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190-00498-07 Rev. A
Garmin G1000 Pilot’s Guide for Cessna Nav III
89
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
TURBOCHARGED AIRCRAFT
Leaning for turbocharged aircraft is done with reference to the Turbine Inlet Temperature (TIT). When the
temperature peaks, the numeric readout (DPEAK) appears below the TIT Indicator and displays the difference
between peak and current TITs, in degrees Fahrenheit (°F). If a peak is not displayed, underscores are shown
until one is established.
Selecting the Engine Leaning Assist function:
From the Lean Display, press the ASSIST Softkey to identify the peak. The TIT deviation from peak is shown
below the TIT Indicator.
Figure 3-8 Lean Display (Turbocharged Aircraft)
Cruise
Manifold
Pressure
4
1
2
5
7
3
6
Model T182T
Model T206H
4
1
2
5
7
3
6