W DOC AIRBUS | AMM A320F

Installation of the Power Supply Unit (PSU)-Video


TASK 23-36-23-400-001-A
Installation of the Power Supply Unit (PSU)-Video


WARNING: ISOLATE THE ELECTRICAL CIRCUITS FROM THE RELATED EQUIPMENT AND THE ENVIRONMENT.
ZONE: 230
ZONE: 240
ZONE: 250
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
230
FWD PASSENGER COMPARTMENT
240
MID PASSENGER COMPARTMENT
250
AFT PASSENGER COMPARTMENT
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 23-36-00-710-001-A
Operational Test of the Passenger Entertainment (Video)
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 25-23-48-000-001-A
Removal of the Cove Light Panel
TASK 25-23-48-400-001-A
Installation of the Cove Light Panel
TASK 23-33-00-00-01
PASSENGER ENTERTAINMENT - DESCRIPTION AND OPERATION
3. Job Set-up
Subtask 23-36-23-860-051-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
   (2) For the location of PSUs refer to paragraph Component Location (Ref. AMM D/O 23-33-00-00).
   (3) Make sure that the applicable cove-light panel(s) is(are) removed (Ref. AMM TASK 25-23-48-000-001).
Subtask 23-36-23-865-057-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2000VUIFE-VCC-AC21MHC02
2000VUIFE-VCC-DC20MHC01
** ON A/C NOT FOR ALL
2000VUPES-VIDEO-CABIN-RH AFT25MHC06
2000VUPES-VIDEO-CABIN-LH23MHC05
2000VUPES-VIDEO-CABIN-RH FWD24MHC04
2000VUPES-VIDEO-CABIN-LH FWD22MHC03
2000VUPES-VIDEO-CONTROL-VCC21MHC02
** ON A/C NOT FOR ALL
2000VUPES-VIDEO-CONTROL-MAIN20MHC01
** ON A/C NOT FOR ALL
2000VUPES-VIDEO-CABIN AFT-RH25MHC06
2000VUPES-VIDEO-CABIN AFT-LH23MHC05
2000VUPES-VIDEO-CABIN FWD-RH24MHC04
2000VUPES-VIDEO-CABIN FWD-LH22MHC03
2000VUPES-VIDEO-CONTROL-VCC-DS/C21MHC02
4. Procedure
Subtask 23-36-23-865-058-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2000VUIFE-VCC-AC21MHC02
2000VUIFE-VCC-DC20MHC01
** ON A/C NOT FOR ALL
2000VUPES-VIDEO-CABIN-RH AFT25MHC06
2000VUPES-VIDEO-CABIN-LH23MHC05
2000VUPES-VIDEO-CABIN-RH FWD24MHC04
2000VUPES-VIDEO-CABIN-LH FWD22MHC03
2000VUPES-VIDEO-CONTROL-VCC21MHC02
** ON A/C NOT FOR ALL
2000VUPES-VIDEO-CONTROL-MAIN20MHC01
** ON A/C NOT FOR ALL
2000VUPES-VIDEO-CABIN AFT-RH25MHC06
2000VUPES-VIDEO-CABIN AFT-LH23MHC05
2000VUPES-VIDEO-CABIN FWD-RH24MHC04
2000VUPES-VIDEO-CABIN FWD-LH22MHC03
2000VUPES-VIDEO-CONTROL-VCC-DS/C21MHC02
Subtask 23-36-23-710-050-A ** ON A/C NOT FOR ALL
B. Operational Test of the Passenger Entertainment System
   (1) Do the operational test of the passenger entertainment system (Ref. AMM TASK 23-36-00-710-001).
5. Close-up
Subtask 23-36-23-410-050-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the applicable cove-light panel (Ref. AMM TASK 25-23-48-400-001).
Subtask 23-36-23-862-050-A ** ON A/C NOT FOR ALL
B. Put the aircraft back to its initial configuration.
   (1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:12:10 UTC