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HYDRAULIC FUSES
IDENTIFICATION
FIN: 2620GM (WHEEL 1), 2622GM (WHEEL 2),
2623GM (WHEEL 3), 2621GM (WHEEL 4)
LOCATION
ZONE: 571 (Wheel 1 & 2), 671 (Wheel 3 & 4)
DESCRIPTION
A hydraulic fuse, installed between the brake
servovalve and the brake, stops the flow in the line
if the leakage exceeds 1.32 U.S. gal/mn (5 l/mn).
The valve is reset when you depressurize the hydraulic
reservoir and when you open the bleed screw.
TMULDDX09-T07 LEVEL 3
EFFECTIVITY 32-43-00 Page 14
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 222
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ALTERNATE BRAKING COMPONENTS - HYDRAULIC FUSES
TMULDDX09-P07 LEVEL 3
EFFECTIVITY 32-43-00 Page 15
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
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WHEELS AND BRAKES - ALTERNATE BRAKING COMPONENTS
HYDRAULIC PRESSURE TRANSDUCER
IDENTIFICATION
FIN: 3068GN
LOCATION
ZONE: 148
DESCRIPTION
The transducer is made of two main sections. The first
section has the pressure-sensing element. It includes
a diaphragm which is under hydraulic pressure. The
diaphragm causes a piezoresistive sensing element to
operate on the Wheatstone bridge principle, according
to the pressure applied.
The transducer is a sealed unit and no maintenance is
necessary or possible.
The pressure transducer sends hydraulic pressure data
to the Brake Yellow Pressure Triple Indicator for
accumulator pressure indication.
RELIEF VALVE
IDENTIFICATION
FIN: 3067GM
LOCATION
ZONE: 148
DESCRIPTION
The hydraulic thermal-pressure relief valve is
calibrated at 3436 psi (237 bars).
It can be manually activated for accumulator
depressurization.
TMULDDX09-T08 LEVEL 3
EFFECTIVITY 32-43-00 Page 16
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 224
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ALTERNATE BRAKING COMPONENTS - HYDRAULIC PRESSURE TRANSDUCER - RELIEF VALVE
TMULDDX09-P08 LEVEL 3
EFFECTIVITY 32-43-00 Page 17
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 225
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THIS PAGE INTENTIONALLY LEFT BLANK
TMULDDX09 LEVEL 3
EFFECTIVITY 32-43-00 Page 18
Aug 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 226
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32 - LANDING GEAR
32-45-00 WHEELS AND BRAKES - PARKING
BRAKE COMPONENTS
CONTENTS:
Accumulator
Pressure Gage
Charging Valve
Parking Brake Electrical Control Valve
Parking Brake Operated Valve
Dual Shuttle Valve
TMULDEX02 LEVEL 3
EFFECTIVITY 32-45-00 Page 1
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 227
ALL
WHEELS AND BRAKES - PARKING BRAKE COMPONENTS
ACCUMULATOR
IDENTIFICATION
FIN: 2582GM
LOCATION
ZONE: 148
DESCRIPTION
The brake yellow pressure accumulator is either
pressurized by the hydraulic system or by the yellow
electric pump.
Filling pressure:
- 1450 psi at 60°F (100 bars at 20°C).
Volume of fluid:
- 164.8 cu.in. (2700 cm3), filled with nitrogen.
PRESSURE GAGE
IDENTIFICATION
FIN: 2585GM
LOCATION
ZONE: 148
DESCRIPTION
The pressure gage indicates the actual nitrogen
pressure.
CHARGING VALVE
IDENTIFICATION
FIN: 2586GM
LOCATION
ZONE: 148
DESCRIPTION
The accumulator is equipped with a charging valve for
nitrogen refilling if necessary.
TMULDEX02-T01 LEVEL 3
EFFECTIVITY 32-45-00 Page 2
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 228
ALL
PARKING BRAKE COMPONENTS - ACCUMULATOR - PRESSURE GAGE - CHARGING VALVE
TMULDEX02-P01 LEVEL 3
EFFECTIVITY 32-45-00 Page 3
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 229
ALL
WHEELS AND BRAKES - PARKING BRAKE COMPONENTS
PARKING BRAKE ELECTRICAL CONTROL VALVE
IDENTIFICATION
FIN: 72GG
LOCATION
　
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