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consists of a trim screwjack and a constant-resisting
load spring-rod that the trim screwjack holds in the
neutral position.
It comprises a system which can override the Auto-Pilot
mode.
AUTO PILOT SOLENOID
IDENTIFICATION
FIN: 16CA
LOCATION
ZONE: 325
COMPONENT DESCRIPTION
This solenoid is controlled by the autopilot to stiffen
the pedals.
TMUFCLX01-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 (AFT)- ARTIFICIAL FEEL AND TRIM UNIT AND A/P SOLENOID
TMUFCLX01-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
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RUDDER CHANNEL COMPONENTS (AFT)
RUDDER TRAVEL LIMITATION UNIT
IDENTIFICATION
FIN: 4CC
LOCATION
ZONE: 325
COMPONENT DESCRIPTION
The travel limitation unit comprises 2 brushless
electric motors separately controlled by an electronic
assembly. Each motor drives a mechanical device linked
to the input levers. Movement is transmitted to 2 RVDTs
and indicate the position of the variable stop.
Two rigging pins are used to set the two levers to the
zero position.
TMUFCLX01-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
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RUDDER CHANNEL COMPONENTS (AFT) - RUDDER TRAVEL LIMITATION UNIT
TMUFCLX01-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 187
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RUDDER CHANNEL COMPONENTS (AFT)
RUDDER SERVOCONTROL
IDENTIFICATION
FIN: 1025GM, 2025GM, 3025GM
LOCATION
ZONE: 325
COMPONENT DESCRIPTION
The rudder is actuated by three identical moving body
servocontrols (interchangeable) which operate
simultaneously.
Each servocontrol is powered by a different hydraulic
system.
TMUFCLX01-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
EFFECTIVITY Page 188
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RUDDER CHANNEL COMPONENTS (AFT) - RUDDER SERVOCONTROL
TMUFCLX01-P04 LEVEL 3
EFFECTIVITY 27-20-00 Page 9
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 189
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RUDDER CHANNEL COMPONENTS (AFT)
YAW DAMPER SERVO-ACTUATOR
IDENTIFICATION
FIN: 3CC1, 3CC2.
LOCATION
ZONE: 325
COMPONENT DESCRIPTION
The two electro-hydraulic servo-actuators are
interchangeable.
The following components are LRUs:
- filter
- solenoid valves
- servovalve
- pressure switch.
No rigging operation is necessary to replace the yaw
damper.
TMUFCLX01-T05 LEVEL 3
EFFECTIVITY 27-20-00 Page 10
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 190
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RUDDER CHANNEL COMPONENTS (AFT) - YAW DAMPER SERVO-ACTUATOR
TMUFCLX01-P05 LEVEL 3
EFFECTIVITY 27-20-00 Page 11
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 191
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RUDDER CHANNEL COMPONENTS (AFT)
TRANSDUCER UNITS
IDENTIFICATION
FIN: 42WV Rudder
2CC Yaw Damper
LOCATION
ZONE: 325
COMPONENT DESCRIPTION
The rudder transducer unit and the yaw damper
transducer unit consist of a casing in which are
installed two RVDTs (energized by 26V 400Hz) driven
by an input lever.
The rudder transducer unit transmits rudder position
information to the EFCS. The other transducer unit
transmits yaw damper position monitoring to the FACs.
TMUFCLX01-T06 LEVEL 3
EFFECTIVITY 27-20-00 Page 12
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 192
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RUDDER CHANNEL COMPONENTS (AFT) - RUDDER AND YAW DAMPER TRANSDUCER UNITS
TMUFCLX01-P06 LEVEL 3
EFFECTIVITY 27-20-00 Page 13
　
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