Designed by Marcel 
         Lobelle, the prototype Fairey Day Bomber, as it was then known, 
         originated as the company's submission to Specification P.27/32 for a 
         two-seat single-engine monoplane bomber capable of carrying 1,000 lbs 
         (454 kg) of bombs for 1,000 miles (1609 km) at 200 mph (322 km/h) which 
         was ordered as a prototype on June 11, 1934. Provision for a radio 
         operator/air gunner was made later, to man a Lewis or Vickers 'K' 
         dorsal machine-gun.This performance was to be bettered by Fairey's 
         aircraft, which was competing against design proposals from Armstrong 
         Whitworth, Bristol and Hawker, but only the Armstrong Whitworth's 
         A.W.29 joined Fairey's prototype in receiving orders. Fairey's 
         contender won the competition, but a first production contract for 155 
         aircraft, to the revised Specification P.23/35, had been placed in 1935 
         even before the prototype had flown. The Battle had accommodation for a 
         crew of three comprising pilot, bomb-aimer/observer, and radio 
         operator/gunner. The first production aircraft was built, like the 
         prototype, at Hayes and flew from the Great West Aerodrome (now part of 
         Heathrow Airport), on 14 April 1937. It was used for performance trials 
         during which it achieved 243 mph (391 km/h) at 16,200 ft (4940 m). A 
         range of 1,050 miles (1690 m) was flown with maximum bomb load.
         The second and 
         subsequent production aircraft came from a production line established 
         at a new purpose-built factory at Heaton Chapel, Stockport, and it was 
         for the Battle that Rolls-Royce received its launching order for the 
         famous 1,030 hp (768 kW) Merlin I engine, which powered the first 136 
         Fairey-built aircraft.
         The aircraft's light 
         alloy and stressed skin construction was a 'first' for Fairey, and the 
         Battle proved to be extremely robust. In general it proved popular with 
         the test pilots at the Aircraft and Armament Experimental Establishment 
         at Martlesham Heath, and at the Royal Aircraft Establishment at 
         Farnborough. It was said to be very easy to fly but the elevator was 
         heavy on take-off; on the other hand the Royal Aircraft Establishment 
         considered the elevator over-light at low speeds. Engine-off stall was 
         described as 'innocuous', but the accommodation came in for some 
         criticism: although the pilot's cockpit was considered to be roomy and 
         comfortable with reasonable forward vision, it could sometimes become 
         extremely hot. The rear gunner, behind the pilot, had his own problems: 
         the screen intended to protect him from the slipstream was badly 
         designed and it shape deflected a downdraught into his face, while the 
         rear vision was described as 'poor'. 
         By the end of 1937, 
         Fairey had built 85 Battles, and the first squadron to receive the new 
         bomber in May 1937 was No.63 at Upwood, Huntingdonshire, where it 
         replaced the Hawker Audax. Other squadrons which re-equipped that year 
         were Nos. 52, 88, 105 and 226.
         As new orders for 
         Battles were placed, production sub-contracts were awarded to Austin 
         Motors at Longbridge, Birmingham. Meantime, the last 19 Battles of the 
         initial Fairey order for 155 were provided with Merlin II engines, and 
         these were fitted also to the Austin-built aircraft. The first Battle 
         from the Longbridge factory flew in July 1938, and 29 had been 
         completed there by the end of the year. By March the following year 
         Austin was producing more than 30 Battles a month, but even then the 
         programme was running late. After 60 Austin-built Battles had been 
         completed, the Merlin II engine was introduced on the production line.
         By the outbreak of 
         World War II more than 1,000 Battles had been delivered, and aircraft 
         of No. 226 Squadron were the first to be sent to France as part of the 
         Advanced Air Striking Force. It was here that the Battle's inability to 
         defend itself against enemy fighters became obvious. On armed daylight 
         reconnaissance missions the type occasionally tangled with Bf 109s, and 
         although one of the latter was destroyed by a Battle's rear gunner in 
         September 1940, the light bombers invariably suffered heavy casualties.
