Zlin Z-126 Trener

Zlin Z-26 Trener

PaísChecoslováquia
TipoAeronaves de treinamento
Produzido1948–1977
ConstruídoDesconhecido

O Zlin Z-26 Trener foi uma aeronave de treinamento básico construída pela empresa tchecoslovaca Moravan. Um monoplano de asa baixa de construção em grande parte de madeira, foi desenvolvido em uma série de treinadores totalmente metálicos. Vários também foram produzidos em variantes acrobáticas, conhecidas como Akrobat.

Fonte: Zlin Z-26 Trener na Wiki

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

Veja também:

Segunda Guerra Mundial: A História Visual Definitiva da Blitzkrieg à Bomba Atômica (DK Definitive Visual Histories) - Amazon Segunda Guerra Mundial: Mapa por Mapa (DK, História, Mapa por Mapa) - Amazônia

Mais informações:

O 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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