W DOC AIRBUS | AMM A320F

Installation of the Seat Row Call/Numbering Light


TASK 23-73-14-400-006-A
Installation of the Seat Row Call/Numbering Light


FIN: 505RH ** ON A/C NOT FOR ALL
FIN: 506RH ** 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 23-73-14-861-057-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
Subtask 23-73-14-865-066-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 A ESS/LINE 2155RHG05
49VUCOM/CIDS/DEU A ESS/LINE 1154RHG04
121VUCOM NAV/CIDS/DEU A NORM/R AFT168RHM14
121VUCOM NAV/CIDS/DEU A NORM/L AFT167RHM13
121VUCOM NAV/CIDS/DEU A NORM/R MID166RHM12
121VUCOM NAV/CIDS/DEU A NORM/L MID165RHM11
121VUCOM NAV/CIDS/DEU A NORM/R FWD164RHM10
121VUCOM NAV/CIDS/DEU A NORM/L FWD163RHM09
4. Procedure
NOTE: If the Seatrow Call/Numbering Light is equipped with LED technologie, install the complete Printed Circuit Board (Ref. AMM 23-73-49 Board - Printed Circuit).
Subtask 23-73-14-420-055-A ** ON A/C NOT FOR ALL
A. Installation of the seatrow call/numbering light
   (1) Install the seatrow call/numbering light (2).
   (2) Put the switch panel cover (4) in position on the PSIU. Move it carefully in the opposite arrow direction until the lugs (5) engage into the recesses of the PSIU. Push the switch panel cover (4) up until the lug (3) engages into the recess (1) of the PSIU.
NOTE: Make sure that the switch panel cover (4) is correctly attached.
Subtask 23-73-14-865-067-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/DEU A NORM/R AFT168RHM14
121VUCOM NAV/CIDS/DEU A NORM/L AFT167RHM13
121VUCOM NAV/CIDS/DEU A NORM/R MID166RHM12
121VUCOM NAV/CIDS/DEU A NORM/L MID165RHM11
121VUCOM NAV/CIDS/DEU A NORM/R FWD164RHM10
121VUCOM NAV/CIDS/DEU A NORM/L FWD163RHM09
49VUCOM/CIDS/DEU A ESS/LINE 2155RHG05
49VUCOM/CIDS/DEU A ESS/LINE 1154RHG04
Subtask 23-73-14-869-052-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 BITE test of the CIDS through the CFDS (Ref. AMM TASK 23-73-00-740-005).
Subtask 23-73-14-710-055-A ** ON A/C NOT FOR ALL
D. Do this test.
ACTION
RESULT
1.In the cabin:

  • Close all passenger/crew doors.

2.In the cabin:
In the cabin:
  • Open a passenger/crew door.
  • All seatrow call/numbering lights come on.
3.On the Programming and Test Panel (PTP) 110RH:
On the PTP 110RH:
  • Push the DISPL ON membrane switch.
  • the CIDS menu page comes on.
  • Push the SYSTEM TEST related membrane switch.
  • The SYSTEM TEST page comes on.
  • Push the CONT related membrane switch until PAX CALL LAMPS comes on.

  • Push the PAX CALL LAMPS related membrane switch.
  • The PAX CALL LAMPS test page comes on with the flashing message:
    WAIT FOR RESPONSE.

  • After not many seconds the
    WAIT FOR RESPONSE message changes to:
    ATA 23-73-14
    TEST OK.
5. Close-up
Subtask 23-73-14-862-055-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] 2026.04.02 06:12:30 UTC