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Zlín Z-26

The Zlin Z-26 Trener was a tandem-seat basic training aircraft built by the Czechoslovakian company Moravan. A low-wing monoplane of largely wooden construction, it was developed into a series of all-metal trainers. Several were also produced in aerobatic variants, known as the Akrobat.

Trener
Z-126 Trener II
Role Training aircraft
Manufacturer Moravan Otrokovice
Produced 1948–1977

The original Z-26 was designed in the 1940s and produced in 1946 to meet a requirement for a basic trainer to replace the Bücker Jungmann and Bestmann. It was a low-wing monoplane of mixed construction, with wooden wings and a welded metal tube fuselage, powered by a single four-cylinder piston engine, the Walter Minor 4-III. It first flew in early 1947, proving superior to the competing Praga 112, and was declared the winner, entering production in 1948.[1]

Later derivatives were also optimised to participate in aerobatic competitions and many were owned by private pilot owners. Both the two-seat Trener and the single-seat Akrobat were considered highly successful, winning several aerobatic awards in the 1960s.[2]

Variants

 
Zlin Z-226T Trener 6 exhibited at the 1957 Paris Air Show

The following variants were progressive improvements on the Z-26:

  • Z-26 – two-seat primary trainer aircraft. 163 built.[3]
  • Z-126 – introduced in 1953, Czech military designation C-105, all-metal wing instead of original wooden wing.[2]
  • Z-226 – more powerful Walter Minor 6-III six-cylinder engine, C-205
    • Z-226A – single-seat aerobatic aircraft. This and subsequent single-seat variants were named the Akrobat.[4]
    • Z-226Bglider tug aircraft
    • Z-226T – basic training version
  • Z-326 – Introduced in 1959, with an electrically retractable undercarriage (standard on future models)[2]
  • Z-526 – with the Walter 6-III carburettor's six-cylinder engine
    • Z-526A – single-seat aerobatic aircraft
    • Z-526F – Improved version. M-137 engine with fuel injector.
  • Z-726 – modified 526 with shortened wings and fuselage

In 1956, deliveries began of the Z326 Trener-Master and Z326A Akrobat.[2] Many sub-variants were also produced, for example the Z-526A and Z-526AFS were aerobatic specials. The production of the family was terminated in the 1970s with Z-726. The Z-726 Universal had reduced wingspan.[2]

Operators

Military operators

  Austria
Austrian Air Force
  Cuba
Cuban Revolutionary Air and Air Defense Force - received about 60 Z-226, Z-326 and Z-526s in the 1960s.[5]
  Czechoslovakia
Czechoslovakian Air Force
  East Germany
Air Forces of the National People's Army[citation needed]
  Egypt
  Iraq[6]
  Mozambique
  Yemen

Specifications (Z-726)

Data from Jane's All The World's Aircraft 1976–77 [7]

General characteristics

  • Crew: two
  • Length: 7.975 m (26 ft 2 in)
  • Wingspan: 9.875 m (32 ft 5 in)
  • Height: 2.06 m (6 ft 9 in)
  • Wing area: 14.89 m2 (160.3 sq ft)
  • Airfoil: root:NACA 2418; tip:NACA 4412
  • Empty weight: 700 kg (1,543 lb)
  • Max takeoff weight: 1,000 kg (2,205 lb)
  • Powerplant: 1 × Avia M 137AZ 6-cyl, air-cooled inverted in-line piston engine, 134 kW (180 hp)

Performance

  • Maximum speed: 236 km/h (147 mph, 127 kn)
  • Cruise speed: 216 km/h (134 mph, 117 kn)
  • Stall speed: 98 km/h (61 mph, 53 kn) (flaps down)
  • Range: 440 km (270 mi, 240 nmi)
  • Service ceiling: 4,500 m (14,800 ft)
  • Rate of climb: 5 m/s (980 ft/min)

See also

References

  1. ^ Mourik 2001, p.61.
  2. ^ a b c d e Frawley 1997, p.198.
  3. ^ Taylor 1989, p.908.
  4. ^ William Greene; The Observer's World Aircraft Directory, Warne, 1961, pp. 318, 334.
  5. ^ Hagedorn 1993, p. 29.
  6. ^ Mourik 2001, p.64.
  7. ^ Taylor 1976, pp. 33–34.
  • Frawley, Gerard. The International Directory of Civil Aircraft. Aerospace Publications Pty Ltd, 1997 ISBN 1-875671-26-9
  • Hagedorn, Daniel P. Central American and Caribbean Air Forces. Tonbridge, Kent, UK: Air-Britain (Historians) Ltd., 1993. ISBN 0-85130-210-6.
  • Mourik, Dick van. "A to Zlin: An Illustrated History of a Light Aircraft Dynasty". Air Enthusiast, No. 93, May/June 2001. Stamford, UK:Key Publishing. ISSN 0143-5450. pp. 59–65.
  • Taylor, John W R. (editor). Jane's All The World's Aircraft 1976–77. London: Jane's Yearbooks, 1976. ISBN 0 354 00538 3.
  • Taylor, Michael J.H. (editor). Jane's Encyclopedia of Aviation. London:Bracken Books, 1989. ISBN 1 85170 324 1.

