Owner's manual

KAP 140 AUTOPILOT SYSTEM
Two Axis Operation
61
Rev. 1
Apr/02
3. The autopilot is responding to the heading select
mode with a left bank. The climb rate has been
decreased, using the button, in preparation
for level off.
4. The autopilot has completed the turn and is
now established on a 010° heading. Desired
altitude has been reached, altitude hold ( )
has been engaged and the aircraft maintains
the reference altitude.
Two Axis Operation
60
KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02
1. The aircraft is well off the ground and estab-
lished at a safe climb rate.
The heading bug on the DG or HSI is turned to
the desired heading of 080° (runway heading).
By depressing the button on the KAP 140,
the autopilot engages into the heading and ver-
tical speed modes and maintains the selected
heading of 080° and current rate of climb.
Note: Press and hold the button for 0.25
seconds to engage the autopilot (applicable
only to software version 03/01 and later).
2. The heading bug on the DG or HSI is turned to
the new desired heading of 010° and the aircraft
begins to respond with an immediate left turn.
N
080°
010
°
123 4
1234
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
GS GS
N
33
30
W
24
21
S
15
12
E
6
3
ı
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
OR
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
GS GS
N
33
30
W
24
21
S
15
12
E
6
3
ı
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
OR
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
GS GS
N
3
3
30
W
2
4
21
S
1
5
12
E
6
3
ı
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
OR
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
GS GS
N
3
3
3
0
W
2
4
2
1
S
1
5
1
2
E
6
3
ı
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
OR
OPERATIONS WITH THE KAP 140
Takeoff And Climb To Assigned Altitude