Typical Kfc 150 Flight Control System (Diagram) - Honeywell KFC 150 Pilot's Manual

TYPICAL KFC 150 FLIGHT CONTROL SYSTEM
VOWLOC/RNAV Static
1
Deviation Pressure
KA
185
MOL-
.
..inunciator
(Optional on some aircraft).
KC 192
Computer1
Glideslope
Deviation
Pitch Altitude1
L
-
Pitch Command/
Roll
Command
KI 256 Flight
Command Indicator
K I
Navigation Indicator
KMT 112
KG 102A
Slaved DG Detector
-
r"s
L
t
E
L I
Controller1
contains
computer
functions,
mode control
buttons, and
annunciator
lights in a
single unit.
Also contains
altitude
1
1
1
Annunciator
1
I
Autopilot Disconnect/
Trim Interrupt
OR
nM.J,n
KA51B
Slaving Accessory
This is a 2-Axis (Pitch and
Roll)
System.
Third Axis Yaw Damper System
(Optional on some aircraft).
unted (May not be included
rol in all Yaw Damper
installations)
T
KC 192 Autopilot
ComputerKontroller
Annunciator
[ I '
7