ZLIN AERO

Zlín Z-142

The Zlín Z‑142 is a four‑seat, low‑wing trainer and touring aircraft produced by the Czech manufacturer ZLIN AERO. Its development began in the early 1970s as an evolution of the successful Z‑37 and Z‑138 agricultural and sport prototypes, with the first flight occurring on 9 May 1972. Designed to replace the older Z‑26 series, the Z‑142 combined a robust steel tube fuselage with a semi‑monocoque aluminum wing, delivering a versatile platform for flight schools, aero clubs, and private owners. Power is supplied by a Lycoming O‑360‑A1A engine delivering 180 hp, driving a two‑position variable‑pitch propeller that gives the aircraft respectable climb performance and a cruise speed of around 200 km/h (108 kn). The cockpit features side‑by‑side seating, dual controls, and a modern avionics suite that can be upgraded to glass‑panel displays. Its forgiving handling, low operating cost, and easy maintenance have made the Z‑142 popular across Eastern Europe and beyond, where it has logged thousands of training hours. The type exemplifies ZLIN AERO’s reputation for solid, economical designs that bridge the gap between basic trainers and light touring aircraft, contributing to the continued vitality of general aviation in the region.

Classification

Production & History

First Flight
1978
Service Entry
1980

Design & Classification

Primary Use
Country of Origin
Manufacturer
ZLIN AERO
Engine
Avia M 337
Operator
Czech Air Force Algerian Air Force Algeria
Wikidata ID
Q17484765