Pilot's Guide

190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
91
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES 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.
Indicates First
Cylinder to Peak
Light Blue Bar
Represents Peak
Figure 3-11 Assist Mode - First Peaked Cylinder (Corvalis)
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.
Indicates Last
Cylinder to Peak
Figure 3-12 Assist Mode - Last Peaked Cylinder (Corvalis)
Temperature Deviation from Peak
(Last Cylinder)