What I would be interested to know is what the planned spin recovery control inputs were. The stick is moved almost continuously at a relatively high frequency with any input never being held for more than about 1 sec. To effect spin recovery in any aircraft you must apply the desired control input then hold it. If, after a specified time or number of turns, there has been no response then the prolonged spin recovery inputs should be applied. This philosophy does not appear to have been used in this case.