Garmin G1000 Piper PA-46 Matrix - Manual (Page 33)

190-01108-00 Rev. B Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix 19
SYSTEM OVERVIEW
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
• PFD1 failure – MFD and PFD2 remain in normal mode.
• MFD failure – Both PFDs automatically switch to reversionary mode.
• PFD2 failure – MFD and PFD1 remain in normal mode.
Figure 1-11 Reversionary Mode
Reversionary mode can be activated manually by pressing a dedicated reversionary switch installed in the
cockpit. Pressing this switch again deactivates reversionary mode.
Each display can be configured to operate in reversionary mode, as follows:
• PFD1 – By pressing the left reversionary switch.
• MFD – By pressing the left or right reversionary switch..
• PFD2 – By pressing the right reversionary switch.
Should the connection between a PFD and the GIA 63W functions become inoperative, the GIA 63W can no
longer communicate with the PFD (refer to Figure 1-1). As a result, the NAV and COM functions provided to
the failed PFD or MFD by the GIA 63W are flagged as invalid (red “X”) on the remaining PFD (see Figure 1-12).
The system reverts to backup paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required.
The change to backup paths is completely automated for all LRUs and no pilot action is required.
Figure 1-12 Inoperative Input (NAV1 Shown)