Avia BH-29

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Table of Contents

Initial Development and Specifications

In the summer of 1927, the Avia company, on its own initiative, developed a trainer aircraft for the Czechoslovak Air Force. The new aircraft, designated BH-29, was a two-seater wooden single-strut biplane, equipped with an 85 hp (63 kW) Walter NZ-85 seven-cylinder air-cooled radial engine.

Prototypes and Testing Challenges

The aircraft’s prototype (registration number L-BONN, later OK-ONN) took to the air on August 29, 1927. During testing, it became clear that the thick-profile wing complicated piloting and prevented the aircraft from achieving its projected performance.

As a result, a second prototype (registration number L-BONQ, later OK-LIR) was built with classic wings and a more powerful Walter NZ-120 engine (120 hp). However, even the modernized version failed to attract the interest of the Czech military.

Unsuccessful Military Adoption and European Tour

An ambitious European promotional tour, advertising the BH-29 across eighteen countries, also proved unsuccessful.

Technical Specifications

Modification	BH-29
Wingspan, m	9. 80
Length, m	7.40
Wing area, m2	25.00
Empty weight	830
Normal takeoff weight	1090
Engine type	1 Piston engine Walter NZ-85
Power, hp	1 х 85
Maximum speed, km/h	145
Cruising speed, km/h	105
Practical range, km	600
Rate of climb, m/min	150
Practical ceiling, m	4000
Crew	2

Image and diagram gallery of the Avia BH-29

Czechoslovakia

ArchivoAéreo Editorial Team

A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.

Sources & Accuracy

The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.

BH-29	BH-29
BH-29	BH-29