Bristol Type 14 / F2B / Curtiss B-3 / B-4 / XB-1 / XB-2 / USAO-1 / O-1 / B-1 / Dayton-Wright XB-1A / USB-1

F.2B

In March 1916 the design was begun of a 120 hp Beardmore powered tractor replacement for the B.E. pusher scouts. The type was designated R.2A and was intended to be armed with one wing mounted Lewis machine gun and another for the observer on a Scarff ring. At the same time a similar design using the 150 hp Hispano Suiza was produced, but lack of power from the Beardmore caused the designer, Captain Frank Barnwell, to produce a new design using the new 190 hp Rolls Royce Falcon and with the designation F.2A. This was an unequal span two bay biplane with its fuselage, tapered to the rear mounted mid way between the wings.
Two prototypes were completed by the early autumn of 1916, one with the Rolls-Royce Falcon engine (A3303), the other with the 150 hp Hispano Suiza. Prototype A3303 was first flown at Filton on 9 September 1916, and after successful trials a first batch of 50 Rolls Royce powered production F.2As was ordered with a synchronized Vickers machine gun mounted in the top of the engine cowling in addition to the Scarff mounted Lewis, entering service with No.48 squadron in February 1917.

Meanwhile the second, Hispano Suiza powered, prototype had been modified to improve the pilot’s view and given a larger fuel tank, increased ammunition stowage and a modified lower wing affording a small increase in gross area. New horizontal tail surfaces of greater span and increased aspect ratio were introduced. Further production machines were ordered with the 190 hp Rolls-Royce Falcon I and the designation F.2B; after the first 150 the 220 hp Falcon II was substituted for a further 50, and production was intended to continue with the 275 hp Falcon III. F.2B deliveries began on 13 April 1917, and the success of this type led to the decision to re-equip all RFC fighter-reconnaissance squadrons with F.2Bs.
By the autumn of 1917 production of the aircraft was outstripping that of the engine, and the 200 hp Hispano Suiza was substituted in the aircraft intended for reconnaissance squadrons, but this proved unreli¬able and was replaced by the 200 hp Sunbeam Arab in a modified nose. Some later F.2Bs were fitted with the 220 hp Siddeley Puma and a number of subcontractors were given contracts to produce the F.2B, 3050 being completed by the end of 1918.

Production continued until September 1919, by which time a total number of 4,747 had been completed, 3,126 of these by the parent company, the last to the RNZAF. Of the final batch, 153 were delivered with the 200hp Sunbeam Arab engine and 18 with the 230hp Siddeley Puma. When the RAF was re-established on a peacetime footing, the F.2B was adopted as standard for the army co-operation role and reinstated in production for this task as the Mk II, others being refurbished to similar standards. Fifty structurally revised aircraft delivered in 1926 were designated as Mk IIIs, all surviving aircraft of this mark being converted in 1928 as dual control Mk IVs for a final total of 3,576. It was finally withdrawn from RAF service in 1932.

Bristol F.2B Mk IV

The greatest number of F.2Bs used the Falcon engines, however, and it was these fighter/reconnaissance machines which won the Bristol Fighter its reputation though only after some severe early setbacks.
The first F.2A unit to arrive in France was 48 Squadron, RFC, in March 1917, and their first patrol ended in disaster. On April 5 six of their fighters were attacked by Manfred von Richthofen’s Jasta 11 and four were shot down. Further combat failures followed before it was realized that the fault lay in the tactics, not in the aircraft. Previous fighting scouts had the observer’s gun as their primary if not only armament, but the F.2As synchronized Vickers was a much more potent combat weapon, and once the pilot’s learned to aim the whole aircraft at the target the Fighter never looked back. F.2Bs of 48 Squadron accounted for 148 enemy aircraft by the time of the Armistice. As well as mounting offensive scouting patrols, F.2Bs were used as bomber escorts and bomber intercepters and on, ground attack missions, for which they could carry up to 12.9 kg (20 lb) fragmentation bombs. Because of their success their introduction to reconnaissance squadrons was delayed almost until the end of the war.

Bristol Fighters also served with distinction in Italy, while in Palestine they equipped 1 Squadron of the Australian Flying Corps. Ross Smith of 1 AFC scored the majority of his victories with the F2B. Numbers were also used by Home Defence squadrons. 3,101 were produced through the end of WW 1.

