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UF94200
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LGCIU CONTROL SIGNALS
TMULDGG01-P01 LEVEL 3
EFFECTIVITY 32-31-00 Page 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
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LANDING GEAR AND DOORS - LGCIU CONTROL SIGNALS
LGCIU 2
Same control signals for LGCIU 2.
Four signals are used by the LGCIU for system
selection:
- two for system 1 status,
- two for system 2 status.
TMULDGG01-T01 LEVEL 3
EFFECTIVITY 32-31-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
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32 - LANDING GEAR
32-60-00 LANDING GEAR AND DOORS - LGCIU
MONITORING INTERFACES
CONTENTS:
ARINC and Indicator Panel
Discrete
TMULDGH01 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
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LANDING GEAR AND DOORS - LGCIU MONITORING INTERFACES
ARINC AND INDICATOR PANEL
After analyzing both gear uplock and downlock signals,
the LGCIU sends up to six signals to the corresponding
lights on the landing gear indicator panel.
TMULDGH01-T01 LEVEL 3
EFFECTIVITY 32-60-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
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LGCIU MONITORING INTERFACES - ARINC AND INDICATOR PANEL
TMULDGH01-P01 LEVEL 3
EFFECTIVITY 32-60-00 Page 3
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TMULDGH01-P02 LEVEL 3
LGCIU MONITORING INTERFACES - DISCRETE - LANDING GEAR COMPRESSED
EFFECTIVITY 32-60-00 Page 4
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TMULDGH01-P03 LEVEL 3
LGCIU MONITORING INTERFACES - DISCRETE
LANDING GEAR EXTENDED - DOWNLOCKED - UPLOCK UNLOCKED
EFFECTIVITY 32-60-00 Page 5
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TMULDGH01 LEVEL 3
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32 - LANDING GEAR
32-11-00 LANDING GEAR AND DOORS - MAIN
LANDING GEAR DESCRIPTION
CONTENTS:
General
Main Fitting
Sliding Tube/Axle
Actuating Cylinder
Side Stay Assembly
Lock Stay
Lock Stay Actuator
Torque Links/Slave Link
Torque Link Damper
TMULDAI09 LEVEL 2
EFFECTIVITY 32-11-00 Page 1
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MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
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LANDING GEAR AND DOORS - MAIN LANDING GEAR DESCRIPTION
GENERAL
Each Main Landing Gear (MLG) includes these parts:
- a main fitting,
- a sliding tube,
- a shock absorber,
- a retraction actuating cylinder,
- a side stay assembly,
- a lock stay assembly and actuator,
- torque and slave links.
TMULDAI09-T01 LEVEL 2
EFFECTIVITY 32-11-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
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MAIN LANDING GEAR DESCRIPTION - GENERAL
TMULDAI09-P01 LEVEL 2
EFFECTIVITY 32-11-00 Page 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
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LANDING GEAR AND DOORS - MAIN LANDING GEAR DESCRIPTION
MAIN FITTING
The main fitting includes:
- the main barrel,
- the drag stay,
- the cross tube,
- the aircraft attachment lugs.
It contains a diaphragm and tube assembly which form
the top of the shock absorber.
A pin connects the diaphragm and the tube assembly.
This pin is located in the two lateral holes in the
main fitting, and contains the shock absorber charging
valve.
A gland housing assembly, at the bottom end of the
main fitting, seals the joint between the main fitting
　
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