Garmin G1000 Quest Kodiak - Manual (Page 69)

190-00590-00 Rev. C Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 3-1
ENGINE INDICATION SYSTEM
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
NOTE: Refer to the Aircraft Flight Manual (AFM) for limitations.
The G1000 Engine Indication System (EIS) for the Quest Kodiak 100 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).
Figure 3-1 Multi Function Display
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
• System Display – Shows numeric readouts of critical engine, fuel, and electrical indicators
• Fuel Display – Shows numeric readouts of fuel indicators and calculations
The Kodiak 100’s EIS instrument types include vertical slider gauges, horizontal bar indicators, digital readouts,
and slide bars. Green bands and readouts indicate normal ranges of operation; yellow and red bands and readouts
indicate caution and warning, respectively. When unsafe operating conditions occur, readouts, pointers, and
labels may change color and flash corresponding to the level of the condition. If sensor data to an instrument
becomes invalid or unavailable, a red “X” is shown across the instrument. White dashes are shown in place of
parameter values when values are out of an instrument’s display range.