Cockpit Reference Guide

Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-02 Rev. B
55
Annunciations & Alerts
Flight
Instruments EIS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
Condition Annunciation Description
Elevator
Mistrim Up A condition has developed causing the
pitch servo to provide a sustained force. Be
prepared to apply nose up control wheel force
upon autopilot disconnect.
Elevator
Mistrim Down A condition has developed causing the
pitch servo to provide a sustained force. Be
prepared to apply nose down control wheel
force upon autopilot disconnect.
Aileron Mistrim Left A condition has developed causing the roll
servo to provide a sustained left force. Ensure
the slip/skid indicator is centered and observe
any maximum fuel imbalance limits.
Aileron Mistrim Right A condition has developed causing the roll
servo to provide a sustained right force.
Ensure the slip/skid indicator is centered and
observe any maximum fuel imbalance limits.
Rudder Mistrim Left A condition has developed causing the yaw
servo to provide a sustained force. Ensure the
slip/skid indicator is centered and observe any
maximum fuel imbalance limits.
Rudder Mistrim Right A condition has developed causing the yaw
servo to provide a sustained force. Ensure the
slip/skid indicator is centered and observe any
maximum fuel imbalance limits.
Preflight Test
Performing preflight system test. Upon
completion, the aural alert will be heard.
Preflight system test has failed.