W DOC AIRBUS | AMM A320F

Installation of the LGCIU


TASK 32-31-71-400-001-A
Installation of the LGCIU


ZONE: 121
ZONE: 122
FIN: 5GA1
FIN: 5GA2
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
121
AVIONICS COMPARTMENT
122
AVIONICS COMPARTMENT
811
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 32-00-00-860-001-A
Flight Configuration Precautions with Electrical Power
TASK 32-00-00-860-001-A-01
Flight Configuration Precautions without Electrical Power
TASK 32-00-00-860-002-A
Ground Configuration after Flight Configuration with Electrical Power
TASK 32-00-00-860-002-A-01
Ground Configuration after Flight Configuration without Electrical Power
TASK 32-31-00-720-002-A
Functional Test of the Normal Extension and Retraction of the Landing Gear
TASK 32-69-00-740-001-A
BITE Check of Landing-Gear Control Interface-Unit (LGCIU) With Use of MCDU to Ensure that Continuous BITE is Operative
3. Job Set-up
Subtask 32-31-71-860-050-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the ground service network is energized (Ref. AMM TASK 24-42-00-861-001).
   (2) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at the access door 811.
   (3) Make sure that the access door 811 is open.
   (4) Make sure that you obeyed the flight configuration precautions (Ref. AMM TASK 32-00-00-860-001).
Subtask 32-31-71-865-059-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUL/G/LGCIU/SYS1/NORM1GAC09
** ON A/C NOT FOR ALL
121VULGCIU/BAT SPLY/SYS259GAR33
121VULGCIU/BAT SPLY/SYS158GAR32
** ON A/C ALL
121VUHYDRAULIC/LGCIU/SYS22GAQ35
121VUHYDRAULIC/LGCIU/SYS1/GRND SPLY52GAQ34
** ON A/C NOT FOR ALL
121VULGCIU/BAT SPLY/SYS259GAR32
121VULGCIU/BAT SPLY/SYS158GAR31
4. Procedure
Subtask 32-31-71-420-050-A
A. Installation of the LGCIU
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Remove the CAP-BLANKING from each electrical connector and receptacle.
   (4) Make sure that all the electrical connections are clean and in the correct condition.
   (5) Install the LGCIU (1) on its rack (3).
   (6) Push the LGCIU (1) on its rack (3) to connect the electrical connectors (2).
   (7) Engage the nuts (4) on the lugs (5) and tighten.
   (8) Make sure that the OBRMs are correctly installed. If they are not installed correctly, push the OBRMs until the locking devices are locked.
Subtask 32-31-71-865-060-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUL/G/LGCIU/SYS1/NORM1GAC09
** ON A/C NOT FOR ALL
121VULGCIU/BAT SPLY/SYS259GAR33
121VULGCIU/BAT SPLY/SYS158GAR32
** ON A/C ALL
121VUHYDRAULIC/LGCIU/SYS22GAQ35
121VUHYDRAULIC/LGCIU/SYS1/GRND SPLY52GAQ34
** ON A/C NOT FOR ALL
121VULGCIU/BAT SPLY/SYS259GAR32
121VULGCIU/BAT SPLY/SYS158GAR31
Subtask 32-31-71-869-054-A
C. After you close the LGCIU circuit breakers, put the aircraft back to the correct (ground) condition (Ref. AMM TASK 32-00-00-860-002).
Subtask 32-31-71-740-050-A
D. Do the BITE test of the landing gear (Ref. AMM TASK 32-69-00-740-001).
NOTE: As an alternative procedure, you can do this test without
the CFDS (Ref. AMM TASK 32-31-00-720-002).
5. Close-up
Subtask 32-31-71-410-050-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the access door 811.
   (3) Remove the access platform(s).
Subtask 32-31-71-862-050-A
B. De-energize the ground service network (Ref. AMM TASK 24-42-00-862-001).
[Rev.10 from 2021] 2026.04.01 04:39:21 UTC