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词条 Zlín Z 26
释义

  1. Variants

  2. Operators

      Military operators  

  3. Specifications (Z-726)

  4. See also

  5. References

{{Refimprove|date=August 2008}}
name = Trenerimage =Image:ZLIN Z.126 TRENER 2 D-EWAC l.jpgcaption =Z-126 Trener II

}}{{Infobox aircraft type

type = Training aircraftmanufacturer = Moravan Otrokovicedesigner =first flight =introduction =retired =status =primary user =more users =produced =1948–1977number built =unit cost =developed from =variants with their own articles =
}}

The Zlin Trener is a family of aircraft that was based on a basic training aircraft, the Z-26.

The original Z-26 was designed in the 1940s and produced in 1946 by the Czechoslovakian company, Moravan 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 Z-26 variants were 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

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.[4]
  • Z-226 – more powerful Walter Minor 6-III six-cylinder engine, C-205
    • Z-226A – single-seat aerobatic aircraft
    • Z-226B – glider tug aircraft
    • Z-226T – basic training version
  • Z-326 – Introduced in 1959, with an electrically retractable undercarriage (standard on future models)[5]
  • 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 – with Walter M 337 supercharged engine.(used in Romania by sportive aviation with M-137 Sh engines under the name Zlin-726 Universal).
    • Z-726K – Improved version.

In 1956, deliveries began of the Z326 Trener-Master and Z326A Akrobat.[6] 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.[7]

Operators

Military operators

{{AUT}}
Austrian Air Force
{{CUB}}
{{CZS}}
Czechoslovakian Air Force
{{DDR}}
{{EGY}}
{{MOZ}}
{{YEM}}

Specifications (Z-726)

{{Aircraft specs
|ref=Jane's All The World's Aircraft 1976–77 [8]
|prime units?=met


|genhide=
|crew=two
|capacity=
|length m=7.975
|length ft=
|length in=
|length note=
|span m=9.875
|span ft=
|span in=
|span note=
|height m=2.06
|height ft=
|height in=
|height note=
|wing area sqm=14.89
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=root:NACA 2418; tip:NACA 4412
|empty weight kg=700
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=1000
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Avia M 137AZ
|eng1 type=6-cyl, air-cooled inverted in-line piston engine
|eng1 kw=134
|eng1 hp=
|eng1 shp=
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=236
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=216
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=98
|stall speed mph=
|stall speed kts=
|stall speed note=(flaps down)
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=440
|range miles=
|range nmi=
|range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=4500
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|climb rate ms=5
|climb rate ftmin=
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|more performance=
|avionics=
}}

See also

{{Commons category-inline|Zlín Z-26}}{{aircontent
|related=
|similar aircraft=
|lists=
|see also=
}}

References

1. ^Mourik 2001, p.61.
2. ^Frawley 1997, p.198.
3. ^Taylor 1989, p.908.
4. ^Frawley 1997, p.198.
5. ^Frawley 1997, p.198.
6. ^Frawley 1997, p.198.
7. ^Frawley 1997, p.198.
8. ^Taylor 1976, pp. 33–34.
  • Frawley, Gerard. The International Directory of Civil Aircraft. Aerospace Publications Pty Ltd, 1997 {{ISBN|1-875671-26-9}}
  • 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}}.
{{Zlín aircraft}}{{DEFAULTSORT:Zlin Z 26}}

6 : Aerobatic aircraft|Czechoslovakian military trainer aircraft 1950–1959|Zlín aircraft|Single-engined tractor aircraft|Low-wing aircraft|Aircraft first flown in 1947

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