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For more information on yaw damper, please refer to Chapter 10, FLIGHT
CONTROLS.
GX_02_007
CRS 2
PUSH DCT
Honeywell
AP FD
CPL
YD
For Training Purposes Only
Sept 04
2-9
P I LOT T R A I N I N G GU I D E
AUTOMATIC FLIGHT CONTROL SYSTEM
PFD ANNUNCIATION
220
LIM LNAV TCS ALT
SPD VAPP VNAV
23500
ATT2
ADC1 0.88 30000
GX_02_008
AP1
TCS
TCS
DN
UP
P
I
T
C
H
VNAV
VS
Pitch
Wheel
AP ENGAGE STATUS
TOUCH CONTROL STEERING (TCS) STATUS
VERTICAL SPEED REFERENCE
VS Target
Readout
VS
Pointer
1000
VS 1000
0
1
2
3
1
VS Target
Bug
VS Speed
Readout
AP
FMS1
HDG
330
1000
VS 1000
0
1
2
3
1
2
3
N
33
30
W
24
21
S
15
12
E
6
3
29.92 IN
220
LIM LNAV AP1 ALT
SPD VAPP VNAV
23500
ATT2
ADC1
20 20
0.88 30000
P I LOT T R A I N I N G GU I D E
AUTOMATIC FLIGHT CONTROL SYSTEM
2-10 For Training Purposes Only
Sept 04
FLIGHT DIRECTOR (FD)
The Flight Director modes of operation can be divided into two major subgroups, the
Lateral modes and the Vertical modes. Only one lateral mode and one vertical mode
may be active (green) at any time; however, one lateral arm (white) mode and up to
two vertical arm (white) modes may be selected.
The armed and active modes are annunciated on both PFDs. Armed modes are
displayed in white below active modes, which are displayed in green. The lateral
modes are annunciated on the left side of the displays and the vertical modes on the
right side, above the attitude sphere. Low bank mode is annunciated via green
eyebrow on top of the attitude sphere.
300
LIM LNAV AP1 VPTH
SPD VOR VPTH
23500
ATT2
ADC1
20 20
0.84 30000
300
LIM LNAV AP1 PIT
SPD VOR VPTH
23500
ATT2
ADC1
20 20
0.84 30000
300
LIM VOR AP1 PIT
SPD VOR VNAV
23500
ATT2
ADC1
20 20
0.84 30000
300
LIM ROL AP1 PIT
SPD VOR VNAV
23500
ATT2
ADC1
20 20
0.84 30000
VNAV
Active mode flashes
for 5 seconds upon
automatic mode
capture.
Active mode flashes
for 5 seconds upon
automatic mode
capture.
VOR
VPTH
GX_02_009
VPTH
VOR
ACTIVE LATERAL MODE
ARMED VERTICAL MODE
ACTIVE VERTICAL MODE
ARMED LATERAL MODE
HDG FLC
LNAV VNAV
Active modes
Armed modes
Low bank
300
280
190
180
LIM HDG AP1 FLC
SPD LNAV VNAV
23500
10000
ATT2
ADC1
20 20
10 10
0.88
265
6
4
30000
20
00
80
60
230
NAV
For Training Purposes Only
Sept 04
2-11
P I LOT T R A I N I N G GU I D E
AUTOMATIC FLIGHT CONTROL SYSTEM
Flight director command bars appear on the PFD whenever a lateral mode is selected.
The FD switch is used to remove flight director command bars. If the AP is on, the offside
button will remove the off-side flight director bar(s) only. If the AP is on, the onside
button is not functional. Flight director command bars are always present on both
PFDs when Go Around (GA), Takeoff (TO) or Windshear Guidance (WS) modes are
active.
20 20
10 10
10 10
20 20
FD Switch:
Used to remove flight director
command bars from the noncoupled
PFD.
GX_02_010
20 20
10 10
10 10
20 20
HDG AP1 FLC
LNAV VNAV 0.88 30000
23500
300
280
260
265
6
4
HDG AP1 FLC
LNAV VNAV 0.88 30000
23500
300
280
260
240 240
265
6
4
COPILOT’S PFD
CRS 1
PUSH DCT
FD
CRS 2
PUSH DCT
Honeywell
FD
PILOT’S PFD
23000
80
20
23000
80
20
20 20
ROL AP1 GA 200
23500
220
30000
CPL
TOGA
buttons
FLIGHT DIRECTOR DATA SOURCE (CPL)
FLIGHT DIRECTOR COMMANDS AND STATUS
20 20
10 10
ROL AP1 GA 200 3000
1500
180
170
160
6
GX_02_011
TOGA
buttons
P I LOT T R A I N I N G GU I D E
AUTOMATIC FLIGHT CONTROL SYSTEM
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Bombardier global AUTOMATIC FLIGHT CONTROL SYSTEM(4)
