W DOC AIRBUS | AMM A320F

Installation of the Cabin Assignment Module


TASK 23-73-19-400-001-A
Installation of the Cabin Assignment Module


FIN: 115RH ** ON A/C NOT FOR ALL
1. Reason for the Job
Self Explanatory
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TASK 23-73-00-740-005-A
BITE-Test of the Cabin Intercommunication Data System (CIDS) through the CFDS
TASK 23-73-00-860-002-A
Cabin Layout Selection
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)
3. Job Set-up
Subtask 23-73-19-861-051-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 23-73-19-865-051-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/DIR ESS/2157RHG02
** ON A/C NOT FOR ALL
49VUCOM/CIDS/DIR ESS/1150RHG01
** ON A/C NOT FOR ALL
49VUCOM DIR ESS/2157RHG02
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/PROG &/TST PNL161RHM07
121VUCOM NAV/CIDS/DIR NORM/2156RHM06
121VUCOM NAV/CIDS/DIR NORM/1151RHM05
121VUCOM/CIDS/DIR 2/BAT146RHP14
121VUCOM/CIDS/DIR 1/BAT147RHP13
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/PROG &/TST PNL161RHM08
121VUCOM NAV/CIDS/DIR NORM/2156RHM07
121VUCOM NAV/CIDS/DIR NORM/1151RHM06
4. Procedure
Subtask 23-73-19-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Cabin Assignment Module (CAM)
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Install the CAM (1).
   (4) Lock the quick-release fasteners (2).
   (5) Make sure that the work area is clean and clear of tools and other items.
Subtask 23-73-19-865-053-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 NAV/CIDS/PROG &/TST PNL161RHM08
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/PROG &/TST PNL161RHM07
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/2156RHM07
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/2156RHM06
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/1151RHM06
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/1151RHM05
49VUCOM/CIDS/DIR ESS/2157RHG02
** ON A/C NOT FOR ALL
49VUCOM DIR ESS/2157RHG02
** ON A/C NOT FOR ALL
49VUCOM/CIDS/DIR ESS/1150RHG01
** ON A/C NOT FOR ALL
121VUCOM/CIDS/DIR 1/BAT147RHP13
121VUCOM/CIDS/DIR 2/BAT146RHP14
Subtask 23-73-19-869-051-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).
Subtask 23-73-19-740-050-A ** ON A/C NOT FOR ALL
D. Do the BITE-test of the Cabin Intercommunication Data System (CIDS).
(Ref. AMM TASK 23-73-00-740-005)
5. Close-up
Subtask 23-73-19-860-051-A ** ON A/C NOT FOR ALL
A. Make sure that the required cabin layout is selected in the CAM.
(Ref. AMM TASK 23-73-00-860-002)
Subtask 23-73-19-862-050-A ** ON A/C NOT FOR ALL
B. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
[Rev.10 from 2021] 2026.03.31 23:17:58 UTC