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14 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
System ystem Overview verview
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
1.4 Secure Digitaligital Cards NOTE: Refer to the Appendices for instructions on updating the aviation database. NOTE: Ensure that the G1000 system is powered off before inserting the SD card.
The GDU 1040A and GDU 1500 data card slots use Secure Digital (SD) cards and are located on the top right portion of the display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database and system software updates as well as terrain database storage.
Install an SD card
Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card should remain flush with the face of the display bezel.
Remove an SD card
Gently press on the SD card to release the spring latch and eject the card.
Figure 1-6 Display Bezel SD Card SlotsPFDMFDSD Card Slots
1.5 Systemystem Power-up NOTE: Refer to the Appendices for AHRS initialization bank angle limitations. NOTE: See the Appendices for additional information regarding system-specific annunciations and alerts.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 15
System ystem Overview verview
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
NOTE: See the Airplane Flight Manual (AFM) 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 1-7. 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 1-8), the MFD Power-up Page displays the following information:
• System version• Copyright• Land database name and version• Obstacle database name and version• Terrain database name and version• Aviation database name, version, and effective dates• Chartview 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 1-8 MFD Power-up PageFigure 1-7 PFD Initialization
16 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
System ystem Overview verview
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
1.6 Systemystem Operationperation
The displays are connected together via a single Ethernet bus, thus allowing for high-speed communication. As shown in Figure 1-1, each GIA 63W is connected to the on-side PFD. This section discusses the normal and reversionary modes of operation as well as the various AHRS modes of the G1000 system.
Normal Operationperation
PFD
In normal mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude and vertical speed), thereby replacing the traditional flight instrument cluster. The PFD also offers control for COM and NAV frequency selection.
MFD
In normal mode, the right portion of the MFD displays a full-color moving map with navigation information, while the left portion of the MFD is dedicated to the Engine Indication and Crew Alerting System (EICAS).
Figure 1-9 gives an example of the G1000 displays in normal mode.
Figure 1-9 Normal OperationMFD PFD1PFD2
Reversionaryeversionary Mode NOTE: The G1000 system alerts the pilot when backup paths are utilized by the LRUs. Refer to the Appendices for further information regarding system-specific alerts.
　
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