External links

  Media related to Zlín Z-26 at Wikimedia Commons

zlín, this, article, needs, additional, citations, verification, please, help, improve, this, article, adding, citations, reliable, sources, unsourced, material, challenged, removed, find, sources, news, newspapers, books, scholar, jstor, august, 2008, learn, . This article needs additional citations for verification Please help improve this article by adding citations to reliable sources Unsourced material may be challenged and removed Find sources Zlin Z 26 news newspapers books scholar JSTOR August 2008 Learn how and when to remove this template message The Zlin Z 26 Trener was a tandem seat basic training aircraft built by the Czechoslovakian company Moravan A low wing monoplane of largely wooden construction it was developed into a series of all metal trainers Several were also produced in aerobatic variants known as the Akrobat TrenerZ 126 Trener IIRole Training aircraftManufacturer Moravan OtrokoviceProduced 1948 1977The original Z 26 was designed in the 1940s and produced in 1946 to meet a requirement for a basic trainer to replace the Bucker Jungmann and Bestmann It was a low wing monoplane of mixed construction with wooden wings and a welded metal tube fuselage powered by a single four cylinder piston engine the Walter Minor 4 III It first flew in early 1947 proving superior to the competing Praga 112 and was declared the winner entering production in 1948 1 Later derivatives were also optimised to participate in aerobatic competitions and many were owned by private pilot owners Both the two seat Trener and the single seat Akrobat were considered highly successful winning several aerobatic awards in the 1960s 2 Contents 1 Variants 2 Operators 2 1 Military operators 3 Specifications Z 726 4 See also 5 References 6 External linksVariants Edit Zlin Z 226T Trener 6 exhibited at the 1957 Paris Air ShowThe following variants were progressive improvements on the Z 26 Z 26 two seat primary trainer aircraft 163 built 3 Z 126 introduced in 1953 Czech military designation C 105 all metal wing instead of original wooden wing 2 Z 226 more powerful Walter Minor 6 III six cylinder engine C 205 Z 226A single seat aerobatic aircraft This and subsequent single seat variants were named the Akrobat 4 Z 226B glider tug aircraft Z 226T basic training version Z 326 Introduced in 1959 with an electrically retractable undercarriage standard on future models 2 Z 526 with the Walter 6 III carburettor s six cylinder engine Z 526A single seat aerobatic aircraft Z 526F Improved version M 137 engine with fuel injector Z 726 modified 526 with shortened wings and fuselage Z 726K with Walter M 337 supercharged engineIn 1956 deliveries began of the Z326 Trener Master and Z326A Akrobat 2 Many sub variants were also produced for example the Z 526A and Z 526AFS were aerobatic specials The production of the family was terminated in the 1970s with Z 726 The Z 726 Universal had reduced wingspan 2 Operators EditMilitary operators Edit Austria Austrian Air Force Cuba Cuban Revolutionary Air and Air Defense Force received about 60 Z 226 Z 326 and Z 526s in the 1960s 5 Czechoslovakia Czechoslovakian Air Force East Germany Air Forces of the National People s Army citation needed Egypt Iraq 6 Mozambique YemenSpecifications Z 726 EditData from Jane s All The World s Aircraft 1976 77 7 General characteristicsCrew two Length 7 975 m 26 ft 2 in Wingspan 9 875 m 32 ft 5 in Height 2 06 m 6 ft 9 in Wing area 14 89 m2 160 3 sq ft Airfoil root NACA 2418 tip NACA 4412 Empty weight 700 kg 1 543 lb Max takeoff weight 1 000 kg 2 205 lb Powerplant 1 Avia M 137AZ 6 cyl air cooled inverted in line piston engine 134 kW 180 hp Performance Maximum speed 236 km h 147 mph 127 kn Cruise speed 216 km h 134 mph 117 kn Stall speed 98 km h 61 mph 53 kn flaps down Range 440 km 270 mi 240 nmi Service ceiling 4 500 m 14 800 ft Rate of climb 5 m s 980 ft min See also EditReferences Edit Mourik 2001 p 61 a b c d e Frawley 1997 p 198 Taylor 1989 p 908 William Greene The Observer s World Aircraft Directory Warne 1961 pp 318 334 Hagedorn 1993 p 29 Mourik 2001 p 64 Taylor 1976 pp 33 34 Frawley Gerard The International Directory of Civil Aircraft Aerospace Publications Pty Ltd 1997 ISBN 1 875671 26 9 Hagedorn Daniel P Central American and Caribbean Air Forces Tonbridge Kent UK Air Britain Historians Ltd 1993 ISBN 0 85130 210 6 Mourik Dick van A to Zlin An Illustrated History of a Light Aircraft Dynasty Air Enthusiast No 93 May June 2001 Stamford UK Key Publishing ISSN 0143 5450 pp 59 65 Taylor John W R editor Jane s All The World s Aircraft 1976 77 London Jane s Yearbooks 1976 ISBN 0 354 00538 3 Taylor Michael J H editor Jane s Encyclopedia of Aviation London Bracken Books 1989 ISBN 1 85170 324 1 External links Edit Media related to Zlin Z 26 at Wikimedia Commons Retrieved from https en wikipedia org w index php title Zlin Z 26 amp oldid 1093975501, wikipedia, wiki, book, books, library,

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