-
push the TEST related line select key.

 -
push and release the NEXT PAGE pushbutton switch until the PAX CALL LAMPS test is indicated.

 -
push the PAX CALL LAMPS related line select key.

On the CFDS-MCDU:
-
the MCDU MENU page comes on.

-
the CFDS page comes on.

-
the SYSTEM REPORT/TEST page comes on.

-
the SYSTEM REPORT/TEST COM page comeson.

-
the CIDS1 (ACT) page comes on.

-
the CIDS1 (ACT) TEST page comes on.

-
the CIDS1 (ACT) PAX CALL LAMPS TESTpage with the message TEST IN PROGRESS comes on.

 -after a some seconds the message changes to TEST OK
 NOTE : An incorrect FAULT message will be recorded for each LED (without
____ bulbs) PAX CALL LAMP, if the test of the related lamps is not deactivated in the CAM.
R 1EFF : 001-049, 051-099, 101-105, 151-154, 1 23-73-00Page C587 1201-207, 1Aug 01/05 1 1 1CES 1

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ACTION RESULT -------------------------------------------------------------------------------
-push the MCDU MENU pushbutton  - the MCDU MENU page comes on.
 switch.

 5. Close-up
________ Subtask 23-73-00-860-151
 A. Put the aircraft back to its initial configuration.
 (1)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002)

 (2)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002)

R 1EFF : 001-049, 051-099, 101-105, 151-154, 1 23-73-00Page C588 1201-207, 1Aug 01/05 1 1 1CES 1R **ON A/C 106-149, 301-399, 401-499,

 TASK 23-73-00-710-035
 Operational Test of the Cabin LED Lamps via MCDU

 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-32-00-860-003 Procedure to Get Access to the SYSTEM REPORT/TEST/COM
 Page
 31-60-00-860-001 EIS Start Procedure
 31-60-00-860-002 EIS Stop Procedure
 33-25-00-710-001 Operational Test of the Passenger Reading

 Light-System
 3. Job Set-up
__________
 Subtask 23-73-00-860-165

 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 (2)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (3)
 Energize the CFDS (Ref. TASK 31-32-00-860-003)

 (4)
 Make sure that a minimum of one cabin door is open.

R 1EFF : 106-149, 301-399, 401-499, 1 23-73-00Page C589 1 1 Aug 01/05 1 1 1CES 1

 (5) Make sure that the Passenger Reading Light-System is energized (Ref. TASK 33-25-00-710-001).
 Subtask 23-73-00-865-186
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05 49VU ENGINE/1/FADEC A/AND EIU 1 2KS1 A04 49VU L/G/LGCIU/SYS1/NORM 1GA C09 49VU AIR COND/CIDS/SDF/DIR2 ESS 18WH C06 49VU AIR COND/CIDS/SDF/DIR1 ESS 15WH C05 49VU AIR COND/CAB/PRESS/CTL1 1HL D09

R **ON A/C 106-149, 401-499,
 49VU COM/CIDS/DIR ESS/2 157RH G02

R **ON A/C 106-149, 301-399, 401-499,
 49VU COM DIR ESS/1 150RH G01 49VU COM/CIDS/FWD ATTND PNL/ESS 171RH H01 49VU COM/CIDS/DEU A ESS/AFT R 172RH HA12 49VU COM/CIDS/DEU A ESS/AFT L 179RH HA11 49VU COM/CIDS/DEU A ESS/FWD R 158RH HA10 49VU COM/CIDS/DEU A ESS/FWD L 159RH HA09
 **ON A/C 301-399,
 49VU COM/CIDS/DEU B/ESS 153RH G03
 49VU COM DIR ESS/2 157RH G02

R **ON A/C 106-149, 401-499,
 121VU COM NAV/CIDS/DEU A NORM/R AFT 168RH M12 121VU COM NAV/CIDS/DEU A NORM/L AFT 167RH M11 121VU COM NAV/CIDS/DEU A NORM/R FWD 164RH M10 121VU COM NAV/CIDS/DEU A NORM/L FWD 163RH M09 121VU COM NAV/CIDS/DEU B/NORM 162RH M08 121VU COM NAV/CIDS/DIR NORM/2 156RH M06
R 1EFF : 106-149, 301-399, 401-499, 1 23-73-00Page C590 1 1 Aug 01/05 1 1 1CES 1

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