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(77 psi - 5.3 bar).
TMUHYDJ02-T11 LEVEL 3
EFFECTIVITY 29-12-00 Page 22
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 140
ALL
BLUE SYSTEM COMPONENTS - RESERVOIR COMPONENTS
TMUHYDJ02-P11 LEVEL 3
EFFECTIVITY 29-12-00 Page 23
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 141
ALL
BLUE SYSTEM COMPONENTS
LOW LEVEL SWITCH
IDENTIFICATION
FIN: 2062GQ
LOCATION
ZONE: 197
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 dampener.
LEVEL TRANSMITTER
IDENTIFICATION
FIN: 2001GQ
LOCATION
ZONE: 197
DESCRIPTION
It gives a visual indication and sends a signal to the
SDAC and to the reservoir quantity indicator on the
green ground service panel for fluid content
indication.
TMUHYDJ02-T12 LEVEL 3
EFFECTIVITY 29-12-00 Page 24
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 142
ALL
BLUE SYSTEM COMPONENTS - RESERVOIR COMPONENTS
TMUHYDJ02-P12 LEVEL 3
EFFECTIVITY 29-12-00 Page 25
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 143
ALL
BLUE SYSTEM COMPONENTS
RETURN MANIFOLD
FILTER
IDENTIFICATION
FIN: 2002GM
LOCATION
ZONE: 197
DESCRIPTION
The LP return filter has a filtration rating of 3 microns.
The bypass device allows fluid to go from the inlet
to the outlet without filtration.
TEMPERATURE TRANSMITTER
IDENTIFICATION
FIN: 2381GR
LOCATION
ZONE: 197
DESCRIPTION
The temperature transmitter connected to the SDAC
comprises:
- a temperature switch which operates at 95 ± 2°C
(203 ± 4°F)
- two temperature transmitters which measure
fluid temperature between - 55°C (+131°F)
and 120°C (248°F).
TMUHYDJ02-T13 LEVEL 3
EFFECTIVITY 29-12-00 Page 26
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 144
ALL
BLUE SYSTEM COMPONENTS
TMUHYDJ02-P13 LEVEL 3
EFFECTIVITY 29-12-00 Page 27
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 145
ALL
BLUE SYSTEM COMPONENTS
GROUND SERVICE PANEL
RESERVOIR DEPRESSURIZATION VALVE
IDENTIFICATION
FIN: 2087GM
LOCATION
ZONE: 197
DESCRIPTION
The reservoir depressurization valve is a manually
operated 2-way valve. It is closed by spring force.
It opens by turning the cap assembly or by
connecting the ground depressurization coupling.
RESERVOIR DRAIN VALVE
IDENTIFICATION
FIN: 2264GM
LOCATION
ZONE: 197
DESCRIPTION
A hollow type drain valve is installed on the service
panel. 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.
GROUND CONNECTORS
IDENTIFICATION
FIN: 2006GM, 2008GM
LOCATION
ZONE: 197
DESCRIPTION
The delivery ground connector (2008 GM) and suction
ground connector (2006 GM) are of the self-sealing
type.
TMUHYDJ02-T14 LEVEL 3
EFFECTIVITY 29-12-00 Page 28
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 146
ALL
BLUE SYSTEM COMPONENTS
TMUHYDJ02-P14 LEVEL 3
EFFECTIVITY 29-12-00 Page 29
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 29 HYDRAULIC POWER
UF94200
EFFECTIVITY Page 147
ALL
BLUE SYSTEM COMPONENTS
RAT GROUND CONTROL PANEL
IDENTIFICATION
FIN: 3GE
LOCATION
ZONE: 197
DESCRIPTION
The RAT ground control panel comprises the controls
to stow the RAT. The GROUND CHECK connector is the
connector for the RAT ground test equipment. The
guarded ARM switch supplies electrical power to the
　
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