Front course ils approach using dg, Two axis operation, Two axis operation 70 71 – BendixKing KAP 140 User Manual
Page 62: Kap 140 autopilot system
N
1
2
3
4
058
°
090
°
238
°
3. At the middle marker, the pilot disengages the
autopilot with the button on the control wheel.
This cancels all operating modes. The flashing
AP annunciationa are displayed and a discon-
nect 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 66, APR cou-
pling occurs (
HDG annunciation changes to
APR), and the glideslope mode is automatically
armed. The autopilot will capture the localizer
and the CDI course index will center.
2. The autopilot is following the localizer. At the
outer marker, the glideslope deviation needle is
at midscale. Altitude hold is automatically disen-
gaged when the glideslope is captured. The
ALT
annunciator extinguishes and
GS is displayed.
The autopilot will make pitch and bank changes
as necessary to maintain localizer and glides-
lope.
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
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
KAP 140 AUTOPILOT SYSTEM
Two Axis Operation
Two Axis Operation
70
71
KAP 140 AUTOPILOT SYSTEM
Rev. 1
Apr/02
Rev. 1
Apr/02
1
2
3
4
Front Course ILS Approach Using DG