Honeywell KAP 140 Pilot's Manual page 75

N
3
4
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
PUSH
G
KAP 140
AP HDG NAV
3. At the desired point, HDG mode is used to initi-
ate the procedure turn. Select HDG and set the
heading bug to 283°. During the procedure turn
outbound, the CDI course index goes off scale
to the right. The aircraft is flying away from the
localizer centerline at a 45° angle on a selected
heading of 283°.
* Check the heading displayed on the DG against
the magnetic compass and reset if necessary.
Rev. 1
Apr/02
270°
N
TO
A
V
GS
FR
OBS
ı
UP
DN
APR REV
ALT
KAP 140 AUTOPILOT SYSTEM
Two Axis Operation
2
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
PUSH
G
KAP 140
AP HDG NAV APR
4. Now you have reset the heading bug to 103°
and made a 180° turn to this heading. This
103° heading will intercept the front course of
058°. You must now select the approach mode
by depressing the APR button on the KAP 140.
* The HDG annunciation will flash for five sec-
onds then extinguish. While the HDG annuncia-
tion is flashing, move the heading bug to the
front course 058°. Since the 45° intercept is
103°, the aircraft will not turn until the front
course is captured.
1
N
TO
A
V
GS
FR
OBS
ı
UP
DN
REV
ALT
67