Garmin G1000 Socata TBM 850 - Manual (Page 103)

190-00709-00 Rev. A Garmin G1000 Pilot’s Guide for the Socata TBM 850 3-13
ENGINE & AIRFRAME SYSTEMS
3.3 CREW ALERTING SYSTEM (CAS)
NOTE: Refer to the Pilot’s Operating Handbook (POH) for emergency procedures.
NOTE: Aural alerts associated with abnormal conditions and advisories are managed through the audio
panels. Refer to the Audio Panel and CNS Section for more information.
The Crew Alerting System (CAS) Display is located in the lower left corner of the EICAS Display (on the MFD)
under normal display conditions. Up to 14 messages can be displayed; when more than 14 messages accumulate,
the scrolling CAS softkeys become available.
When CAS messages are present while in Reversionary Mode, the CAS Window appears on the display along
with the flight instruments and EIS. The window size increases to fit up to 14 CAS messages; if more than 14
messages are generated, the messages can be scrolled through using the CAS softkeys (two left-most softkeys).
Figure 3-19 CAS Messages
Reversionary Mode
CAS
Window
Normal Mode
CAS
Display