Personnel of 1 AFC with one of their Bristol Fighters in 1918

In July 1917 the Bristol Fighter was adopted by the British War Office as the standard model for all fighter-reconnaissance squadrons. This led to a greater demand for the aircraft than the British and Colonial Aeroplane Company could handle, so production was undertaken by several other companies. As production of the aircraft increased Rolls-Royce found they could not keep up with the demand for Falcon engines, so several alternative powerplants were tried before the 200 hp Sunbeam Arab was chosen. Although Bristol Fighters fitted with this engine tended to be somewhat underpowered, such was the demand for the aircraft that several hundred were delivered to the Royal Flying Corps.

It proved so successful that it equipped 14 RFC squadrons and remained in RAF service until 1932. After the First World War the F.2B became the standard RAF army cooperation aircraft, serving with the RAF until 1932 in Germany, the Middle East and India. Small numbers were supplied to Belgium, Greece, the Republic of Ireland, New Zea¬land, Norway and Spain, and SABCA in Belgium built 40, with 300 hp Hispano Suiza engines, under licence in 1925. In 1927 a Mexican purchasing commission placed contracts in the UK for 10 new Hispano-Suiza engined Bristol Fighters.

The Bristol Fighter saw service in New Zealand when a pair of First World War standard aircraft (H1557 and H1558) arrived in August 1919. A further five (6856-6859, and 7120) arrived in 1825 and 1926, and together they formed the backbone of the New Zealand Permanent Air Force and later the Royal New Zealand Air Force. Operating as Army co-operation, advanced trainers and aerial survey aircraft, they were used extensively, and for a time in the 1920s and early 1930s they were the only armed aircraft in the country. By the time the surviving four aircraft were withdrawn in 1936 (two had been destroyed in fatal crashes and one was withdrawn in 1930 because of its ago) they were the last Bristol Fighters in service anywhere in the world.

Production of the Bristol Fighter continued until 1919, by which time approximately 4469 had been built. In a modified form and known as the Mark IIIa, it continued in service in RAF Army Co-operation Squadrons until 1932.

Bristol Fighter (Type 14) F2B Fighter Mk II serial 22 served Baldonnel from 4 Nov 1925 to July 1935.

The US Army had become interested in the type when the United States entered the First World War in 1917, and a contract for 1,000 planes placed with Fisher Body Corp was cancelled and reassigned to Curtiss, to be powered by the 400hp Liberty 12. The Liberty proved too heavy for the airframe and was responsible for a series of crashes. McCook Field experiments on the pattern plane supplied by RAF (A7207) showed that its Hispano-Suiza was the ideal match, so the contract was cancelled in July 1918 after 26 planes (AS34232/34257) had been built as O-1. Most of those were rebuilt with a monocoque plywood fuselage and refitted with 300hp Wright-Hisso H, others experimentally with 280hp Liberty 8, and all redesignated as B-1.

Curtiss USAO-1

Further production as B-1 was then handed over to Dayton-Wright. Two prototypes of another modified F.2B design were produced as the B 3 and B 4 (later XB 1 and XB 2), and 40 production aircraft with the designation XB-1A, powered by 300 hp Wright engines and armed with twin Browning machine guns, were built by Dayton-Wright as night observation aircraft.

Replica:
Storo Bristol F.2B

Gallery

Bristol F2A
Engine: 190 hp Falcon I.
Span: 11.96 m (39 ft 3 in).
Length: 7.85 m (25 ft 9 in).
Gross weight: 1210 kg (2670 lb).
Maximum speed: 177 km/h (110 mph).

F2B Fighter
Engine: Rolls Royce Falcon III, 275 hp
Wingspan: 39 ft 3 in / 11.99 m
Wing area: 37.68 sq.m / 405.58 sq ft
Wing chord: 5 ft. 6 in.
Length: 25 ft 10 in / 7.87 m
Height: 9 ft 9 in / 2.97 m
Empty weight: 875 kg / 1929 lb
Max take off weight: 2593.1 lb / 1176.0 kg
Fuel capacity: 45 gal
Max. speed: 110 kts / 203 km/h / 125 mph at SL
Service ceiling: 10827 ft / 3300 m
Absolute ceiling: 21,500 ft
Range: 252 nm / 467 km
Rate-of-Climb: 869ft/min (265m/min)
Climb to 6500 ft: 6.5 min
Endurance: 3 hours.
Crew: 2
Armament: 1x MG 7,7mm Vickers, 1 or 2 x MG 7,7mm Lewis
Bombload: 12 x 20 lb / 240 lb. (110 kg.)

