CESSNA
MODEL 208B 867 SHP
GARMIN G1000
AVIONICS/AUTOPILOT
ATTITUDE FAIL AND/OR RED X OVER HEADING DISPLAY
ON PFD
IF BOTH SIDES
1. Attitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
Turn off air conditioner to reference magnetic compass.
2. Heading . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
3. Land as soon as practical.
•
The autopilot will disconnect and may not be reengaged.
•
Reference the GPS track on MFD/PFD map to improve
situational awareness. GPS will continue to display
correct GPS based map, position, and track.
•
Air conditioner will affect the magnetic compass.
IF ONE SIDE ONLY
1. Standby Attitude Gyro. . . . . . . . . . . . . . . . . . . . . . . . MONITOR
2. Affected PFD SENSOR Softkey . . . . . . . . . . . . . . . . . . . PRESS
3. Affected PFD AHRS1 or AHRS2 Softkey . . . . . . . . . . . SELECT
4. PFD ADI Displays . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM
(amber BOTH ON AHRS1 or AHRS2 shown on both PFDs)
The autopilot will disconnect and may not be reengaged.
FAA APPROVED
208BPHCUS-00
ABNORMAL PROCEDURES
(Continued)
(using standby attitude gyro)
NOTE
(using magnetic compass)
NOTE
NOTE
SECTION 3
(opposite side AHRS)
U.S.
3-77