-
test of the output stage of the BAT FAULT warning control,

 -
test of the output stage of the RAT & CSM/G warning control,

 -
test of the output stage of the APU start inhibition control,

 -
test of specific external wiring of the BCL,

 -watchdog test.

 B.
 Test from the CFDS The same tests as those applicable to power up are performed, plus a test for correct operation of the FAULT legend of BAT1(2) pushbutton switches and of RAT & EMER GEN annunciator which lasts 6 seconds.

 C.
 Monitoring of the BCL System When the BCL is supplied, the peripheral circuits are monitored through validation of the inputs (for example the position of the auxiliary contact of the battery contactor shall be coherent with the order).

 D.
 Communication with the MCDU and/or ECAM When a class 1 failure occurs, a BITE message is transmitted to the MCDU via an ARINC 429 serial data link and a failure indication is transmitted to the ECAM. In case of BAT FAULT warning, the crew is informed by:

 -a local amber warning on the overhead panel,

 -the single chime,

 -an amber caution on the main instrument panel.
 The warning page is displayed on the upper ECAM display unit and, at the
 same time, the ELEC page is displayed on the lower ECAM display unit:
 (Ref. Fig. 004, 005)

 NOTE : For some more information, see ATA (Ref. 31-51-00).
____

 INTENTIONALLY BLANK

R 1 1

24-38-00Page 17
1 1 Feb 01/00 1 1 1CES 1

 BAT 1 FAULT - Lower and Upper ECAM Display Unit Figure 004 (SHEET 1)
 1EFF : 1 1R 1CES  ALL  1 11 1 24-38-00 Page 18 Feb 01/00

 BAT 1 FAULT - Lower and Upper ECAM Display Unit
 Figure 004 (SHEET 2)
 1EFF :  ALL  1  24-38-00 Page 19 
1  1  Feb 01/00
 1  1
 1CES  1

 BAT 2 FAULT - Lower and Upper ECAM Display Unit
 Figure 005 (SHEET 1)
 1EFF :  ALL  1  24-38-00 Page 20 
1  1  Feb 01/00
 1  1
 1CES  1

 BAT 2 FAULT - Lower and Upper ECAM Display Unit
 Figure 005 (SHEET 2)
 1EFF :  ALL  1  24-38-00 Page 21 
1  1  Feb 01/00
 1  1
 1CES  1

 In case of BCL FAULT warning, the crew is informed by the BCL FAULT message displayed on the upper ECAM display unit whereas the ELEC page is displayed on the lower ECAM display unit. Class 3 failures can be read using the CFDS. Maintenance personnel must localize the failures by means of CFDS readouts (Ref. Fig. 006)
 NOTE : If a BAT pushbutton switch is released (OFF position), the BAT OFF
____ warning is displayed on the upper ECAM display unit whereas the ELEC page is displayed on the lower ECAM display unit.
 The BITE messages generated by the BCL's are:
 -------------------------------------------------------------------------------| ATA REF. | MESSAGE | CLASS | COMMENT | |----------|----------------------|-------|-----------------------------------| | 24-38-51 | BATTERY 1 (or 2) | I | Battery thermal runaway or | | | | | internal short circuit | |----------|----------------------|-------|-----------------------------------| | 24-28-51 | STATIC INVERTER 3XB | I | Failure of static inverter | |----------|----------------------|-------|-----------------------------------| | 24-38-55 | CHECK CONTACTOR | I | Failure of battery contactor | | | 6PB1 (or 6PB2) | | control of status circuit | | | BCL1 (or BCL2) | | | | | CIRCUIT | | | |----------|----------------------|-------|-----------------------------------| | 24-38-00 | PUSHBUTTON 7PB1 | I | Failure of control P/BSW circuit | | | (or 7PB2) / BCL1 | | | | | (or BCL2) CIRCUIT | | | |--------- |----------------------|-------|-----------------------------------| | 24-38-00 | SHUNT 3PB1 (or 3PB2) | I | Failure of current acquisition | | | /BCL1 (or BCL2) | | circuit | | | CIRCUIT | | | |--------- |----------------------|-------|-----------------------------------| | 24-38-00 | FUSE 4PB1 (or 4PB2) | I | Fuse blown | |----------|----------------------|-------|-----------------------------------| | 24-38-34 | BCL1 (or BCL2) | I | Failure of: | | | | | -analogic/numeric converter | | | | | -battery contactor control | |----------|----------------------|-------|-----------------------------------| | 24-38-00 | CHECK DC BAT BUS | I | Failure of BCL BAT BUS supply | | | 3PP/BCL1 (or BCL2) | | | |----------|----------------------|-------|-----------------------------------| | 24-38-34 | BCL1 (or BCL2) | III | Failure of: | | | | | -WATCH DOG | | | | | -BAT FAULT control | | | | | -APU START VALID control |
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM ELECTRICAL POWER 電源2(52)