Section 3 Engine Indication System (Eis) - Garmin G1000 Pilot's Manual

SECTION 3 ENGINE INDICATION SYSTEM (EIS)

Refer to the Pilot's Operating Handbook (POH) for limitations.
NOTE:
The G1000 Engine Indication System (EIS) displays critical engine, electrical, fuel, and other system parameters
on the left side of the Multi Function Display (MFD) during normal operations. In reversionary mode, the
displays are re-configured to present Primary Flight Display (PFD) symbology together with the EIS (refer to the
System Overview for information about Reversionary Mode).
EIS
EIS information is presented in three displays, accessed using the ENGINE Softkey on the MFD:
• Engine Display – Default display, shows all critical engine, fuel, and electrical indicators
• Lean Display – Provides engine leaning information
• System Display – Shows numeric readouts of critical engine, fuel, and electrical indicators
The Tachometer and Engine Manifold Pressure Gauge (Models 182T, T182T, 206H, and T206H) are present at
the top of all three displays. All displays also show fuel flow and quantity.
EIS instrument types include round dial gauges, horizontal bar indicators, bar graphs, and digital readouts.
Green and white bands indicate normal ranges of operation; yellow and red bands indicate caution and warning,
respectively. When unsafe operating conditions occur, readouts and labels change color corresponding to the
level of the condition; warnings also flash. Readouts and pointers on the horizontal bar indicators appear in white
to indicate normal operation and change to yellow or red to indicate caution or warning conditions. If sensory
data to an instrument becomes invalid or unavailable, a red "X" is shown across the instrument.
190-00498-01 Rev. A
Figure 3-1 Multi Function Display
Garmin G1000 Pilot's Guide for Cessna Nav III
EIS
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