F2B
Engine: Sunbeam Arab, 200 hp
Empty weight: 1733 lb
Loaded weight: 2630 lb
Wing area: 406 sq.ft
Wing loading: 6.4 lb/sq.ft
Armament: 1 x Vickers mg, 1 or 2 Lewis mg
Crew: 2

F2B
Engine: Hispano-Suiza, 200 hp
Span: 39 ft 3 in
Length: 24 ft 9 in
Height: 9 t 6 in
Empty weight: 1733 lb
Loaded weight: 2630 lb
Wing area: 406 sq.ft
Wing loading: 6.4 lb/sq.ft
Armament: 1 x Vickers mg, 1 or 2 Lewis mg
Crew: 2
Climb to 6500 ft: 8.7 min

Bristol F2A

In March 1916 the design was begun of a 120 hp Beardmore powered tractor replacement for the B.E. pusher scouts. The type was desig¬nated R.2A and was intended to be armed with one wing mounted Lewis machine gun and another for the observer on a Scarff ring. At the same time a similar design using the 150 hp Hispano Suiza was produced, but lack of power from the Beardmore caused the designer, Captain Frank Barnwell, to produce a new design using the new 190 hp Rolls Royce Falcon and with the designation F.2A. This was an unequal span two bay biplane with its fuselage, tapered to the rear mounted mid way between the wings.

The first of two prototypes was flown on 9 September 1916, one with the Rolls¬-Royce engine, the other with the 150 hp Hispano Suiza. After successful trials a first batch of 50 Rolls Royce powered pro-duction F.2As was ordered on 28 August armed with a single forward-firing 0.393 Vickers machine gun controlled by a Constantinesco interrupter mechanism to fire through the propeller arc, and either single or twin 0.303 Lewis machine guns on a Scarff ring in the observer’s position.

Deliveries began early in 1917 and it entered service in March 1917 as the first British two-seat fighter. Compared to single-seat fighters of the day such as the Sopwith Pup and Camel the Bristol Fighter was huge, with a wingspan of almost 40 feet and weighing almost a ton fully loaded. Initial operational experience in April 1917 was disappointing, due to the combat techniques used. Confidence in the type was restored when newly-evolved methods were proved successful.

Meanwhile, the improved model had been evolved, the 51st and subsequent production aircraft being of this standard, and delivery of the F.2B resulting in the withdrawal from frontline use of the F.2A.

Take-off weight: 1210 kg / 2668 lb
Empty weight: 783 kg / 1726 lb
Wingspan: 11.96 m / 39 ft 3 in
Length: 7.87 m / 25 ft 10 in
Height: 2.89 m / 9 ft 6 in
Wing area: 36.14 sq.m / 389.01 sq ft
Max. speed: 177 km/h / 110 mph

Bristol S2A

A derivative of the Scout D intended to meet an Admiralty specification for a two-seat fighter, the S.2A had side-by-side seating and was intended to be armed with a single 7.7mm Lewis gun. In the event, it was rejected by the Admiralty in favour of the Sopwith 1/2 Strutter, but work continued on the two prototypes at the request of the War Office which envisaged the type as potential an advanced trainer for the RFC.
The two prototypes were completed in May and June 1916 respectively, being powered by the 110hp Clerget engine (although one was later re-engined with a 100hp Gnome Monosoupape), and were delivered to the Central Flying School at Upavon. They were found to be manoeuvrable and fast, but no further development was undertaken.

Take-off weight: 635 kg / 1400 lb
Wingspan: 8.58 m / 28 ft 2 in
Length: 6.48 m / 21 ft 3 in
Height: 3.05 m / 10 ft 0 in
Max. speed: 153 km/h / 95 mph

Bristol R.2A

In 1916, Captain Barnwell, not satisfied with the Royal Aircraft Company R.E.8, of the Bristol Aeroplane Company produced the 120 hp Beardmore powered tractor R.2A.

This R.2A was a two-seat machine with a pilot-operated forward-firing synchronised Lewis Gun, and an observer close behind with a folding seat to enable him to stand and fire a single Lewis gun mounted on a rotating ring. To improve the pilot’s view, and the rear gunner’s forward field of fire, the wings were mounted low in relation to the fuselage. Towards the rear of the aircraft, the fuselage was tapered to a small cross section and about a third of the fin and rudder was placed below the horizontal tailplane; increasing the gunner’s field of fire in that direction. After some modification, an engine change and armament rethink, the company received an order for 50 aircraft. The first of these flew on 09 September 1916.

The R.2A was to have been powered by a 120 hp Beardmore engine, but by this stage Rolls-Royce had produced the 190 hp Falcon I. Bramwell decided that with the extra power provided by the Falcon I the R.2A could be transformed from a reconnaissance aircraft to a fighter, so it duly became the F.2A.

