- Variants
- Operators Military operators
- Specifications (Z-726)
- See also
- References
{{Refimprove|date=August 2008}}name = Trener | image =Image:ZLIN Z.126 TRENER 2 D-EWAC l.jpg | caption =Z-126 Trener II }}{{Infobox aircraft type | type = Training aircraft | manufacturer = Moravan Otrokovice | designer = | first flight = | introduction = | retired = | status = | primary user = | more users = | produced =1948–1977 | number 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] VariantsThe 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= }}References1. ^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 |