W DOC AIRBUS | AMM A320F

Installation of the Wall Disconnect Box (WDB)


TASK 23-33-47-400-803-A
Installation of the Wall Disconnect Box (WDB)


FIN: 50MK1 ** ON A/C NOT FOR ALL
FIN: 50MK2 ** ON A/C NOT FOR ALL
FIN: 50MK3 ** ON A/C NOT FOR ALL
FIN: 50MK4 ** ON A/C NOT FOR ALL
FIN: 50MK5 ** ON A/C NOT FOR ALL
FIN: 50MK6 ** ON A/C NOT FOR ALL
FIN: 50MK7 ** ON A/C NOT FOR ALL
FIN: 50MK8 ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TASK 23-33-00-710-005-A
Operational Test of the Integrated In-Flight Entertainment (IFE) System
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 25-23-44-000-001-A
Removal of the Lower Sidewall Panels (Dado Panels)
TASK 25-23-44-400-001-A
Installation of the Lower Sidewall Panels (Dado Panels)
3. Job Set-up
Subtask 23-33-47-865-063-A ** ON A/C NOT FOR ALL
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2000VUPES-VIDEO-CONTROL-VCC-DS/C21MHC02
2000VUPES-VIDEO-CONTROL-MAIN20MHC01
2000VUPES-MUSIC-CABIN AFT-RH25MKD05
2000VUPES-MUSIC-CABIN AFT-LH22MKD04
2000VUPES-MUSIC-CABIN FWD-RH24MKD03
2000VUPES-MUSIC-CABIN FWD-LH23MKD02
2000VUPES-MUSIC - CTL21MKD01
Subtask 23-33-47-860-054-A ** ON A/C NOT FOR ALL
B. Preparation for Installation
   (1) Make sure that the applicable lower sidewall panel in the area of the related WDB is removed (Ref. AMM TASK 25-23-44-000-001).
   (2) Make sure that the protection cap (10) of the related WDB (8) is removed.
4. Procedure
Subtask 23-33-47-420-052-A ** ON A/C NOT FOR ALL
A. Installation of the Wall Disconnect Box (WDB)
   (1) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (2) Clean the component interfaces and the adjacent area.
   (3) Do an inspection of the component interfaces and the adjacent area.
   (4) Put the insulation strip (7), the WDB (8) and the protective cover (13) carefully into position.
   (5) Install the screws (11) and the washers (12).
   (6) If applicable, install the spacers (5) and (4) and the cable support (3).
   (7) Install the screw (1) and the washer (2).
   (8) Remove the blanking caps from the electrical connector(s) (6).
   (9) Make sure that the electrical connector(s) are clean and in the correct condition.
   (10) Connect the electrical connector(s) (6) to the WDB (8) as identified during the removal procedure.
   (11) Safety the electrical connector(s) (6).
CAUTION: MAKE SURE THAT THE SPRING LATCHES CORRECTLY HOLD THE CONNECTOR IN THE FULLY ENGAGED POSITION. THE SPRING LATCHES PREVENT UNWANTED MOVEMENT OF THE CONNECTOR, AND THUS THE RISK OF ARCING, WHICH CAN CAUSE DAMAGE TO THE UNIT.
   (12) Safety the electrical connector(s) (6) with the spring latches.
Subtask 23-33-47-865-064-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2000VUPES-VIDEO-CONTROL-VCC-DS/C21MHC02
2000VUPES-VIDEO-CONTROL-MAIN20MHC01
2000VUPES-MUSIC-CABIN AFT-RH25MKD05
2000VUPES-MUSIC-CABIN AFT-LH22MKD04
2000VUPES-MUSIC-CABIN FWD-RH24MKD03
2000VUPES-MUSIC-CABIN FWD-LH23MKD02
2000VUPES-MUSIC - CTL21MKD01
Subtask 23-33-47-710-053-A ** ON A/C NOT FOR ALL
C. Do the operational test of the integrated In-Flight Entertainment (IFE) system (Ref. AMM TASK 23-33-00-710-005).
5. Close-up
Subtask 23-33-47-410-052-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) Put the protection cap (10) in position and tighten the fasteners (9).
   (3) Install the related lower sidewall panel (Ref. AMM TASK 25-23-44-400-001).
Subtask 23-33-47-862-052-A ** ON A/C NOT FOR ALL
B. De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001)
[Rev.10 from 2021] 2026.04.02 06:12:08 UTC