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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 134
ALL
SPOILER SERVO CONTROL OPERATION - LOCKED MODE
TMUFCLJ02-P02 LEVEL 3
EFFECTIVITY 27-64-00 Page 5
Oct 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 135
ALL
SPOILER SERVO CONTROL OPERATION
MANUAL MODE
To be unlocked, the servo control actuator must be
depressurized.
The maintenance unlocking device can be engaged thanks
to a key equipped with a red flame. This tool can not
be removed when the servo control is in maintenance
mode.
Once the maintenance unlocking device is engaged the
spoiler surface can be raised manually for inspection
purposes.
TMUFCLJ02-T03 LEVEL 3
EFFECTIVITY 27-64-00 Page 6
Oct 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 136
ALL
SPOILER SERVO CONTROL OPERATION - MANUAL MODE
TMUFCLJ02-P03 LEVEL 3
EFFECTIVITY 27-64-00 Page 7
Oct 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 137
ALL
SELF EXAMINATION
Following a hydraulic system failure in flight,
what does each spoiler do ?
A - It is retracted by the biased
servo-valve.
B - It is retracted by aerodynamical forces
and locked.
C - It is locked and stops in its actual
position.
How can a spoiler be raised on ground ?
A - By de pressurizing the hydraulic system
and using the maintenance unlocking
device.
B - By pressing the SEC p/b on the flight
control panel.
C - By using the maintenance unlocking
device with the actuator pressurized and
SEC p/b operated
TMUFCLJ02 LEVEL 3
EFFECTIVITY 27-64-00 Page 8
Oct 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 138
ALL
27 - FLIGHT CONTROLS
27-60-00 SPOILER COMPONENTS
CONTENTS:
Spoiler Servo Control
Spoiler Servo Control Filter
Spoiler Servo Control Servo Valve
TMUFCLT02 LEVEL 3
EFFECTIVITY 27-60-00 Page 1
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 139
ALL
SPOILER COMPONENTS
SPOILER SERVO CONTROL
IDENTIFICATION
FIN: 31CE1, 31CE2, 31CE3, 31CE4, 31CE5, 31CE6, 31CE7,
31CE8, 31CE9, 31CE10.
LOCATION
ZONE: 574, 674, 583, 683, 584, 684, 585, 685.
SPOILER SERVO CONTROL FILTER
IDENTIFICATION
FIN:
LOCATION
ZONE: 574, 674, 583, 683, 584, 684, 585, 685.
SPOILER SERVO CONTROL SERVO VALVE
IDENTIFICATION
FIN:
LOCATION
ZONE: 574, 674, 583, 683, 584, 684, 585, 685.
TMUFCLT02-T01 LEVEL 3
EFFECTIVITY 27-60-00 Page 2
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 140
ALL
SPOILER COMPONENTS - SPOILER SERVO CONTROL - SPOILER SERVO CONTROL FILTER - SPOILER SERVO
CONTROL SERVO VALVE
TMUFCLT02-P01 LEVEL 3
EFFECTIVITY 27-60-00 Page 3
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 141
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUFCLT02 LEVEL 3
EFFECTIVITY 27-60-00 Page 4
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 142
ALL
27 - FLIGHT CONTROLS
27-22-00 RUDDER TRIM ACTUATOR (D/O)
CONTENTS:
General
Controls
Description/Operation
Self examination
TMUFCAK01 LEVEL 3
EFFECTIVITY 27-22-00 Page 1
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 143
ALL
RUDDER TRIM ACTUATOR (D/O)
GENERAL
The rudder trim actuator is installed on the rudder
system, in the tail area and is one of the mechanical
inputs of the rudder servocontrols.
The rudder trim actuator enables the zero force
position of the artificial feel and trim unit to be
adjusted.
CONTROLS
The rudder trim actuator is an electromechanical unit
　
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