Garmin G1000 Piper PA-46 Matrix - Manual (Page 548)

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix 190-01108-00 Rev. B
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL FEA
TURES
APPENDICES
INDEX
534
APPENDIX A
Figure A-3 Comparator and Reversionary Sensor Annunciation Windows
Comparator
Window
Reversionary
Sensor
Window
REVERSIONARY SENSOR ANNUNCIATIONS
Reversionary Sensor
Window Text
Condition
BOTH ON ADC1 Both PFDs are displaying data from the number one Air Data Computer.
BOTH ON ADC2 Both PFDs are displaying data from the number two Air Data Computer.
BOTH ON AHRS1 Both PFDs are displaying data from the number one Attitude & Heading Reference System.
BOTH ON AHRS2 Both PFDs are displaying data from the number two Attitude & Heading Reference System.
BOTH ON GPS1 Both PFDs are displaying data from the number one GPS receiver.
BOTH ON GPS2 Both PFDs are displaying data from the number two GPS receiver.
USING ADC1 PFD2 is displaying data from the #1 Air Data Computer.
USING ADC2 PFD1 is displaying data from the #2 Air Data Computer.
USING AHRS1 PFD2 is displaying data from the #1 AHRS.
USING AHRS2 PFD1 is displaying data from the #2 AHRS.
USING GPS1 PFD2 is displaying data from the #1 GPS.
USING GPS2 PFD1 is displaying data from the #2 GPS.
G1000 SYSTEM ANNUNCIATIONS
When a new message is issued, the MSG Softkey flashes to alert the flight crew of a new message. It continues
to flash until acknowledged by pressing the softkey. Active messages are displayed in white text. Messages that
have become inactive change to gray text. The
MSG Softkey flashes if the state of a displayed message changes
or a new message is displayed. The inactive messages can be removed from the Message Window by pressing
the flashing
MSG Softkey.
The G1000 System Messages convey messages to the flight crew regarding problems with the G1000 system.
Typically, a large red ‘X’ appears in a window when a related LRU fails or detects invalid data.
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.