SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
3.2LEAN DISPLAY
NOTE: The pilot should follow the engine manufacturer’s recommended leaning procedures in the Pilot’s Operating Handbook (POH).
1Engine Manifold Pressure Gauge (MAN IN)
Models 182T, T182T, 206H, T206H – Displays engine power in inches of mercury (in Hg). Turbocharged aircraft have a red portion of the gaugeindicatingthemaximummanifoldpressure range. A white tick mark is displayed indicating the cruise manifold pressure (Model T182 only).
2Tachometer (RPM) – Shows propeller speeds in revolutions per minute (rpm). Red range indicates propeller overspeed warning; a white high-rpmrangeindicatesabovenormaloperating speeds (Models 172S, 206H and T206H).
3Fuel Flow (FFLOW GPH) – Shows the current fuel flow in gallons per hour (gph).
4 Turbine Inlet Temperature Indicator (TIT) Models T182T and T206H – Displays the temperature at the turbine inlet in degrees Fahrenheit (°F). When the ASSIST Softkey is pressed, the TIT deviation from peak (∆PEAK) is displayed below the indicator.
5Exhaust Gas Temperature Bar Graph (EGT
°F) – Displays the exhaust gas temperature of all cylinders in degrees Fahrenheit (°F); a readout for the selected cylinder (by default, the hottest cylinder) is shown below the bar graph. The selected cylinder is indicated in light blue. Cylinders whose EGTs are in the normal range
appear in white. Pressing the ASSIST Softkey causes the EGT deviation from peak (∆PEAK)
for the selected cylinder to be displayed below the indicator.
6Cylinder Head Temperature Indicator (CHT)
– Shows the head temperatures of all cylinders in degrees Fahrenheit (°F); a readout for the selectedcylinder(bydefault,thehottestcylinder) is shown below the bar graph. The selected cylinder is indicated in light blue. Cylinders whose CHTs are in the normal range appear in white. Cylinders whose CHTs enter the caution and warning ranges appear in yellow and red, respectively.
7Fuel Quantity Indicator (FUEL QTY GAL)
– Shows the quantity of fuel in the left and right fuel tanks (left–L and right–R). When full, the indicator displays to 35 gallons per side (26 gallons for the Models 172R and 172S).
3-4 |
Garmin G1000 Cockpit Reference Guide for the Cessna Nav III |
190-00384-07 Rev.A |
SECTION 3 – ENGINE INDICATION SYSTEM (EIS)
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Model 172R |
Model 172S |
Model 182T |
Model 206H |
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Figure 3-3 Lean Display (Normally-aspirated Aircraft) |
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Hollow Block
Represents
Peak
190-00384-07 Rev.A |
Garmin G1000 Cockpit Reference Guide for the Cessna Nav III |
3-5 |
SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
1 |
Cruise |
1 |
Manifold |
Pressure
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Model T182T |
Model T206H |
Figure 3-4 Lean Display (Turbocharged Aircraft)
The Lean Display is accessed by pressing the ENGINE Softkey followed by the LEAN Softkey and provides information for performing engine leaning.
From the Lean Display, the pilot can utilize the CYL SLCT and ASSIST softkeys to obtain information about specific cylinders. Pressing the CYL SLCT (Cylinder Select) Softkey cycles through the cylinders (i.e., changes the cylinder indicated on the bar graphs in light blue). This softkey is disabled when the ASSIST Softkey is pressed or when a cylinder experiences a caution or warning condition; the softkey remains disabled until the temperature returns to normal.
3-6 |
Garmin G1000 Cockpit Reference Guide for the Cessna Nav III |
190-00384-07 Rev.A |