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N
33
30
W
24
VOR1
9.9NM
OJC
NAV2
39.3NM
113.00
TOP
NAV2
NAV1
DME
9.9NM
117.95 178°
NAV1
DME
–.––NM
NO DATA
GPS
54.6NM
BUM
NAV1
DME LABEL
BEARING
SOURCE
POINTER
ICON
NO WAYPOINT
SELECTED
BEARING 1
INFORMATION
WINDOW
BEARING 2
INFORMATION
WINDOW
BEARING 1
POINTER
BEARING 2
POINTER
DME
INFORMATION
WINDOW
POINTER
ICON
BEARING
SOURCE
STATION
IDENTIFIER
GPS DISTANCE TO
BEARING SOURCE
DME DISTANCE
FREQUENCY
TUNING MODE
Figure 16-27. HSI With Bearing and DME Indication
Wind Data Box
The wind data box appears above the DME
window. There are three wind presentations,
which indicate the calculated wind velocity.
When the window is selected for display,
but window information is invalid or
unavailable, the window displays NO WIND
DATA (Figure 16-28).
Traffic Alerts
When the TIS detects a traffic hazard, an
amber/black TRAFFIC box appears to the
right of the top of the airspeed scale. If a traffic
alert occurs, the inset map scales to the appropriate
range. If the range on the map is set
appropriately, an amber symbol appears on
the map with a track vector.
AFCS Alerts
The AFCS presents alerts in the system status
field near the top of the airspeed scale.
Air Temperatures (RAT and ISA)
The ram air temperature (RAT) display is at
the lower-left corner of the PFD display area
(Figure 16-29). The ISA (International
Standard Atmosphere) temperature display is
immediately right of the RAT box. The ISA
temperature box indicates the difference between
ISA temperature and the OAT.
System Time Box
A box in the lower-right corner of the PFD indicates
time as referenced by satellite data
(Figure 16-30). The time is displayed as local
time (LCL) in 12-hour or 24-hour format, or
as Coordinated Universal Time (UTC).
Generic Timer
A generic timer may be set and operated by the
pilot (Figure 16-31). It displays hours/minutes/
seconds, counting up or counting down.
Access is through the TMR/REF softkey.
16-26 510OM-00
CITATION MUSTANG OPERATING MANUAL
HDG 035°
21
S
15
12
E
6
3
N
33
30
W
24
305
GPS
RAT 0°C ISA +15°C
130
M1 2.4011
RAT 0°C ISA +15°C
HDG 035°
15
12
E
6
3
N
33
145
GPS
RAT 0°C
ISA +15°C
130
120
125
60
750
1000
750
1000
27
200
27
7500
5.0
UP
0
142.8 N2% 142.8
OIL
PSI
°C
FUEL
LBS
PPH
DC VOLTS
DC AMPS
CABIN PRESS
ALT FT
DIFF PSI
FLAPS
BATT VOLTS
°C
27
200
125
60
NORMAL DISPLAY REVERSIONARY MODE
Figure 16-29. Ram Air Temperature Box
OPTION 3 OFF
OPTION 1 OPTION 2
Figure 16-28. Wind Data Box
21
S
15
12
E
6
3
N
33
30
W
24
117° 4
14900
30.04IN
CRS 633°
TERM
XPDR1 1259 ALT R LCL 17:12:20
LCL 17:41:40
Figure 16-30. System Time Box
MULTIFUNCTION
DISPLAY
DESCRIPTION
This section provides a basic discussion of
MFD displays and controls, and is intended to
provide the pilot a useful understanding of
the purpose and organization of the MFD
(Figure 16-32).
The G1000 includes a single 15-inch MFD in
the center of the instrument panel. The MFD
provides indications for:
• EICAS
• Moving-map displays (with depictions of
navigation references and flight hazards)
• Information pages on waypoints, instrument
flight rule (IFR) procedures, airports,
airways, and navaids
• Flight planning
• Navigation status indications
• System status indications
The MFD also provides an alternate display
for essential flight instrumentation from either
PFD through the use of reversionary mode.
The MFD has many possible settings and
displays. For additional details, refer to the
supplemental G1000 manuals and documents
supplied with the Citation Mustang.
MFD CONTROLS
The MFD is controlled by softkeys across the
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CITATION MUSTANG OPERATING MANUAL 2(23)
