Garmin Software Version 0858.07 User's Guide Page 74

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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
58
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
ALT 2 LOAD Alternator 2 load exceeds 24 amps. Single Chime
BUS1 VOLT LO Bus 1 voltage less than 24VDC. Single Chime
BUS2 VOLT LO Bus 2 voltage less than 24VDC. Single Chime
ADVISORY ANNUNCIATION
Annunciation Text Alerts Window Message Audio Alert
BUSES TIED Bus 2 is tied to Bus 1. 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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