Zlín Z-26

Airplanes

Length

7.975 m

Flat Wing Span

9.875 m

Height

2.06 m

Flat Wing Area

14.89 m²

Cruise Speed

216 km/h

Max Speed

236 km/h

Max Ceiling

4500 m

Number of Engines

Maximum Take-Off Weight

1 t (paragliders: kg)

Maximum Range

440 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Zlín Z-26	1	440

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Ambrosini S.1001	Alfa Romeo 110	7.8	9.9	3	Compare
Auster Aiglet Trainer	De Havilland Gipsy Major	7.0104	9.7536		Compare
Blackburn Type D	Gnome Omega	8	9.78		Compare
Beechcraft CT-134 Musketeer		7.62	9.7536	2	Compare
Beechcraft Model 17 Staggerwing		7.9248	9.7536		Compare
Boeing X-45		7.9248	10.0584		Compare

All data (20 fields)

Name: Zlín Z-26
Manufacturer: Zlínská Letecká Akciová Spolecnost
Description: The Zlin Z-26 Trenér was a tandem-seat basic training aircraft built by the Czechoslovak company Moravan.
Production End: 1977-01-01
Designer: Zlínská Letecká Akciová Spolecnost
Type: Training aircraft
Length (m): 7.975
Height (m): 2.06
Max Speed (km/h): 236
Cruise Speed (km/h): 216
Min Speed (km/h): 98
Max Ceiling (m): 4500
Rate of Climb (m/s): 5
National Origin: Czechoslovakia
Powerplant Description: 1 × Avia M 137AZ 6-cyl, air-cooled inverted in-line piston engine, 134 kW (180 hp) each
Primary Users: Czechoslovak Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Zl%C3%ADn_Z-26
Flat Wing Span (m): 9.875
Flat Wing Area (m²): 14.89
Number of Engines: 1