Garmin da42-l360 User Manual

Page of 102
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
57
Annunciations & Alerts
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Pr
ocedur
es
Hazar
d
Avoidance
Additional
Featur
es
Abnormal
Oper
ation
Annun/
Alerts
Appendix
Index
Condition
Annunciation  Description
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.
Preflight Test
Performing preflight system test.  Upon 
completion, the aural alert will be heard.
Preflight system test has failed.
terrAin-svs Alerts
Alert Type
PFD/MFD 
TERRAIN-SVS 
Page
Annunciation
MFD
Pop-Up Alert
Aural 
Message
Reduced Required Terrain 
Clearance Warning (RTC)
“Warning; Terrain, 
Terrain”
Imminent Terrain Impact 
Warning (ITI)
“Warning; Terrain, 
Terrain”
Reduced Required Obstacle 
Clearance Warning (ROC)
“Warning; Obstacle, 
Obstacle”
Imminent Obstacle Impact 
Warning (IOI)
“Warning; Obstacle, 
Obstacle”