Standard stall recovery as far as I am aware for all types has been standardised by a huge number of people far more intelligent than me as follows:
Disconnect Ap/AT as needed
Smoothly apply nose down pitch control to reduce angle of attack until the signs of the stall have ceased.
Roll in the shortest direction to wings level. Etc.
The first two actions hold true in every fixed wing aeroplane under normal flight conditions (ie not aerobatics). How you roll wings level will depend on type, don't use rudder in a 737 but on biz jets perhaps it is appropriate.
The sooner the industry wakes up to the fact that, a wing drop is a sing of the stall and that applying nose down pitch control is the first and most important action, the better.