System Page - Garmin G1000 Pilot's Manual

ENGINE INDICATION SYSTEM

6.4 SYSTEM PAGE

The System Page is accessed by pressing the SYSTEM
softkey. Underneath the dial gauges, critical readouts are
separated into three categories: System, Fuel Calculation,
and Electrical.
NOTE: Refer to the Pilot's Operating Handbook
(POH) for limitations.
Propeller Sync
Indicator
Oil
Temperature
Fuel
Remaining
Alternator
Load
6-6
Manifold
Pressure Gauge
Tachometer
Pressure
Fuel Used
Bus Voltage
Figure 6-7 System Page
Garmin G1000 Pilot's Guide for Beechcraft 58/G58
System Readouts
Oil temperature and pressure for both engines are
displayed in degrees Celsius and pounds per square inch
(psi), respectively.
Fuel Calculations
NOTE: Fuel calculations do not use the aircraft
Fuel Quantity Indicator and are calculated from
the last time the fuel used was reset.
The fuel calculation portion of the System Page is
based on the fuel flow totalizer. The totalizer amount of
fuel remaining (GAL REM) and the quantity of fuel used
(GAL USED) are both displayed. The pilot may adjust the
fuel remaining amount for totalizer calculations using the
following softkeys:
• DEC FUEL – Decreases totalizer-based fuel
remaining in 1-gal increments
• INC FUEL – Increases totalizer-based fuel
remaining in 1-gal increments
• 166 GAL – Resets totalizer-based fuel remaining
to 166 gal and fuel used display to zero
Oil
• 194 GAL – Resets totalizer-based fuel remaining
to 194 gal and fuel used display to zero
Once set by the pilot, the amount of fuel remaining is
adjusted for fuel burn.
Electrical Readouts
The load (current) for each alternator is shown as a
percentage of the capacity (100 A). Bus voltages are also
displayed.
190-00629-00 Rev. B