Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-00 Rev. A
3-2
ENGINE & AIRFRAME SYSTEMS
In the event of a display failure, depending on the failed display(s), the remaining 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
CAS
Window
Figure 3-2 Reversionary Mode
