Garmin DA40 GPS Receiver User Manual


 
190-00592-06 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA40/40F
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
483
APPENDIX A
G1000 SYSTEM ANNUNCIATIONS
NOTE: Upon power-up, certain windows remain invalid as G1000 equipment begins to initialize. All windows
should be operational within one minute of power-up. If any window continues to remain flagged, the
G1000 System should be serviced by a Garmin-authorized repair facility.
When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with
the failed data (refer to Figure B-1 for all possible flags and the responsible LRUs). Refer to the Aircraft Flight
Manual (AFM) for additional information regarding pilot responses to these annunciations.
GIA 63/63W
Integrated
Avionics Units
GRS 77 AHRS
OR
GMU 44
Magnetometer
GDC 74A
Air Data
Computer
GEA 71
Engine
Airframe Unit
OR
GIA 63/63W
Integrated
Avionics Unit
GDC 74A
Air Data
Computer
Figure A-4 G1000 System Failure Annunciations
GTX 33 Transponder OR
GIA 63/63W Integrated Avionics Units
GIA 63/63W Integrated Avionics Units
Database
Mismatch in
PFD and MFD
The status of detected LRUs can be checked on the AUX - System Status Page (Figure A-2). Active LRUs
are indicated by green check marks; failed, by red ‘X’s. Failed LRUs should be noted and a service center or
Garmin-authorized dealer informed.
Viewing LRU information:
1) Use the FMS Knob to select the AUX - System Status Page.
2) To place the cursor in the ‘LRU Info’ Box,
a) Select the LRU Softkey.
Or:
a) Press the MENU Key.
b) With ‘Select LRU Window’ highlighted, press the ENT Key.
3) Use the FMS Knob to scroll through the box to view LRU status information.