Search
Close this search box.

Zlin Z 26 Trener

The Zlin Z-26 Trener, a basic training aircraft with tandem seats, was produced by the Czechoslovakian firm Moravan.

Initially built mainly from wood, this low-wing monoplane evolved into a series of all-metal trainers.

Moreover, several aerobatic versions, branded as the Akrobat, were developed.

The original Z-26, designed in the 1940s and produced in 1946, was intended to serve as a basic trainer to succeed the Bücker Jungmann and Bestmann.

This low-wing monoplane was of mixed construction, with wooden wings and a welded metal tube fuselage, and it was equipped with a single four-cylinder piston engine known as the Walter Minor 4-III.

The Z-26 took to the skies in early 1947, outperforming the rival Praga 112 and consequently being selected for production in 1948.

Subsequent models were tailored for aerobatic competitions, with many privately owned by pilots.

The two-seat Trener and the single-seat Akrobat models garnered considerable success, securing multiple aerobatic awards during the 1960s.

Variants

Z-26

Two-seat primary trainer aircraft, 163 built.

Z-126

Introduced in 1953, Czech military designation C-105,

All-metal wing instead of original wooden wing.

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, it has an electrically retractable undercarriage. 

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 engine

Specifications

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 take-off weight

1,000 kg (2,205 lb)

Powerplant

1 × Avia M 137AZ 6-cyl,

Air-cooled inverted inline 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).

Sources
Zlins, Typenschau No.3- Detlef Billig.
www.zlinaircraft.eu.

 

 

Share on facebook