Honeywell KAP 140 Pilot's Manual page 113

D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
PUSH
G
KAP 140
AP HDG NAV
3. At the desired point, heading mode is used to
initiate the procedure turn. During the procedure
turn outbound, the deviation bar shows that the
aircraft is flying away from the GPS course 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
TO
GS
FR
OBS
ı
ARM BARO
UP
DN
APR REV
ALT
KAP 140 AUTOPILOT SYSTEM
Two Axis/Altitude Preselect Operations
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
PUSH
G
KAP 140
AP HDG
4. The heading bug has been set to 103° and the
aircraft has made a left turn to this heading.
The GPS's Leg/OBS mode switching is set to
Leg mode and the OBS is set to 058°. Select
approach mode by depressing the APR button.
*The HDG annunciation will flash for five sec-
onds then extinguish. While the HDG annuncia-
tion is flashing, move the heading bug to 058°.
Since the 45° intercept is 103°, the aircraft will
not turn until the course is captured.
TO
GS
FR
OBS
ı
ARM BARO
UP
DN
NAV APR REV
ALT
105