Garmin G1000 King Air C90GT - Manual (Page 536)

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-01 Rev. A
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL FEA
TURES
APPENDICES
INDEX
522
APPENDIX A
• Audio Alerting System: The G1000 System issues audio alert tones when specific system conditions are met.
See the Alert Level Definitions Section for more information. The annunciation tone may be tested from the
AUX - System Status Page.
Testing the system annunciation tone and annunciator lights:
1) Use the FMS Knob to select the AUX - System Status Page.
2) Select the ANN TEST Softkey.
Or :
a) Press the MENU Key.
b) Highlight ‘Enable Annunciator Test Mode’ and press the ENT Key.
Figure A-2 System Status Page, System Annunciation Testing
Press to Test
Annunciation Tone and
Annunciation Lights
ALERT LEVEL DEFINITIONS
The G1000 Alerting System, as installed in Hawker Beechcraft C90A/GT aircraft, uses one alert level.
• ANNUNCIATION OR MESSAGE ADVISORY: This level of alert provides general information.
An annunciation alert is accompanied by a flashing ‘ADVISORY’ Softkey annunciation (see Figure A-3).
Pressing the ADVISORY Softkey acknowledges the presence of the annunciation alert.
Message advisory alerts issue a flashing ‘ADVISORY’ Softkey annunciation (see Figure A-3). Pressing the
ADVISORY Softkey acknowledges the presence of the message advisory alert and displays the alert text
message in the Alerts Window.
Figure A-3 Softkey Annunciation (ALERTS Softkey Labels)