What actions are taken when applying OCF boldface while in a steady-state spin?

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When applying OCF (Operating Control of Flight) boldface during a steady-state spin, the emphasis is placed on implementing appropriate anti-spin control inputs. This is vital because the primary goal in a spin situation is to regain control of the aircraft and recover from the spin safely. Anti-spin inputs typically involve a combination of control inputs such as full opposite rudder and forward control stick to reduce the angle of attack and enhance the chances of recovery from the spin.

The other options, while potentially relevant in different flying contexts, do not directly address the critical action required to recover from a spin. Throttle adjustments are often necessary in various flight scenarios but aren’t the priority in a spin recovery. Trim settings can aid in flight stability, but they don’t directly correlate with the immediate actions required in a spin recovery situation. Similarly, altitude maintenance may be a strategic consideration during flight but is not an immediate action during the process of spin recovery. Thus, focusing on anti-spin control inputs is the most pertinent and effective measure to address the situation.

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