SECTION 3 CESSNA
EMERGENCY PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
AUTOPILOT OR ELECTRIC TRIM FAILURE
RED PTRM MESSAGE COMES ON
1. Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . GRASP FIRMLY
(regain control of airplane)
2. AP/TRIM DISC Button. . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
(high elevator control forces possible)
3. ELEVATOR TRIM . . . . . . . . . . . . . . . . . . ADJUST MANUALLY
(as necessary)
Actuate each half of the pilot and copilot manual electric
pitch trim switches separately to make sure trim does not
actuate with only one half switch.
IF RED PTRM MESSAGE REMAINS ON
4. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . DO NOT RE-ENGAGE
5. A/P CONT Circuit Breaker. . . . . . . . . . . . . . . . . OPEN (pull out)
(AVN BUS 1, second row, third breaker from left side)
Following an autopilot, autotrim or manual electric
trim system malfunction, do not engage the
autopilot until the cause of the malfunction has
been corrected.
IF RED PTRM MESSAGE GOES OFF
4. Continue flight as planned without the use of the autopilot.
Following an autopilot, autotrim or manual electric
trim system malfunction, do not engage the
autopilot until the cause of the malfunction has
been corrected.
208BPHCUS-00
3-36