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| 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.
 | A three-view drawing (711 x 1065) |
| MODEL | R.W.D. 10 |
| PERFORMANCE |
| Max. speed | 230 km/h | 143 mph |
| lxbfYeaa, e-mail, 14.03.2024 05:58 20 reply | | Barry, 07.06.2016 18:49 There were some 22 plus the prototype built, the last two being completed in 1938. Extremely aerobatic they were retired from use in 9139.
Power plant 1 x 120 h.p PZInz Junior inverted 4 cylinder air cooled
Span 24'7" Length 20'4" Height 6'3" Wing area 97 sq ft
Empty weight 770 lb Loaded weight 1,050 lb
Max speed 135 mph Range 224 miles
Service ceiling 19,680 ft reply | | huaren, 20.06.2011 05:18 powered as standard by a 82kW P.Z. Inz Junior inline engine, had a maximum speed of 230km /h. reply |
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