Garmin G1000H Manual De Usuario

190-01255-00  Rev. B

81

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).

• The Engine Indication System (EIS) strip displays engine, electrical and fuel information on the MFD.

• The Crew 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.