
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-03 Rev. A
63
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 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 of the test, the aural alert will be
heard.
Preflight system test has failed.
TAWS-B ALERTS
Alert Type
PFD/MFD
TAWS-B Page
Annunciation
MFD
Pop-Up Alert
Aural Message
Excessive Descent
Rate Warning (EDR)
“Pull Up”
Reduced Required
Terrain Clearance
Warning (RTC)
or
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
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