Owner's manual

KAP 140 AUTOPILOT SYSTEM
Introduction
7
Rev. 1
Apr/02
LR
2 MIN.
TURN COORDINATOR
NO PITCH
INFORMATION
D.C. ELEC.
N
33
30
W
24
21
S
15
12
E
6
3
PUSH
P
U
S
H
AIR
N
S
E
W
TO
FR
33
30
24
21
15
12
6
3
OBS
GS
N
A
V
ı
N
GS GS
3
3
3
0
W
2
4
2
1
S
1
5
1
2
E
6
3
ı
NAV HDG
ı
K
C
S
3
0
5
MAN
CW
AUTO
CCW
-
+
Turn Coordinator
Directional Gyro KI 204 or other Course
Deviation Indicator
(not included)
KC 140 Two Axis with
Altitude Preselect
Computer/Controller/
Annunciator
contains computer
functions, mode
control buttons,
and annunciations
in a single unit. Also
contains static pressure
sensor and accelerometer.
KS 271C Roll Servo
KS 270C Pitch Servo
KS 272C Pitch Trim Servo
KI 525A Pictorial
Navigation Indicator
KCS 55A Slaved
Compass System
(Optional)
KG102A
Slaved DG
KMT 112
Flux Detector
OR
KA 51B
Slaving Accessory
Manual
Electrical Trim
Autopilot
Disconnect/
Trim Interrupt
Control
WheelSteering
(optional)
AP
G
KFC 140
HDG NAV APR REV
ALT
ARM BARO
DN
UP
TRIM
FAIL
Glideslope
Deviation
VOR/LOC/
RNAV/
GPS
Deviation
Middle
Marker
Static
Pressure
Baro
Setting
Encoding
Altimeter
KAP 140 Two Axis/Altitude Preselect System Diagram