BendixKing KAP 140 - Manual (Page 58)

KAP 140 AUTOPILOT SYSTEM
Two Axis Operation Two Axis Operation
62 63 KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02 Rev. 1
Apr/02
3. When the computed capture point is reached,
the ROL annunciation changes to NAV and a
right turn is initiated by the autopilot.
4. The turn is complete and the autopilot is track-
ing the GPS course.
L R
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
L R
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
N
1
2
3
4
40
°
010
°
1. Continuing on heading 010°, a GPS waypoint is
established. A 30° intercept is desired.
2. The HDG button is depressed to select ROL
mode which will allow an “all angle intercept”.
GPS data is selected for the CDI and the OBS is
set to 040°. The
NAV button is depressed and
NAV ARM is annunciated. ROL will change to
HDG and flash for five seconds. ROL will then
be redisplayed. While the HDG 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
L R
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
L R
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
* Description of GPS operation based on Bendix/King GPS receiver. Others may
require different operation.