W DOC AIRBUS | AMM A320F

Installation of the Flight Attendant Panel


TASK 23-73-12-400-007-A
Installation of the Flight 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 23-32-36-400-001-A
Installation of the Integrated Prerecorded Announcement and Boarding Music (PRAM) Flashcard
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 23-73-00-869-001-A
OBRM - Download Procedure
TASK 23-73-19-400-002-A
Installation of the Cabin Assignment Module
TASK 23-73-21-400-001-A
Installation of the On-Board Replaceable Module
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 23-73-12-861-064-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 23-73-12-865-071-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
49VUCOM/CIDS/FLT ATTND PNL/ESS171RHH01
** ON A/C NOT FOR ALL
49VUAIR COND/CIDS/SDF/DIR2 ESS18WHC06
49VUAIR COND/CIDS/SDF/DIR1 ESS15WHC05
** ON A/C NOT FOR ALL
49VUCOM DIR ESS/2157RHG02
** ON A/C NOT FOR ALL
49VUCOM/CIDS/FLT ATTND PNL/ESS171RHG03
49VUCOM NAV/CIDS/DIR2 ESS157RHG02
49VUCOM NAV/CIDS/DIR1 ESS150RHG01
** ON A/C NOT FOR ALL
121VUCOM CIDS FWD ATTND PNL170RHQ14
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/2156RHM06
121VUCOM NAV/CIDS/DIR NORM/1151RHM05
** ON A/C NOT FOR ALL
121VUCOM/FAP1/NORM170RHQ14
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/2156RHM07
121VUCOM NAV/CIDS/DIR NORM/1151RHM06
121VUCOM NAV/CIDS/FWD ATTND/PNL170RHQ14
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR2 NORM156RHM06
121VUCOM NAV/CIDS/DIR1 NORM151RHM05
121VUCOM/CIDS/FWD ATTND PNL/BAT149RHQ13
** ON A/C NOT FOR ALL
121VUCOM/CIDS/FLT ATTND PANL/BAT149RHQ13
** ON A/C NOT FOR ALL
121VUCOM/CIDS/DIR 2/BAT146RHP14
121VUCOM/CIDS/DIR 1/BAT147RHP13
** ON A/C NOT FOR ALL
122VUAIR COND/CIDS/SDF/DIR NORM/214WHT18
122VUAIR COND/CIDS/SDF/DIR NORM/117WHT17
4. Procedure
Subtask 23-73-12-420-057-A ** ON A/C NOT FOR ALL
A. Installation of the Flight Attendant Panel (FAP)
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Put the FAP (3) in position on the holder (7) and install the screws (6) and the washers (5).
   (4) Adjust the FAP (3) to the middle of the cover-cutting.
   (5) Tighten the screws (6).
   (6) Remove the CAP-BLANKING from each electrical connector and receptacle.
   (7) Make sure that all the electrical connections are clean and in the correct condition.
   (8) Connect the electrical connectors (4).
   (9) Make sure that the work area is clean and clear of tools and other items.
   (10) Make sure that you push the CAM, the OBRM and the optional I-PRAM into the correct slots and not into one of the other slots. All slots have the same dimensions.

NOTE: The inscription THIS SIDE UP on the CAM, on the OBRM and on the optional I-PRAM must point up when they are installed.
   (11) Install the Cabin Assignment Module (CAM) 115RH.
(Ref. AMM TASK 23-73-19-400-002)
   (12) Install the On-Board Replaceable Module (OBRM) 116RH.
(Ref. AMM TASK 23-73-21-400-001)
   (13) If an Integrated PRAM Flashcard (I-PRAM) 117RH was removed during the FAP 120RH removal procedure, install the I-PRAM again (Ref. AMM TASK 23-32-36-400-001).
   (14) Close the cover (2) with the quick-release fastener (1).
Subtask 23-73-12-865-072-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 FWD ATTND PNL170RHQ14
** ON A/C NOT FOR ALL
121VUCOM/FAP1/NORM170RHQ14
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/FWD ATTND/PNL170RHQ14
** ON A/C NOT FOR ALL
49VUCOM/CIDS/FLT ATTND PNL/ESS171RHH01
** ON A/C NOT FOR ALL
49VUCOM/CIDS/FLT ATTND PNL/ESS171RHG03
** ON A/C NOT FOR ALL
121VUCOM/CIDS/FLT ATTND PANL/BAT149RHQ13
** ON A/C NOT FOR ALL
121VUCOM/CIDS/FWD ATTND PNL/BAT149RHQ13
** ON A/C NOT FOR ALL
122VUAIR COND/CIDS/SDF/DIR NORM/117WHT17
122VUAIR COND/CIDS/SDF/DIR NORM/214WHT18
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR2 NORM156RHM06
** 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/DIR1 NORM151RHM05
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/1151RHM06
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/1151RHM05
** ON A/C NOT FOR ALL
49VUAIR COND/CIDS/SDF/DIR2 ESS18WHC06
49VUAIR COND/CIDS/SDF/DIR1 ESS15WHC05
** ON A/C NOT FOR ALL
49VUCOM NAV/CIDS/DIR2 ESS157RHG02
** ON A/C NOT FOR ALL
49VUCOM/CIDS/DIR ESS/2157RHG02
** ON A/C NOT FOR ALL
49VUCOM DIR ESS/2157RHG02
** ON A/C NOT FOR ALL
49VUCOM NAV/CIDS/DIR1 ESS150RHG01
** 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 23-73-12-869-056-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 23-73-12-970-056-A ** ON A/C NOT FOR ALL
D. Do the OBRM download procedure
(Ref. AMM TASK 23-73-00-869-001).
Subtask 23-73-12-740-057-A ** ON A/C NOT FOR ALL
E. Do the Interface and Power-Up Test of the CIDS
(Ref. AMM TASK 23-73-00-740-005).
5. Close-up
Subtask 23-73-12-862-057-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 04:42:36 UTC