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IDENTIFICATION
FIN: 25CE1, 25CE2
LOCATION
ZONE: 121, 122
COMPONENT DESCRIPTION
The transducer units (RVDTs) send Rudder pedal
positions to the EFCS.
Left and right units are not interchangeable.
TMUFCLW01-T02 LEVEL 3
EFFECTIVITY 27-20-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
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RUDDER CHANNEL COMPONENTS (FWD) - RUDDER PEDAL POSITION TRANSMITTER
TMUFCLW01-P02 LEVEL 3
EFFECTIVITY 27-20-00 Page 5
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 175
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RUDDER CHANNEL COMPONENTS (FWD)
CABLE TENSION REGULATOR
IDENTIFICATION
FIN: 103CM
LOCATION
ZONE: 125
COMPONENT DESCRIPTION
The tension regulator maintains a constant tension on
the cable. This absorbs relative variations in length
due to thermal expansion, cabin pressurization and
structural deformations.
TMUFCLW01-T03 LEVEL 3
EFFECTIVITY 27-20-00 Page 6
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 176
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RUDDER CHANNEL COMPONENTS (FWD) - CABLE TENSION REGULATOR
TMUFCLW01-P03 LEVEL 3
EFFECTIVITY 27-20-00 Page 7
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 177
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RUDDER CHANNEL COMPONENTS (FWD)
RUDDER TRIM CONTROL SWITCH
IDENTIFICATION
FIN: 9CC
LOCATION
ZONE: 211
PANEL: 110VU
COMPONENT DESCRIPTION
This is a 3 position rotary switch spring loaded to
the neutral (center) position.
The direction of rudder trim travel depends on the
direction of the switch rotation (Left or Right), the
rudder trim value is indicated on the digital
indicator.
The reset p/b switch permits the rudder trim to be
reset to zero.
TMUFCLW01-T04 LEVEL 3
EFFECTIVITY 27-20-00 Page 8
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
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RUDDER CHANNEL COMPONENTS (FWD) - RUDDER TRIM CONTROL SWITCH
TMUFCLW01-P04 LEVEL 3
EFFECTIVITY 27-20-00 Page 9
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUFCLW01 LEVEL 3
EFFECTIVITY 27-20-00 Page 10
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 180
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27 - FLIGHT CONTROLS
27-20-00 RUDDER CHANNEL COMPONENTS (AFT)
CONTENTS:
Rudder Trim Actuator
Rudder Artificial Feel and Trim Unit and A/P Solenoid
Rudder Travel Limitation Unit
Rudder Servocontrol
Yaw Damper Servo-Actuator
Transducer Units
Centering Spring Rods
TMUFCLX01 LEVEL 3
EFFECTIVITY 27-20-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 181
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RUDDER CHANNEL COMPONENTS (AFT)
RUDDER TRIM ACTUATOR
IDENTIFICATION
FIN: 10CC
LOCATION
ZONE: 325
COMPONENT DESCRIPTION
The rudder trim actuator has two independant DC motors
(electronic assembly) coupled to a reduction gear
driving the output shaft via a torque limiter.
The output shaft drives 4 RVDTs.
An externally visible index shows the zero position
of the output shaft.
The electronic module is an LRU.
The output shaft includes a rigging point to get the
neutral position.
TMUFCLX01-T01 LEVEL 3
EFFECTIVITY 27-20-00 Page 2
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 182
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RUDDER CHANNEL COMPONENTS (AFT) - RUDDER TRIM ACTUATOR
TMUFCLX01-P01 LEVEL 3
EFFECTIVITY 27-20-00 Page 3
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 183
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RUDDER CHANNEL COMPONENTS (AFT)
RUDDER ARTIFICIAL FEEL AND TRIM UNIT
LOCATION
ZONE: 325
COMPONENT DESCRIPTION
The artificial feel is engaged in Auto-Pilot mode. It
　
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