190-00709-04 Rev. A
Garmin G1000 Pilot’s Guide for the Socata TBM 850
43
SYSTEM OVERVIEW
mFD D
ata
B
aR
F
ielDs
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)
• 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)
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’. At this setting, leaving the departure airport the CDI range is set to 1.0 nm and
gradually ramps up to 2 nm beyond 30 nm from the departure airport. The CDI range is set to 2.0 nautical
miles during the en route phase of flight. Within 30 nm of the destination airport, the CDI range gradually
ramps down to 1.0 nm (terminal area). During approach operations, the CDI range ramps down even
further to 0.3 nm. This transition normally occurs within 2.0 nm of the final approach fix (FAF).
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 system 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.
The GPS CDI Box on the System Setup Page displays the following:
• Selected CDI range (auto, 2 nm, 1 nm, 0.3 nm)
• Current system CDI range (2 nm, 1 nm, 0.3 nm)
Summary of Contents for SOCATA TBM850
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