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[<strong>Su</strong>-<strong>25T</strong> Frogfoot]<br />
<strong>DCS</strong><br />
may increase in roll to the point of causing a wing-over, where the aircraft will roll violently toward<br />
one side. To correct this and counteract the stall, push the stick forward.<br />
When flying in normal <strong>Fli</strong>ght Configuration and Maneuvering Configuration, a spin can only be<br />
induced intentionally. In normal <strong>Fli</strong>ght Configuration and Maneuvering Configuration, the spin will be<br />
alleviated once the stick is placed into its neutral position. To expedite the recovery out of the spin,<br />
the standard technique is to push the stick forward and apply opposite rudder.<br />
When flying in Take-off/Landing Configuration, a spin can be entered unintentionally if the angle of<br />
attack reaches beyond critical limits, especially if the aircraft’s center of gravity is aft of center. The<br />
CG will shift aft in an <strong>Su</strong>-25 if the cannon ammunition has been expended and is always aft in the <strong>Su</strong>-<br />
<strong>25T</strong>. Once the aircraft has entered a spin in this configuration, it is practically impossible to recover.<br />
Eagle Dynamics 49
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