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HYDRAULIC MOTORS
IDENTIFICATION
FIN:
LOCATION
ZONE: 147, 148
COMPONENT DESCRIPTION
The Green or Yellow hydraulic motors may be inoperative
provided the Blue SLAT motor to remains operative
(refer to MMEL 27-51-01 A).
If the yellow flap motor fails and then the blue slat
motor, the flaps and slats system will operate on the
green system only.
This will involve a green low pressure and therefore
may lead to an under speed detection by SFCC 1 & 2
which will cause the system to lock.
To prevent such an event, the blue slat motor must be
operational if the aircraft is to be dispatched with
an inoperative yellow flap hydraulic motor.
TMUFCTR01-T01 LEVEL 3
EFFECTIVITY 27-54-00 Page 2
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 380
ALL
TMUFCTR01-P01 LEVEL 3
FLAPS POWER CONTROL UNIT COMPONENTS - VALVE BLOCKS - HYDRAULIC MOTORS - PRESSURE OFF
BRAKES - POSITION PICK OFF UNITS
EFFECTIVITY 27-54-00 Page 3
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 381
ALL
FLAPS POWER CONTROL UNIT COMPONENTS
PRESSURE OFF BRAKES
IDENTIFICATION
FIN:
LOCATION
ZONE: 147, 148
COMPONENT DESCRIPTION
To replace the Pressure Off Brake, the associated
hydraulic motor must be removed first.
They are identical to those installed on the slats
PCU.
POSITION PICK OFF UNITS
IDENTIFICATION
FIN: 3CN, 27CV
LOCATION
ZONE: 147, 148
COMPONENT DESCRIPTION
The IPPU and FPPU are identical to those fitted on the
slats PCU.
They are identical and interchangeable with the APPU
and can be replaced without removing the PCU from the
A/C.
TMUFCTR01-T01 LEVEL 3
EFFECTIVITY 27-54-00 Page 4
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 382
ALL
27 - FLIGHT CONTROLS
27-84-00 SLATS POWER CONTROL UNIT
COMPONENTS
CONTENTS:
PCU Valve Blocks
PCU Hydraulic Motors
Pressure Off Brakes
Instrument Position Pick Off Units / Feedback Position
Pick Off Units
TMUFCTT01 LEVEL 3
EFFECTIVITY 27-84-00 Page 1
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 383
ALL
SLATS POWER CONTROL UNIT COMPONENTS
PCU VALVE BLOCKS
IDENTIFICATION
FIN: 25CV, 26CV
LOCATION
ZONE: 147, 148
COMPONENT DESCRIPTION
Valve blocks are identical and interchangeable with
those fitted to the flap PCU.
The solenoid valves, identical and interchangeable can
be replaced without removing the valve blocks from the
PCU.
PCU HYDRAULIC MOTORS
IDENTIFICATION
FIN:
LOCATION
ZONE: 147, 148
COMPONENT DESCRIPTION
Slat and Flap Control System no2 slat channel may be
inoperative provided:
1) Slats, flaps and associated monitoring and
protection systems are fully operable on SFCS no1 and
2) Operation of SFCS 1 Wing Tip Brakes are confirmed
by test before each flight and
3) All ELACs, SECs, LGCIUs, RAs, FACs and ADIRS are
operative.
TMUFCTT01-T01 LEVEL 3
EFFECTIVITY 27-84-00 Page 2
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 384
ALL
SLATS POWER CONTROL UNIT COMPONENTS - PCU VALVE BLOCKS - PCU HYDRAULIC MOTORS
TMUFCTT01-P01 LEVEL 3
EFFECTIVITY 27-84-00 Page 3
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 385
ALL
SLATS POWER CONTROL UNIT COMPONENTS
PRESSURE OFF BRAKES
IDENTIFICATION
FIN:
LOCATION
ZONE: 147, 148
COMPONENT DESCRIPTION
To replace the POB, the associated motor must be
removed first.
Instrument Position Pick Off Units / Feedback Position
Pick Off Units
IDENTIFICATION
FIN: 4CN, 28CV
LOCATION
ZONE: 147, 148
COMPONENT DESCRIPTION
The IPPU and FPPU are identical and interchangeable
with the APPU and can be replaced without removing the
PCU.
They are identical to those fitted on the flap PCU.
TMUFCTT01-T02 LEVEL 3
EFFECTIVITY 27-84-00 Page 4
Mar 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
　
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