Hold the controls in this position until the rotation stops, then;
Neutralize the controls.
Check power to idle.
Level the wings by reference to the horizon.
Commence a smooth pullout. Ensure a minimum of 120 KIAS and do not
exceed 4.5 "Gs" or 24 units AOA.
Continue the pullout until the nose is positioned to the level flight attitude.
Recover with a minimum loss of altitude; emphasis is on smooth control
Check the oil pressure for a minimum of 40 psi.
Add power to the normal cruise power setting.
Check and report the oil pressure.
viii. Secure the autoignition.
During a spin, left and right fuel caution lights may illuminate
regardless of fuel state. Propeller RPM may decrease below normal
Erect spins with the propeller feathered are prohibited. Due to
reduced airflow, spin recovery may NOT be possible with the
propeller fully feathered. If propeller-feathering action is noted
during a spin, initiate recovery immediately.
Not reducing the power setting to 200 ft-lbs. after rolling wings level from the
Becoming disoriented and not initiating recovery.
Not neutralizing the controls as the rotation stops.
FLIGHT PROCEDURES 6-35