Garmin G1000 Quest Kodiak - Manual (Page 429)

190-00590-01 Rev. B Garmin G1000 Pilot’s Guide for the Quest Kodiak 100
SY
STEM
O
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VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
417
APPENDIX A
NORMAL OPERATING ANNUNCIATION
Annunciation Window Text Alerts Window Message Audio Alert
ENG INLET NRM Engine inlet is in normal position. None
MESSAGE ADVISORY ALERTS
Alerts Window Message Audio Alert
AVN FAN 1 FAIL – Avionics cooling fan #1 is inoperative. None
AVN FAN 2 FAIL – Avionics cooling fan #2 is inoperative. None
AURAL ALERTS
Aural 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” The Traffic Information Service (TIS) has issued a Traffic Advisory alert.
“TIS not available” The aircraft is outside the Traffic Information Service (TIS) coverage area.
“Traffic, Traffic” Played when first Traffic Advisory (TA) is issued. “Traffic” for each subsequent TA.
“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.
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-6. 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:
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.
ROL 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.
ROL NO COMP No data from one or both roll sensors..