Cessna SKYCATCHER 162 - Spins

CESSNA SECTION 6
MODEL 162 EMERGENCY PROCEDURES
GARMIN G300
U.S.
SPINS
Should an inadvertent spin occur, the following recovery procedure
should be used:
1. IMMEDIATELY RETARD THROTTLE TO IDLE POSITION.
2. PLACE AILERONS IN NEUTRAL POSITION.
3. APPLY AND HOLD FULL RUDDER OPPOSITE TO THE
DIRECTION OF ROTATION AND MOVE CONTROL STICK
BRISKLY FORWARD FAR ENOUGH TO BREAK THE STALL.
Full down elevator may be required at aft center of gravity
loadings to assure optimum recoveries.
4. HOLD THESE CONTROL INPUTS UNTIL ROTATION STOPS.
Premature relaxation of the control inputs may extend the
recovery.
5. AS ROTATION STOPS, NEUTRALIZE RUDDER, WINGS
LEVEL, FLAPS UP AND MAKE A SMOOTH RECOVERY
FROM THE RESULTING DIVE. AVOID OVERSTRESSING
AND OVERSPEEDING THE AIRFRAME.
NOTE
If the rate of the spin makes determining the direction of
rotation difficult, the magenta turn rate trend vector in the
heading strip over the PFD Attitude Indicator will show the
rate and direction of the turn. The HSI compass card will
rotate in the opposite direction. Hold full rudder opposite the
direction of the turn indicated by the turn rate trend vector.
162PHUS-00
6-35