KLM MD-11 - Directional Control System

MD-11 Flight Crew Operations Manual
k
Flight Controls -
Functional Schematic
Flt.50.2
Directional Control System
DB1-2-1731
11 15
SLAT DISAG
180 185
98 123 16 5 159 160
179
99
10
CONFIGURATION
9
159
140 141
148 143
99 120
167 150
150 155
148 153
1-2-3
RUDDER
MECHANICAL
CONTROL &
TRIM
ADJUSTMENT
OVERRIDE &
LOAD FEEL
MECHANISM
FLIGHT
CONTROL
COMPUTER-2
HYD
SYS 1
1-2-3
LOWER RUDDER
OVERRIDE &
LOAD FEEL
MECHANISM
REVERSIBLE
MOTOR PUMP
FLOW
CONT ROL
PRESSURE
OPERATED
SHUT OFF VALVE
HYD
HORIZONTAL
STABILIZER
CONTROL
VALVE
UPPER
RUDDER
LOWER
RUDDER
HYD
SYS 3
A/P & YAW DAMP
POSITION
COMPENSATOR
A
C
T
U
A
T
O
R
HYD SYS 2
FLIGHT
CONTROL
COMPUTER-1
A
C
T
U
A
T
O
R
POSITION
A/P & YAW DAMP
UPPER RUDDER
2-1 NON-
REVERSIBLE
MOTOR PUMP
FLOW
CONT ROL
PRESSURE
OPERATED
HYD
HYD
COMPENSATOR
HYD SYS 2
SYS 2
FROM 2-1 NRMP
3-2 NON-
SYS 2
SYS 1
SHUT OFF VALVE
SYSTEM DISPLAY
DEU
DEU
RUDDER
PEDALS
RUDDER TRIM
KNOB
October 02, 2006