190-00663-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT
4-39
AUDIO PANEL AND CNS
PFD FAILURE, DUAL SYSTEM
If PFD1 fails, COM1 and NAV1 display a red X on both remaining displays. NAV1 is unavailable. COM1
automatically tunes 121.500 MHz, but the frequency is not shown. The COM1 emergency frequency is available
to both the copilot and pilot.
Figure 4-54 Frequency Section of MFD Display after PFD1 Failure
Emergency Channel
Loaded Automatically
If PFD2 fails, COM2 and NAV2 display a red X on the remaining PFD display. NAV2 is unavailable. COM2
tunes 121.500 MHz, but the frequency is not shown. The COM2 emergency frequency is available to both the
copilot and pilot.
Figure 4-55 PFD1 Display after PFD2 Failure
Содержание G1000:Beechcraft Baron 58/G58
Страница 1: ...Hawker Beechcraft C90A GT...
Страница 12: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A x TABLE OF CONTENTS BLANK PAGE...
Страница 106: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A 3 10 ENGINE INDICATION SYSTEM BLANK PAGE...
Страница 380: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A 6 88 HAZARD AVOIDANCE BLANK PAGE...
Страница 430: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A 7 50 AFCS BLANK PAGE...
Страница 522: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A C 8 APPENDIX C BLANK PAGE...
Страница 528: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A D 6 APPENDIX D BLANK PAGE...
Страница 538: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A I 6 INDEX BLANK PAGE...