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TMULD2I01-P05 LEVEL 3
EFFECTIVITY 32-00-00 Page 11
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 125
ALL
LANDING GEAR COMPONENTS
NLG ACTUATING CYLINDER
IDENTIFICATION
FIN: 2527GM
LOCATION
ZONE: 711
NLG UPLOCK BOX
IDENTIFICATION
FIN: 2530GM
LOCATION
ZONE: 123
TMULD2I01-T06 LEVEL 3
EFFECTIVITY 32-00-00 Page 12
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 126
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LANDING GEAR COMPONENTS - NLG ACTUATING CYLINDER - NLG UPLOCK BOX
TMULD2I01-P06 LEVEL 3
EFFECTIVITY 32-00-00 Page 13
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 127
ALL
LANDING GEAR COMPONENTS
NLG DOOR ACTUATING CYLINDER
IDENTIFICATION
FIN: 2531GM
LOCATION
ZONE: 123
NLG DOOR UPLOCK BOX
IDENTIFICATION
FIN: 2534GM
LOCATION
ZONE: 123
TMULD2I01-T07 LEVEL 3
EFFECTIVITY 32-00-00 Page 14
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 128
ALL
LANDING GEAR COMPONENTS - NLG DOOR ACTUATING CYLINDER - NLG DOOR UPLOCK BOX
TMULD2I01-P07 LEVEL 3
EFFECTIVITY 32-00-00 Page 15
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 129
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LANDING GEAR COMPONENTS
CUT-OUT VALVE
IDENTIFICATION
FIN: 2515GM
LOCATION
ZONE: 147
DESCRIPTION
Shuts off the high pressure supply and connects the
entire landing gear hydraulic system to the return
circuit during free fall extension.
TMULD2I01-T08 LEVEL 3
EFFECTIVITY 32-00-00 Page 16
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 130
ALL
LANDING GEAR COMPONENTS - CUT-OUT VALVE
TMULD2I01-P08 LEVEL 3
EFFECTIVITY 32-00-00 Page 17
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 131
ALL
LANDING GEAR COMPONENTS
VENT VALVES
IDENTIFICATION
FIN: 2532GM (NLG), 2516GM (MLG)
LOCATION
ZONE: 124, 148
DESCRIPTION
There are two identical mechanically operated vent
valves in the landing gear free fall extension system.
During landing gear free fall extension, operation of
the vent valve connects door close and gear raise lines
to the return circuit.
TMULD2I01-T09 LEVEL 3
EFFECTIVITY 32-00-00 Page 18
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
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LANDING GEAR COMPONENTS - VENT VALVES
TMULD2I01-P09 LEVEL 3
EFFECTIVITY 32-00-00 Page 19
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 133
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LANDING GEAR COMPONENTS
DOOR BYPASS VALVES
IDENTIFICATION
FIN: 2533GM (NLG), 2517GM (LH), 2518GM (RH)
LOCATION
ZONE: 123, 147, 148
DESCRIPTION
Each bypass valve isolates its corresponding door
hydraulic actuator from the landing gear hydraulic
supply during ground opening of landing gear door(s).
Weight: 0,88 kg (1.94 lb).
TMULD2I01-T10 LEVEL 3
EFFECTIVITY 32-00-00 Page 20
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 134
ALL
LANDING GEAR COMPONENTS - DOOR BYPASS VALVES
TMULD2I01-P10 LEVEL 3
EFFECTIVITY 32-00-00 Page 21
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MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 135
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TMULD2I01 LEVEL 3
EFFECTIVITY 32-00-00 Page 22
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UF94200
EFFECTIVITY Page 136
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32 - LANDING GEAR
32-40-00 WHEELS AND BRAKES - BRAKE SYSTEM
PRESENTATION
CONTENTS:
Normal Braking
Normal Braking by Auto Brake
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