SECTION 3
ABNORMAL PROCEDURES
AVIONICS/AUTOPILOT
AMBER AIL OR AIL INDICATION COMES ON
1. Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . GRIP FIRMLY
2. AP/TRIM DISC Button. . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
The yaw damper does not need to be disconnected for this
procedure. Therefore it is permissible to use the left half of
either manual electric pitch trim switch or one press of the
AP button on the autopilot mode control panel to disconnect
the autopilot.
3. AILERON TRIM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRIM
4. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE (as desired)
AMBER
ELE OR
1. Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . GRIP FIRMLY
2. AP/TRIM DISC Button. . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
The yaw damper does not need to be disconnected for this
procedure. Therefore it is permissible to use the left half of
either manual electric pitch trim switch or one press of the
AP button on the autopilot mode control panel to disconnect
the autopilot.
3. Elevator Trim Switch . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
4. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE (as desired)
AMBER RUD OR RUD INDICATION COMES ON
1. Rudder Pedals . . . . . . . . . . . . . . . . . . . . . . . . . HOLD FIRMLY
2. AP/TRIM DISC Button. . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
3. RUD TRIM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
4. Autopilot and Yaw Damper . . . . . . . . . . . ENGAGE (as desired)
3-66
(high aileron control forces possible)
NOTE
ELE INDICATION COMES ON
(high elevator control forces possible)
NOTE
(high rudder control forces possible)
U.S.
CESSNA
MODEL 208B 867 SHP
GARMIN G1000
FAA APPROVED
208BPHCUS-00