W DOC AIRBUS | AMM A320F

Operational Test of the Loudspeaker through the MCDU


TASK 23-73-00-710-036-A
Operational Test of the Loudspeaker through the MCDU


ZONE: 200
1. Reason for the Job
To verify the loudspeaker operation in the cabin and all lavatories.
2. Job Set-up Information
 A. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
200
UPPER HALF FUSELAGE
 B. Referenced Information
REFERENCE
DESIGNATION
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 31-32-00-860-003-A
Procedure to Get Access to the SYSTEM REPORT/TEST/COM Page
TASK 31-60-00-860-001-A
EIS Start Procedure
TASK 31-60-00-860-002-A
EIS Stop Procedure
3. Job Set-up
Subtask 23-73-00-860-167-A
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
   (3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
   (4) Get Access to the SYSTEM REPORT/TEST/COM page of the Centralized Fault Display System (CFDS)
(Ref. AMM TASK 31-32-00-860-003).
   (5) Make sure that a minimum of one cabin door is open.
Subtask 23-73-00-865-187-A
B. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUENGINE/2/FADEC A/AND EIU 22KS2A05
49VUENGINE/1/FADEC A/AND EIU 12KS1A04
49VUL/G/LGCIU/SYS1/NORM1GAC09
49VUAIR COND/CAB/PRESS/CTL11HLD09
** ON A/C NOT FOR ALL
121VUENGINE/ENG2/FADEC B4KS2Q40
** ON A/C NOT FOR ALL
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R41
** ON A/C ALL
121VUHYDRAULIC/LGCIU/SYS22GAQ35
** ON A/C NOT FOR ALL
121VUENGINE/ENG2/FADEC B/AND EIU24KS2Q40
** ON A/C NOT FOR ALL
121VUENGINE/ENG2/FADEC B/AND EIU24KS2R41
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R40
** ON A/C ALL
122VUAIR COND/CAB PRESS/CTL/22HLY22
4. Procedure
Subtask 23-73-00-710-299-A ** ON A/C NOT FOR ALL
A. Do this test
ACTION
RESULT
1.On the CFDS-MCDU:
On the CFDS-MCDU:
  • push the CIDS1 related line select key.
  • the CIDS1 main menu page shows.
  • push the OP TESTS line select key.
  • the CIDS1 OP TESTS page shows.
  • push the LOUDSPEAKERS ACTIVATION line select key.
  • the CIDS1 OP TEST OF LOUDSPEAKER page shows.

  • the message LOUDSPEAKERS ACTIVATED shows.

In the cabin and in all lavatories:
  • you hear a test tone.
2.On the CFDS-MCDU:
In the cabin and in all lavatories:
  • push the RETURN line select key until the SYSTEM REPORT/TEST page shows.
  • the test tone stops.
3.On the CFDS-MCDU:
On the CFDS-MCDU:
  • push the MCDU MENU pushbutton.
  • the MCDU MENU page shows.
Subtask 23-73-00-710-299-B ** ON A/C NOT FOR ALL
A. Do this test
ACTION
RESULT
1.On the CFDS-MCDU:
On the CFDS-MCDU:
  • push the CIDS1 related line select key.
  • the CIDS1 main menu page shows.
  • push the TEST related line select key.
  • the first CIDS1 TEST page shows.
  • push the NEXT PAGE function key.
  • the second CIDS1 TEST page shows.
  • push the LOUDSPEAKERS related line select key.
  • the message LOUDSPEAKER ON/ LOUDSPEAKER OFF shows.

In the cabin and in all lavatories:
  • push the LOUDSPEAKER ON related line select key.
  • you hear a test tone.
2.On the CFDS-MCDU:
In the cabin and in all lavatories:
  • push the RETURN line select key until the SYSTEM REPORT/TEST page shows.
  • the test tone stops.
3.On the CFDS-MCDU:
On the CFDS-MCDU:
  • push the MCDU MENU pushbutton.
  • the MCDU MENU page shows.
5. Close-up
Subtask 23-73-00-860-168-A
A. Put the aircraft back to its initial configuration.
   (1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
   (2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
[Rev.10 from 2021] 2026.03.31 23:17:30 UTC