User Guide

Garmin G1000 EIS Pilot’s Guide for Mooney M20M & M20R 190-00447-01 Rev. A 7-2
ENGINE INDICATION SYSTEM
Long Range Tanks (optional)
The Long Range tank option allows for 55 gallons per
side (110 total). The indicator range is the same as the
standard tank. The pointers will remain at Full until the
quantity decreases below 44.5 gallons.
NOTE: Refer to the Aircraft Flight Manual (AFM)
for limitations regarding fuel quantity.
Fuel Flow GPH Indicator (Normally Aspirated)
The Fuel Flow indicator displays current fuel flow in
gallons per hour (GPH). The indicator ranges from 0 to
30. This indicator does not have a color band.
Fuel Pressure Indicator (Turbocharged)
The Fuel Pressure indicator displays the fuel pressure
in pounds per square inch (PSI).
• Green – Normal
• Yellow – Caution
• Red – Warning (minimum and maximum)
Oil Pressure Indicator
The Oil Pressure indicator displays the pressure of
the oil supplied to the engine in pounds per square inch
(PSI).
• Green – Normal
• Yellow – Caution (low and high indications are
on turbocharged aircraft only)
• Red – Warning (minimum and maximum)
Oil Temperature Indicator
The Oil Temperature indicator displays the engine oil
temperature in degrees Fahrenheit.
• Green – Normal
• Red – Warning
EGT Indicator (Normally Aspirated)
The EGT (Exhaust Gas Temperature) indicator dis-
plays the exhaust gas temperature of the hottest cylinder
in degrees Fahrenheit.
• White – Normal
• Red – Warning
TIT Indicator (Turbocharged)
The TIT (Turbine Inlet Temperature) indicator displays
the temperature at the turbine inlet in degrees Fahrenheit.
• Green – Normal
• Red – Warning
CHT Indicator
The CHT (Cylinder Head Temperature) indicator dis-
plays the temperature of the hottest cylinder in degrees
Fahrenheit. The number of the hottest cylinder appears
in the triangle pointer.
• Green – Normal
• Red – Warning
Voltmeter
The Voltmeter displays the bus voltage for the selected
battery (i.e., VOLTS1 or VOLTS2).
Ammeter
The Ammeter displays the battery amperage for the
selected battery (i.e., BAT1 or BAT2).
NOTE: Refer to the Aircraft Flight Manual (AFM)
for limitations.