Owner's manual
KAP 140 AUTOPILOT SYSTEM
Two Axis/Altitude Preselect Operations Two Axis/Altitude Preselect Operations
92 93
KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02
Rev. 1
Apr/02
3. When the computed capture point is reached,
the annunciation changes to and a
right turn is initiated by the autopilot.
4. The turn is complete and the autopilot is track-
ing the GPS course.
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
ARM BARO
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
ARM BARO
N
1
2
3
4
4
0
°
010
°
1. Continuing on heading 010°, a GPS waypoint is
established. A 30° intercept is desired.
2. The button is depressed to select
mode which will allow an “all angle intercept”.
GPS data is selected for the CDI and the OBS is
set to 040°. The button is depressed and
is annunciated. will change to
and flash for five seconds. will then
be redisplayed. While the annunciation is
flashing, move the heading bug to the desired
course of 040°. The aircraft will remain wings
level until the capture point.
GPS Capture 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
ARM BARO
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
ARM BARO
* Description of GPS operation based on Bendix/King GPS receiver. Others may
require different operation.