
Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A/GT
190-00664-01 Rev. A 55
Annunciations & Alerts
Flight
Instruments
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features Annun/Alerts Appendix Index
Condition Annunciation Description
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.
TAWS ALERTS
Alert Type
PFD/MFD
TAWS-B 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; Ter-
rain 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”
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