Garmin G1000 Cockpit Reference Guide for the DA42
190-00406-06 Rev. A
51
Annunciations & Alerts
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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.
VOICE ALERTS
Voice Alert
Description
“Minimums, minimums” The aircraft has descended below the preset barometric minimum
descent altitude.
“Vertical track”
The aircraft is one minute from Top of Descent. Issued only when
vertical navigation is enabled.
“Traffic”
Played when a Traffic Advisory (TA) is issued.
“Traffic Not Available”
The aircraft is outside the Traffic Information Service (TIS) coverage area.
“Traffic, Traffic”
Played when a Traffic Advisory (TA) is issued (TAS system).
“Traffic Advisory System
Test Passed”
Played when the TAS system passes a pilot-initiated self test.
“Traffic Advisory System
Test Failed”
Played when the TAS system fails a pilot-initiated self test.
Summary of Contents for DA42 G1000
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