Bristol 21A Scout F.1

The problems with the Arab engine in the Scout F led to an investigation of possible alternative power plants, and it was decided to adapt the third prototype airframe to take a new 14-cylinder two-row Brazil-Straker (later Cosmos Engineering) Mercury radial of 347hp. Designated Scout F.1, the aircraft was first flown on 6 September 1918, and proved to possess an excellent performance, establishing new unofficial climb records in April 1919.
By that time, further development of the Mercury engine had been abandoned and no more work on the Scout F.1 was undertaken.

Engine: Brazil-Straker Mercury 14-cylinder radial, 347hp
Take-off weight: 1025 kg / 2260 lb
Wingspan: 9.03 m / 29 ft 8 in
Length: 6.09 m / 19 ft 12 in
Height: 2.54 m / 8 ft 4 in
Wing area: 24.15 sq.m / 259.95 sq ft
Max. speed: 233 km/h / 145 mph

Bristol Scout F

Originally intended for a 200hp Hispano-Suiza engine, the Scout F was initiated by Frank Barnwell in June 1917, subsequently being redesigned to take a 200hp Sunbeam Arab II eight-cylinder water-cooled engine. This power plant had been ordered into large-scale production in January 1917, before adequate testing had been undertaken.

Bristol Scout F Article

Six prototypes of the Scout F were ordered, the first of these flying in March 1918, by which time it had been decided to complete only the first two aircraft with Arab engines. The Scout F possessed excellent flying qualities, but its Arab engine proved totally unreliable. Nevertheless, the second prototype was completed and flown, flight testing continuing into 1919. Armament comprised two synchronised 7.7mm Vickers guns.

Engine: 200hp Hispano-Suiza
Take-off weight: 1002 kg / 2209 lb
Empty weight: 651 kg / 1435 lb
Wingspan: 9.03 m / 29 ft 8 in
Length: 6.35 m / 20 ft 10 in
Height: 2.54 m / 8 ft 4 in
Wing area: 24.15 sq.m / 259.95 sq ft
Max. speed: 222 km/h / 138 mph
Armament: 2 x 7.7mm Vickers guns

Bristol Scout A / B / C / D

Scout D

A single-seat sports biplane designed by Frank Barnwell, was first flown on 23 February 1914, with an 80 hp Gnome engine, and retrospectively known as the Scout A,

Bristol Scout A / B / C / D Article

Two Scout Bs completed six months later were intended for reconnaissance, were officially unarmed, but one of which was fitted with a rifle on each side of the fuselage and angled outward to avoid hitting the propeller when fired. They were sent to France.

The Scout B was followed by 161 Scout Cs (74 for the RN and 87 for the RFC) which, again, were officially unarmed, although in the field the fitting of pistols, rifles and carbines was common, while some RN Scouts carried 24-round canisters of Ranken darts which it was intended to use against Zeppelins.

Scout C

An installation of cavalry carbine on a later production Scout C enabled Capt. Lanoe Hawker of 6 Sqn to shoot down one enemy aircraft in flames, drive another down and damage a third in quick succession on July 25, 1915. All three enemy aircraft were armed with machine-guns and Capt. Hawker was awarded the Victoria Cross.

The Scout D was a revised design which, completed in November 1915, had provision for a fixed synchronised 7.7mm Vickers gun. The Scout D was the first model for which armament was officially intended, though relatively few of these had the synchronised Vickers gun and the armament of others varied considerably. Some having a 7.7mm fixed Lewis gun firing straight ahead without synchronising equipment and others having a movable Lewis above the upper wing.

Scout D

A number of modifications were made at Bristol’s and the type was varied from the D-1 to D-5. Engines varied from the 80 hp Gnome and Le Rhone to the 100 hp Gnome Monosoupape, 110 hp Le Rhone, and 130 hp Clerget. Over 200 were built before the type was abandoned.

Of the 210 examples built, 80 went to the RN, of which 50 had 100hp Gnome Monosoupape engines and the remainder the 80hp Gnome. Most of those delivered to the RFC ultimately had the 80hp Le Rhone engines.

The Scout C and D had early limited use by the Australian 1 AFC in Egypt where Lt L.J. Wackett used one in experiments with a synchronised machine gun.

Altogether 236 Scouts were delivered to the RFC, and 137 to the RNAS.

Some RNAS machines had a Lewis gun mounted above the top wing. RFC Scout D’s had a Vickers gun above their front fuselage.

