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Garmin G1000 Cockpit Reference Guide for the Cessna Caravan
190-00748-05 Rev. A
70
Annunciations & Alerts
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
REVERSIONARY SENSOR ANNUNCIATIONS
Reversionary
Sensor Window
Text
Condition
BOTH ON ADC1
Both PFDs are displaying data from the number one Air Data Computer.
BOTH ON ADC2
Both PFDs are displaying data from the number two Air Data Computer.
BOTH ON AHRS1
Both PFDs are displaying data from the number one Attitude & Heading
Reference System.
BOTH ON AHRS2
Both PFDs are displaying data from the number two Attitude & Heading
Reference System.
BOTH ON GPS1
Both PFDs are displaying data from the number one GPS receiver.
BOTH ON GPS2
Both PFDs are displaying data from the number two GPS receiver.
USING ADC1
PFD2 is displaying data from the #1 Air Data Computer.
USING ADC2
PFD1 is displaying data from the #2 Air Data Computer.
USING AHRS1
PFD2 is displaying data from the #1 AHRS.
USING AHRS2
PFD1 is displaying data from the #2 AHRS.
USING GPS1
PFD2 is displaying data from the #1 GPS.
USING GPS2
PFD1 is displaying data from the #2 GPS.
AFCS ALERTS
Alert Condition Annunciation Description
Rudder Mistrim
Right
Yaw servo providing sustained force in the indicated
direction. Aircraft rudder retrim after substantial pitch and
power changes required.
Rudder Mistrim
Left
Aileron Mistrim
Right
Roll servo providing sustained force in the indicated direction
Aileron Mistrim
Left
Elevator Mistrim
Down
Pitch servo providing sustained force in the indicated
direction. May indicate a failure of the pitch trim servo or
trim system.
Elevator Mistrim
Up
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