Cockpit Reference Guide

Garmin G1000
®
Cockpit Reference Guide for the Cessna CitationJet Model 525
190-01130-00 Rev. A
76
Annunciations & Alerts
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
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.
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.