         As the period of the 
         so-called 'phoney war' came to an end, the Battle squadrons were thrown 
         in on 10 May 1940 to try to stop the advancing German ground forces. 
         Without fighter escort, and attacking from a height of only 250 ft (76 
         m) with delayed-action bombs the Battles came under heavy ground fire, 
         losing 13 of the 32 aircraft sent on the mission, while all the others 
         were damaged. The next day seven out of eight were lost, and on 12 May 
         five Battles of No.12 Squadron, flown by volunteer crews, attacked two 
         vital road bridges over the Albert Canal. In the face of extremely 
         heavy ground fire the attack was pressed home and one bridge seriously 
         damaged, but at a cost of all five aircraft. The first RAF Victoria 
         Crosses of World War II were awarded posthumously to Flying Officer D.E. 
         Garland and his observer, Sergeant T. Gray, who led the formation.
         Further heavy losses 
         came on 14 May, when 35 out of 63 Battles failed to return from attacks 
         against bridges and troop concentrations. These losses marked the end 
         of the Battle's career as a day bomber, and although a few remained in 
         front-line service until late 1940 the survivors were mostly diverted 
         to other duties. The most important of these was for training, and 100 
         were built as dual-control trainers with separate cockpits, while 266 
         target-towing variants were also supplied.
         The last production 
         aircraft, Austin-built, was a target tug, and it was delivered on 2 
         September 1940. It brought total Battle production to 2,185 including 
         the prototype, 1,156 being built by Fairey and 1,029 by Austin Motors.
         Canada used a large 
         number of Battles for training and target towing in the Commonwealth 
         Air Training Plan, the first being supplied to the Royal Canadian Air 
         Force at Camp Borden in August 1939. They were the vanguard of 739 of 
         these aircraft, this total including seven airframes for instructional 
         purposes. Under the Empire Air Training Scheme (EATS), Australia took 
         delivery of 366 of the type between June 1940 and December 1943 
         consisting of four British-built Battles and 360 assembled in 
         Australia, including 30 target tugs, while other export customers were 
         Belgium (18), Turkey (28), South Africa (161) and Eire (Ireland), where 
         an RAF aircraft which landed at Waterford in 1941 was interned and 
         later taken over by the Air Corps.
         A number of Battles 
         were used as test-beds for such engines as the Napier Dagger and Sabre; 
         Bristol Hercules and Taurus; Rolls-Royce Merlin X and the 1,280 hp (955 
         kw) Merlin XII with chin radiator; and the Fairey Prince. Other Battles 
         were used for experiments with various types of propellers.
         Variants
         Battle B.Mk I - First 
         production type with one Rolls-Royce Merlin I 12-cylinder Vee 
         liquid-cooled piston engine with a single stage, single speed 
         supercharger and rated at 890 hp (656 kW) for take-off at sea level 
         using 87 octane fuel, and developing a maximum power rating of 1,030 hp 
         (768 kW) at 3,000 rpm at 16,250 ft (4940 m) for short periods using 87 
         octane fuel driving a three bladed dual pitch airscrew. 136 aircraft 
         built.
         Battle B.Mk II - 
         Identical to the Battle Mk I but fitted with one Rolls-Royce Merlin II 
         12-cylinder Vee liquid-cooled piston engine with a single stage, single 
         speed supercharger and rated at 880 hp (664 kW) for take-off at sea 
         level, and developing a maximum power rating of 1,440 hp (1074 kW) at 
         3,000 rpm at 5,500 ft (1680 m) for short periods using 87 octane fuel 
         driving a three bladed dual pitch airscrew. The Merlin II replaced the 
         unsatisfactory ramp type of cylinder head with a Kestrel style flat 
         combustion chamber. 78 aircraft built.
         Battle B.Mk III - 
         Identical to the Battle Mk II but fitted with one Rolls-Royce Merlin 
         III 12-cylinder Vee liquid-cooled piston engine with a single stage, 
         single speed supercharger and rated at 880 hp (664 kW) for take-off at 
         sea level, and developing a maximum power rating of 1,440 hp (1074 kW) 
         at 3,000 rpm at 5,500 ft (1680 m) for short periods using 87 octane 
         fuel driving a three bladed dual pitch airscrew. The Merlin III was 
         adapted for the use of a constant-speed propeller and a constant-speed 
         unit.
