R.W.D. 10
1933
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R.W.D. 10

To provide Polish flying clubs with an aerobatic trainer, the R.W.D. team developed yet another braced high-wing monoplane, the single-seat R.W.D.10, of which the prototype flew for the first time in April 1933. Development of this aircraft to certification stage proved difficult, certification not being gained until 1936, but eventually about 30 aircraft were built. Production aircraft were somewhat refined by comparison with the prototype and these 7.50m span aircraft, powered as standard by a 82kW P.Z. Inz Junior inline engine, had a maximum speed of 230km/h.

3-View 
R.W.D. 10A three-view drawing (711 x 1065)


Specification 
 MODELR.W.D. 10
 PERFORMANCE
    Max. speed230 km/h143 mph

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