Owner's manual

KAP 140 AUTOPILOT SYSTEM
Two Axis Operation Two Axis Operation
74 75
KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02
Rev. 1
Apr/02
N
1
2
3
4
058
°
270°
238
°
283
°
103
°
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°.
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 button.
The annunciation will flash for five sec-
onds then extinguish. Move the heading bug
within five seconds to 058°. Since the 45°
intercept is 103°, the aircraft will not turn until
the course is captured.
1. The aircraft is in mode approaching the
IAF. Approach arm is indicated on the GPS
annunciator.*
2. Upon waypoint alerting at the IAF, the heading
bug is set to 238°, the GPS’s Leg/OBS mode
switching is set to OBS mode and the OBS is
set to 238°. The autopilot initiates a left turn to
track the 238° GPS course.
Outbound on GPS Approach Using DG
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
AP
G
KAP 140
HDG NAV APR REV
ALT
DN
UP
N
33
30
W
24
21
S
15
12
E
6
3
P
U
S
H
PUSH
TO
FR
N
S
E
W
33
30
24
21
15
12
6
3
OBS
GS
ı
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
AP
G
KAP 140
HDG NAV APR REV
ALT
DN
UP
N
33
30
W
24
21
S
15
12
E
6
3
P
U
S
H
PUSH
TO
FR
N
S
E
W
33
30
24
21
15
12
6
3
OBS
GS
ı
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
AP
G
KAP 140
HDG NAV APR REV
ALT
DN
UP
N
33
30
W
24
21
S
15
12
E
6
3
P
U
S
H
PUSH
TO
FR
N
S
E
W
33
30
24
21
15
12
6
3
OBS
GS
ı
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
AP
G
KAP 140
HDG NAV APR REV
ALT
DN
UP
N
33
30
W
24
21
S
15
12
E
6
3
P
U
S
H
PUSH
TO
FR
N
S
E
W
33
30
24
21
15
12
6
3
OBS
GS
ı
* Description of GPS operation based on Bendix/King GPS receiver. Others may
require different operation.