Gallery

Scout C
Engine: 80 hp Le Rhone, or Gnome, or 110 hp Clerget
Wing span: 24 ft 7 in
Wing area: 198 sq ft
Length: 20 ft 8 in
Height: 8 ft 6 in
Fuel capacity: 16 Gal
Endurance: 2 hr
Service ceiling: 11,000 ft

Scout C
Engine: 80 hp Clerget
Wing span: 24 ft 7 in
Wing area: 198 sq ft
Length: 20 ft 8 in
Height: 8 ft 6 in
Empty weight: 750 lb
MTOW: 1089 lb
Fuel capacity: 16 Gal
Max speed: 94 mph at SL
Endurance: 2 hr
Service ceiling: 11,000 ft

Scout D
Engine: 1 x Gnome, 80hp.
Wingspan: 24 ft 5 in
Wing area: 198 sq.ft
Length: 20 ft 7 in
Height: 8 ft 6 in
Empty weight: 757 lb
Loaded weight: 1195 lb
Max speed: 98 mph at SL
Service ceiling: 15,500 ft
ROC: 385 fpm to 6500 ft
Endurance: 2 hr 30 min
Seats: 1

Scout D
Engine: 1 x Le Rhone 9, 80hp.
Length: 20 ft 8 in (6.02m)
Wingspan: 27.33ft (8.33m)
Wing area: 18.39 sq.m / 197.95 sq ft
Height: 8 ft 6 in (2.59m)
Maximum Speed: 100mph (161kmh; 87kts)
Rate-of-Climb: 540ft/min (165m/min)
Service Ceiling: 13,999ft (4,267m)
Armament: 1 x 7.7mm machine gun
Crew: 1
Empty Weight: 761lbs (345kg)
Maximum Take-Off Weight: 1,250lbs (567kg)

Scout D
Engine: 1 x Gnome Monosoupape, 100hp
Max speed: 104 mph at SL

Scout D
Engine: 1 x Le Rhone, 110hp.

Scout D
Engine: 1 x Clerget, 130hp.

Bristol / British & Colonial Aeroplane Company Ltd

In 1910 Sir George White, the wealthy owner of the Bristol Tramways Company, formed the Bristol and Colonial Aeroplane Company Ltd. With head offices in Bristol and a factory at nearby Filton, the aircraft produced by the company were generally known as ‘Bristols’.

Bristol Article

Founded at Bristol, Somerset, in February 1910 as British & Colonial Aeroplane Company Ltd, a factory was set up in two sheds in the village of Filton in south Gloucestershire, just north of Bristol. Sir George White was a wealthy Bristol businessman and his company was registered on 19 February 1910 with a capital of £25,000.
First began construction of a number of biplanes under license from Societe Zodiac, but these were not completed because the sample aircraft bought from France could not be induced to take to the air.

First aircraft produced were Bristol biplanes, usually known as the Boxkite, which initially were little more than copies of the Henry Farman biplane. The first of these, the Boxkite, was based on a Henri Farman design. The Boxkite made its debut at the Third International Aero Exhibition in 1911 and went on to become the first commercially produced aircraft in Britain with two per week rolling out of the factory. It was sold to the British and Russian military as well as being exported throughout the British Empire.

Flying schools established at Larkhill, on Salisbury Plain, and at Brooklands, Surrey, 1911. February 1911 Deutsche Bristol-Werke established at Halberstadt, Germany, to operate a flying school and build Bristol airplanes; arrangement canceled June 23,1914.

First military aircraft were monoplanes designed by Henri Coanda; No. 105 shared third place with a Deperdussin in the Military Aeroplane Competition of 1912. Bristol Scout, or “Baby Biplane”, evolved by Frank Barnwell 1914. The two-seat Bristol Fighter entered service in 1917 and became regarded as the best general-purpose combat aircraft of the First World War.
During the final year of the war the company produced 2,000 aeroplanes from its own factories. By the Armistice the payroll had risen from 200 in August 1914 to 3,000 and the original tram sheds were now part of a factory with eight acres of floor space.
Following the acquisition of the Cosmos Engineering Company in 1920, the Bristol Company was also a major builder of aero engines.
Renamed the Bristol Aeroplane Company on 9 February 1920. Problems of readjustment and survival were intensified by the general world wide economic depression that succeeded the brief postwar boom. Diversification was one of the expedients adopted to keep the nucleus of the skilled workfiorce in being at Filton. Aircraft manufacture was augmented by produc¬tion of bus and coach bodies and later of motor car bodies.
Between the wars Bristol Bulldog biplanes had equipped nine RAF Squadrons by 1932 and were most widely used fighter until 1936.
In 1935, Bristol’s directors, realising that the company’s capital resources were inadequate, resolved on 15 June to re organise the firm as a public limited liability company with a share capital of £1.2million.
Bristol Type 138A of 1936 captured world altitude record in September, 1936, then regained it from Italy in June 1937 with an altitude of 16,440m. Bristol Type 142, built as executive aircraft for Lord Rothermere, became the military Blenheim, an important light bomber in the early Second World War period. Beaufighter, first flown July 1939, became RAF’s first nightfighter, subsequently an important antishipping aircraft armed with rockets, torpedoes, and bombs.
Designed and built prototype of eight-engined 100- passenger Brabazon I, first flew September 4, 1949; scrapped 1953 for financial/political/technical reasons. Type 170 Freighter first flown December 2, 1945 and 213 built subsequently.
Turboprop powered Britannia first flew August 16, 1952, made the first non-stop airliner flight London, Vancouver (8,208km), June 29, 1957, and first North Atlantic passenger service to be flown by a turbine-powered airliner on December 19 of the same year.
A helicopter department was set up in 1945 as part of the aircraft division at Filton. Austrian born Raoul Hafner headed a research and development team which produced the Type 171 Sycamore. Subsequently entering service with RAF as its first British-designed helicopter in 1952.

