Section 3 Engine Indication System - Garmin G1000:Beechcraft Baron 58/G58 User Manual

SECTION 3 ENGINE INDICATION SYSTEM

The G1000 Engine Indication System (EIS) displays critical engine and fuel flow parameters on the left side of
the Multi Function Display (MFD) during normal operations (Figure 3-1). In Reversionary Mode, the displays are
re-configured to present Primary Flight Display (PFD) symbology together with the EIS (Figure 3-12).
EIS information is presented using gauges and digital readouts. Green ranges on the instrument scales indicate
normal ranges of operation; yellow and red bands indicate caution and warning, respectively. White or uncolored
bands indicate areas outside of normal operation not yet in the caution or warning ranges. During normal
operating conditions, an instrument' s pointer appears in white and the readout text is green.
When an unsafe operating condition occurs, the pointer and readout color change to yellow or red, indicating
a caution or warning. If a cautionary time limit is exceeded, the pointers and digits may flash red, even if the
parameter is still within in the cautionary range. If the sensor data for a parameter becomes invalid or unavailable,
a red "X" is displayed across the indicator and/or readout.
190-00663-00 Rev. A
EIS Display
Figure 3-1 MFD (C90A/GT)
Garmin G1000 Pilot's Guide for the Hawker Beechcraft C90A/GT
ENGINE INDICATION SYSTEM
3-1