Zlin Z-126 Trener

Zlin Z-26 Trener

PaeseCecoslovacchia
digitareAerei da addestramento
Prodotto1948–1977
CostruitoInconsapevole

Le Zlin Z-26 Trener era un aereo da addestramento di base biposto costruito dalla società cecoslovacca Moravan. Un monoplano ad ala bassa di costruzione in gran parte in legno, è stato sviluppato in una serie di addestratori interamente in metallo. Molti sono stati prodotti anche in varianti acrobatiche, conosciute come Akrobat.

fonte: Zlin Z-26 Trener su Wiki

Zlin Z-126 Trener
FotografoUnknow
LocalizzazioneInconsapevole
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Pilot's Handbook of Aeronautical Knowledge (2023): FAA-H-8083-25C - Amazon

Vedi anche:

Seconda guerra mondiale: la storia visiva definitiva dalla guerra lampo alla bomba atomica (DK Definitive Visual Histories) - Amazon Seconda guerra mondiale Mappa per Mappa (DK Storia Mappa per Mappa) - Amazon

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Le Zlin Z-26 Trener was a tandem-seat basic training aircraft built by the Czechoslovakian company Moravan in the late 1940s. 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 on October 20, 1947, and entered production in 1948. It was designed to replace the Bücker Jungmann and Bestmann as the primary trainer for the Czechoslovakian Air Force. The Z-26 Trener was later developed into a series of all-metal trainers with retractable undercarriage and more powerful engines. The most successful variants were the Z-326 Trener-Master and the Z-526 Trener 6, which were also used for aerobatic competitions and demonstrations. Several single-seat versions were also produced, known as the Akrobat. The Zlin trainers were exported to many countries around the world and won several awards for their performance and maneuverability. The Zlin Z-26 Trener was a versatile and reliable aircraft that served as an excellent platform for basic training and aerobatics. It had a wingspan of 10.29 m (33 ft 9 in), a length of 7.8 m (25 ft 7 in), and a height of 2.06 m (6 ft 9 in). It had a maximum takeoff weight of 820 kg (1,808 lb) and a cruising speed of 195 km/h (121 mph). It had a service ceiling of 5,300 m (17,388 ft) and a range of 485 km (301 mi). It could perform loops, rolls, spins, snaps, hammerheads, cuban eights, immelmans, split-ses etc.

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