Garmin G2000 Cockpit Reference Manual page 25

1
Exhaust Gas Temperature
(EGT °F)
2
Alternator Amps
(ALT AMPS)
3
Oxygen Outlet Pressure Gauge
(OXY OUTLET PSI)
4
Anti-ice Time Remaining
(A-ICE TIME REM)
5
Oxygen Quantity Gauge
(OXY QTY PSI)
6
Cylinder Head Temperature
(CHT °F)
7
Fuel Calculations Group
(GAL REM, GAL USED,
ENDUR, RANGE NM)
Enabling/Disabling the Oxygen System:
1) From the Home Screen on the Touchscreen Controller, touch Aircraft
Systems.
2) Touch the Oxygen Button. When the button annunciator is green, oxygen
is enabled, annunciator is gray when disabled.
190-01264-01 Rev. A Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240
Engine Indication System
For each cylinder, the exhaust gas temperatures
are shown in degrees Fahrenheit (°F). Each bar
segment on the graph represents 25 degrees.
Currents for the right and left alternators are
displayed using vertical bar indicators and
readouts
Oxygen outlet pressure in psi. Gauge ranges
are dependent on the oxygen outlet pressure
system.
Anti-ice time remaining based on the remaining
fluid quantity. (Optional).
Oxygen amount in psi; note that gauge
increment is 100 psi.
For each cylinder, the head temperatures are
shown in degrees Fahrenheit (°F). Each bar
segment on the graph represents 100 degrees.
The fuel totalizer fuel remaining and used
and the totalizer-based endurance and range
calculations are displayed
9