Owner's manual
KAP 140 AUTOPILOT SYSTEM
Two Axis/Altitude Preselect Operations Two Axis/Altitude Preselect Operations
110 111
KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02
Rev. 1
Apr/02
N
1
2
3
4
0
5
8
°
090°
2
3
8
°
FAF
3. At the MDA, the 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. The flashing annunciations are dis-
played 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 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 button for 0.25
seconds to engage the autopilot (applicable
only to software version 03/01 and later).
1. Continuing the maneuver on page 106,
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, is depressed to activate vertical
speed mode. The desired descent rate is
obtained using the button.
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
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
ARM BARO
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
ARM BARO
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
ARM BARO
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
ARM BARO