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Avia BH-6 Fighter

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Avia BH-6 Fighter

The Avia BH-6 was a fighter aircraft developed by the Czechoslovak firm Avia. It was designed by engineers Pavel Beneš and Miroslav Hain, commissioned by the Czechoslovak Air Force. The designers focused heavily on achieving clean aerodynamic forms, simultaneously developing both a biplane (BH-6) and a monoplane (BH-7) variant.

Innovative Design and Development

The aircraft featured traditional wooden construction and was armed with two 7.7-mm Vickers machine guns. The BH-6 prototype underwent flight tests in 1923, conceived as a biplane alongside the BH-7 monoplane, which was powered by a V-shaped Hispano-Suiza 8Fb engine manufactured in Czechoslovakia by “Skoda.”

Both aircraft, largely fabric-covered wooden structures, shared an identical thin, elongated fuselage, tail unit, and landing gear. The BH-6’s wing arrangement was particularly unusual: a flat upper wing, with a smaller span than the lower wing, was held above the fuselage by a single streamlined strut. The lower wing, featuring a transverse V, was separated from the upper wing on each side by individual interplane struts angled inwards from bottom to top.

Flight Testing and Fate

Tragically, the sole BH-6 aircraft was lost in an aviation accident almost immediately after its flight tests commenced, bringing an early end to its promising development.

Technical Specifications

Modification BH-6
Wingspan, m 9. 98
Length, m 6. 47
Height, m 2. 88
Wing area, m2 22. 60
Empty weight 878
Normal takeoff weight 1180
Engine type 1 Piston engine Hispano-Suiza 8 Ba
Power, hp 1 x 300
Maximum speed, km/h 220
Cruising speed, km/h 200
Practical range, km 500
Practical ceiling, m 7000
Crew 1
Armament two forward-firing 7.7-mm Vickers machine guns

Image and diagram gallery of the Avia BH-6 Fighter

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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.