W DOC AIRBUS | AMM A320F

Installation of the Forward Attendant Panel


TASK 23-73-12-400-002-A
Installation of the Forward Attendant Panel


FIN: 120RH ** 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 23-73-00-861-001-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 23-73-12-861-053-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 24-41-00-861-002).
Subtask 23-73-12-865-054-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
121VUCOM /CIDS/FWD ATTND/PNL170RHQ14
** ON A/C NOT FOR ALL
121VUCOM /CIDS/FLT ATTND/PNL170RHQ14
** ON A/C NOT FOR ALL
121VUCOM/FAP1/NORM170RHQ14
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/FWD ATTND/PNL170RHQ14
4. Procedure
Subtask 23-73-12-420-052-B ** ON A/C NOT FOR ALL
A. Installation of the FAP
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Install the FAP (3) with the screws (4) and the washers (5).
   (4) Remove the CAP-BLANKING from each electrical connector and receptacle.
   (5) Connect the electrical connector (6).
   (6) Make sure that the work area is clean and clear of tools and other items.
   (7) Close the cover (2) with the locking magnets (1).
Subtask 23-73-12-865-055-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
121VUCOM /CIDS/FWD ATTND/PNL170RHQ14
** ON A/C NOT FOR ALL
121VUCOM /CIDS/FLT ATTND/PNL170RHQ14
** ON A/C NOT FOR ALL
121VUCOM/FAP1/NORM170RHQ14
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/FWD ATTND/PNL170RHQ14
Subtask 23-73-12-869-051-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 23-73-12-740-051-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 23-73-12-862-051-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] 2026.04.01 04:42:30 UTC