BendixKing KAP 140 - Manual (Page 40)

KAP 140 AUTOPILOT SYSTEM
Single Axis Operation Single Axis Operation
32 33 KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02 Rev. 1
Apr/02
L R
2 MIN.
TURN COORDINATOR
NO PITCH INFORMATION
D.C. ELEC.
GS GS N
3 3
30
W
24 21
S
1 5
12
E
6 3
ı
AP
G KAP 140
HDG NAV APR REV
N
33
30
W
24 21
S
15
12
E
6 3
P U S H PUSH
OR
L R
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
GS GS
N
33
3 0
W
24
21 S
15
1 2
E
6
3
ı
AP
G
KAP 140
HDG NAV APR REV
N
33
30
W
24
21 S
15
12
E
6
3
P U S H PUSH
OR
N
080 °
010
°
1 2 3 4
1 2 3 4
L R
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
N
33
30
W 24
21
S
15
12
E 6
3
P U S H PUSH
OR
L R
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
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
3. The autopilot is responding to the heading select
mode with a left bank.
4. The autopilot has completed the turn and is
now established on a 010° heading.
1. The aircraft is well off the ground and estab-
lished at a desired climb rate.
The heading bug on the DG or HSI is turned to
the desired heading of 080° (runway heading).
By depressing the
HDG button on the KAP 140,
the autopilot engages into the heading mode
and maintains the selected heading of 080°.
Note: Press and hold the
AP 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.
Note: The autopilot controls only the roll axis. The PILOT must maintain control of
the pitch and yaw axis.