Owner's manual

KAP 140 AUTOPILOT SYSTEM
Single Axis Operation Single Axis Operation
50 51
KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02
Rev. 1
Apr/02
N
1
2
3
4
0
5
8
°
090°
2
3
8
°
FAF
3. At the missed approach point, the pilot disen-
gages the autopilot with the button on the con-
trol wheel. This cancels all operating modes.
The flashing annunciations are displayed and
a disconnect tone will sound.
4. The pilot initiates the missed approach and sta-
bilizes the aircraft in the climb. The heading
bug is set to the missed approach heading of
090°. By depressing the HDG button on the
KAP 140, the autopilot engages into the head-
ing mode, commencing a right turn to a head-
ing of 090°.
Note: Press and hold the button for 0.25
seconds to engage the autopilot (applicable
only to software version 03/01 and later).
1. Continuing the maneuver on page 46,
mode capture occurs. The autopilot initiates a
left turn to track the 058° GPS course.
Approach active is indicated on the GPS
annunciator.*
2. The autopilot is following the GPS course. The
autopilot will make the bank changes as neces-
sary to maintain the GPS course.
Inbound 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
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
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
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
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.