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Zlín XIII

From Wikipedia, the free encyclopedia
Zlín XIII
In two seat configuration
RoleRacing aircraft
Type of aircraft
National originCzechoslovakia
ManufacturerZlínská letecká společnost, a. s. (Zlín)
DesignerJaroslav Lonek
First flight1937
StatusMuseum
Number built1

TheZlín XIII was a fast single or two seat aircraft, designed and built inCzechoslovakia in the late 1930s. Its development was ended by the disruption of Czechoslovakia in the approach toWorld War II.

Design and development

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The Zlín XIII was a very aerodynamically clean, low-powered, all woodmonoplane with a one-piece,low set, tapered wing equipped withflaps. It was powered by a 97 kW (130 hp)Walter Minor four cylinderinverted engine, driving a two blade propeller and with a fixed,faired tailwheelundercarriage. The enclosedcockpit placed the pilot well behind the wingtrailing edge with a passenger seat ahead of him; a change ofcanopy to a shorter version, together with a forward fairing, removed the forward seat. This versatility was intended to allow the type XIII to operate as either a high speed executive transport or as a single seat competition aircraft.[1][2][3]

The Zlín XIII was displayed as a two seater at the 10thPrague Aero Show in July 1937, having made its first flight earlier in the year.[1] It was entered into theFrenchCircuit de l'Est race, but arrived late too late to compete. TheGerman annexation of theSudetenland in 1938, and the subsequent fragmentation of Czechoslovakia ended development and prevented production, so only the prototype was built.[3]

Aircraft on display

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In single seat form

Specifications

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Data fromNational Technical Museum (Prague)[2]

General characteristics

  • Crew: 1 or 2
  • Length: 6.8 m (22 ft 4 in)
  • Wingspan: 7.0 m (23 ft 0 in)
  • Empty weight: 450 kg (992 lb)
  • Gross weight: 650 kg (1,433 lb)[3]
  • Powerplant: 1 ×Walter Major-4 four cylinder inverted inline, air cooled, 97 kW (130 hp)[1]
  • Propellers: 2-bladedRatier[2]

Performance

  • Maximum speed: 300 km/h (190 mph, 160 kn)
  • Range: 700 km (430 mi, 380 nmi)
  • Service ceiling: 5,600 m (18,400 ft)[3]
  • Time to altitude: 3.25 min to 1,000 m (3,281 ft)

References

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  1. ^abc"Prague Aero Show".Flight.XXXII (1490): Supplement, page a. 15 July 1937.
  2. ^abcd"Zlín XIII at the National Technical Museum". Retrieved12 September 2014.
  3. ^abcd"Zlin XIII". Retrieved13 September 2014.

Further reading

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Wikimedia Commons has media related toZlín Z-XIII.
  • Plocek, Pierre (September 2003). "Un chef-d'oeuvre tchécoslovaque: Zlin XIII" [A Czech Masterpiece: The Zlin XIII].Le Fana de l'Aviation (in French) (406):60–64.ISSN 0757-4169.
Aircraft produced byZlín and Moravan
Manufacturer
designations
By name
1 Unknown/not assigned
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