BendixKing KAP 140 - Manual (Page 67)

KAP 140 AUTOPILOT SYSTEM
Two Axis Operation Two Axis Operation
80 81 KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02 Rev. 1
Apr/02
N
1
2
3
4
05
8°
090 °
23
8°
FAF
3. At the MDA, the ALT button is depressed caus-
ing the autopilot to level off and maintain a con-
stant altitude. At the MAP the pilot disengages
the autopilot with the button on the control
wheel. A flashing
AP annunciation is displayed
and a distinctive tone will sound.
4. The pilot initiates the missed approach and sta-
bilizes the aircraft in the climb. The heading
bug is set to the missed approach heading of
090°. By depressing the
HDG button on the
KAP 140, the autopilot engages into the head-
ing and vertical speed modes, commencing a
right turn to a heading of 090° and maintaining
the rate of climb existing at engagement.
Note: Press and hold the
AP button for 0.25
seconds to engage the autopilot (applicable
only to software version 03/01 and later).
1. Continuing the maneuver on page 76, APR
mode capture occurs. The autopilot initiates a
left turn to track the 058° GPS course.
* Approach active is indicated on the GPS
annunciator.
2. At the FAF, ALT is depressed to activate vertical
speed mode. The desired descent rate is
obtained using the
DN button.
Remember, speed needs to be controlled with
the throttle.
Inbound on GPS Approach Using HSI
* Description of GPS operation based on Bendix/King GPS receiver. Others may
require different operation.
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
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