Garmin G1000 Socata TBM 850 - Manual (Page 555)

190-00709-02 Rev. B Garmin G1000 Pilot’s Guide for the Socata TBM 850
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
541
APPENDIX A
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-3 G1000 System Messages
Messages Window
Message Softkey
Annunciation
System
Annunciation
Red ‘X’
Figure A-4 G1000 System Failure Annunciations
GDC 74B Air
Data Computer
GTX 33/D Transponder
Or
GIA 63W Integrated
Avionics Units
GDC 74B Air
Data Computer
GEA 71 Engine
Airframe Unit
Or
GIA 63W
Integrated
Avionics Unit
GIA 63W Integrated
Avionics Units
GRS 77 AHRS
Or
GMU 44
Magnetometer
GIA 63W Integrated
Avionics Units
GIA 63W Integrated
Avionics Units