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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
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TMUFCTT01-P02 LEVEL 3
SLATS POWER CONTROL UNIT COMPONENTS - PRESSURE OFF BRAKES - POSITION PICK OFF UNITS
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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TMUFCTT01 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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27 - FLIGHT CONTROLS
27-00-00 SLATS/FLAPS WARNINGS
CONTENTS:
Slats/Flaps Fault
Slats/Flaps Locked
TMUFC1701 LEVEL 3
EFFECTIVITY 27-00-00 Page 1
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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SLATS/FLAPS WARNINGS
SLATS/FLAPS FAULT
The present configuration is position 2 in flight.
In case of slat or flap fault, the MASTER CAUTION comes
on, an aural warning sounds and the word FLAP becomes
amber.
The failure is displayed on the ECAM page.
In this example, the selected flap position has not
been reached, the position number and the triangle
remain cyan and the green line turns to amber.
TMUFC1701-T01 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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SLATS/FLAPS WARNINGS - SLATS/FLAPS FAULT
TMUFC1701-P01 LEVEL 3
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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SLATS/FLAPS WARNINGS
SLATS/FLAPS LOCKED
The present configuration is 3 position.
In case of locked slat or flap, the MASTER CAUTION
comes on, an aural warning sounds and the word FLAP
becomes amber.
The failure is displayed on the ECAM page.
In this example, the selected slat position has not
been reached, the position number and the triangle
remain cyan and the green line turns to amber.
TMUFC1701-T02 LEVEL 3
EFFECTIVITY 27-00-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 392
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SLATS/FLAPS WARNINGS - SLATS/FLAPS LOCKED
TMUFC1701-P02 LEVEL 3
EFFECTIVITY 27-00-00 Page 5
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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TMUFC1701 LEVEL 3
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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27 - FLIGHT CONTROLS
27-00-00 SLAT FLAP CONTROL COMPUTER
CONTROL INTERFACES
CONTENTS:
Command Sensor Unit (CSU)
LH and RH Asymmetry Position Pick off Units (APPUs)
Feedback Position Pick off Units (FPPU)
LH and RH Wing Tip Brakes
Power Control Unit (PCU)
Air Data/Inertial Reference Units (ADIRUs)
Landing Gear and Control Interface Units 1 and 2
(LGCIU1 and 2)
Centralized Fault and Display Interface Unit (CFDIU)
TMUFCTF02 LEVEL 3
EFFECTIVITY 27-00-00 Page 1
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MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 395
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SLAT FLAP CONTROL COMPUTER CONTROL INTERFACES
COMMAND SENSOR UNIT (CSU)
The Command Sensor Unit sends two discrete signals to
each channel for a new Slat/Flap position demand.
LH and RH ASYMMETRY Position Pick off Units (APPUs)
The Asymmetry Position Pick Off Units send synchro
signals to each channel for asymmetry detection and
system monitoring.
FEEDBACK Position Pick off Units (FPPU)
The position of the Power Control Unit output shaft
is measured by the Feedback Position Pick Off Unit and
sent to the computers for system control and
monitoring.
WING TIP BRAKES (WTB)
Discrete outputs from the computers are sent to the
Wing Tip Brakes for solenoid valve control.
POWER CONTROL UNIT (PCU)
Discrete outputs from the computers are transmitted
to the Power Control Unit for solenoid valve control.
　
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