Garmin Software Version 0857.09 User's Guide Page 78

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-03 Rev. A
62
Annunciations & Alerts
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
Annunciation
Text
Alerts Window Message Audio Alert
OIL PRESS LO L or R oil press is between 30 and 10 psi. Single Chime
FUEL QTY LO L or R fuel qty is less than or equal to 13 gal. Single Chime
ALT LOAD L or R alternator load exceeds 100 amps. Single Chime
ADVISORY ANNUNCIATION
Annunciation
Text
Alerts Window Message Audio Alert
BUSES TIED Right Bus is tied to Left Bus. None
ALERT MESSAGE
Alerts Window Message Audio Alert
PFD FAN FAILThe cooling fan for the PFD is inoperative.
None
MFD FAN FAILThe cooling fan for the MFD is inoperative.
None
AVIONICS FANThe cooling fan for remote avionics is inoperative.
None
AFCS ALERTS
Condition Annunciation Description
Pitch Failure Pitch axis control failure. AP is inoperative.
Roll Failure Roll axis control failure. AP is inoperative.
MET Switch Stuck, or Pitch
Trim Axis Control Failure
If annunciated when AP is engaged, take control
of the aircraft and disengage the autopilot. If
annunciated when AP is not engaged, move
each half of the MET switch separately to check
if a stuck switch is causing the annunciation.
Yaw Damper Failure YD control failure; AP also inoperative
System Failure AP and MET are unavailable. FD may still be
available.
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.
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