Originally Posted by
Clandestino
Benign stall characteristics regarding the certification testing mean there is pronounced stall buffet, there is natural tendency to pitch down at stall (it doesn't imply it has be such that it can not be overriden by application of controls), there is no violent roll associated with airflow separation and aeroplane can be unstalled using conventional technique.
Sure - what I was getting at was that the design should not, for example, suffer an aggressive wing-down tendency once stalled. Your description is more precise than mine.
My information regarding the flight testing regime is a little vague in respect to precisely how far stall testing went, and does not specify whether going beyond the stall boundary was performed or not. If you have better info, it's all good.
