Honeywell PRIMUS 1000 - Airspeed Display; Airspeed;Mach Reference Bug and Display

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
4-45
Electronic Flight Instrument System (EFIS)
AIRSPEED DISPLAY
The airspeed section of the PFDis shown in figure 4--24. A description
of airspeed annunciations is given below.
AD--50918--R1@
9
1
260
280
220
200
240
260
.410
M
Vmo/Mmo
INDICATOR BAR
AIRSPEED SET
BUG
AIRSPEED REFERENECE
LINE
VSPEED
SET BUGS
1
R
2
AP
V
1
R
V
2
V
PP
VA
AIRSPEED TREND
VECTOR
9
1
60
80
240
I
A
S
160
AIRSPEED
COMPARISON
MONITOR
ANNUNCIATOR
TAKEOFF VSPEED
SET DISPLAY
2
135 2
125 R
120 1
AIRSPEED BUG
DIGITAL DISPLAY
ROLLING AIRSPEED
DIGITAL DISPLAY
MACH DISPLAY
IAS ANALOG SCALE
Airspeed Display
Figure 4--24
D V
MO
Overspeed Bar -- The V
mo
is a fixed red bar originating at V
MO
and extending to the scale’s end. This bar is located along the right
side of the airspeed scale.
D Airspeed/Mach Reference Bug and Display -- Using the guidance
controller SPD set knob, and engaging the flight director SPD mode,
thepilot--adjustableairspeedorMachreference isdisplayed abovethe
airspeed tape. The corresponding airspeed bug is shown on the right
side of the airspeed tape. The digital display and bug are both cyan.