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does not change to the active until the
user presses the COM frequency transfer key.
AUX Page Group
The AUX page group provides auxiliary information
and data entry pages for the pilot.
These include:
• WEIGHT PLANNING
• TRIP PLANNING
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CITATION MUSTANG OPERATING MANUAL
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CITATION MUSTANG OPERATING MANUAL
• UTILITY
• GPS STATUS
• SYSTEM SETUP
• XM INFORMATION
• SYSTEM STATUS
• DIAGNOSTICS (available on ground
only for maintenance purposes)
For details on the functions of each of these
pages, refer to the supplemental G1000 documents
supplied with the aircraft.
NRST Page Group
The NRST page group displays a moving
map showing aircraft position relative to the
following:
• AIRPORTS
• INTERSECTIONS
• NDB
• VOR
• USER WPTS
• FREQUENCIES
• AIRSPACES
The moving map initially displays the course
to the nearest resource as a dotted/dashed
white line.
FPL Page Group
The FPL page group includes these pages:
• ACTIVE FLIGHT PLAN—Including
vertical navigation.
• FLIGHT PLAN CATALOG—Allows
the pilot to store several flight plans for
future use.
NAVIGATION STATUS BOX
The navigation data bar is the center area
across the top of the MFD. It displays four
fields of real time, GPS derived, navigation
data. The four fields are pilot adjustable and
can display the following options:
• BRG—Bearing (to the active waypoint)
• DIS—Distance (to the active waypoint)
• DTK—Desired track (to the active waypoint)
• ETA—Estimated time of arrival (to the
active waypoint)
• ETE—Estimated time enroute (to the
active waypoint)
• ESA—Enroute safe altitude for the entire
route of flight
• GS—Groundspeed
• MSA—Minimum safe altitude within a
10-mile radius of the aircraft
• TAS—True airspeed (taken from the
GDC 74B)
• TKE—Track angle error
• TRK—Track angle
• VSR—Vertical speed required
• XTK—Crosstrack error
The fields can be selected in the AUX–SYSTEM
SETUP page under the MFD DATA BAR
FIELDS box.
FLIGHT MANAGEMENT
SYSTEM
WEIGHT PLANNING
Before flight, when the G1000 initializes, the
AUX–WEIGHT PLANNING page appears.
The pilot uses the dual FMS knob to move
through the windows of the page, and enter current
data for the flight. Pressing the EMPTY
WT softkey sets the cursor to that entry, and
the pilot corrects as appropriate, then enters
data for other weights. Fuel weights may be
automatically entered from the current EICAS
indications by pressing the FOB SYNC softkey.
During aircraft operation, fuel flow and
ETE can be automatically determined from
actual operation, and the blank calculated
fields display corresponding calculated data.
FMS AND FLIGHT PLANS
A FMS provides for flight navigation planning
and enroute status monitoring. The FMS primarily
operates through the flight plan pages
of the MFD, which allow the pilot to enter a
flight plan with an entire flight profile, from
takeoff to landing. Both lateral and vertical
navigation courses may be entered into the
flight plan. The flight plan may be used to
guide the flight by the:
• Pilot viewing the FPL and MAP pages
for general reference
• Pilot using the FD to follow the flight plan
• Aircraft using the AP to follow the
flight plan
Flight plans changed or terminated in flight
may be stored for future use and may be
deleted.
Computers for these functions are in the displays.
GPS navigation data (provided from
the GIAs) is the primary navigation source
that is automatically selected flight plan status
tracking. Any one of the displays can perform
the FMS functions. Airspeed and altitude
information from the ADC may also be used,
depending on flight plan configuration.
MFD/FMS FLIGHT PLAN
CONTROLS AND INDICATIONS
The MFD/FMS controller provides primary
control of these functions. PFDs may also be
set to display smaller windows containing
FMS information and maps. Corresponding
controls on the PFD bezels may be used to
control the FMS.
NOTE
Most explanations in this section are
based on the assumption the user is
using the MFD and the MFD/FMS
controller. Some (but not all) FMS
　
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