Typical Kap 100 Autopilot System (Diagram) - Honeywell KFC 150 Pilot's Manual

TYPICAL KAP 100 AUTOPILOT SYSTEM
KA
185
Mode Annunciator
(Optional on some aircraft).
KG
258
Attitude
Reference Indicator
Middle VOWLOC/RNAV
KC 190
Computer/
Controller/
Annunciator
I
Roll Attitude
Heading Select
&
Course Datum
I
I
I
I
I
I
I
I
I
I
I
I
I
KG 107 KI
204
or other Course
I
Directional Gyro Deviation Indicator
I
(not included).
I
. . . . . . . . . . . . . . . . . . . . .
OR
. . . . . . . . . . . . . . . . . . . . . . .
-
KG 102A
I
1
+
L ,
Slaved DG
I
I
I
I
I I
- 1
KMT112
I
I
Navigation Indicator
-
Detector
I
7
4
I
KI 3.cm
ricioriai Flux
I
I
I
I R
( 7 )
I
I
KCS 55A Slaved
I
I
Compass System
I
(Optional)
KA
51A
a - 5 1 B
I
I
I
Slaving Accessory
I
contains
computer
functions, mode
control buttons,
and annunciator
lights in a
single unit.
-D
KS 179
Pitch Trim
Servo
Autopilot Disconnecff
This is a Single-Axis (Roll) System.
Manual Electric
I
Trim (Optional)
Control Wheel
Steering (Optional)
9