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sections welded together. The top of the reservoir has
a manifold for the components of the air pressurization
system. The reservoir is divided into two parts. The
lower part is always full. A transfer tube enables
hydraulic fluid exchange with the upper part which
constitutes the fluid reserve.
TMUHYDI03-T09 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
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TMUHYDI03-P09 LEVEL 3
GREEN SYSTEM COMPONENTS - RESERVOIR
EFFECTIVITY 29-11-00 Page 19
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 105
ALL
GREEN SYSTEM COMPONENTS
DRAIN VALVE
IDENTIFICATION
FIN: 1264GM
LOCATION
ZONE: 148
DESCRIPTION
A hollow type drain valve is installed at the bottom
of the reservoir. The valve is opened by turning
(counter-clockwise) and pushing the bushing/valve pin
assembly. Then the bushing is rotated clockwise to
lock the valve in the open position.
LOW LEVEL SWITCH
IDENTIFICATION
FIN: 1062GQ
LOCATION
ZONE: 148
DESCRIPTION
The low level switch is a float operated switch which
includes a relay and a magnet which keeps the contacts
open when the float is high. A metal shroud around the
float operates as a damper for small changes in the
fluid level.
TMUHYDI03-T10 LEVEL 3
EFFECTIVITY 29-11-00 Page 20
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 106
ALL
GREEN SYSTEM COMPONENTS - RESERVOIR COMPONENTS
TMUHYDI03-P10 LEVEL 3
EFFECTIVITY 29-11-00 Page 21
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 107
ALL
GREEN SYSTEM COMPONENTS
AIR PRESSURE GAGE
IDENTIFICATION
FIN: 1383GM
LOCATION
ZONE: 148
DESCRIPTION
The reservoir pressure gage displays the air pressure
in a range of 0-75 psi (0-5 bar).
AIR PRESSURE SWITCH
IDENTIFICATION
FIN: 1384GH
LOCATION
ZONE: 148
DESCRIPTION
The air pressure switch closes when the pressure
decreases to 22 ± 1.5 psi (1.5 ± 0.1 bar).The contacts
open when the pressure increases to 25 psi (1.7 bar).
AIR RELIEF VALVE
IDENTIFICATION
FIN: 1005GM
LOCATION
ZONE: 148
DESCRIPTION
The air relief valve relieves pressure to the
atmosphere in the event of a system overpressurization
(77 psi/5.3 bar).
TMUHYDI03-T11 LEVEL 3
EFFECTIVITY 29-11-00 Page 22
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 108
ALL
GREEN SYSTEM COMPONENTS - RESERVOIR COMPONENTS
TMUHYDI03-P11 LEVEL 3
EFFECTIVITY 29-11-00 Page 23
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 109
ALL
GREEN SYSTEM COMPONENTS
LEVEL TRANSMITTER
IDENTIFICATION
FIN: 1001GQ
LOCATION
ZONE: 148
DESCRIPTION
The level transmitter permits:
- Direct reading of the hydraulic fluid level.
- Transmission of the level indication to the cockpit.
It includes an arm fitted with a float which drives a
gear train on a magnetic coupling. The synchro
transmitter shaft supports a pointer to permit direct
reading of the fluid level.
TMUHYDI03-T12 LEVEL 3
EFFECTIVITY 29-11-00 Page 24
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 110
ALL
TMUHYDI03-P12 LEVEL 3
GREEN SYSTEM COMPONENTS - RESERVOIR COMPONENTS
EFFECTIVITY 29-11-00 Page 25
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 111
ALL
GREEN SYSTEM COMPONENTS
RETURN MANIFOLD
The LP return manifold is the connection point for
return lines from different parts of the LP system.
The LP filter and a temperature transmitter are
directly connected to the manifold.
LP RETURN FILTER
IDENTIFICATION
FIN: 1002GM
LOCATION
ZONE: 148
DESCRIPTION
The LP RETURN filter has a filtration rating of 3
　
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