This training double-seater had its maiden flight near Salzburg/Austria in 1940. It was based on an advanced concept of the Mü10 'Milan' with flaps and retractable gear. Circles had to be flown almost exclusively with the rudder, since the aileron efficiency was close to zero. Until November 1941, it absolved 45 hours of flight until it was grounded due to the WW2 situation.

Wing span 19m
Wing area 18.8m²
Aspect ratio 19.2
Wing load 24.0kg/m²
Empty weight 260kg
Max. weight 450kg
Min. sink rate(72km/h) 0.7m/s
Glide ratio (83km/h) 29

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