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190-00498-00 Rev. A
Garmin G1000 Pilot’s Guide for Cessna Nav III
1-10
SYSTEM OVERVIEW
1.5 SYSTEM POWER-UP
The G1000 system is integrated with the aircraft
electrical system and receives power directly from electrical
busses. The Garmin G1000 PFD/MFD and supporting
sub-systems include both power-on and continuous built-
in test features that exercise the processor, RAM, ROM,
external inputs and outputs to provide safe operation.
While the system begins to initialize, test annunciations
are displayed to the pilot at power-up, as shown in the
following figure. All system annunciations should be
cleared within one (1) minute of power-up. The
Audio
Panel also annunciates all bezel lights briefly upon power-
up.
NOTE: Please see the Aircraft Flight Manual
(AFM) for specific procedures concerning
avionics power application and emergency
power supply operation.
Figure 1-4 PFD Initialization
On the PFD, the AHRS system displays the ‘AHRS
ALIGN: Keep Wings Level’ message and begins to initialize.
The AHRS should display valid attitude and heading fields
within one (1) minute of power-up. The AHRS can align
itself both while taxiing and during level flight.
NOTE: Please refer to the Pilot’s Guide
Appendices for AHRS initialization bank angle
limitations.
NOTE: See the Annunciations and Alerts Pilot’s
Guide for additional information regarding
system annunciations and alerts.
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