Garmin G1000 Manual De Usuario
190-00498-07 Rev. A
Garmin G1000 Pilot’s Guide for Cessna Nav III
13
SYSTEM OVERVIEW
SY
STEM
O
VER
VIEW
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
ANCE
AFCS
ADDITIONAL
FEA
TURES
TURES
APPENDICES
INDEX
1.5 SYSTEM POWER-UP
NOTE:
See the Aircraft Flight Manual (AFM) for specific procedures concerning avionics power application
and emergency power supply operation.
NOTE:
Refer to Appendix A for system-specific annunciations and alerts.
The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical
busses. The 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.
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 1-7. All system annunciations
should disappear typically within the first minute of power-up. Upon power-up, key annunciator lights also
become momentarily illuminated on the Audio Panel.
become momentarily illuminated on the Audio Panel.
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 the first minute of power-up. The AHRS can align itself
both while taxiing and during level flight.
both while taxiing and during level flight.
When the MFD powers up, the power-up screen (Figure 1-8) displays the following information:
• System version
• Copyright
• Land database name and version
• Safe Taxi database information
• Terrain database name and version
• Copyright
• Land database name and version
• Safe Taxi database information
• Terrain database name and version
• Obstacle database name and version
• Navigation database name, version, and effective dates
• Airport Directory name, version and effective dates
• FliteCharts/ChartView database information
• Navigation database name, version, and effective dates
• Airport Directory name, version and effective dates
• FliteCharts/ChartView database information
Current database information includes database type, cycle number, or valid operating dates. Review the listed
information for currency (to ensure that no databases have expired).
Pressing the ENT Key (or right-most softkey) acknowledges this information, and the Navigation Map Page is
displayed upon pressing the key a second time. When the system has acquired a sufficient number of satellites to
determine a position, the aircraft’s current position is shown on the Navigation Map Page.
determine a position, the aircraft’s current position is shown on the Navigation Map Page.
Figure 1-7 PFD Initialization
Figure 1-8 MFD Power-Up Screen (172R shown)