Garmin G900X Pilot’s Guide
190-00726-00 Rev. J
112
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
NORMALLY-ASPIRATED
When the
ASSIST
Softkey is pressed, the system initially highlights the number and EGT readout of the
cylinder with the hottest EGT. For the O-540-series, O-360-series, and O-320-series engines, the Carburetor
Temperature Indicator is removed from the display.
When the first peak is detected, the cylinder numbers disappear, “1st” is annunciated in light blue below that
cylinder’s EGT bar, the temperature is marked in light blue on the graph, and the EGT readout is outlined.
Figure 3-21 Leaning Assist Mode (IO-360-series)
Indicates First
Cylinder to Peak
Light Blue Bar
Represents Peak
Temperature
Deviation from Peak
(First Cylinder)
The system continues to detect peak EGTs for each cylinder as the fuel flow is decreased and the peak of
each cylinder’s EGT is indicated by a light blue marker. The last cylinder to peak is denoted by the “Last”
annunciation below its bar on the graph and the EGT readout is outlined in light blue.
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