Honeywell KAP 140 Manual page 15

D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
Turn Coordinator
AIR
N
PUSH
Directional Gyro KI 204 or other Course
NAV HDG
N
GS GS
ı
KI 525A Pictorial
Navigation Indicator
KCS 55A Slaved
Compass System
(Optional)
KAP 140 Two Axis/Altitude Preselect System Diagram
Rev. 1
Apr/02
VOR/LOC/
RNAV/
Baro
GPS
Setting
Deviation
Glideslope
Deviation
G
KFC 140
AP HDG NAV
N
N
TO
A
V
GS
FR
OBS
ı
Deviation Indicator
(not included)
OR
KG102A
Slaved DG
Flux Detector
+
AUTO MAN
CCW CW
KA 51B
Slaving Accessory
KAP 140 AUTOPILOT SYSTEM
Encoding
Altimeter
Middle Static
Marker Pressure
ARM BARO
TRIM
UP FAIL
DN
APR REV ALT
KMT 112
WheelSteering
(optional)
Introduction
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
Trim Interrupt
Control
Autopilot
Disconnect/
Manual
Electrical Trim
7