avia.wikisort.org - Aeroplane
The Zlin Z-526 Akrobat is a Czech sports plane used in aerobatics.
| Zlin Z-526 | |
|---|---|
 | |
| Role | Sports plane |
| Manufacturer | Zlin Aircraft |
| First flight | 1959 |
| Number built | 1,400+ |
History
The Z-526 was originally designed by Zlin Aircraft in 1959. Its two-seat version is called the Trener-Master
The Z 526's layout was organized with the pilot in the rear, and the student in front. The aircraft could be equipped also with tip tanks and a constant speed propeller. The Z-526F was introduced in 1968 and was equipped with a 135 kW (180 hp) Avia M 137A engine, the export version Z-526L differing by being equipped with a 150 kW (200 hp) Lycoming AEIO-360 flat-four. Single-seat versions included the Z-526A, Z-526AS, and the Z-526AFS.
The Z-526 AFM was built between 1981 and 1984 and was powered by a 155 kW (210 hp) Avia M337 engine, had tip tanks and a lengthened fuselage. The aircraft was later developed into the Zlin Z-726.
More than 1,400 Z-526s were manufactured, many for military and private flying schools.
Variants
- Z-526
- Two-seat version
- Z-526A
- Single-seat version
- Z-526AF
- Single-seat version
- Z-526AFS
- Single-seat version
- Z-526AFM Condor
- powered by an Avia M337 inverted six-cylinder engine giving 210hp(157kW)
Aircraft On Display
- Serbia
- Z-526M - Museum of Aviation (Belgrade) in Belgrade[1]
Specifications (Z-526 Trener-Master)
Data from Jane's all the World's Aircraft 1968–69[2]
General characteristics
- Crew: 2 (526A / 526F - 1)
- Length: 7.8 m (25 ft 7 in)
- Wingspan: 10.6 m (34 ft 9 in)
- Height: 2.06 m (6 ft 9 in)
- Wing area: 15.45 m2 (166.3 sq ft)
- Airfoil: root: NACA 2418; tip: NACA 4412[3]
- Empty weight: 680 kg (1,499 lb)
- Z 526A 650 kg (1,430 lb)
- Max takeoff weight: 975 kg (2,150 lb) (trainer)
- 940 kg (2,070 lb) (aerobatic)
- Z 526A 830 kg (1,830 lb) (aerobatic)
- Fuel capacity: 2x 45 l (12 US gal; 9.9 imp gal) tanks in the wing roots, with a 7 l (1.8 US gal; 1.5 imp gal) gravity collector tank in the fuselage.
- Powerplant: 1 × Walter Minor 6-III 6-cylinder air-cooled inverted in-line piston engine, 120 kW (160 hp) (later variants 155 kW (208 hp) Avia M337)
- Propellers: 2-bladed V 503, 1.9 m (6 ft 3 in) diameter constant-speed propeller
Performance
- Maximum speed: 220 km/h (140 mph, 120 kn) at sea level
- Cruise speed: 208 km/h (129 mph, 112 kn) (70% power)
- Landing speed: 78 km/h (48 mph; 42 kn)
- Never exceed speed: 320 km/h (200 mph, 170 kn)
- Range: 580 km (360 mi, 310 nmi)
- Ferry range: 610 km (380 mi, 330 nmi) with wing-tip tanks
- Service ceiling: 5,000 m (16,000 ft)
- Rate of climb: 5 m/s (980 ft/min) at sea level
- Take-off run: 220 m (720 ft)
- Landing run: 135 m (443 ft)
References
- "Muzej Yugoslovenskog Ratnog Vazduhoplovstva - Belgrade - Serbia".
- Taylor, John W.R., ed. (1968). Jane's all the World's Aircraft 1968–69. London: Sampson Low, Marston & Company. p. 26.
- Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.
External links
- Moravan Aeroplanes, Inc., The Czech Republic - manufacturer
- Zlin Treners -This aeroplane teaches you to fly!-
На других языках
[de] Zlín Z-526
Die Zlín Z-526 ist ein tschechoslowakisches Sport- und Kunstflugzeug der Trenér-Reihe. Die zweisitzigen Ausführungen tragen den Beinamen Trenér Master, die einsitzigen werden als Akrobat und Akrobat Spezial bezeichnet. Bekannt wurde die Z-526 durch den Gewinn der Kunstflug-Weltmeisterschaft 1968 in der Einzel- (Erwin Bläske, DDR)[1] und Mannschaftswertung (DDR).- [en] Zlín Z 526
[it] Zlín Z-526
Lo Zlín Z-526 è un aereo multiuso, monomotore monoplano ad ala bassa con capacità acrobatiche, sviluppato dagli anni sessanta dall'allora azienda aeronautica cecoslovacca Morovan.Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
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