3-6 SPINS
Should a spin be entered inadvertently, the following recovery technique
should be used.
1. Bring the power lever to the IDLE position.
2. Place the ailerons in the NEUTRAL position.
3. Apply and HOLD full rudder, opposite to the direction of rotation.
4. Immediately after the rudder reaches its stop, move the control wheel
briskly forward, far enough to break the stall. (Full down elevator may be
required to break the stall in an aft C.G. loading.)
5. Hold these control inputs until the rotation completely stops.
6. As the rotation stops, return the rudder to neutral and make a smooth
recovery from the resulting dive. If the aps were extended as the spin was
entered, retract the aps to prevent a ap overspeed condition.
WARNING: This airplane is certied in the normal category and
intentional spinning of the aircraft is prohibited.
To Next Page
Loading...