         Battle B.Mk IV - 
         Identical to the Battle Mk III but fitted with one Rolls-Royce Merlin 
         IV 12-cylinder Vee liquid-cooled piston engine with a single stage, 
         single speed supercharger and rated at 1,030 hp (768 kW) for take-off 
         and 1,440 hp (1074 kW) at 3,000 rpm at 5,500 ft (1680 m) for short 
         periods using 87 octane fuel driving a three bladed dual pitch 
         airscrew. This mark of Merlin engine differs by using a pressurised 70 
         percent water and 30 percent ethylene-glycol mixture for engine 
         cooling.
         Battle B.Mk V - 
         Identical to the Battle Mk IV but fitted with one Rolls-Royce Merlin V 
         12-cylinder Vee liquid-cooled piston engine with a single stage, single 
         speed supercharger and rated at 1,030 hp (768 kW) for take-off and 
         1,440 hp (1074 kW) at 3,000 rpm at 5,500 ft (1680 m) for short periods 
         using 87 octane fuel driving a three bladed dual pitch airscrew. 
         
         Battle TT.Mk I - Last 
         production variant for use as target tug, with hydraulic winch on port 
         side of fuselage and drogue stowage box below rear fuselage. Production 
         started in February 1940 with all being built by Austin Motors and 
         using Rolls-Royce Merlin III engines. 200 built by Fairey and 66 by 
         Austin.
         Battle TT - Battles 
         that were converted to target tugs. Number unknown.
         Battle T - After the 
         Fairey Battle was retired from frontline service, several training 
         units used the type unmodified, but rear-seat visibility was inadequate 
         leading to the development of a special dual-control trainer. This 
         designation includes converted dual-control trainers as well. Numbers 
         unknown.
         Battle T.Mk I - 
         Starting in 1939 a special dual-control trainer with similar tandem 
         cockpits was produced. 200 built by Austin.
         Battle IT - Fairey 
         Battle's modified to carry a Bristol Type I single-gun dorsal turret in 
         place of rear cockpit. Two prototypes were tested in UK and another 204 
         aircraft were converted in Canada.
         Battle IIT - A single 
         RCAF aircraft with a Bristol Type I single-gun dorsal turret and fitted 
         with a Wright GR-1820-G3B Cyclone 9-cylinder radial engine using 91 
         octane fuel rated at 875 hp (652 kW) for take-off with a normal power 
         rating of 840 hp (626 kW) at 8,700 ft (2650 m).
         Belgian Battle - 
         Sixteen Fairey Battles ordered for the Belgian Aéronautique Militaire 
         in 1938, and assembled by Avions Fairey at Gosselies from Stockport 
         built components and equipped with the Rolls-Royce Merlin III engine. 
         They differed from the British Battles by having the radiator placed 
         further forward. Based in Evère-Bruxelles with the 5e Escadrille, 
         Groupe III, 3e Regiment, they took part in a single mission against 
         bridges over the Albert Canal in May 1940.
         Experimental - This 
         category includes many one-off experimental aircraft used for testing 
         various engines and propellers. Engines tested include the Napier 
         Dagger and Sabre, the Bristol Hercules (fixed down and faired in 
         undercarriage) and Taurus, the Rolls-Royce Merlin X and XII with chin 
         radiator and the Fairey P.24 Prince.
         Specifications (Fairey 
         Battle Mk I)
         Type: Three Seat 
         Light Bomber, Target Tug & Gunnery Trainer 
         Accommodation/Crew: 
         Pilot, Bomb-aimer/Observer, and Wireless Operator/Gunner.
