Garmin SOCATA TBM850, Pilot'S Manual

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190-00709-04 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
89
ENGINE & AIRFRAME SYSTEMS
SECTION 3 ENGINE AND AIRFRAME SYSTEMS
NOTE:
Refer to the Pilot’s Operating Handbook (POH) for limitations.
The G1000 offers improved flight operations and reduces crew workload by automatically monitoring critical
system parameters and providing system alerts during all phases of flight using the following:
• The Engine Indication System (EIS) displays electrical, fuel, engine, pressurization, and flight control
information on the left side of the Multi Function Display (MFD).
• Synoptics pages are provided for monitoring the status of the doors, de-icing systems, electrical, and fuel.
• 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 on the left side of the MFD.
In combination with these, aural alerts, additional avionics messages, and master indicators are used to inform
the crew of aberrant flight conditions. The system also provides an improved level of maintenance data for the
ground crew.
Figure 3-1 Multi Function Display
EICAS Display