Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT
190-00663-00 Rev. A
A-4
APPENDIX A
VOICE ALERTS
The following audio alerts are announced by the system using a voice of male or female gender (see the AUX
- System Setup Page for the default configured voice gender; contact a Garmin-authorized service center to
change the audio alert voice). If the optional Terrain Awareness and Warning System is installed, voice alerts
are also generated (refer to the TAWS Alerts section).
Voice Alert
Alert Trigger
“Minimums, Minimums” Issued when the aircraft transitions through the minimum descent altitude/decision height (MDA/DH)
“Vertical Track”
Aircraft is one minute from Top of Descent - issued only when vertical navigation is enabled
“Traffic”
TIS voice alert - issued when a Traffic Advisory (TA) is issued
“Traffic Not Available” TIS voice alert - issued when the traffic system fails or cannot communicate
COMPARATOR ANNUNCIATIONS
The Comparator monitors critical values generated by redundant sensors. If differences in the sensors exceed
a specified amount, this discrepency is annunciated in the Comparator Window as a ‘MISCOMP’ (miscompare)
as seen in Figure A-1. If one or both of the sensed values are unavailable, it is annunciated as a ‘NO COMP’ (no
compare). The following is a list of the possible annunciations:
Figure A-1 Sensor Comparator Window
Comparator
Window
Comparator Window Text
Condition
ALT MISCOMP
Difference in altitude sensors is > 200 ft.
IAS MISCOMP
If both airspeed sensors detect < 35 knots, this is inhibited.
If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 knots.
If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 knots.
HDG MISCOMP
Difference in heading sensors is > 6 degrees.
PIT MISCOMP
Difference in pitch sensors is > 5 degrees.
ROLL MISCOMP
Difference in roll sensors is > 6 degrees.
ALT NO COMP
No data from one or both altitude sensors.
IAS NO COMP
No data from one or both airspeed sensors.
HDG NO COMP
No data from one or both heading sensors.
PIT NO COMP
No data from one or both pitch sensors.
ROLL NO COMP
No data from one or both roll sensors..
Summary of Contents for G1000:Beechcraft Baron 58/G58
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