Garmin G1000 Pilot's Manual page 122

ENGINE INDICATION SYSTEM
1 Manifold Pressure
2 Tachometer
3 Fuel Quantity
4
Fuel Flow
5 Calculated Fuel Used
Calculated Fuel Remaining
6
Oil Pressure
7
Oil Temperature
8
9 Cabin Temperature
Battery Current
10
11 Emergency Battery Voltage
12 Essential Buss Voltage
Main Alternator Current
13
Standby Alternator Current
102
Displays engine manifold pressure inches of mercury (IN HG).
Turbocharged Aircraft – Maximum manifold pressure range displayed in red.
Displays engine tachometer in revolutions per minute (RPM).
Displays left (L) and right (R FUEL QTY) fuel quantity in gallons (GAL).
Displays fuel flow in gallons per hour (gph)
Displays the calculated amount of fuel used based on the totalizer fuel flow.
Displays the amount of fuel remaining set by the pilot and adjusted for fuel burn.
Displays oil pressure in pounds per square inch (PSI).
Displays oil temperature in degrees Fahrenheit (°F).
Displays the temperature inside the cabin in degrees Fahrenheit (°F).
Displays battery current in amperes (A).
Displays the emergency battery current in voltage (V).
Displays the essential bus current in voltage (V).
Displays main alternator current in amperes (A).
In the even the main alternator fails, the system will change to display the standby
alternator.
Garmin G1000 Pilot's Guide for the Piper PA-32 Saratoga
190-02692-00 Rev. A