1955

In January 1956 the Bristol Aeroplane Company had reorganised into three wholly owned companies; Bristol Aircraft Ltd, Bristol Aero-Engines Ltd, and Bristol Cars Ltd.

September 1957

Four years later Bristol Aircraft Ltd joined with Vickers Ltd and English Electric to become the British Aircraft Corporation.

In 1960 Westland Aircraft took over the Bristol Helicopter Department.

In 1960 Bristol Aircraft Ltd joined with Vickers Ltd and English Electric to become the British Aircraft Corporation.

Bristol Aero Engines (formerly Bristol Engine Company) merged with Armstrong Siddeley Motors in 1959 to form Bristol Siddeley Engines Limited (BSEL) which in turn was taken over by Rolls-Royce in 1966.

Research and development ot the tandem-rotor helicopters resulted in Type 192 Belvedere which entered service with the RAF, in 1961.

On 28 December 1963 the separate companies merged their identities and Bristol Aircraft Ltd became the Filton Division of BAC. Four years later the Bristol title was lost from the engine side when Bristol Siddeley Engines Ltd became the Bristol Engine Division of Rolls Royce Ltd. The nationalisation of the aircraft industry in 1977 resulted in the formation of British Aerospace (BAe) and the works at Filton became part of the Weybridge Bristol Division of BAe Aircraft Group while the BAC Guided Weapons Division at Fillon became part of the Stevenage Bristol Divi¬sion of the BAe Dynamics Group.

Bristol Aero Engines (formerly Bristol Engine Company) merged with Armstrong Siddeley Motors in 1959 to form Bristol Siddeley Engines Limited (BSEL) which in turn was taken over by Rolls-Royce in 1966.

Breguet Bre.16

At the same as the Breguet 16 was being developed, a two-seat fighter, a version of the Breguet 14, was being built. It had originally been on the drawing board back in 1916, and had been submitted to the STAe for consideration. Rejected by them, the design had stayed on the drawing board, but the requirement for a long-range escort fighter at the beginning of 1918 caused it to be resurrected.

An enlarged version of the Breguet 14 appeared at the beginning of 1918, the Breguet 16 Bn2. This was designed for use as night-bomber, and the increased wingspan of 17m enabled it to carry sufficient fuel for long missions, as well as armament for major attacks.

The Breguet 16 had three pairs of inter-plane struts either side instead of two, and differently shaped vertical tail surfaces.

Maximum bomb load was 550kg. Breguet 16s remained in service in Morocco and Syria until March 1927.

Breguet Bre.14 / Br.13 / AV 1 / Breguet-Latécoère 14 / Latécoère Breguet

Breguet 14

The Breguet 13, or AV 1, as it was known at the time, had a conventional look. The prototype took to the air on 21 November 1916 powered by a 220 hp Renault engine, with Louis Bleriot at the controls. After extensive trials by company test pilots, the aircraft was delivered to Aviation Militaire in January 1917 for their assessment. It immediately became apparent that the aircraft was far in advance of anything the British or the Germans had.

The STAe (Section Technical Aeronautique) had stipulated earlier in November that they wanted four types of aircraft, a three seat, long-range reconnaissance plane, a three-seat bomber, a two-seat army co-operation plane, and a two-seat fighter. Breguet submitted the aircraft stating variants of the aircraft could cover all the requirements.

