Honeywell KAP 140 Pilot's Manual page 14

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Introduction
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)
6
VOR/LOC/RNAV/
GPS Deviation
Glideslope
Deviation
G
KAP 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 Two Axis System Diagram
KAP 140 AUTOPILOT SYSTEM
Static
Pressure
Middle
Marker
TRIM
FAIL
DN
UP
APR
REV
ALT
KMT 112
Control
WheelSteering
(optional)
KC 140 Two Axis
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
Autopilot
Disconnect/
Trim Interrupt
Manual
Electrical Trim
Rev. 1
Apr/02

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