190-00820-11 Rev. A
Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin
91
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
SECTION 3 ENGINE INDICATION SYSTEM
The Engine Indication System (EIS) displays critical engine, electrical, fuel, optional ice protection, and other
system parameters on the left side of the Multi Function Display (MFD) during normal operations (Figure 3-1).
EIS information can be fully expanded to an entire page (EIS - Engine Page) using the
ENGINE
Softkey. In
Reversionary Mode, the display-combines Primary Flight Display (PFD) symbology with the EIS.
EIS Display
Figure 3-1 MFD (SR20)
Green bands on the instruments indicate normal ranges of operation; amber and red bands indicate caution
and warning, respectively. White or uncolored bands indicate areas outside of normal operation. When unsafe
operating conditions occur, the corresponding displays, pointers and labels change color corresponding to the
level of the condition; warnings also flash (except fuel at destination). If sensory data to an instrument becomes
invalid or unavailable, a red 'X' is displayed across the instrument. However, the numeric displays in the Fuel
Calculation Box, TKS FIKI Anti Ice Box (optional), and the density altitude in the Air Data Box are replaced with
dashes instead of red 'X's when the data is invalid or out of range.
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