-------------------------------------------------------------------------------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.
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-------------------------------------------------------------------------------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.
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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.
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Avionics blower fault
Figure 001
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Avionics extract fault
Figure 002
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Avionics system fault
Figure 003
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Avionics skin valve fault
Figure 004
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Pack 1(2) overheat
Figure 005
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Pack 1(2) fault
Figure 006
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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 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 指示/记录系统 6(11)
