Garmin G1000 Manual page 106

ENGINE & AIRFRAME SYSTEMS
In the event of a display failure, depending on the failed display(s), the functioning display(s) 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 trim 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. Synoptics are not available while in Reversionary
Mode.
EIS
Display
92
Figure 3-2 Reversionary Mode
Garmin G1000 Pilot's Guide for the Socata TBM 850/900
CAS
Window
190-00709-05 Rev. D