Cockpit Reference Guide
Garmin G1000 Pilot’s Guide for the Piper PA-46 Meridian
190-00763-02 Rev. A
88
ENGINE INDICATION AND CREW ALERTING SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
In the event of a display failure, depending on the failed display(s), the display(s) operating in Reversionary
Mode may be re-configured to present Primary Flight Display (PFD) symbology together with engine and CAS
information (refer to the System Overview for more information about Reversionary Mode). In Reversionary
Mode, engine, pressurization, fuel, electrical, and flight control data is presented in an abbreviated format on the
left of the display.
CAS messages appear in a window on the right of the display.
EIS
Display
CAS
Window
Figure 3-2 Reversionary Mode










