BendixKing KAP 140 - Manual (Page 65)

KAP 140 AUTOPILOT SYSTEM
Two Axis Operation Two Axis Operation
76 77 KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02 Rev. 1
Apr/02
3. At the desired point, heading mode is used to
initiate the procedure turn. During the procedure
turn outbound, the deviation bar shows that the
aircraft is flying away from the GPS course at a
45° angle on a selected heading of 283°.
4. The heading bug has been set to 103° and the
aircraft has made a left turn to this heading.
The GPS’s Leg/OBS mode switching is set to
Leg mode and the course pointer is set to
058°. Select approach mode by depressing the
APR button.
1. The aircraft is in APR mode approaching the
IAF. Approach arm is indicated on the GPS
annunciator.*
2. Upon waypoint alerting at the IAF, the course
pointer is set to 238°, the GPS’s Leg/OBS mode
switching is set to OBS mode. The autopilot ini-
tiates a left turn to track the 238° GPS course.
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
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
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
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
1 2
3
4
058
°
270 °
238
°
283°
103°
Outbound on GPS Approach Using HSI
* Description of GPS operation based on Bendix/King GPS receiver. Others may
require different operation.