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STOW/RESET selector switch.
Indication lights are checked by using the LAMP test
pushbutton. The indication lights come on during the
RAT retraction.
The RAT control panel is protected by means of a cover
provided with a window so that the indication lights
can be seen with the cover in the closed position.
TMUHYDJ02-T15 LEVEL 3
EFFECTIVITY 29-12-00 Page 30
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 148
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BLUE SYSTEM COMPONENTS
TMUHYDJ02-P15 LEVEL 3
EFFECTIVITY 29-12-00 Page 31
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
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UF94200
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUHYDJ02 LEVEL 3
EFFECTIVITY 29-12-00 Page 32
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 150
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29 - HYDRAULIC POWER
29-13-00 YELLOW SYSTEM COMPONENTS
CONTENTS:
Leakage Measurement Manifold
High Pressure Manifold
Electric Pump Protection
Electric Pump
Engine Driven Pump 2
EDP 2 Case Drain Filter
EDP 2 Pressure Switch
Engine Fire Valve
Reservoir
Return Manifold
Ground Service Panel
TMUHYDK03 LEVEL 3
EFFECTIVITY 29-13-00 Page 1
Jul 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 151
ALL
YELLOW SYSTEM COMPONENTS
SAFETY PRECAUTIONS
WARNING: When using the manual depressurization valve
put on hand and eye protection and keep away
from the outlet of the valve. The air can be
hot and contain particles of dust and/or
hydraulic fluid.
LEAKAGE MEASUREMENT MANIFOLD
IDENTIFICATION
FIN : 3146 GM
LOCATION
ZONE : 196
DESCRIPTION
The ground leakage measurement manifolds of the three
hydraulic systems are identical.The manifold has two
pairs of inlet ports, identified as A and B. As only
one pair is used, the other one is sealed.The three
outlet ports are identified as C, D and E.The 2-way
spool valves are manually opened for ground maintenance
tasks only.
TMUHYDK03-T01 LEVEL 3
EFFECTIVITY 29-13-00 Page 2
Jul 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 152
ALL
YELLOW SYSTEM COMPONENTS - LEAKAGE MEASUREMENT MANIFOLD
TMUHYDK03-P01 LEVEL 3
EFFECTIVITY 29-13-00 Page 3
Jul 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 153
ALL
YELLOW SYSTEM COMPONENTS
HIGH PRESSURE MANIFOLD
IDENTIFICATION
FIN: 3011GM
LOCATION
ZONE: 196
DESCRIPTION
The HP manifold has ports which connect it to the other
parts:
- a system pressure inlet from pumps and ground
supply
- Two outlets to the Leak Measurement System
Manifold
- One outlet and one inlet to the PTU manifold
- One connection to the accumulator/cargo doors
selector valve/brake manifold
FILTER
IDENTIFICATION
FIN: 3048GM
LOCATION
ZONE: 196
DESCRIPTION
The filter element is of the replaceable type. It
cannot be cleaned.
The filter also includes a clogging indicator which
has to be reset manually after replacement of the
filter element.
An anti-spill device is also included in the filter
in order to prevent any hydraulic fluid flow when the
filter element and the bowl are removed.
The HP filter has a filtration rating of 15 microns.
TMUHYDK03-T02 LEVEL 3
EFFECTIVITY 29-13-00 Page 4
Jul 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 154
ALL
YELLOW SYSTEM COMPONENTS - HP MANIFOLD
TMUHYDK03-P02 LEVEL 3
EFFECTIVITY 29-13-00 Page 5
Jul 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 155
ALL
YELLOW SYSTEM COMPONENTS
PRESSURE TRANSDUCER
IDENTIFICATION
FIN: 3065GN
LOCATION
ZONE: 196
DESCRIPTION
The pressure transducer measures the system pressure
and sends signals to the SDAC for ECAM display and to
ELAC 1/2 for Flight Control System.
　
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