The Breguet 14 has two-bay wings, each with two aluminium spars, wooden leading-edge and ribs and fabric covering. The fuselage was of aluminium tube with fabric covering, except for metal top decking around the cockpits. Tail surfaces were fabric covered steel-tube structures. Conventional controls, with ailerons on the top wing only. Full span flaps on the lower wings dropped automatically at 70 mph to increase lift. Fuel was in two fuel tanks aft of the engine.

Breguet Bre.14 Article

The 14B.2 bomber version was fitted with Michelin bomb racks.

Breguet factory in 1918 assembling XIV A2

On 6 March 1917, impressed by the aircraft, the Aviation Militaire ordered 150 Breguet AV 1s (Breguet 13) to be used for reconnaissance. At the same time, the Michelin Company received an order for 150 Breguet AV 2s (Breguet 14), the bomber version. Because the aircraft were almost identical, it was decided to use the same designation for both – Breguet 14. In the months up until September 1917, orders totalling another 475 aircraft were placed.

Because demand was now outstripping supply, other companies were brought in to build the Breguet 14 under licence: Ballenger (3), Darracq (330), Farman (22), Sidam (300) and Paul Schmitt (275). The Paul Schmitt Company was already in the process of building a bomber, but the Breguet 14 had to take precedence, although they still managed to complete their own orders.

As far as the military was concern, the Breguet 14 was adaptable. It underwent numerous modifications, none of which affected its performance. On some of the aircraft, the wingspan and flap size was reduced. Different engines were tried, and various types of armament were installed and tested. Among these was one of the first air ambulances – the Breguet 14S (Sanitaire). The fuselage was modified to enable two stretchers to be carried inside.

Almost every escadrille was supplied with the Breguet 14, including the overseas units. During the short period of the war in which the USAS was involved, they purchased almost 400 of the aircraft. The first of their bombardment units, the 96th Aero Squadron carried out their first mission in June 1918 using Breguet 14 bombers.

Renault 300 hp and metal fuselage

Powered by a Renault 12 Fcy water-cooled inline engine of 300hp / 238.5kW, the metal cowling was extensively louvred and a distinctive frontal radiator was fitted. The pilot was seated in the front and the gunner/observer behind. The Bre 14 A2 was armed with a single 7.7mm forward-fixed Lewis machine gun on the left side of the fuselage and an additional set of 7.7mm Lewis machine guns on a mounting in the rear cockpit. External stores could be carried when in the full bomber role.

Breguet XIV Observer position and camera

The prototype flew for the first time on 21 November 1916.

Türk Hava Kuvvetleri assembled 16 Bréguet XIV A-2 in 1924 for the Turkish Air Force.

The reconnaissance version was followed into production by the bomber in the summer of 1917, the latter differing in having Breguet-designed automatic trailing-edge flaps on the lower wings and transparent panels in the sides of the observer’s cockpit. Late production examples of both versions had horn-balanced ailerons, the B2 aircraft thus equipped doing away with the trailing-edge flaps.

Breguet XIV A2 camera position

The B2 version could be fitted with an additional Lewis gun that fired downwards through the rear fuselage floor and had a maximum bomb load of 256kg, carried on underwing racks.
A single-seat long-range version, known as the Bre 14 B1, was also built in limited numbers during 1918, and was intended to bomb Berlin. In fact it was little used and never mounted an attack on the German capital. Breguet 14 also equipped American and Belgian units during World War I, some powered by Italian Fiat A-12 and A-12bis engines.
The Bre 14 A2 reconnaissance version and the Bre 14 B2 bomber equipped at least 71 French escadrilles on the Western Front by November 1918 and were also used by units in Serbia, Greece, Macedonia and Morocco.
Many ex-French aircraft were handed over to Poland in 1919 and these took part in the fighting with Russia in 1920. The type formed part of the initial equipment of the Czech air arm, and others were operated in Brazil, China (70 with 298kW Lorraine-Dietrich engines), Denmark, Finland, Greece, Japan, Portugal and Spain. The Spanish equipped four squadrons in Morocco in 1922, using them on missions against Riff tribesmen. A further 40 were obtained in 1923. A small number of float variants were also built, mostly with a central main float and small wingtip stabilising floats.
During 1919 Breguet 14 made a number of long-distance flights and Louis Breguet founded the Compagnie des Messageries Aeriennes with them, making regular air mail flights linking Paris with Brussels and London. These Bre 14 had special mail containers fitted under the wings. A cabin version with provision for two passengers was built as the Breguet 14T.
Later came the improved Bre 14Tbis and the three-passenger Breguet 14T2. During the 1920s, the Lignes Aeriennes Latecoere company used more than 100 Breguet 14 in various versions on its routes between Toulouse and Dakar (West Africa) and between Natal and Santiago di Chile in South America. The Br 14S air ambulance, adapted from the Breguet 14T, was widely operated in the 1920s during the campaigns in Morocco and Syria. Each could carry two stretchers in the rear fuselage.

