Garmin G1000 Piper PA-46 Matrix - Manual (Page 109)

190-01108-00 Rev. B Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix 95
ENGINE INDICATION AND CREW ALERTING SYSTEM
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
3.2 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 15 messages can be displayed; when more than 15 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 3-17 CAS Messages
Reversionary Mode
CAS
Window
Normal Mode
CAS
Display