Garmin Software Version 0534.15 Guide de l'utilisateur Page 27

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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-04 Rev. A 11
Engine Indication System
Flight
Instruments EIS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
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.
Assist Mode - First Peaked Cylinder (Corvalis)
Temperature Deviation from Peak
(First Cylinder)
Indicates
First
Cylinder
to Peak
Light
Blue Bar
Represents
Peak
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.
Assist Mode - Last Peaked Cylinder (Corvalis)
Indicates
Last
Cylinder to
Peak
Temperature Deviation from Peak
(Last Cylinder)
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