-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. Access to the ECAM OEB DATABASE
 A. On one of the MCDUs, turn the  The MCDU is on.
 OFF/BRT knob
 B. Push the MCDU MENU mode key  The MCDU MENU page comes into view.
 C. Push the line key adjacent to  The SYSTEM REPORT/TEST menu page comes
 the SYSTEM REPORT/TEST  into view.
 indication.
 D. Push the line key adjacent to  The instruments menu page comes into
 the INST indication.  view.
 E. Push the line key adjacent to  The ECAM 1 or2 first page comes into
 the ECAM 1 or2 indication.  view.
 F. Push the line key adjacent to  The ECAM 1 or 2 OEB DATABASE page comes
 the OEB DATABASE indication.  into view. 

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-51-00Page 322 1 1 Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------NOTE : If the data base of the FWC1 or FWC2 is not valid, the VERSION is
____ replaced by XXX and the check sum is replaced by XXXXX adjacent to the FWC1 or FWC2.
 2. Access to the FWC1 List
 A. Push the key line adjacent to The ECAM OEB DATABASE FWC1 LIST XXX
 the LIST FWC1 information.  comes into view. (XXX=04A for example=VERSION reference)
 B. Push the NEXT PAGE key. The other pages come into view.
 3. Access to the FWC2 List
 A. Push the key line adjacent to The ECAM OEB DATABASE FWC2 LIST 05A
 the LIST FWC2 information.  comes into view. (XXX=05A for example=VERSION reference)
 B. Push the NEXT PAGE key The other pages come into view.
 5. Close-up
________ Subtask 31-51-00-860-061
 A. Put the aircraft back to its initial configuration.
 (1)
 On the MCDU, push the line key adjacent to the RETURN indication until the CFDS MENU page comes into view.

 (2)
 Set the BRT/OFF knob to OFF, the MCDU is off

 (3)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002)

 (4)
 Put the system back to the serviceable condition.

 (5)
 Put the aircraft back to the serviceable condition.

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-51-00Page 323 1 1 Aug 01/05 1 1 1CES 1

 CENTRAL WARNING SYSTEM - AIR CONDITIONING - DESCRIPTION AND OPERATION
_____________________________________________________________________
 1. Operation/Control and Indication
________________________________ Hereafter are given all the warning pages related to the air conditioning which mention :
 -
the name of the failure

 -
the detector (item of equipment providing the fault to the warning system)

 -
the system page automatically called

 -
the MASTER lights actived by the failure

 -
the ATA chapter number

 -
the flight phases which inhibit the failure

 -
the local warning

 -
the operational sequence of the crew actions with associated warning
 title.

R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 31-51-21Page 1 1201-203, 1May 01/05 1 1 1CES 1

 Avionics blower fault
 Figure 001

R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 31-51-21Page 2 1201-203, 1May 01/05 1 1 1CES 1

 Avionics extract fault
 Figure 002

R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 31-51-21Page 3 1201-203, 1May 01/05 1 1 1CES 1

 Avionics system fault
 Figure 003

R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 31-51-21Page 4 1201-203, 1May 01/05 1 1 1CES 1

 Avionics skin valve fault
 Figure 004

R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 31-51-21Page 5 1201-203, 1May 01/05 1 1 1CES 1

 Pack 1(2) overheat
 Figure 005

R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 31-51-21Page 6 1201-203, 1May 01/05 1 1 1CES 1

 Pack 1(2) fault
 Figure 006

R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 31-51-21Page 7 1201-203, 1May 01/05 1 1 1CES 1

 Pack 1(2) controller fault
 Figure 007

R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 31-51-21Page 8 1201-203, 1May 01/05 1 1 1CES 1
　
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