         Design: Design 
         Team lead by Marcel Lobelle 
         Manufacturer: 
         The Fairey Aviation Company Limited based in Hayes, Middlesex with 
         production facilities in Heaton Chapel, Stockport (Cheshire). A shadow 
         factory was established at Austin Motors Limited in Cofton Hackett, 
         Longbridge (Birmingham) building aircraft to Specification 32/36. 16 
         aircraft were assembled by Avions Fairey in Gosselies, Belgium.
         Powerplant: One 
         Rolls-Royce Merlin I piston engine rated at 890 hp (664 kW) for 
         take-off at sea level, and developing a maximum power rating of 1,030 
         hp (768 kW) at 3,000 rpm at 16,250 ft (4940 m) for short periods. A 
         three-bladed Hamilton Standard (de Havilland built) dual pitch 
         propeller was standard. Settings were fully fine or fully coarse even 
         though they were only 20º apart. At altitude, selecting fully coarse 
         cut the Merlin's rpm in half. When 100 Octane fuel became available it 
         enabled the boost pressure to double from 6 lbs/square inch to 9 - 12 
         lbs/square inch allowing the same engine to make a maximum power rating 
         of over 1,300 hp (970 kW).
         Performance: 
         Maximum speed 257 mph (414 km/h) at 20,000 ft (6100 m); cruising speed 
         210 mph (338 km/h); service ceiling 25,000 ft (7620 m); initial climb 
         rate 920 ft (280 m) per minute.
         Fuel Capacity: 
         212 Imp gal (254,6 US gal), plus 45 Imp gal (54 US gal) in fuselage 
         tank, plus 33 Imp gal (39.6 US gal) in wing tank.
         Oil Capacity: 
         Unknown.
         Range: 1,000 
         miles (1609 km) at 16,000 ft (4875 m) at 200 mph (322 km/h) with 1,000 
         lbs (454 kg) of bombs.
         Weights & Loadings: 
         Empty 6,647 lbs (3015 kg) with a maximum take-off weight of 10,792 lbs 
         (4895 kg).
         Dimensions: Span 
         54 ft 0 in (16.46 m); length 42 ft 1 3/4 in (12.85 m); height 15 ft 6 
         in (4.72 m); wing area 422.0 sq ft (39.20 sq m); wing aspect ratio 
         6.91.
         Defensive Armament: 
         One forward firing 7.7 mm (0.303 in) Browning machine-gun in in the 
         starboard wing with a 400 round magazine and combat ciné camera and one 
         rearward firing 7.7 mm (0.303 in) Vickers 'K' machine-gun in the rear 
         cockpit with 485 rounds. Early aircraft had a 7.7 mm (0.303 in) Lewis 
         machine-gun until replaced by the Vickers 'K' machine-gun. During the 
         Battle for France, crews often hastily added a ventral gun below the 
         fuselage just aft of the wing. This gun was aimed by the third crew 
         member using a mirror sight.
         Disposable Ordnance: Up to 1,000 lbs (454 kg) of bombs carried 
         internally in four inner wing bomb cells. The internal wing bomb cells 
         had racks that were lowered and attached to the bombs and then 
         hydraulically raised the bombs into their cells. These hydraulic racks 
         could also be extended below the wing for dive bombing attacks. A 
         single 250 lbs (114 kg) bomb could be carried externally under each 
         wing at the expense of range.
         
          - 
          
4 × 250 lbs (114 kg) 
          bombs in the wing bomb cells, and
            
 
          - 
          
2 × 250 lbs (114 kg) 
          bombs on underwing racks (with reduced range) 
 
         
         Variants: Battle 
         B.Mk I, B.Mk II, B.Mk III, B.Mk IV, B.Mk V, TT.Mk I.
         Equipment/Avionics: 
         R.1082 radio and T.1083 transmitter.
         History: First 
         flight (prototype), 10 March 1936; production Mk I June 1937; final 
         delivery January 1941; withdrawn from service 1949.
         Operators: 
         United Kingdom (RAF), Canada (RCAF), Australia (RAAF), South Africa (SAAF), 
         Belgium (18), Turkey (28), Ireland (1), Greece (12), Poland (1 - never 
         delivered).