Main overview :
Z-43 is a all-metal, single-engine low-wing monoplane. Wings are all metal design duralumin coated. The front part of fuselage steel tube welded and it”s coated by removable fibreglass covers, the rear part of fuselage is a duralumin half shell design. Plane is equipped with in-line, invert six cylinder engine AVIA M-337 AK with 156 kW (210 HP), supercharged by ůstandard radial compressor. Plane is also equipped with two blade, during flight adjustable propeller AVIA V-500A with 2000 mm diameter. Fixed main nose type gear makes flat steel springs, controllable front wheel is placed left from longitudinal axis of the plane.
History :
After successful production of the Z-26 aircraft family, the Czechoslovak aircraft manufacturer Moravan n.p. Otrokovice, began design of a new series of training aircraft, known as the Z-40 family. Unlike the previous tandem-seat aircraft the Z-40 family featured a side by side cockpit. It was available in two basic variants, a two seat trainer, the Zlín Z-42, and a four seat aircraft, the Zlin Z-43 capable of being used both as a trainer and a tourer. The resulting design is a single-engined low-wing monoplane of all metal construction and a fixed nosewheel undercarriage. The Z 43 shares 80% of its structure with the Z 42, but is fitted with a revised fuselage accommodating a four seater cabin and a more powerful engine. The Z-43's have wings with a little bit greater span. The Z-43 first flew on 10 December 1968, with production starting in 1972. Production of this type ended in 1977 after 80 aircraft were built.
Main technical data :
Engine model |
M 337 AK |
Engine power |
156 kW /210 k |
Max. speed |
286 km/h |
Travel speed |
180 km/h |
Max. range |
950 km |
Service ceiling |
5000 m |
Empty weight |
730 kg |
Max. take-off weight |
1350kg |
Wingspan |
9,76 m |
Length |
7,75 m |
Height |
2,91 m |
|