W DOC AIRBUS | AMM A320F

Removal of the Battery Charge Limiter (BCL)


TASK 24-38-34-000-001-A
Removal of the Battery Charge Limiter (BCL)


ZONE: 126
FIN: 1PB1
FIN: 1PB2
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
126
LATERAL AVIONIC COMPARTMENT
822
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
3. Job Set-up
Subtask 24-38-34-860-050-A
A. Aircraft Maintenance Configuration
   (1) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
   (2) In the cockpit, on the overhead panel 35VU, release the BAT pushbutton switches.
   (3) In the cockpit, on the overhead panel 35VU, put a WARNING NOTICE(S) to tell the persons not to operate the batteries.
Subtask 24-38-34-010-050-A
B. Get access to the avionics compartment.
   (1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE at the avionics compartment door 822.
   (2) Open the access door 822.
   (3) Open the access panel of the BATTERY power center 105VU.
Subtask 24-38-34-865-050-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
FOR FIN: 1PB1 (BCL1)
105VUELEC/BAT REF/BCL19PB1F01
105VUELEC/BAT BUS/REF/BCL18PB1G01
FOR FIN: 1PB2 (BCL2)
105VUELEC/BAT REF/BCL29PB2F02
105VUELEC/BAT BUS/REF/BCL28PB2J02
4. Procedure
Subtask 24-38-34-020-050-A
A. Removal of the Battery Charge Limiter
   (1) Disconnect the connector (2).
   (2) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
   (3) Loosen and remove the four screws (4) and the washers (3).
   (4) Remove the battery charge limiter (1).
[Rev.10 from 2021] 2026.04.01 05:49:12 UTC