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Letov Š-10

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Letov Š-10
General information
RoleTrainer aircraft
National originCzechoslovakia
ManufacturerLetov Kbely
ServiceCzechoslovak Air Force
Masaryk Aviation League
Number built51
History
ConcludedNovember 1936
Developed fromHansa-Brandenburg B.I
Developed intoLetov Š-18
SuccessorsPraga E-39

The Letov Š-10 was a biplane trainer aircraft produced in the 1920s by the Czechoslovak company Letov Kbely. It was a licensed copy of the German design Hansa-Brandenburg B.I and could hold 2 people. The Š-10 served in the Czechoslovak Air Force and later were acquired by aeroclubs and organizations of the Masaryk Aviation League (Czech: Masarykova letecká liga).

Origin and development

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The Letov Š-10 was a licensed copy of the Hansa-Brandenburg B.I series 76, which is widely used by the Austro-Hungarian Aviation Troops. This type of plane was among the most numerous aircraft found in Czechoslovakia after or shortly after independence, and later it was decided to further increase the number of aircraft produced via domestic production. Aero Vodochody created the Aero Ae-10, and in 1922 the production of 51 Š-10s was started at the Letov factory.[1][2][3] The Š-10s were equipped with a six-cylinder in-line Mercedes D.I engine, the pistons of whose rear cylinders were excessively flooded with oil when stationary on the ground, which earned the aircraft the nickname "anchovy" or "sardine".[2][4] Another unofficial nickname for the Ae-10 and Š-10 types was "little firecracker",[4] which they shared with the original Brandenburg B.I.[2]

Operational history

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The Š-10 served the Czechoslovak Air Force, along with its related Aero Ae-10 aircraft, as a basic pilot training aircraft. Even though it was soon supplemented by the more modern Š-18, it was not completely replaced in military service until the introduction of the Praga E-39 aircraft in the early 1930s. The Š-10 was characterized by considerable stability, flight safety and overall ease of piloting,[2] which led to its popularity among pilots, but was soon felt to be a certain deficiency, as these features failed to adequately prepare students for piloting more demanding combat aircraft.[1][2] After being withdrawn from military service, some of the Š-10s were acquired by aeroclubs and organizations of the Masaryk Aviation League (MLL). The Š-10.1 aircraft, named "Zdena", served at the MLL branch in Nymburk until November 1936.[5]

Operators

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Specifications

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Source:[6]

Technical data

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  • Crew: 2 (instructor and student)
  • Span: 12.30 m (40.4 ft)
  • Length: 8.40 m (27.6 ft)
  • Bearing area: 36.52 m2 (393.1 sq ft)
  • Empty weight: 668 kg (1,473 lb)
  • Takeoff weight: 966 kg (2,130 lb)
  • Powerplant: 1 × liquid-cooled six-cylinder in-line Mercedes D.I engine
  • Power of the drive unit: 74 kW (100 hp)

Performance

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  • Maximum speed: 130 km/h (81 mph)
  • Cruising speed: 90 km/h (56 mph)
  • Climb capacity: can climb to 1,000 m elevation in 9 minutes and 30 seconds
  • Range: 400 km (250 mi)

References

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  1. ^ a b Němeček 1983, p. 35.
  2. ^ a b c d e Rajlich & Sehnal 1993, p. 24.
  3. ^ Taylor, Michael J.H., ed. "Letov S-10." Jane's Encyclopedia of Aviation. New York: Crescent, 1993. p. 573. ISBN 0 517 10316 8.
  4. ^ a b Němeček 1983, p. 36.
  5. ^ Rajlich & Sehnal 1993, p. 41.
  6. ^ Němeček 1983, pp. 244–245.

Sources

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  • Němeček, Václav (1983). Československá letadla (1918-1945) [Czechoslovak aircraft (1918-1945)] (in Czech) (3rd ed.). Naše vojsko.
  • Rajlich, Jiří; Sehnal, Jiří (1993). Vzduch je naše moře: Československé letectví 1918-1939 [The Air is Our Sea: Czechoslovak Aviation 1918-1939] (in Czech) (1 ed.). Naše vojsko. ISBN 80-206-0221-6.