Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-04 Rev. A
616
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. Selecting 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.
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.
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 selecting 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 selecting
the flashing
MSG
Softkey.
Message Advisories are displayed in the Messages Window and convey messages to the flight crew regarding
problems with the G1000 or certain aircraft systems. Typically, a large red ‘X’ appears in a window when a
related LRU fails or detects invalid data.
The following section describes various system annunciations. Refer to the POH for additional information
regarding pilot responses to these annunciations.
Содержание SOCATA TBM850
Страница 1: ...G1000 Integrated Flight Deck Pilot s Guide...
Страница 2: ......
Страница 10: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A vi REVISION INFORMATION Blank Page...
Страница 64: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A 50 SYSTEM OVERVIEW Blank Page...
Страница 102: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A 88 FLIGHT INSTRUMENTS Blank Page...
Страница 166: ...190 00709 04 Rev A Garmin G1000 Pilot s Guide for the Socata TBM 850 152 AUDIO PANEL AND CNS Blank Page...
Страница 482: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A 468 HAZARD AVOIDANCE Blank Page...
Страница 682: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A I 8 INDEX Blank Page...
Страница 683: ......