Garmin G1000H Bell 407GX Pilot's Guide - Page 93
Engine and Crew Alerting systems, ENGINE INDICATION & CREW ALERTING SYSTEM - flight deck
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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). • 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. PFD Power Situation Indicator Dual Tachometer MFD EIS Strip CAS Window Figure 3-1 EIS (Normal) 190-01255-00 Rev. A Garmin G1000H™ Pilot's Guide for the Bell 407GX 81