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ZONE: 148
DESCRIPTION
The parking-brake electrical control-valve comprises:
- a linear transmitter which operates the
hydromechanical valve,
- a pressure limiter for the dual shuttle valve
supply,
- a replaceable desiccant cartridge,
- two thermal fuses.
THERMAL FUSES
A thermal fuse protects each linear transmitter coil
from overheat.
It is possible to reset the fuse after removal of the
transparent cover.
DESICCANT CARTRIDGE
A replaceable desiccant cartridge indicates the
humidity conditions. The cartridge is blue and becomes
pink when in contact with water.
TMULDEX02-T02 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
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UF94200
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PARKING BRAKE COMPONENTS - PARKING BRAKE ELECTRICAL CONTROL VALVE
TMULDEX02-P02 LEVEL 3
EFFECTIVITY 32-45-00 Page 5
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 231
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WHEELS AND BRAKES - PARKING BRAKE COMPONENTS
PARKING BRAKE OPERATED VALVE
IDENTIFICATION
FIN: 2579GM
LOCATION
ZONE: 148
DESCRIPTION
The parking brake operated valve, installed between
the brake automatic selector and the dual valve, shuts
off supply to the alternate brake system to prevent
leakage through the distribution dual valve.
Parking brake pressure is delivered through port C.
Pressure from the automatic selector is delivered
through port A.
Port B is connected to the dual valve.
TMULDEX02-T03 LEVEL 3
EFFECTIVITY 32-45-00 Page 6
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 232
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PARKING BRAKE COMPONENTS - PARKING BRAKE OPERATED VALVE
TMULDEX02-P03 LEVEL 3
EFFECTIVITY 32-45-00 Page 7
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 233
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WHEELS AND BRAKES - PARKING BRAKE COMPONENTS
DUAL SHUTTLE VALVE
IDENTIFICATION
FIN: 2578GM
LOCATION
ZONE: 148
DESCRIPTION
The dual shuttle valve includes two valves, one for
each main gear, installed in a single block adjacent
to the alternate brake distribution dual valve.
Each valve is used to select either the alternate
system (E or/and D) (spring biased position) or the
parking brake system (A), to supply the corresponding
gear (C or/and B).
TMULDEX02-T04 LEVEL 3
EFFECTIVITY 32-45-00 Page 8
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 234
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TMULDEX02-P04 LEVEL 3
PARKING BRAKE COMPONENTS - DUAL SHUTTLE VALVE
EFFECTIVITY 32-45-00 Page 9
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 235
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THIS PAGE INTENTIONALLY LEFT BLANK
TMULDEX02 LEVEL 3
EFFECTIVITY 32-45-00 Page 10
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 236
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32 - LANDING GEAR
32-40-00 WHEEL AND BRAKE COMPONENTS
CONTENTS:
Main Landing Gear Wheels
Main Landing Gear Tires
Carbon Brakes
Tachometers
Main Landing Gear Drive Tachometers
Axle Wheel Adapter Sleeves
Nose Landing Gear Wheels
Nose Landing Gear Tires
Nose Landing Gear Axle Sleeves
TMULDJX04 LEVEL 3
EFFECTIVITY 32-40-00 Page 1
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 237
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WHEEL AND BRAKE COMPONENTS
MAIN LANDING GEAR WHEELS
IDENTIFICATION
FIN: 2651GM (WHEEL 1), 2649GM (WHEEL 2),
2652GM (WHEEL 3), 2650GM (WHEEL 4)
LOCATION
ZONE: 731 (WHEEL 1 & 2), 741 (WHEEL 3 & 4)
DESCRIPTION
The MLG wheels consist of two forged light alloy
half-wheels attached together with high-tensile steel
bolts and self-locking nuts.
An O-ring seal is put between the two half-wheels.
The wheel is equipped with :
- one standard inflating valve,
- one bolt which you can replace by a valve with
an incorporated pressure indicator (PSI type).
- six fuse plugs deflate the tire in the event
　
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本文鏈接地址：ATA 32 LANDING GEAR(32)