A320飞机维护手册 AMM Communications 通讯3(80)

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 (Ref. Fig. 065A) **ON A/C 151-199,
 (Ref. Fig. 065B) **ON A/C 201-210,
 (Ref. Fig. 065C) **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
 (Ref. Fig. 066, 067, 068)
 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page B8 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 Failure Transmission List
 Figure 060

 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page B9 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 Failure Transmission List
 Figure 061

 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page B10 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 Failure Transmission List
 Figure 062

 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page B11 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 Failure Transmission List
 Figure 063

 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page B12 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 Failure Transmission List
 Figure 064

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page B13 1201-299, 1Config-1 Aug 01/05 1 1 1CES 1

 Failure Transmission List
 Figure 065

R 1EFF : 001-049, 101-105, 1 23-73-00Page B14 1 1 Config-1 Aug 01/05 1 1 1CES 1

 Failure Transmission List
 Figure 065A

R 1EFF : 051-099, 211-299, 1 23-73-00Page B15 1 1 Config-1 Aug 01/05 1 1 1CES 1

 Failure Transmission List
 Figure 065B

R 1EFF : 151-199, 1 23-73-00Page B16 1 1 Config-1 Aug 01/05 1 1 1CES 1

 Failure Transmission List
 Figure 065C

R 1EFF : 201-210, 1 23-73-00Page B17 1 1 Config-1 Aug 01/05 1 1 1CES 1

 Failure Transmission List
 Figure 066

 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page B18 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 Failure Transmission List
 Figure 067

 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page B19 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 Failure Transmission List
 Figure 068

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page B20 1201-299, 1Config-1 Aug 01/05 1 1 1CES 1 **ON A/C 001-049, 051-099, 101-105, 201-299,

 F. CIDS Power-Up Test
 (1)
 Conditions of Power-Up Test initialization

 (a)
 A/C configuration: A- A/C on ground with all cabin doors closed B- A/C on ground with all engines stopped and at least one cabin door open

 (b)
 The computer must be de-energized for a time of:

 -
A/C in config. A-: 10 sec

 -
A/C in config. B-: 10 sec

 

 

 (2)
 Progress of Power-Up Test

 (a)
 Duration:

 -
A/C in config. A-: approx. 60 sec

 -
A/C in config. B-: approx. 180 sec

 

 (b)
 Flight compartment repercussions (ECAM warning, audio warning, pushbutton flashing..if any..): A/C in config. A- or B-.

 

 1_ ECAM maintenance status:
 'CIDS 1' and/or 'CIDS 2' come on and go off after completion
 either:
 - at the same time or,
 - seperately or,
 - approx. 30 sec after completion of the power-up test.
 2_ Audio Control Panel:
 - ATT light flashes for approx. 60 sec
 NOTE : The following repercussions can be observed in the____
 cabin:
 A/C in config. A-:
 - after approx. 25 sec cabin lights go off for approx.
 2 sec
 - two chimes are heard 30 sec after power-up test
 initialization
 A/C in config. B-:
 - after approx. 25 sec, cabin lights go off for approx.
 2 sec 

R 1EFF : 001-049, 051-099, 101-105, 201-299, 1 23-73-00Page B21 1 1 Config-1 Aug 01/05 1 1 1CES 1

 -after approx. 35 sec, call/seatrow numbering lights and signs flash for approx. 10/15 sec (boardind config.)
 -two chimes are heard approx. 120 sec after power-up test initialization
 (3) Results of Power-Up Tests Flight compartment repercussions (if any) in case of test pass/test failed.
 (a)
 Test pass :

 -none

 (b)
 Test failed :

 1_ In case of CIDS 1 or CIDS 2 failure:
 - ECAM maintenance status
 'CIDS 1' or 'CIDS 2' white indication

 2 In case of CIDS 1 and CIDS 2 failure:
_
 -Master caution light comes on
 -ECAM warning: 'COM CIDS 1 + 2 FAULT' 'CIDS' (INOP system)
 **ON A/C 151-199,
　
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