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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. 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.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
507
Appendix A
TAWS ALERTS
Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
Alert Type
PFD/MFD TAWS Page Annunciation
MFD Map Page
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”*
Reduced Required Obstacle Clearance Warning (ROC)*
or
“Obstacle, Obstacle; Pull Up, Pull Up”*
or
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”
Imminent Obstacle Impact Warning (IOI)
or*
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull Up, Pull Up”*
Reduced Required Terrain Clearance Caution (RTC)*
or
“Caution, Terrain; Caution, Terrain”*
or
“Terrain Ahead; Terrain Ahead”
Imminent Terrain Impact Caution (ITI)
or*
“Terrain Ahead; Terrain Ahead”
or
“Caution, Terrain; Caution, Terrain”*
Reduced Required Obstacle Clearance Caution (ROC)*
or
“Caution, Obstacle; Caution, Obstacle”*
or
“Obstacle Ahead; Obstacle Ahead”
Imminent Obstacle Impact Caution (IOI)
or*
“Obstacle Ahead; Obstacle Ahead”
or
“Caution, Obstacle; Caution, Obstacle”*
Premature Descent Alert Caution (PDA)
“Too Low, Terrain”
Altitude Callout “500”
None
None
“Five-Hundred”
Excessive Descent Rate Caution (EDR)
“Sink Rate”
Negative Climb Rate Caution (NCR)*
or
“Don’t Sink”*
or
“Too Low, Terrain”
* Mustang defualt configuration
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES 508
Appendix A
TAWS Systemystem Statustatustatus Annunciationsnnunciations
Alert Type
PFD/MFD TAWS Page Annunciation
MFD
Pop-Up Alert
Aural Message
TAWS System Test Fail
None
“TAWS System Failure”
TAWS Alerting is disabled
None
None
No GPS position or excessively degraded GPS signal
None
“TAWS Not Available”
System Test in progress
None
None
System Test pass
None
None
“TAWS System Test OK”
Other G1000 Aural Alerts
Aural Alert
Description
“Minimums, minimums”
　
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