Garmin G1000 Manual De Usuario

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190-00498-07  Rev. A
Garmin G1000 Pilot’s Guide for Cessna Nav III
17
SYSTEM OVERVIEW
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
G1000 SYSTEM ANNUNCIATIONS
 NOTE: 
For a detailed description of all annunciations and alerts, refer to Appendix A.  Refer to the Pilot’s 
Operating Handbook (POH) for additional information regarding pilot responses to these annunciations.
When an LRU or an LRU function fails, a large red “X” is typically displayed on windows associated with 
the failed data (Figure 1-13 displays all possible flags and responsible LRUs).  Upon G1000 power-up, certain 
windows remain invalid as equipment begins to initialize.  All windows should be operational within one 
minute of power-up.  If any window remains flagged, the G1000 system should be serviced by a Garmin-
authorized repair facility.
Figure 1-13  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
Database 
Mismatch in PFD 
and MFD
SOFTKEY FUNCTION
The softkeys are located along the bottoms of the displays.  The softkeys shown depend on the softkey level 
or page being displayed.  The bezel keys below the softkeys can be used to select the appropriate softkey.  When 
a softkey is selected, its color changes to black text on gray background and remains this way until it is turned 
off, at which time it reverts to white text on black background.
Softkey Names 
(Displayed)
Figure 1-14  Softkeys (Second-Level PFD Configuration)
Bezel-Mounted 
Softkeys (Press)
Softkey 
On