Pilot's Guide

190-01461-00 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
89
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
EIS DISPLAY (REVERSIONARY MODE)
Should a system detected failure occur on the MFD, the PFD automatically enters reversionary mode. Should
a system detected failure occur on the PFD, reversionary mode must be activated manually, if desired. Refer to
the System Overview section for more information.
The Engine Display, in reversionary mode, is identical to the normal EIS Display on the MFD.
Figure 3-14 Reversionary Mode (EIS Shown)
EIS Display