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• Heading Select Mode with the Selected Heading set to 90° left of the current heading
Figure 7-48 Emergency Descent ModeSelectedAltitudeSet to15000 ftFlight Level Change Mode ActiveHeading Select Mode ActiveAutopilot EngagedSelected Heading Set 90° Left of Current HeadingEmergency Decent Mode Annunciation
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-02 Rev. B
413
Additional Featureseatures
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Section 8 Additional Featureseatures NOTE: With the availability of SafeTaxi, ChartView, or FliteCharts in electronic form, it is still advisable to carry another source of charts on board the aircraft.
Additional features of the system include the following:
• Synthetic Vision System (SVS)
• SafeTaxi® diagrams
• ChartView and FliteCharts® electronic charts
• XM Radio entertainment for the passengers
• Scheduler
The optional Synthetic Vision System (SVS) provides a three-dimensional forward view of terrain features on the PFD. SVS imagery shows the pilot’s view of relevant features in relation to the aircraft attitude.
SafeTaxi diagrams provide detailed taxiway, runway, and ramp information at more than 700 airports in the United States. By decreasing range on an airport that has a SafeTaxi diagram available, a close up view of the airport layout can be seen.
The optional ChartView and FliteCharts provide on-board electronic terminal procedures charts. Electronic charts offer the convenience of rapid access to essential information. Either ChartView or FliteCharts may be configured in the system, but not both.
The optional XM Radio entertainment audio feature of the GDL 69A Data Link Receiver handles more than 170 channels of music, news, and sports. XM Radio offers more entertainment choices and longer range coverage than commercial broadcast stations.
The Scheduler feature can be used to enter and display short term or long term reminder messages such as Switch fuel tanks, Change oil, or Altimeter-Transponder Check in the Messages Window on the PFD.
Optional checklists help to quickly find the proper procedure on the ground or during flight.
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-02 Rev. B
414
Additional Featureseatures
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
8.1 Synthetic Vision Systemystem (SVS) Noteote: When Synthetic Vision System (SVS) is installed in the G1000 the X-Pointer Command Bars cannot be used when SVS is in use. Refer to the AFCS Section and Flight Instruments Section for more information. NOTE: SVS requires a terrain database that has a resolution of nine arc-seconds. NOTE: SVS is not intended to be used alone for aircraft control, navigation, obstacle and terrain avoidance, or to avoid other aircraft.
The optional Synthetic Vision System (SVS) is a visual enhancement to the G1000 Integrated Flight Deck. SVS depicts a forward-looking attitude display of the topography immediately in front of the aircraft. The field of view is 30 degrees to the left and 35 degrees to the right. SVS information is shown on the Primary Flight Display (PFD), or on the Multifunction Display (MFD) in Reversionary Mode (Figure 8‑76). The depicted imagery is derived from the aircraft attitude, heading, GPS three-dimensional position, and a nine arc-second database of terrain, obstacles, and other relevant features. The terrain data resolution of nine arc-seconds, meaning that the terrain elevation contours are stored in squares measuring nine arc-seconds on each side, is required for the operation of SVS. Loss of any of the required data, including temporary loss of the GPS signal, will cause SVS to be disabled until the required data is restored.
The SVS terrain display shows land contours, large water features, towers, and other obstacles over 200’ AGL that are included in the obstacle database. Cultural features on the ground such as roads, highways, railroad tracks, cities, and state boundaries are not displayed even if those features are found on the MFD map. The terrain display also includes a north–south east–west grid to assist in orientation relative to the terrain. The colors used to display the terrain elevation contours are similar to that of the topo map display.
The Terrain Awareness and Warning System (TAWS) is integrated within SVS to provide visual and auditory alerts to indicate the presence of terrain and obstacle threats relevant to the projected flight path. Terrain alerts are displayed in red and yellow shading on the PFD.
　
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