The Forges et Ateliers de Construction Latecoere began its interest in aviation in 1917 with an aircraft works at Toulouse-Montaudron. In 1917 P-G Latécoère turned from making munitions to licence-building aircraft for the Aviation Militaire Française. Total wartime production amounted to 800 licenced Breguet XIV and Salmson 2A.2 2-seat reconaissance bomber biplanes.

Initially, these licenced airframes do not seem to have received Latécoère designations. The licenced XIVs were refered to as Breguet-Latécoère 14s (or sometimes Latécoère Breguets). The designation Laté 1 may have been applied to licenced Brequets but there is some confusion with a 1918 2-seat fighter (of original Latécoère design?).

Latécoère converted large number of Breguet XIVs for civilian used in 1921-23 (190 for use by Aéropostale alone). None of these civil conversions seem to have received distinct Laté-x designations. Namings were as follows:

  • Breguet-Latécoère 14.A2: straightforward de-militarized mailplane conv., 1922
  • Breguet-Latécoère 14 Torpedo: passenger conv. for Aéropostale, 1922-23
  • Breguet-Latécoère 14.B2: (970) Latécoère inflight refueling experiments, 1922

The ‘Torpedo’ name comes from the designation of Breguet’s own 14T and 14Tbis passenger conversions. Like the 14Ts, the Breguet-Latécoère 14 Torpedo was an aft cabin conversion as distinct from the cabin 14 ‘Salon’ conversions.

Breguet XIX TF Super Bidon Point d’Interrogation

Production was spread over seven manufacturers, in addition to the Louis Breguet factory at Velizy, near Paris, and 7800 of the type were built up to 1926, more than 2,500 appearing after the war ended in 1918.

The Breguet 14s were sold to 22 countries. There were fourteen variations that included using a number of engines and a large number of modifications. The type would continually see service in frontline French forces up until 1932.

Gallery

Replica: Salis Breguet XIVP

Br.13
Engine: 1 x Gnome, 160 hp
Wingspan: 49 ft 7 in / 15.3 m
Length: 27 ft 10 in / 8.5 m
Height: 10 ft 9 in / 3.3 m
Empty weight: 2094 lb / 950 kg
Loaded weight: 2876 lb / 1350 kg
Max speed: 62 mph / 100 kph
Armament: 1 x Hotchkiss mg
Bombload: Flechettes

Breguet Bre.14A
Engine: 1 x Renault 12Fcx, 220kW
Wingspan: 14.4 m / 47 ft 3 in
Length: 9.0 m / 29 ft 6 in
Height: 3.3 m / 10 ft 10 in
Wing area: 49.0 sq.m / 527.43 sq ft
Take-off weight: 1740 kg / 3836 lb
Empty weight: 1140 kg / 2513 lb
Fuel capacity: 57.2 gal
Max. speed: 180 km/h / 112 mph
Ceiling: 6000 m / 19700 ft
Range: 900 km / 559 miles
Crew: 2
Armament: 3 machine-guns, 300kg of bombs

Breguet Bre.14B2
Engine: 1 x Renault 12 Fcy water-cooled inline, 300hp.
Length: 29.10ft (8.87m)
Wing span: 48.92ft (14.91m)
Height: 10.83ft (3.30m)
Empty Weight: 2,282lbs (1,035kg)
Maximum Take-Off Weight: 3,483lbs (1,580kg)
Fuel capacity: 57.2 gal
Maximum Speed: 121mph (195kmh; 105kts)
Maximum Range: 301miles (485km)
Cruise: 75 mph.
Service Ceiling: 13,993ft (4,265m; 2.7miles)
Armament:
1 x 7.7mm Lewis machine gun in forward-fixed firing position.
2 x 7.7mm Lewis machine guns on mounting in rear cockpit.
Up to 573lbs of external ordnance.
Accommodation: 2
Hardpoints: 4

Breguet XIX Super Bidon Point d’Interrogation
Engine: Hispano-Suiza 12 LB, 650 hp
Wingspan: 18.30 m
Length: 10.72 m
Height: 4.08 m
Wing area: 59.94 m²
Max weight: 6375 kg
Max speed: 250 km/h
Ceiling: 6700 m
Range: 9000 km