W DOC AIRBUS | AMM A320F

Installation of the Switch Panel


TASK 23-73-23-400-001-A
Installation of the Switch Panel


1. Reason for the Job
Self Explanatory
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TASK 23-73-00-710-040-A
Operational Test of the Cabin/Cockpit Incident Alert System
TASK 23-73-00-740-005-B
Interface and Power-Up Test of the Cabin Intercommunication Data System (CIDS) through the CFDS
TASK 23-73-00-861-001-A
Energize the Cabin Intercommunication Data System (CIDS)
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 26-10-00-740-801-A
BITE Test of the Smoke Detection Function - System Test
3. Job Set-up
Subtask 23-73-23-861-051-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002)
Subtask 23-73-23-865-061-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
49VUCOM/CIDS/DEU B/ESS153RHG03
121VUCOM / CIDS / DEU B / NORM FWD193RHM09
121VUCOM/CIDS/DEU B/BAT143RHN12
2001VUCIDS-DEU B-NORM-AFT194RHC08
4. Procedure
Subtask 23-73-23-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Switch Panel 2080VU
   (1) Do an inspection of the component interfaces and the adjacent area.
   (2) Clean the component interfaces and the adjacent area.
   (3) Remove the CAP-BLANKING from each electrical connector and receptacle.
   (4) Make sure that all the electrical connections are clean and in the correct condition.
   (5) Connect the electrical connectors (3) to the switch panel (2).
   (6) Install the switch panel (2) and make sure that the spring clips (1) lock with a click.
   (7) Make sure that the work area is clean and clear of tools and other items.
Subtask 23-73-23-865-058-A ** ON A/C NOT FOR ALL
B. Remove the safety clips and tags and close these circuit breakers in this sequence:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUCOM / CIDS / DEU B / NORM FWD193RHM09
2001VUCIDS-DEU B-NORM-AFT194RHC08
49VUCOM/CIDS/DEU B/ESS153RHG03
121VUCOM/CIDS/DEU B/BAT143RHN12
Subtask 23-73-23-869-050-A ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
   (1) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
   (2) Do the Interface and Power-Up test of the Cabin Intercommunication Data System (CIDS)
(Ref. AMM TASK 23-73-00-740-005).
Subtask 23-73-23-740-050-B ** ON A/C NOT FOR ALL
D. Do the BITE test of the smoke detection function - system test
(Ref. AMM TASK 26-10-00-740-801).
Subtask 23-73-23-710-050-A ** ON A/C NOT FOR ALL
E. Do the operational test of the Cabin/Cockpit Incident Alert System.
(Ref. AMM TASK 23-73-00-710-040)
5. Close-up
Subtask 23-73-23-862-050-A ** ON A/C NOT FOR ALL
A. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
[Rev.10 from 2021] 2026.03.31 23:18:12 UTC