The B-34 was an all-metal single-bay biplane of conventional configuration, with
tailwheel undercarriage. The mainwheels of the prototype were fitted with
large spats. The first
prototype underwent testing from 2 February 1932, leading to a large number of modifications being made, in particular the
tail and engine
cowling designs were considerably revised. The resulting
B-34.1 served as the prototype for the 12 production machines ordered by the Czechoslovak Air Force. These had an even larger vertical tail,
interplane struts of narrower chord, and no wheel spats. A second prototype, the
B-34.2 was fitted with an Avia Rr 29
radial engine but was never actually flown with it as the engine was not sufficiently developed. It was, however, offered to the Air Force under the redesignation
B-234. The second prototype was then fitted with an inline
Hispano-Suiza 12Ybrs piston engine, and later redesignated
B-534.1. ==Operational history==