Beagle
FULL POWER and Control Column centrally forward until Stall Identification ceases.
I was criticised on a check flight with an FIC for the order in which I explained standard stall recovery.
I was told it should be control column forward to reduce the angle of attack of the wings and then apply full power.
Reason ? The effect of applying full power causes the nose to raise which increases the angle of attack, thereby prolonging the stall !!
Therefore standard stall recovery:
Relax the back pressure to reduce the angle of attack of the wings.
Apply full power.
Maintain aircraft in balance by controlling yaw with rudder.
Once speed increases past Vx, select a climbing attitude.
Check carb heat to off, unless selected off as airspeed was reducing.
To quote a legendary CFI, instructing is all about terminology ! I realise its being pedantic......however that was the critique of a recent check flight
TJ