Owner's manual

N
1
2
3
4
270°
058°
238°
2
8
3
°
103
°
KAP 140 AUTOPILOT SYSTEM
Two Axis Operation Two Axis Operation
68 69
KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02
Rev. 1
Apr/02
3. At the desired point, mode is used to initi-
ate the procedure turn. Select and set the
heading bug to 283°. During the procedure turn
outbound, the deviation bar shows that the air-
craft is flying away from the localizer centerline
at a 45° angle on a selected heading of 283°.
4. Now you have reset the heading bug to 103°
and made a 180° turn to this heading. The
103° heading will intercept the front course of
058°. You must now select the approach mode
by depressing the button on the KAP 140.
Automatic capture of the localizer will occur.
1. The aircraft is heading 270° with heading and
altitude hold engaged. To intercept and fly the
ILS front course outbound, set the front course
on the HSI and depress the back course ( )
button. The back course ( ) mode is
selected to go outbound on the front course.
The capture point is now being computed
based on closure rate.
2. When the computed capture point is reached,
mode is cancelled and reverse localizer
mode is automatically activated and a left turn
outbound on the localizer is initiated by the
autopilot.
.
Outbound On Front Course For Procedure Turn To ILS Approach Using HSI
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
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
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
GS GS
N
33
3
0
W
24
2
1
S
15
1
2
E
6
3
ı
AP
G
KAP 140
HDG NAV APR REV
ALT
DN
UP
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