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operations can also be performed with
a PFD and its controls. This section
provides limited operating information
for training purposes only. For
more detailed and current instructions,
refer to the AFM, the Garmin
G1000 Pilot’s Guide, and the Garmin
G1000 Cockpit Reference Guide.
Flight plans and their associated map and information
pages are normally presented on
the MFD. The FPL (flight plan) page group includes
two types of pages:
• ACTIVE FLIGHT PLAN—Flight plan
currently active in the G1000, including
VNAV
• FLIGHT PLAN CATALOG—List of all
flight plans stored in the G1000
Both FPL pages may be viewed on the MFD.
Courses and waypoints in an active flight plan
are depicted on the MAP–NAVIGATION MAP
page (and other maps) of the MFD. The course
for the active leg of an active flight plan is displayed
as a magenta line. Other legs of the
course display as white lines.
USER-DEFINED WAYPOINTS
The user may define new waypoints for use in
navigation. This is helpful in FMS operations
to allow maximum flexibility in flight planning.
User-defined waypoints are necessary
when a waypoint is not stored in the navigation
database. The pilot enters user-defined
waypoints into the WPT–USER WPT INFORMATION
page. These waypoints may be selected,
as needed, through the FPL (flight
plan) pages.
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IFR PROCEDURES
IFR procedures are stored in the database and
can be included in flight plans. The procedures
include:
• Standard instrument departures (SIDs)
• Arrival procedures (standard terminal
arrival routes [STARs])
• Approach procedures
VERTICAL NAVIGATION
The MFD/FMS controller provides for vertical
navigation (VNAV) capability in-flight
planning (Figure 16-35). This feature is available
for enroute/terminal cruise and descent
operations when VNAV has been enabled and
a VNAV flight plan (with at least one vertical
waypoint) has been activated. Vertical DIRECT
TO also provides VNAV functions. The
flight director/AFCS may be armed for VNAV
at any time; however, no target altitudes are
captured during a climb.
VNAV indications include the following:
• VNAV TARGET ALTITUDE—As preset
by the pilot, that altitude in MSL to
be reached by flying a programmed vertical
speed.
• VERTICAL DEVIATION INDICATOR—
This symbol indicates deviations
from the correct flight path; thereby allowing
the pilot (or AFCS) to make adjustments
in pitch, as required, to
maintain the selected vertical profile.
• REQUIRED VERTICAL SPEED—The
vertical speed rate required to achieve
the preselected altitude within that distance
defined by the programmed flight
plan.
For more information on vertical navigation,
refer to the Garmin manuals and guides supplied
with your Citation Mustang.
AUTOMATIC FLIGHT
CONTROL SYSTEM
DESCRIPTION
The Mustang includes an AFCS that provides
flight guidance and automatic flight control.
The automatic flight control system includes
three primary functions:
• Flight director
• Autopilot
• Yaw damper
• Manual electric pitch trim
The AFCS controller (above the MFD) provides
control of these functions, and the PFDs
provide necessary indications (Figure 16-36
and Table 16-8). Computers for these functions
are in the GIAs and the servos. If either
GIA fails, the other GIA performs the FD
functions. If both GIAs fail, the AFCS is not
operational.
The FD and AP follow the same sources of
data for AFCS guidance. If AP is engaged, the
information is used to control the airplane. If
the FD is engaged, the information is used to
guide the pilot.
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3600
4
4
2
2
13400
0
13300
13200
13000
12900
131
20
80
00
V
-1250
29.92IN
VNAV
TARGET
ALTITUDE
REQUIRED
VERTICAL
SPEED
VERTICAL
DEVIATION
INDICATOR
Figure 16-35. VNAV Indications
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1 2 3 4 5 6 7 8
19 18 17 16 15 14 13 12 11 10 9
Figure 16-36. AFCS Controller
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# CONTROL DESCRIPTION
1 HDG Key Selects/deselects Heading Select Mode.
2 APR Key Selects/deselects Approach Mode.
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