SECTION 3 CESSNA
ABNORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
AVIONICS/AUTOPILOT
AMBER AIL OR AIL INDICATION COMES ON
1. Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . GRIP FIRMLY
2. AP/TRIM DISC Button. . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
(high aileron control forces possible)
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 ELE INDICATION COMES ON
1. Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . GRIP FIRMLY
2. AP/TRIM DISC Button. . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
(high elevator control forces possible)
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
(high rudder control forces possible)
3. RUD TRIM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
4. Autopilot and Yaw Damper . . . . . . . . . . . ENGAGE (as desired)
208BPHCUS-003-66