 13,927 lb / 6317 kg
Maximum take-off: 7083 kg (15,615 lb)
Maximum speed: 591 km/h (367 mph) at 4265 m (14,000 ft)
ROC: 2050 fpm / 625 m/min
Service ceiling 9725 m (31,900 ft)
Range internal fuel: 760 mi / 1223 km
Range max: 2148 km (1,335 miles)
Armament: four 20-mm Hispano cannon
Bombload: 16 27-kg (60-lb) rockets or two 454-kg (l,000-lb) bombs.
AS.5
Engine One 2,259hp Rolls Royce Griffon 74
Wing span: 12.55 m (41 ft 2 in)
Length: 11.56 m (37 ft 11 in)
Height: 14 ft 4 in
Empty weight 9,674 lb
Gross weight: 7300 kg (16100 lb)
Maximum speed: 618 km/h (384 mph)
Initial Rate of Climb: 6 mins 50 secs to 10,000 ft
Ceiling: 28,400 ft
Endurance: 6.5 hours
Armament: 4 x 20 mm cannon Hispano
Bombload: 2 x 1,000 lb bombs or 16 x 60 lb rockets
Crew 2
Fairey Firefly Mk. 6 ASR
Engine: Rolls-Royce Griffon 74, 2245 hp
Wing Span: 41ft (12.50m)
Length: 37ft (11.28m)
Height: 15ft 6in(4.7m)
Range: 1,070 miles(1,772 km) w/ 2 @ 90Imp.Gal drop tanks
Speed: 345 mph (555 km/h)
Armament: two or four 20mm canon two drop tanks or ASR equipment
Bombload: 3000 lb / 1359 kg
Firefly 7
Engine: Rolls-Royce Griffon 74, 1145 hp
Wingspan: 44 ft 6 in / 13.56 m
Length: 38 ft 3 in / 11.65 m
Height: 14 ft 4 in / 4.37 m
Empty weight: 11,016 lb / 4997 kg
Loaded weight: 13,970 lb / 6337 kg
Bombload: 3000 lb / 1359 kg
Firefly 8
Engine: Rolls-Royce Griffon
Span: 43 ft 6 in
Length: 38 ft 3 in
![]() FR.5
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