CESSNA
SECTION 3
MODEL 208B 867 SHP
EMERGENCY PROCEDURES
GARMIN G1000
U.S.
FAA APPROVED
SPINS
Intentional spins are prohibited in this airplane. Should an inadvertent
spin occur, the following recovery technique can be used.
1.
RETARD POWER LEVER TO IDLE POSITION.
2.
PLACE AILERONS IN NEUTRAL POSITION.
3.
APPLY AND
HOLD
FULL RUDDER OPPOSITE TO THE
DIRECTION OF ROTATION.
4.
IMMEDIATELY
AFTER
THE RUDDER REACHES THE STOP,
MOVE THE CONTROL WHEEL
BRISKLY
FORWARD FAR
ENOUGH TO BREAK THE STALL. Full down elevator will be
required at aft center of gravity loadings to assure optimum
recoveries.
5.
HOLD
THESE CONTROL INPUTS UNTIL ROTATION STOPS.
Premature relaxation of the control inputs may extend the
recovery.
6.
AS ROTATION STOPS, NEUTRALIZE RUDDER AND MAKE A
SMOOTH RECOVERY FROM THE RESULTING DIVE.
NOTE
If the rate of the spin makes determining the direction of
rotation difficult, the magenta turn rate indicator at the top of
the HSI compass card will show the rate and direction of
the turn. The HSI compass card will rotate in the opposite
direction. Hold opposite rudder to the turn vector direction.
208BPHCUS-00
3-49
Summary of Contents for Cessna Grand Caravan Ex 208B
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