Garmin G1000:Socata Pilot's Manual page 47

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UDIO LERTS
The Audio Alert Box on the System Setup Page allows the audio alert voice to be set to male or female.
To change the audio alert voice:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
2) Turn the large FMS Knob to highlight the voice in the Audio Alert Box.
3) Turn the small FMS Knob to display and highlight the desired voice and press the ENT Key.
MFD D
ATA
The MFD Data Bar Fields Box on the System Setup Page displays the current configuration of the MFD
Navigation Status Box. By default, the Navigation Status Bar is set to display ground speed (GS), distance
to next waypoint (DIS), estimated time en route (ETE), and en route safe altitude (ESA).
To change the information shown in an MFD Navigation Status Bar field:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
2) Turn the large FMS Knob to highlight the desired field number in the MFD Data Bar Fields Box.
3) Turn the small FMS Knob to display and scroll through the data options list and press the ENT Key when the
desired data selection is highlighted.
The following data may be selected for display in each of the four fields of the Navigation Status Box.
• Bearing (BRG)
• Distance (DIS)
• Desired Track (DTK)
• En Route Safe Altitude (ESA)
• Estimated Time of Arrival (ETA)
• Estimated Time En Route (ETE)
• Ground Speed (GS)
• Minimum Safe Altitude (MSA)
GPS CDI
The GPS CDI Box on the System Setup Page allows the pilot to define the range for the on-screen course
deviation indicator (CDI). The range values represent full range deflection for the CDI to either side. The
default setting is 'AUTO'. Refer to the Flight Instruments sections for a discussion on CDI scaling.
If a lower CDI range setting is selected (i.e., 1.0 or 0.3 nm), the higher range settings are not selected
during any phase of flight. For example, if 1.0 nm is selected, the G1000 uses this for en route and terminal
phases and ramps down to 0.3 nm during an approach. Note that the Receiver Autonomous Integrity
Monitoring (RAIM) protection limits follow the selected CDI range and corresponding flight phases.
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AR IELDS
Garmin G1000 Pilot's Guide for the Socata TBM 850
SYSTEM OVERVIEW
• True Air Speed (TAS)
• Track Angle Error (TKE)
• Track (TRK)
• Vertical Speed Required (VSR)
• Crosstrack Error (XTK)
• Fuel Over Destination (FOD)
• Fuel On Board (FOB)
• Endurance (END)
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