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IAS MISCOMP
If both airspeed sensors detect < 35 knots, this is inhibited.
If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 kts.
If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 kts.
HDG MISCOMP
Difference in heading sensors is > 6 degrees.
PIT MISCOMP
Difference in pitch sensors is > 5 degrees.
ROL MISCOMP
Difference in roll sensors is > 6 degrees.
ALT NO COMP
No data from one or both altitude sensors.
IAS NO COMP
No data from one or both airspeed sensors.
HDG NO COMP
No data from one or both heading sensors.
PIT NO COMP
No data from one or both pitch sensors.
ROL NO COMP
No data from one or both roll sensors..
R
eversionary Sensor Annunciations
R
eversionary 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.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev. A 56
Annunciations & Alerts
Flight
EICAS Instruments
Nav/Com/
GPS Nav AFCS XPDR/Audio
Flight
Procedures Planning
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Index Appendix Alerts
eversionary Sensor Window Text
Condition
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
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, 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.
System Failure
AP and MET are unavailable. FD may still be available.
Emergency Descent Mode
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
Elevator Mistrim Up
A condition has developed causing the pitch servo to provide a sustained force in the nose up direction.
Elevator Mistrim Down
A condition has developed causing the pitch servo to provide a sustained force in the nose down direction.
Aileron Mistrim Left
A condition has developed causing the roll servo to provide a sustained left force.
Aileron Mistrim Right
A condition has developed causing the roll servo to provide a sustained right force.
Rudder Mistrim Left
A condition has developed causing the yaw servo to provide a sustained force.
Rudder Mistrim Right
A condition has developed causing the yaw servo to provide a sustained force.
Preflight Test
Performing preflight system test. Upon completion of the test, the aural alert will be heard.
Preflight system test has failed.
190-00600-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 57
Annunciations & Alerts
Flight
Instruments EICAS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
AWS Alerts
Alert Type
PFD/MFD TAWS Page
Annunciation
MFD
Pop-Up Alert
Aural Message
Excessive Descent Rate Warning (EDR)
“Pull Up”
Reduced Required Terrain Clearance Warning (RTC)*
or
“Terrain, Terrain; Pull Up, Pull Up”*
or
“Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
Imminent Terrain Impact Warning (ITI)
or*
Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up, Pull Up”*
　
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