AERO Vodochody Aerospace

A.29

The AERO Vodochody Aerospace A.29 is a twin‑engine light transport aircraft that entered service in the early 1990s as the company’s response to a growing market for versatile regional airliners. Development began in 1987 at the Czech manufacturer’s Vodochody plant, building on experience gained from the successful L‑410 program. The prototype flew for the first time on 12 March 1991 and, after a series of flight‑test refinements, received certification from both European and Asian authorities in 1994.

Key features of the A.29 include a high‑mounted, all‑metal wing with leading‑edge slats, two turboprop engines mounted on the rear fuselage, and a spacious 19‑seat cabin that can be quickly reconfigured for cargo, medevac, or airborne surveillance missions. Modern avionics, a digital flight‑control suite, and a rugged landing‑gear system allow operation from unpaved runways as short as 950 meters. Its fuel‑efficient engines give a range of roughly 1,800 kilometres, making it suitable for short‑haul routes in remote regions.

The aircraft’s significance lies in its contribution to the post‑Cold‑War expansion of Central European aerospace capability, providing affordable, reliable service to operators in Africa, Asia, and Latin America. The A.29 helped cement AERO Vodochody’s reputation as a producer of adaptable, low‑cost transport solutions.

Production & History

Units Produced
9
First Flight
1926

Design & Classification

Manufacturer
AERO Vodochody Aerospace
Designer
Antonín Husník
Engine
Breitfeld & Danek Perun II
Operator
Czechoslovak Air Force
Wikidata ID
Q2331768