SPAD S.XI

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SPAD S.XI
Spad XVI.jpg
Spad XVI at National Air and Space Museum
Role Reconnaissance aircraft
Manufacturer SPAD
Designer Louis Béchereau
Primary users Aéronautique Militaire
Red Army
Number built 1,000

The SPAD S.XI or SPAD 11 was a French two-seat biplane reconnaissance aircraft of the First World War. The SPAD 11 was the work of Louis Béchereau, chief designer of the Société Pour L'Aviation et ses Dérivés (SPAD), who also designed the highly successful SPAD 7 and SPAD 13 single-seat fighter aircraft. It was developed under military specification C2, which called for a two-seat fighter aircraft. As a result of its failure to meet the levels of performance and agility demanded by the C2 specification, the SPAD 11 was used, along with the more successful Salmson 2 and Breguet 14, to replace aging Sopwith 1½ Strutter and Dorand AR reconnaissance aircraft. Persistent problems with the SPAD 11 led to its early replacement by the SPAD S.XVI or SPAD 16 variant.

SPAD S.XI[edit]

The SPAD 11 had some resemblance to Béchereau's single-seat fighters and employed much the same method of simple construction. Longer and heavier than the fighters, the SPAD 11's lower wings were designed with cut-outs to improve the observer's view of the ground. The aircraft was armed with a single 0.303-inch (7.7 mm) Vickers machine gun firing forward and a single Lewis machine gun of the same calibre on a flexible mount for the observer. Testing of the SPAD 11 showed a poor performance, said to be little better than that of the SPAD A.2 of 1915 and it was rejected as a C2 class fighter aircraft, being reclassified as an A2 reconnaissance aircraft.

Further problems were encountered with the SPAD 11's Hispano-Suiza 8B engine. Some aircraft were fitted with a 12-cylinder Renault engine, but this lowered the aircraft's poor performance yet more. Handling problems were encountered, including tail-heaviness, making the aircraft tiring to fly, and a propensity to stall. In spite of these flaws, the SPAD was still superior to the Sopwiths and Dorands, and 12 squadrons were fully equipped with SPAD 11s. Some 1,000 SPAD 11s were built, most of which were out of service by the autumn of 1918, generally replaced by the SPAD S.XVI.

Three Belgian squadrons used the SPAD 11 and two from the United States. The SPAD 11 was unpopular in American service, as in French, and so much so that one of the two squadrons issued with SPADs replaced them with Sopwith 1½ Strutters. Uruguay purchased a small number of aircraft after the war and some examples are known to have been used by Russia and Japan.

A single SPAD 11 was modified as a night-fighter, fitted with a searchlight on a framework mounted ahead of the propellor, under the Cn2 specification.[1]

SPAD S.XVI[edit]

The SPAD 16 was a development of the SPAD 11. Essentially a SPAD 11 with a Lorraine-Dietrich engine of 240 bhp, or 250 bhp according to some sources. The new engine, while more powerful, resulted in a heavier aircraft and performance was slightly inferior to the SPAD 11. The original handling problems were largely unresolved.

The SPAD 16 arrived at the front line around the end of 1917. It equipped 27 French squadrons and 305 two-seater SPADs, mainly SPAD 16s, were in service with French reconnaissance squadrons at the armistice, as opposed to 530 Salmson and 645 Breguet reconnaissance aircraft. The SPAD 16 served with five post-war French squadrons.

Six SPAD 16s were bought by the United States. One of these, flown by Billy Mitchell, is preserved at the National Air and Space Museum. He personally flew reconnaissance missions in it when combat started in the Château-Thierry sector in July, 1918.

The exact number of SPAD 16s built is uncertain but was probably around 1,000.

Operators[edit]

 Belgium
 France
 Japan
 Italy
 Russia /  Soviet Union
 Uruguay
 United States

Specifications (SPAD S.XI A2)[edit]

Data from The Complete Book of Fighters[1]

General characteristics

  • Crew: 2
  • Length: 7.84 m (25 ft 9 in)
  • Wingspan: 11.21 m (36 ft 9 in)
  • Height: 2.80 m (9 ft 2 in)
  • Wing area: 30.00 m2 (322.9 sq ft)
  • Empty weight: 679 kg (1,497 lb)
  • Gross weight: 1,035 kg (2,282 lb)
  • Powerplant: 1 × Hispano-Suiza 8Bc water-cooled V-8 engine, 160 kW (220 hp)

Performance

  • Maximum speed: 180 km/h (112 mph; 97 kn)
  • Endurance: 2.25 hr
  • Service ceiling: 7,000 m (22,966 ft) [2]
  • Time to altitude: 3,000 m (9,850 ft) in 12.6 min

Armament

References[edit]

Notes
  1. ^ a b Green and Swanborough 1994, p. 542.
  2. ^ Angelucci 1983, p. 44.
  3. ^ Munson 1967, p. 164.
Bibliography
  • Angelucci, Enzo. The Rand McNally Encyclopedia of Military Aircraft, 1914-1980. San Diego, California: The Military Press, 1983. ISBN 0-517-41021-4.
  • Davilla, James J., & Soltan, Arthur M., French Aircraft of the First World War. Stratford, Connecticut: Flying Machines Press, 1997. ISBN 0-9637110-4-0
  • Green, William and Gordon Swanborough. The Complete Book of Fighters. New York: Smithmark, 1994. ISBN 0-8317-3939-8.
  • Munson, Kenneth. Aircraft of World War I. London: Ian Allan, 1967. ISBN 0-7110-0356-4.

External links[edit]