Engine indication system – Garmin G1000 Piper PA32 User Manual
Page 90
Garmin G1000 Pilot’s Guide for Piper PA32
190-00692-00 Rev. B
3-10
ENGINE INDICATION SYSTEM
1
Engine Manifold Pressure
Gauge (MAN IN HG)
Displays manifold pressure in inches of Mercury (in Hg) to indicate engine power
Turbocharged Aircraft – Maximum manifold pressure range displayed in red
2
Tachometer
(RPM)
Displays propeller speed in revolutions per minute (rpm); the red range
indicates propeller overspeed
3
Fuel Quantity Indicator
(FUEL QTY GAL)
Displays the amount of fuel in gallons (gal) for each tank, labeled ‘L’ (left)
and ‘R’ (right)
4
Fuel Flow Indicator
(FFLOW GPH)
Displays fuel flow in gallons per hour (gph)
5
Turbine Inlet Temperature
Indicator (TIT °F)
Turbocharged aircraft
Displays the temperature at the turbine inlet in degrees Fahrenheit (°F)
6
Exhaust Gas Temperature
Bar Graph (EGT °F)
Normally-aspirated aircraft
Displays exhaust gas temperatures (EGT) for all cylinders in °F; the readout
is for the hottest cylinder
7
Cylinder Head
Temperature Bar Graph
(CHT °F)
Displays head temperatures for all cylinders with a readout for the hottest
cylinder in °F