Zlin Trener
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Trener | |
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Z-126 Trener II |
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Type | Training aircraft |
Manufacturer | Moravan Otrokovice |
Produced | 1953-? |
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 late 1940s and produced in early 1950s by the Czechoslovakian company, Moravan Otrokovice. It was powered by a single four-cylinder piston engine, the Walter Minor 4-III.
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[edit] Variants
The following variants were progressive improvements on the Z-26:
- Z-26 - two-seat primary trainer aircraft.
- Z-126 - all-metal wing instead of original wooden wing
- Z-226 - more powerful Walter Minor 6-III six-cylinder engine, A.K.A. C-205
- Z-226A - single-seat aerobatic aircraft
- Z-226B - glider tug aircraft
- Z-226T - basic training version
- Z-326 - with an electrically retractable undercarriage
- Z-526 - with the Walter M 137 six-cylinder engine
- Z-526A - single-seat aerobatic aircraft
- Z-526F - Improved version.
- 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.
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.
[edit] Military Operators
[edit] Specifications (Z-26)
General characteristics
- Crew: Two (pilot and instructor)
- Length: 7.42 m (24 ft 4 in)
- Wingspan: 10.28 m (33 ft 9 in)
- Height: ()
- Wing area: 14.9 m² (160.3 ft²)
- Empty weight: 510 kg (1,122 lb)
- Max takeoff weight: 765 kg (1,683 lb)
- Powerplant: 1× Walter Minor 4-III, 78 kW (105 hp)
Performance
- Maximum speed: 205 km/h (110 knots, 126 mph)
- Cruise speed: 180 km/h (97 knots, 111 mph)
- Range: 600 km (324 nm, 370 mi)
- Service ceiling 4,800 m (15,744 ft)
- Rate of climb: 3.3 m/s (649.5 ft/min)
- Wing loading: 51.5 kg/m² (10.5 lb/ft²)
[edit] See also
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