Garmin G1000 Mooney M20TN - Manual (Page 71)

190-00647-00 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 3-1
EIS
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1 INTRODUCTION
NOTE: Refer to the Aircraft Flight Manual (AFM) for limitations.
The G1000 Engine Indication System (EIS) for the Mooney M20M, M20R, and M20TN 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 remaining display unit is re-configured to present Primary Flight
Display (PFD) symbology together with the EIS (refer to the System Overview for information about reversionary
mode).
EIS
Figure 3-1 Multi Function Display (M20M)
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 indications
The Engine Manifold Pressure Gauge, Tachometer, and Fuel Quantity Indicators are present at the top of all
three displays. EIS instrument types include gauges, bar graphs, numeric readouts, and slide bars. Green bands
(or the absence thereof; e.g., on the EGT Indicator) indicate normal ranges of operation; yellow and red bands
indicate caution and warning, respectively. When unsafe operating conditions occur, readouts and labels may
change color corresponding to the level of the condition. The 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.