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

Integrated flight deck diamond da40/40f
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SECTION 3 ENGINE INDICATION SYSTEM

The G1000 Engine Indication System (EIS) for the Diamond DA40/40F 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 Display
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 Engine Manifold Pressure Gauge and Tachometer are shown at the top of all three displays.
Instrument types include dial gauges, horizontal bar indicators, digital readouts, and bar graphs. Green bands
indicate normal ranges of operation; yellow and red bands indicate caution and warning, respectively. White
bands indicate areas outside of normal operation not yet in the caution or warning ranges. Readouts, labels, and
pointers indicators appear in white to indicate normal operation and may 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
displayed across the instrument.
190-00592-02 Rev. A
Figure 3-1 MFD (DA40)
Garmin G1000 Pilot's Guide for the Diamond DA40/40F
ENGINE INDICATION SYSTEM
3-1

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