Typical Kap 150 Autopilot System (Diagram) - Honeywell KFC 150 Pilot's Manual

TYPICAL KAP 150 AUTOPILOT SYSTEM
VOR/LOC/RNAV Static
Deviation Pressure
KC
191
Computer/
Glideslope Middle
Devi?ion Marker Controller/
Annunciator
contains
computer
functions, mode
control buttons,
and annunciator
lights in a
single unit.
Also contains
altitude
sensor.
Pitch Attitude/
KG
238
Attituae
Reference Indicator
I I I I
1 1 1 1
Heading Select
&
Course Datum
I
KG107 KI 204 or other Course
I
I
Directional Gyro Deviation Indicator
I
I
(not included).
I I
I -
I
I
I
I
I
/
I
[rim Interrupt
t
KMT 112
I
I - Y
d
I
I
Flux
I
KI 525A Pictorial
I
Navigation Indicator
I
I
I
I
KCS 55A Slaved
m
I
n R
AI
I
slaving
ACC~S!
. . . . . . . . . . . . . . . . . . . . . . . .
This is a 2-Axis (Pitch and Roll) System.
Third Axis Yaw Damper System
(Optional on some aircraft).
I
5 L 1 "
n o r r f r
Panel-Mounted (May not be included
Switch installations)
YD Annunciator
18
Yaw Control in all Yaw Damper
T
I
KC
I J I M U l U ~ l l U l
ComputedController
Annunciator
r"
Roll
Crossfeed
Yaw Servo
KRG 331
Rate Gyro Yaw Computer
L