Max Holste MH.52 - Development and Construction

Development and Construction

Developed in the mid-1940s, the MH.52 was a low-wing cantilever monoplane with twin fins and rudders and a fixed tricycle landing gear. It had a cockpit with side-by-side seating for the pilot and trainee or passenger. The canopy was framed with forward-opening transparent sliding doors. The prototype first flew on 21 August 1945. The aircraft was powered by a variety of inline engines developing between 95 and 150hp (71 to 112kW).

A development of the MH.52 was the sole MH.53 Cadet which had a fixed tailwheel landing gear and a lower powered 135hp (101kW) de Havilland Gipsy Major 10 engine.

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