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During precision approach operations, glideslope
position is indicated by a diamond on a
glide-slope scale, which is on the left edge of the
altitude display (Table 16-4 and Figure 16-21).
Marker Beacon
When passing over a marker beacon, a small
box appears at the top left of the altitude display
(Figure 16-22). The box appears differently
for different beacons:
• Outer marker—Blue box with black
letter “O”
• Middle marker—Amber box with black
letter “M”
• Inner marker—White box with black
letter “I”
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CITATION MUSTANG OPERATING MANUAL
1800
0
1700
1600
1400
1300
15 20
40
00
G
M
29.92IN
MARKER
BEACON
ANNUNCIATION
GLIDE-SLOPE
INDICATOR
Figure 16-21. Glide-Slope Indicator
INDICATOR G G V
BUG ICON
(GLIDESLOPE) (GLIDEPATH) (VERTICAL DEVIATION)
Table 16-4. VERTICAL DEVIATION
DISPLAY
FLIGHT PHASE ANNUNCIATION AUTO CDI SCALING
DEPARTURE DPRT 0.3 NM
OCEANIC OCN 2.0 NM
ENROUTE ENR 2.0 NM
TERMINAL MODE TERM 1.0 NM
APPROACH LNAV 1.0 NM DECREASING TO
(NON-PRECISION) 350 FT DEPENDING ON
VARIABLES
APPROACH LNAV +V 1.0 NM DECREASING TO
(VERTICAL 350 FT DEPENDING ON
GUIDANCE) VARIABLES
APPROACH L/V NAV 1.0 NM DECREASING TO
(LNAV/VNAV) 350 FT DEPENDING ON
VARIABLES
APPROACH LPV 1.0 NM DECREASING TO
(LPV) 350 FT DEPENDING ON
VARIABLES
MISSED APPROACH MAPR 0.3 NM
Table 16-3. Flight Phases and CDI Scaling
Vertical Speed
Vertical Speed Indication
The vertical speed indication is through a
fixed index scale on the right side of the altitude
scale, and through a moving black pointer
box with white digits indicating current vertical
speed (when greater than 100 fpm up or
down) (Figure 16-23). A negative number indicates
descent. The vertical speed indication
displays in 50-foot increments.
Vertical Speed Reference Box and
Bug
A reference vertical speed set through the
AFCS indicates on the vertical speed scale by
a notched cyan bug on the scale and a vertical
speed indicated with cyan digits in a box at the
top of the scale.
INSET MAP
The pilot may activate a small moving map or
inset in the lower left corner of the PFD. The
PFD inset map can contain much of the same
information as available in the full-size moving
map on the MFD.
AUXILIARY INFORMATION
WINDOW
In the lower-right corner of the PFD, an auxiliary
information window can be set to display
information from the system, including:
• Nearest airports, with basic information
as currently recorded in the navigation
database (NRST softkey)
• ADF and distance measuring equipment
(DME) tuning (ADF/DME softkey)
• Flight plan display and entry (FPL key)
• Garmin system messages (MSG softkey)
• PDF setup (MENU key)
• References (TMR/REF softkey)
• Flight plan procedures (PROC key)
• Direct-To (D➞ Key)
Also use this window to select a waypoint
from the database and/or to display information
about the waypoint.
REVERSIONARY MODE
To provide emergency backup of the MFD and
PFDs, and to provide flexibility in display
modes, the G1000 has a reversionary mode that
causes both the PFD and the MFD to display
the essential information for continued flight.
In the event of display failure, the display
modes are as follows:
• PFD1 failure—MFD enters reversionary
mode; PFD2 remains in normal mode.
• MFD failure—PFDI and PFD2 enter
reversionary mode.
• PFD2 failure—PFD1 and the MFD remain
in normal mode.
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CITATION MUSTANG OPERATING MANUAL
4
4
2
2
VERTICAL 500
SPEED
POINTER
Figure 16-23. Vertical Speed Indicator
1800 M
0
O M I
ALTIMETER
OUTER MARKER MIDDLE MARKER INNER MARKER
Figure 16-22. Marker Beacon Indications
Reversionary mode can be manually selected for
the onside display and the MFD by pressing
the large red DISPLAY BACKUP button at the
bottom of either audio control panel. Pressing
the red DISPLAY BACKUP button a second
time returns both displays to normal mode.
In reversionary mode, the left edge of the display
includes a single-column of EICAS information
condensed from the normal two-column
EICAS display on the MFD. Additionally, a
CAS message window appears on the right
　
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