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on the airspeed tape by a red/white
“barber pole” (Figure 16-7) The flap speed
references represent the airspeed limits when
the aircraft is below 18,000 feet. A red lowspeed
awareness range extends up from the
bottom of the tape to indicate VLSA.
AIRSPEED
TREND VECTOR
VSPEED
ACTUAL SPEED REFERENCES
REFERENCE
APPROACH SPEED CUE
Figure 16-6. Airspeed Indicator
Airspeed References
Airspeed references, or flags, appear on the
outside right edge of the tape display fixed to
their corresponding airspeed (Table 16-2).
Takeoff and landing speed flags can be displayed
and adjusted in the reference window
using the TMR/REF softkey. Takeoff references
are automatically turned off when airspeed
reaches 160 kt (see Figure 16-6).
A reference approach speed cue appears as
an open green circle on the right edge of the
tape display. The open green circle represents
1.3 VS1 (see Figure 16-6).
Flap Speed References
Maximum flap-extension speeds are indicated
on the outside right edge of the tape display
by reference flags similar to the V-speed flag
(Figure 16-8). Maximum speed for takeoff/approach
flaps is indicated by a flag labeled
“TA”. Maximum speed for landing flaps is indicated
by a flag labeled “LD.” The flap reference
speed flag cannot be turned off or
adjusted by the pilot.
AFCS Selected Airspeed Box and Bug
When the AFCS is set to a selected airspeed
during flight level change mode, the selected
airspeed appears in a box at the top of the display,
and a corresponding notched blue bug appears
on the inside right edge of the airspeed
display (Figure 16-9).
510OM-00 16-13
CITATION MUSTANG OPERATING MANUAL
Figure 16-7. Red Pointer
Vspeed Flag
V1 1
VR R
V2 2
VENR E
VAPR AP
VREF RF
Table 16-2. V-SPEED TABLE
FLAP SPEED
REFERENCES
130
Figure 16-8. Flap Speed
210
240
230
250 220KT
220
AIRSPEED
REFERENCE
AIRSPEED
REFERENCE
BUG
Figure 16-9. AFCS Reference
Mach Window
At the bottom of the airspeed tape display, a
window indicates the Mach number, depending
upon aircraft altitude or airspeed.
Attitude and Turn Coordination
At the center of the PFD is the attitude indication
(Figure 16-10). The amber symbol represents
the airplane, and the amber bars represent
the wingtips. The horizon line is white, with
brown (ground) below and blue (sky) above.
The horizon line indicates 0° pitch. Pitch lines
are at 2.5° intervals above and below the horizon
line and are labeled at 10° intervals. Red
chevrons indicate extreme pitch at greater than
50° nose-up or 30° nose-down (Figure 16-11).
Roll indication is provided by an arc at the top
of the display that rotates with the horizon
line. The arc has major tick marks at 30° and
60°, and minor tick marks at 10°, 20° and 45°.
Turn Coordination (Slip/Skid)
Turn coordination is indicated by a small sliding
bar (slider) under the attitude display roll
pointer (Figure 16-12). The slider deflects a
full width left or right of the roll pointer to indicate
the same condition as indicated by a ball
positioned one ball width to the left or right
of center in a conventional instrument.
Flight Director Command Bars
The single-cue command bars vertically move
together to indicate pitch commands and bank
left or right to indicate roll commands (Figure
16-13). Command bars that display as a cross
16-14 510OM-00
CITATION MUSTANG OPERATING MANUAL
30 30
60 60
40
50
40
50
10 10
40
30
20
40
30
20
NOSE HIGH NOSE LOW
Figure 16-11. Pitch Attitude Warnings
20 Figure 16-12. Slip/Skid Indication
20
10
20
10
10 10
1
9
8
7
6
5
4
3
2
5
6
7
8
4
3
2
9
1
ROLL POINTER
ROLL SCALE ZERO
SKY REPRESENTATION
SLIP/SKID INDICATOR
PITCH SCALE
LAND REPRESENTATION
AIRCRAFT SYMBOL
HORIZON LINE
ROLL SCALE
Figure 16-10. Attitude Indication
pointer move independently to indicate pitch
(horizontal bar) and roll (vertical bar) commands.
Both PFDs show the same command
bar format (Figure 16-14).
To change the flight director format, activate
the FD FRMT softkey using the PFD softkey.
The pilot can then choose between SNGL CUE
　
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