BendixKing KAP 140 - Manual (Page 76)

KAP 140 AUTOPILOT SYSTEM
Two Axis/Altitude Preselect Operations Two Axis/Altitude Preselect Operations
90 91 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 ALT DN
UP
N
33
30
W
24 21
S
15
12
E
6 3
P U S H PUSH
OR
ARM BARO
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 ALT DN
UP
N
33
30
W
24
21 S
15
12
E
6
3
P U S H PUSH
OR
ARM BARO
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 ALT DN
UP
N
33
30
W 24
21
S
15
12
E 6
3
P U S H PUSH
OR
ARM BARO
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 ALT DN
UP
N
33
30
W 24
21
S
15
12
E 6
3
P U S H PUSH
OR
ARM BARO
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. The climb rate has been
decreased, using the
DN button, in preparation
for level out. The vertical speed value will be
displayed upon selection of the
DN button and
will remain for three seconds.
4. Desired altitude has been reached and auto-
matic altitude capture occurs. 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 safe 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 and ver-
tical speed modes and maintains the selected
heading of 080° and current rate of climb.
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. A
cruise altitude of 7,000 feet is entered using the
rotary knobs. Altitude
ARM annunciation occurs
automatically upon selection.