Reversionary Sensor Annunciations; Afcs Alerts - Garmin G1000 Reference Manual

Annunciations & Alerts

REVERSIONARY SENSOR ANNUNCIATIONS

Reversionary
Sensor Window
Text
BOTH ON ADC1
BOTH ON ADC2
BOTH ON AHRS1
BOTH ON AHRS2
BOTH ON GPS1
BOTH ON GPS2
USING ADC1
USING ADC2
USING AHRS1
USING AHRS2
USING GPS1
USING GPS2

AFCS ALERTS

Condition Annunciation Description
Pitch Failure
Roll Failure
Pitch Trim Axis
Control Failure
Yaw Damper
Failure
System Failure
Elevator Mistrim
Up
Elevator Mistrim
Down
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Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT/GTi
Both PFDs are displaying data from the number one Air Data Computer.
Both PFDs are displaying data from the number two Air Data Computer.
Both PFDs are displaying data from the number one Attitude & Heading Reference
System.
Both PFDs are displaying data from the number two Attitude & Heading Reference
System.
Both PFDs are displaying data from the number one GPS receiver.
Both PFDs are displaying data from the number two GPS receiver.
PFD2 is displaying data from the #1 Air Data Computer.
PFD1 is displaying data from the #2 Air Data Computer.
PFD2 is displaying data from the #1 AHRS.
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.
Roll axis control failure.
If annunciated when AP is engaged, a failure has occurred in
the pitch trim system.
YD control failure.
AP and MET are unavailable. FD may still be available.
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.
Condition
190-00664-02 Rev. B