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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 211
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EFCS CONTROL INTERFACE
PILOT ORDERS
The pilot orders like side stick, speed brake, ground
spoiler or throttle position signals, are transmitted
to the ELACs and SECs.
According to these inputs and their control laws, the
computers calculate the elevator, aileron, spoiler,
THS and rudder deflection.
TMUFCLG02-T01 LEVEL 3
EFFECTIVITY 27-90-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 212
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EFCS CONTROL INTERFACE - PILOT ORDERS
TMUFCLG02-P01 LEVEL 3
EFFECTIVITY 27-90-00 Page 3
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 213
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EFCS CONTROL INTERFACE
FLIGHT CONTROL PANELS
Push buttons located on the overhead panels (23VU and
24VU) are used to engage/disengage or reset their
respective computer’s software.
TMUFCLG02-T02 LEVEL 3
EFFECTIVITY 27-90-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
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EFCS CONTROL INTERFACE - FLIGHT CONTROL PANELS
TMUFCLG02-P02 LEVEL 3
EFFECTIVITY 27-90-00 Page 5
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 215
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EFCS CONTROL INTERFACE
HYDRAULIC PRESSURE
The hydraulic pressure status is sent to the ELACs and
SECs for activation or deactivation of the related
servo controls and laws.
TMUFCLG02-T03 LEVEL 3
EFFECTIVITY 27-90-00 Page 6
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
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TMUFCLG02-P03 LEVEL 3
EFCS CONTROL INTERFACE - HYDRAULIC PRESSURE
EFFECTIVITY 27-90-00 Page 7
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 217
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EFCS CONTROL INTERFACE
RUDDER PEDAL POSITION
The rudder pedal position is sent to the ELACs for
turn coordination computation, which is then performed
through the FACs.
TMUFCLG02-T04 LEVEL 3
EFFECTIVITY 27-90-00 Page 8
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 218
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EFCS CONTROL INTERFACE - RUDDER PEDAL POSITION
TMUFCLG02-P04 LEVEL 3
EFFECTIVITY 27-90-00 Page 9
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 219
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EFCS CONTROL INTERFACE
FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC)
If the auto pilot is active, pitch, roll and yaw orders
computed by the FMGC are sent to the ELACs and FACs,
which control and monitor the surface deflections.
TMUFCLG02-T05 LEVEL 3
EFFECTIVITY 27-90-00 Page 10
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 220
ALL
EFCS CONTROL INTERFACE - FMGC
TMUFCLG02-P05 LEVEL 3
EFFECTIVITY 27-90-00 Page 11
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 221
ALL
EFCS CONTROL INTERFACE
FLIGHT AUGMENTATION COMPUTER (FAC)
The FACs receive rudder deflection information
computed either by the ELACs or FMGCs for dutch roll
damping, engine failure compensation and turn
coordination.
TMUFCLG02-T06 LEVEL 3
EFFECTIVITY 27-90-00 Page 12
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 222
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EFCS CONTROL INTERFACE - FAC
TMUFCLG02-P06 LEVEL 3
EFFECTIVITY 27-90-00 Page 13
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 223
ALL
EFCS CONTROL INTERFACE
AIR DATA INERTIAL REFERENCE SYSTEM (ADIRS)
The ADIRS transmits air data and inertial reference
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