Garmin G900X Pilot's Manual page 114

ENGINE INDICATION SYSTEM
1
Engine Manifold Pressure
Gauge (MAN IN HG)
2
Tachometer (RPM)
3
Fuel Flow
(FFLOW GPH)
4 Turbo Inlet Temperature
Indicator (TIT °F)
TSIO-550-E only
5
Exhaust Gas Temperature
Bar Graph (EGT °F)
6
Cylinder Head
Temperature Bar Graph
(CHT °F)
7 Flap Position and Trim
Indicators
(FLAPS, ELEV TRIM,
RUDDER TRIM,
AILERON TRIM)
3-22
Displays manifold pressure in inches of Mercury (in Hg) to indicate engine
power
Displays propeller speed in revolutions per minute (rpm)
Overspeed warning: 2700 rpm for all but IO-540 (2575 rpm)
Displays fuel flow in gallons per hour (gph)
Displays the temperature for the right (R) and left (L) turbo inlets in °F; the
left readout corresponds to the "L" indication, and the right readout to
the "R" indication
Displays exhaust gas temperatures (EGT) for all cylinders in °F; the readout
is for the hottest cylinder
Displays head temperatures for all cylinders with a readout for the hottest
cylinder in °F
Displays flap position and elevator, rudder, and aileron trim along slide bars
Up to three trim indicators may be installed; aileron and rudder trim are
mutually exclusive.
Garmin G900X Pilot's Guide 190-00726-00 Rev. A