Garmin G1000:Piper Pilot's Manual page 90

ENGINE INDICATION SYSTEM
1
Engine Manifold Pressure
Gauge (MAN IN HG)
2
Tachometer
(RPM)
3 Fuel Quantity Indicator
(FUEL QTY GAL)
4
Fuel Flow Indicator
(FFLOW GPH)
5 Turbine Inlet Temperature
Indicator (TIT °F)
Turbocharged aircraft
6
Exhaust Gas Temperature
Bar Graph (EGT °F)
Normally-aspirated aircraft
7
Cylinder Head
Temperature Bar Graph
(CHT °F)
3-10
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 the amount of fuel in gallons (gal) for each tank, labeled 'L' (left)
and 'R' (right)
Displays fuel flow in gallons per hour (gph)
Displays the temperature at the turbine inlet in degrees Fahrenheit (°F)
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
Garmin G1000 Pilot's Guide for Piper PA32 190-00692-00 Rev. B