Garmin G1000 Quest Kodiak - Manual (Page 431)

190-00590-01 Rev. B Garmin G1000 Pilot’s Guide for the Quest Kodiak 100
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
419
APPENDIX A
G1000 SYSTEM ANNUNCIATIONS
When a new alert is issued, the ALERT Softkey will flash to alert the pilot of a new message. It will continue
to flash until acknowledged by pressing the softkey. Active alerts are displayed in white text. Alerts that have
become inactive will change to gray text. The
ALERT Softkey will flash if the state of a displayed alert changes
or a new alert is displayed. The inactive alerts can be removed from the Alert Window by pressing the flashing
ALERT Softkey.
The G1000 System Messages convey messages to the pilot regarding problems with the G1000 system. When
an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with the failed data.
The following section describes various system annunciations. Refer to the POH for additional information
regarding pilot responses to these annunciations.
NOTE: Upon power-up of the G1000 system, certain windows remain invalid as G1000 equipment begins to
initialize. All windows should be operational within one minute of power-up. Should any window continue
to remain flagged, the G1000 system should be serviced by a Garmin-authorized repair facility.
Figure A-5 G1000 System Failure Annunciations
GDC 74A Air
Data Computer
GTX 33 Transponder
OR
GIA 63/W Integrated
Avionics Units
GDC 74A Air
Data Computer
GEA 71 Engine
Airframe Unit
OR
GIA 63/W
Integrated
Avionics Unit
GIA 63/W Integrated
Avionics Units
GRS 77 AHRS
OR
GMU 44
Magnetometer
GIA 63/W
Integrated
Avionics Units
GIA 63/W
Integrated
Avionics Units