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seconds, when active.
LNAV capture will also occur when the airplane is within 2.5 miles of the desired
track, and moving away from it.
LNAV capture will occur when the airplane is at a calculated point, as a function of
track record and groundspeed, if the airplane is flying towards the desired track.
The FD will transition automatically (NAV to NAV transfer) from FMS navigation to a
LOC or VOR approach via the APR, or BC button. The selected NAV source must be
FMS, NAV radio must be tuned to the approach frequency and preview mode selected,
to allow a NAV transfer to occur.
The previewed approach is armed by pushing the APR or BC switch on guidance
panel. When LOC or BC captures, it replaces LNAV.
If the active vertical mode was not VNAV prior to capture, the vertical mode remains
unchanged. If the active vertical mode was VNAV prior to capture, then ALT mode
will replace the vertical mode.
If armed approach mode was APR (ILS), then GS is armed with LOC capture and GS
will capture when GS criteria is met.
DESIRED TRACK
LNAV capture will occur when the airplane
is within 2.5 miles of the desired track, and
moving away from it.
GX_02_021
DESIRED TRACK
LNAV capture will occur when the airplane is at
a calculated point, as a function of track error and
groundspeed, if the airplane is flying towards the
desired track.
GX_02_022
P I LOT T R A I N I N G GU I D E
AUTOMATIC FLIGHT CONTROL SYSTEM
2-26 For Training Purposes Only
Sept 04
Previewed Approach
DTK
360
HDG
330
SRP
N
33
30
W
24
21
S
15
12
E
6
3
23.4NM
FMS1
LOC1
Preview
Navigation
Source
Preview
Course
Pointer
GX_02_023
For Training Purposes Only
Sept 04
2-27
P I LOT T R A I N I N G GU I D E
AUTOMATIC FLIGHT CONTROL SYSTEM
BEARING (BRG) SOURCE
Bearing information VOR1, ADF1 or FMS1 and bearing information VOR2, ADF2 or
FMS2 is selected on either the pilot’s and/or the copilot’s PFD control panel, located
on the glareshield.
MINIMUMS
RAD BARO IN Hpa
NAV SRC BARO SET
BRG V/L FMS BRG
HSI
Honeywell PUSH STD
MINIMUMS
RAD BARO IN Hpa
NAV SRC BARO SET
BRG V/L FMS BRG
HSI
Honeywell PUSH STD
CRS
360
HDG
030
VOR 1
VOR 2
N
33
30
W
24
21
S
15
12
E
6
3
HDG
030
VOR 1
N
33
30
W
24
21
S
15
12
E
6
3
BRG BRG
GX_02_024
VOR1
VOR2
ADF1
ADF2
FMS1
FMS2
PFD CONTROL PANEL
NOTE:
Pushing BRG button(s) will
toggle the following in sequence:
- VOR
- ADF
- FMS
- Blank
P I LOT T R A I N I N G GU I D E
AUTOMATIC FLIGHT CONTROL SYSTEM
2-28 For Training Purposes Only
Sept 04
VOR/LOC NAV SOURCE
NAV source, VOR/LOC, is selectable on either the pilot’s and/or the copilot’s PFD
control panel.
NOTE
Pushing V/L button will toggle the NAV source in the following
sequence:
on-side VOR/LOC — X-side VOR/LOC — on-side VOR/LOC.
CRS
360
HDG
030
VOR 1
N
33
30
W
24
21
S
15
12
E
6
3
VOR1
CRS
360
HDG
030
VOR
VOR 2
N
33
30
W
24
21
S
15
12
E
6
3
VOR2
NAV SRC
V/L FMS BRG
GX_02_025
PILOT’S PFD COPILOT’S PFD
On-Side
CRS
360
HDG
030
VOR
VOR 2
N
33
30
W
24
21
S
15
12
E
6
3
VOR2
CRS
360
HDG
030
VOR
VOR 2
N
33
30
W
24
21
S
15
12
E
6
3
VOR2
GX_02_026
PILOT’S PFD COPILOT’S PFD
X-Side
For Training Purposes Only
Sept 04
2-29
P I LOT T R A I N I N G GU I D E
AUTOMATIC FLIGHT CONTROL SYSTEM
FMS NAV SOURCE
FMS source, FMS1, FMS2, FMS3 (if installed) or Navigation Display Unit (NDU),
also referred to as Lasertrack (LTRK) (if installed) is selectable on either the pilot’s
and/or the copilot’s PFD control panel.
NOTE
If V/L is the primary NAV source, pushing the FMS button will
　
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