Afcs Alerts - Garmin G1000 Reference Manual

Annunciations & Alerts
reversionary
sensor Window
text
USING AHRS2
USING GPS1
USING GPS2

AFCs Alerts

Condition Annunciation Description
Pitch Failure
Roll Failure
MET Switch Stuck,
or Pitch Trim Axis
Control Failure
System Failure
Emergency
Descent Mode
Elevator Mistrim
Up
Elevator Mistrim
Down
Aileron Mistrim
Left
Aileron Mistrim
Right
Rudder Mistrim
Left
Rudder Mistrim
Right
Preflight Test
56
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
PFD1 is displaying data from the #2 AHRS.
PFD2 is displaying data from the #1 GPS.
PFD1 is displaying data from the #2 GPS.
Pitch axis control failure. AP is inoperative.
Roll axis control failure. AP is inoperative.
If annunciated when AP is engaged, a failure has occurred in
the pitch trim system. If annunciated when AP is not engaged,
a failed or stuck switch is causing the annunciation.
AP and MET are unavailable. FD may still be available.
AP engaged when aircraft altitude above 30,000 ft and
cabin pressurization is lost. Selected Heading set 90° left
of current heading; Selected Altitude set to 15000 ft
A condition has developed causing the pitch servo to
provide a sustained force in the nose up direction.
A condition has developed causing the pitch servo to
provide a sustained force in the nose down direction.
A condition has developed causing the roll servo to provide
a sustained left force.
A condition has developed causing the roll servo to provide
a sustained right force.
A condition has developed causing the yaw servo to
provide a sustained force.
A condition has developed causing the yaw servo to provide a
sustained force.
Performing preflight system test. Upon completion of the
test, the aural alert will be heard.
Preflight system test has failed.
Condition
190-00600-02 Rev. A