Garmin G1000 Piper PA32 - Manual (Page 82)

Garmin G1000 Pilot’s Guide for Piper PA32 190-00692-00 Rev. B 3-2
ENGINE INDICATION SYSTEM
3.1 EIS DISPLAY
NOTE: The Fuel Quantity Indicator displays only to 50 gallons per side when full.
The EIS Display shows all critical engine, fuel, and electrical indicators at the left of the MFD. In reversionary
mode, the Engine Display is identical to the EIS Display normally shown on the MFD.
1 Engine Manifold Pressure
Gauge (MAN IN)
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 Oil Temperature Indicator
(OIL °F)
Displays oil temperature in degrees Fahrenheit (°F)
6 Oil Pressure Indicator
(OIL PSI)
Displays oil pressure in pounds per square inch (psi)
7 Exhaust Gas Temperature
Indicator (EGT °F)
Normally-aspirated Aircraft
Displays exhaust gas temperature (EGT) of the hottest cylinder in °F
8 Turbine Inlet Temperature
Indicator (TIT °F)
Turbocharged Aircraft
Displays the temperature at the turbine inlet in °F
9 Cylinder Head Temperature
Indicator (CHT °F)
Displays the temperature of the hottest cylinder in °F
10 Emergency Battery Voltage
(EMER BATT)
Displays voltage for the emergency battery
11 Essential Bus Voltage
(ESS BUS)
Displays voltage for the essential bus
12 Main Alternator Current
(MAIN ALT)
Displays main alternator current in amperes (A)
If the main alternator fails, changes to display standby alternator current