Garmin G1000 King Air C90GT - Manual (Page 101)

190-00663-01 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT
ENGINE INDICATION SYSTEM
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
87
ENGINE INDICATION SYSTEM
SECTION 3 ENGINE INDICATION SYSTEM
NOTE: The gauges displayed and the values shown in this section are taken from the Hawker Beechcraft
C90A/GT baseline configuration. Refer to the Pilot’s Operating Handbook (POH) and FAA Approved Airplane
Flight Manual (AFM) for specific values and operating limitations.
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 Display
Figure 3-1 MFD (C90A/GT)
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.