-
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
-------------------------------------------------------------------------------
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
-------------------------------------------------------------------------------
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM Communications 通讯4(79)