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190-01255-00 Rev. B
Garmin G1000H
™
Pilot’s Guide for the Bell 407GX
81
ENGINE INDICATION & CREW ALERTING SYSTEM
SECTION 3 ENGINE AND CREW ALERTING SYSTEMS
NOTE: Refer to the Rotorcraft Flight Manual (RFM) for limitations.
The G1000H Integrated Flight Deck offers improved flight operations and reduces pilot workload by
automatically monitoring critical system parameters and providing system alerts during all phases of flight using
the following:
•The Power Situation Indicator (PSI) and Dual Tachometer display engine information on the Primary
Flight Display (PFD). A larger version of the PSI and Dual Tachometer is also available on the Engine Page on
the Multi Function Display (MFD).
•TheEngine Indication System (EIS) strip displays engine, electrical and fuel information on the MFD.
•TheCrew Alerting System (CAS) displays advisories, cautions, and warnings to communicate conditions,
statuses, and system failures. CAS messages are grouped by level of importance and color-coded based on
urgency and appear in a window to the right of the Altimeter on the PFD and on the Engine page Alerts window
on the MFD.
In combination with these, aural alerts, additional avionics messages, and master indicators are used to inform
the crew of aberrant flight conditions.
Figure 3-1 EIS (Normal)
EIS Strip
MFD
CAS
Window
PFD
Power
Situation
Indicator
Dual
Tachometer