W DOC AIRBUS | AMM A320F

Removal of the GCU-1(2)


TASK 24-22-34-000-001-A
Removal of the GCU-1(2)


CAUTION: USE ONLY THE GROUND SERVICE NETWORK TO SUPPLY THE AIRCRAFT WITH AC AND DC POWER. YOU CAN CAUSE DAMAGE TO THE EQUIPMENT DURING ITS REMOVAL/ INSTALLATION IF THE RELATED NETWORK IS NOT ISOLATED.
ZONE: 121
FIN: 1XU1
FIN: 1XU2
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
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
121
AVIONICS COMPARTMENT
811
 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 24-22-34-860-050-A
A. Aircraft Maintenance Configuration
   (1) Energize the Ground Service network (Ref. AMM TASK 24-42-00-861-001).
   (2) In the cockpit, put a WARNING NOTICE(S) to tell persons not to operate the pushbutton switches (ENG MASTER 1(2)) on the pylon panel 115VU (ENG panel)
Subtask 24-22-34-865-052-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
FOR FIN: 1XU1 (GCU1)
122VUELEC/GCU/12XU1T26
FOR FIN: 1XU2 (GCU2)
122VUELEC/GCU/22XU2T27
Subtask 24-22-34-010-052-A
C. Get Access
   (1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE at the access door 811 of the avionics compartment.
   (2) Open the access door 811.
4. Procedure
Subtask 24-22-34-020-052-A
A. Removal of the GCU
   (1) Loosen the 2 knurled nuts (1).
   (2) Lower the 2 knurled nuts (1) to disengage the 2 studs (2).
   (3) Carefully pull the handle (3) of the GCU (4) until the GCU is disconnected from the rack receptacle (5).
   (4) Remove the GCU from the rack (6).
   (5) Put CAP - BLANKING on the rack receptacle (5) and on the GCU connector.
[Rev.10 from 2021] 2026.03.31 23:22:10 UTC