System overview – Garmin G1000 Piper PA-46 Matrix User Manual
Page 31
190-01108-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
17
SYSTEM OVERVIEW
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
NOTE:
See the Pilot’s Operating Handbook (POH) for specific procedures concerning avionics power
application and emergency power supply operation.
The G1000 system is integrated with the aircraft electrical system and receives power directly from electrical
busses. The G1000 PFDs, 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.
During system initialization, test annunciations are displayed, as shown in Figure 1-8. All system annunciations
should disappear typically within one minute of power-up. Upon power-up, key annunciator lights also become
momentarily illuminated on the audio panels, the control units and the display bezels.
On the PFD, the AHRS begins to initialize and displays ‘AHRS ALIGN: Keep Wings Level’. The AHRS should
display valid attitude and heading fields typically within one minute of power-up. The AHRS can align itself both
while taxiing and during level flight.
When the MFD powers up (Figure 1-9), the MFD Power-up Page displays the following information:
• System version
• Copyright
• Land database name and version
• Terrain database name and version
• Airport Terrain database name and version
• Obstacle database name and version
• Aviation database name, version, and effective dates
• ChartView or FliteCharts database information
• Safe Taxi database information
Current database information includes the valid operating dates, cycle number and database type. When this
information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted
to continue. Pressing the ENT Key acknowledges this information and displays the Auxiliary (AUX) Weight
Planning Page.
Figure 1-9 MFD Power-up Page
Figure 1-8 PFD Initialization