Man, if I had $1 for every time those words came out of my mouth I'd have my own 421 by now...
I notice for the Elevator, you say "ELEVATOR TO
RECOVER ONCE OUT OF THE SPIN". Is this referring to the pitching to a level flight attitude, assuming the spin will stop solely through the application of rudder after the aggravation (P&A) is removed? I can think of several aggravated and non-aggraved spin modes in a few different aircraft where this wouldn't work (or work fast enough). You can mash the recovery rudder and everything will just keep spinning until the elevator is moved in attempt to reduce the AOA. Direction and amount amount of control displacement being dependent on whether the spin is upright or inverted, the type of airplane and nature of the spin. This is also assuming the elevator is still effective in the spin condition, which might not be the case in the airplanes you're in..?
For E, I use, Elevator- Put the stick where it Isn't. This is based on the idea of AOA control and too much pulling or pushing contributed to the situation. That, and I try to differentiate between the Beggs and P.A.R.E recovery procedures.
Thanks for taking the time to respond! When someone jumps in the pool and starts talking about inverted spins in a King Air, this usually happens...