Garmin G1000 King Air C90GT - Manual (Page 149)

190-009663-01 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 135
AUDIO PANEL AND CNS
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
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 4-49 Frequency Section of PFD2 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 4-50 PFD1 Display after PFD2 Failure