No I wasn't. I was referring to STANDARD STALL RECOVERY:
FULL POWER and, at the same time, Control Column Centrally Forward until a pitch attitude is reached at which the stall identification/sign/symptom (call it what you will) ceases. Maintain that pitch attitude
Then - and only then - level wings and recover from the descent.
AT ALL TIMES during Standard Stall Recovery, Rudder is only used to maintain balanced flight .
All the BS about 'torque effects', 'secondary effect of power inviting an incipient spin' on this thread should be ignored. If a wing drops at the stall, do not attempt to control it with aileron, rudder or anything else - just let it drop. Then follow Standard Stall Recovery and use aileron to roll the wings level, rudder only as required to maintain balanced flight WHEN THE STALL HAS CEASED!!