System Display - Garmin G900X Pilot's Manual

ENGINE INDICATION SYSTEM

SYSTEM DISPLAY

Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time
NOTE:
the fuel was reset.
The EIS System Display shows the engine manifold pressure, tachometer, various system parameters, and
fuel calculations. Fuel calculations are based on the displayed fuel remaining (GAL REM) and the fuel flow
totalizer.
Accessing the EIS System Display:
1) Select the ENGINE Softkey.
2) Select the SYSTEM Softkey.
3) To return to the default Engine Display, select the ENGINE or BACK Softkey.
Adjusting the fuel totalizer quantity:
From the System Display, select the DEC FUEL or INC FUEL Softkey to adjust the fuel remaining (GAL REM).
Resetting the fuel totalizer:
From the System Display, select the RST FUEL Softkey. This also resets the fuel remaining (GAL REM) to zero.
1
Engine Manifold Pressure
Gauge (MAN IN)
2
Tachometer (RPM)
3 Oil Temperature (OIL °F) Displays oil temperature in degrees Fahrenheit (°F)
4
Oil Pressure
(OIL PSI)
5
Main Bus Voltage
(MAIN V)
6
Alternator Current
(ALT A)
7
Fuel Flow Indicator
(FFLOW GPH)
8
Calculated Fuel
Remaining
(GAL REM)
9
Calculated Fuel Used
(GAL USED)
3-26
Displays manifold pressure in inches of Mercury (in Hg) to indicate engine power
Turbocharged Aircraft – Maximum manifold pressure range displayed in red
Displays propeller speed in revolutions per minute (rpm); the red range
indicates propeller overspeed
Displays oil pressure in pounds per square inch (psi)
Displays the main bus voltage
Displays the alternator current in amperes (A)
Displays fuel flow in gallons per hour (gph)
Displays the amount of fuel remaining set by the pilot and adjusted for fuel
burn
Displays the calculated amount of fuel used based on the totalizer fuel
flow
Garmin G900X Pilot's Guide 190-00726-00 Rev. A