W DOC AIRBUS | AMM A320F

Removal of the CSM/G Control Unit


TASK 24-24-34-000-001-A
Removal of the CSM/G Control Unit


ZONE: 125
FIN: 1XE
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
125
LATERAL AVIONIC COMPARTMENT
812, 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 24-24-34-860-050-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 EMER ELEC PWR section of the overhead panel 21VU, put a WARNING NOTICE(S) to tell persons not to operate the pushbutton switches.
Subtask 24-24-34-010-050-A
B. Get access to the avionics compartment.
   (1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE at the access doors 812 and 822 of the avionics compartment.
   (2) Open the access doors 812 and 822.
Subtask 24-24-34-865-050-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
105VUELEC/CSM/G /EV AUTO/SPLY7XEC01
106VUCSM/G /EV/MAN/SPLY6XEB04
4. Procedure
Subtask 24-24-34-020-050-A
A. Removal of the GCU
   (1) Disconnect the electrical connector (4).
   (2) Loosen the 4 screws (3).
   (3) Hold the CSM/G control unit (1).
   (4) Remove the screws (3) and the washers (2).
   (5) Remove the CSM/G control unit (1).
   (6) Put CAP - BLANKING on the electrical connector (4) and the electrical receptacle (5).
[Rev.10 from 2021] 2026.03.31 23:22:38 UTC