Garmin G1000 PDAs & Smartphones User Manual


 
Garmin G1000 Pilot’s Guide for Cessna Nav III
190-00498-07 Rev. A
88
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
NORMALLY-ASPIRATED AIRCRAFT
For normally-aspirated aircraft, when a cylinder peaks, its peak is represented by a light blue block on the
EGT Bar Graph. The EGT readout for the peaked cylinder number, indicated on the bar graph in light blue,
appears directly beneath the bar graph. The system automatically switches to the first peak obtained and
displays the temperature deviation from peak (DPEAK) in degrees Fahrenheit (°F) below the EGT readout.
Selecting the Engine Leaning Assist function:
From the Lean Display, press the ASSIST Softkey to identify the peak. The peak temperature for the selected
cylinder is indicated with a blue block on the EGT Bar Graph and the temperature deviation from peak is shown
underneath the EGT Bar Graph.
Figure 3-7 Lean Display (Normally-Aspirated Aircraft)
Model 172S
2
5
3
7
6
Model 182T
6
3
1
2
5
7
7
2
3
6
5
Model 172R
Light Blue
Block
Represents
Peak
Model 206H
6
3
1
2
5
7