Garmin G1000:Beechcraft Baron 58/G58, Руководство пользователя

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190-00663-00 Rev. A
Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT
A-5
APPENDIX A
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.
Figure A-2 Reversionary Sensor Windows
Reversionary
Sensor
Window
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.
XSIDE ADC
The PFDs are displaying data from the cross-side Air Data Computer.
XSIDE AHRS The PFDs are displaying data from the cross-side Attitude & Heading Reference System.
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.
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.