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Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 124
ALL
AILERON SERVO CONTROL OPERATION - DAMPING MODE
TMUFCLI01-P02 LEVEL 3
EFFECTIVITY 27-14-00 Page 5
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 125
ALL
SELF EXAMINATION
When is the aileron servo-control actuator in
damping mode ?
A - When there is no command signal to the
servo valve.
B - Only when the solenoid valve is
de-energized.
C - When the solenoid valve is de-energized
or the actuator is not pressurized.
TMUFCLI01 LEVEL 3
EFFECTIVITY 27-14-00 Page 6
Oct 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 126
ALL
27 - FLIGHT CONTROLS
27-14-00 AILERON COMPONENTS
CONTENTS:
Aileron Servo Control
Hydraulic Filter
Servo Valve
Solenoid Valve
Mode Selector Valve Transducer
TMUFCLQ01 LEVEL 3
EFFECTIVITY 27-14-00 Page 1
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 127
ALL
AILERON COMPONENTS
AILERON SERVO CONTROL
IDENTIFICATION
FIN: 33CE1, 33CE2, 33CE3, 33CE4
LOCATION
ZONE: 575, 675
COMPONENT DESCRIPTION
If one Aileron Servo Control is inoperative it must
remain mechanically connected and hydraulically
supplied for dispatch.
HYDRAULIC FILTER
IDENTIFICATION
FIN:
LOCATION
ZONE: 575, 675
SERVO VALVE
IDENTIFICATION
FIN:
LOCATION
ZONE: 575, 675
SOLENOID VALVE
IDENTIFICATION
FIN:
LOCATION
ZONE: 575, 675
MODE SELECTOR VALVE TRANSDUCER
IDENTIFICATION
FIN:
LOCATION
ZONE: 575, 675
TMUFCLQ01-T01 LEVEL 3
EFFECTIVITY 27-14-00 Page 2
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 128
ALL
AILERON COMPONENTS - AILERON SERVO CONTROL - HYDRAULIC FILTER - SERVO VALVE -
SOLENOID VALVE - MODE SELECTOR VALVE TRANSDUCER
TMUFCLQ01-P01 LEVEL 3
EFFECTIVITY 27-14-00 Page 3
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 129
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUFCLQ01-T01 LEVEL 3
EFFECTIVITY 27-14-00 Page 4
Aug 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 130
ALL
27 - FLIGHT CONTROLS
27-64-00 SPOILER SERVO CONTROL OPERATION
CONTENTS:
Active Mode
Biased Mode
Locked Mode
Manual Mode
Self Examination
TMUFCLJ02 LEVEL 3
EFFECTIVITY 27-64-00 Page 1
Oct 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 131
ALL
SPOILER SERVO CONTROL OPERATION
ACTIVE MODE
In active mode the spoiler servo control actuator is
hydraulically supplied.
According to the command signal to the servo valve the
spoiler surface will extend or retract.
BIASED MODE
The servo-control actuator is pressurized.
Due to an electrical failure the command signal is
lost.
The biased servo valve pressurizes the retraction
chamber.
The spoiler actuator stays pressurized and the spoiler
remains retracted.
TMUFCLJ02-T01 LEVEL 3
EFFECTIVITY 27-64-00 Page 2
Oct 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 132
ALL
SPOILER SERVO CONTROL OPERATION - ACTIVE MODE - BIASED MODE
TMUFCLJ02-P01 LEVEL 3
EFFECTIVITY 27-64-00 Page 3
Oct 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 133
ALL
SPOILER SERVO CONTROL OPERATION
LOCKED MODE
In locked mode, the hydraulic pressure is lost.
The closing valve closes the retraction chamber.
The surface can only be moved towards the retracted
position, pushed by aerodynamical forces.
TMUFCLJ02-T02 LEVEL 3
EFFECTIVITY 27-64-00 Page 4
Oct 31/98
　
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