Reversionary Sensor Annunciations; G1000 System Annunciations - Garmin G1000:Beechcraft Baron 58/G58 User Manual

REVERSIONARY SENSOR ANNUNCIATIONS

Reversionary sensor selection is annunciated in the Reversionary Sensor Window, as shown in Figure A-2.
These annunciations reflect reversionary sensors selected on one or both PFDs. Pressing the SENSOR Softkey
gives access to ADC1 , ADC2 , AHRS1 , and AHRS2 Softkeys. These softkeys allow manual switching of sensors. In
the case of certain types of sensor failures, the G1000 may make some sensor selections automatically. The GPS
sensor cannot be switched manually.
Reversionary Sensor
Window Text
BOTH ON ADC1
BOTH ON ADC2
BOTH ON AHRS1
BOTH ON AHRS2
BOTH ON GPS1
BOTH ON GPS2
XSIDE ADC
XSIDE AHRS

G1000 SYSTEM ANNUNCIATIONS

When a new message is issued, the ALERTS 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 ALERTS 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 ALERTS 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 AFM/POH for
additional information regarding pilot responses to these annunciations.
Upon power-up of the G1000 system, certain windows remain invalid as G1000 equipment begins to
NOTE:
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.
190-00663-00 Rev. A
Figure A-2 Reversionary Sensor Windows
Both PFDs are displaying data from the number one Air Data Computer.
Both PFDs are displaying data from the number two Air Data Computer.
Both PFDs are displaying data from the number one Attitude & Heading Reference System.
Both PFDs are displaying data from the number two Attitude & Heading Reference System.
Both PFDs are displaying data from the number one GPS receiver.
Both PFDs are displaying data from the number two GPS receiver.
The PFDs are displaying data from the cross-side Air Data Computer.
The PFDs are displaying data from the cross-side Attitude & Heading Reference System.
Garmin G1000 Pilot's Guide for the Hawker Beechcraft C90A/GT
Reversionary
Sensor
Window
Condition
APPENDIX A
A-5