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Selecting the BACK Softkey, or waiting during 45 seconds of softkey inactivity, returns the system to the top level softkeys.
Volume
Radio volume is controlled at each passenger station.
482 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Additional Features eatures
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
8.6 Scheduler
The Scheduler feature can be used to enter and display reminder messages (e.g., Hot Section Inspection or Phase 1 Maintenance Check) in the Messages Window on the PFD. Messages can be set to display based on a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently whenever the message timer reaches zero (periodic). Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed. When power is cycled, all messages are retained until deleted, and message timer countdown is resumed.
Figure 8-74 Scheduler (Utility Page)
Entering a scheduler message:
1) Select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the first empty scheduler message naming field.
4) Use the FMS Knob to enter the message text to be displayed in the Messages Window and press the ENT Key.
5) Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type.
6) Turn the small FMS Knob to select the message type:
• Event—Message issued at the specified date/time
• One-time—Message issued when the message timer reaches zero (default setting)
• Periodic—Message issued each time the message timer reaches zero
7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field.
8) For periodic and one-time message, use the FMS Knob to enter the timer value (HH:MM:SS) from which to countdown and press the ENT Key.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 483
Additional Features eatures
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
9) For event-based messages:
a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key.
b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field.
c) Use the FMS Knob to enter the desired time (HH:MM) and press the ENT Key.
10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message.
Deleting a scheduler message:
1) Select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted.
4) Press the CLR Key to clear the message text. If the CLR Key is pressed again, the message is restored.
5) Press the ENT Key while the message line is cleared to clear the message text.
Scheduler messages appear in the Messages Window on the PFD. When a scheduler message is waiting, the MSG Softkey label flashes. Pressing the MSG Softkey opens the Messages Window and acknowledges the scheduler message. Pressing the MSG Softkey again removes the Messages Window from the display, and the scheduler message is deleted from the message queue.
Figure 8-75 PFD Messages Window
484 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Additional Features eatures
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
8.7 Abnormal Operationperation
SVS Troubleshootingleshooting
SVS is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVS is disabled when valid attitude or heading data is not available for the display. In case of invalid SVS data, the PFD display reverts to the standard blue-over-brown attitude display.
SVS becomes disabled without the following data resources:
• Attitude data
• Heading data
• GPS position data
• 9 Arc-second Terrain data
• Obstacle data
• TAWS function is not available, in test mode, or failed
• The position of the aircraft exceeds the range of the terrain database.
Reversionaryeversionary Mode
SVS can be displayed on the Multifunction Display (MFD) in Reversionary Mode. If it is enabled when switching to Reversionary Mode, SVS will take up to 30 seconds to be displayed. The standard, non-SVS PFD display will be shown in the interim.
　
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