R  EFF : 001-049, 101-105, 107-107, 151-199, 49-00-00Page 227 201-210, Config-2 Aug 01/05
 CES
 (3) De-energize the ground service network (Ref. TASK 24-42-00-862-001), if not longer necessary.
 NOTE : Make sure that the APU air intake-flap is closed, before you
____ set the BAT 1 and BAT 2 pushbutton switches to the off position, if necessary.
R  EFF : 001-049, 101-105, 107-107, 151-199, 49-00-00Page 228 201-210, Config-2 Aug 01/05
 CES  TASK 49-00-00-860-009- 01
 1. Reason for the Job
 APU Shutdown by Batteries (131-9(A)) __________________ Self Explanatory
 2. Job Set-up Information______________________ Not Applicable __________
3. Job Set-up
 Subtask 49-00-00-860-122
 A. Not applicable.
 4. Procedure
_________ Subtask 49-00-00-860-123
 A. Shutdown of the APU
 CAUTION : OBEY THE SAFETY PRECAUTIONS.
_______
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the APU section on the panel 25VU: - push the APU MASTER SW pushbutton switch to the off position. On the APU section on the panel 25VU:- the ON legend in the APU MASTER SWpushbutton switch goes off. 
 After the cooldown cycle is complete: - the APU shutdown sequence starts. 
 On the APU section on the panel 25VU: - the AVAIL legend in the APU START pushbutton switch goes off. 
R  EFF : 001-049, 101-105, 107-107, 151-199, 49-00-00Page 229 201-210, Config-2 Aug 01/05
 CES  5. Close-up
________ Subtask 49-00-00-860-124
 A. Put the aircraft back to its initial configuration.
R  EFF : 001-049, 101-105, 107-107, 151-199, 49-00-00Page 230 201-210, Config-2 Aug 01/05
 CES
 TASK 49-00-00-970-001
 Access to the Data Memory Module (DMM) Report (131-9(A))
 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 31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST Menu Page
 3. Job Set-up
__________ Subtask 49-00-00-861-063
 A. Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002)
 Subtask 49-00-00-865-134
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
R  EFF : 001-049, 101-105, 107-107, 151-199, 49-00-00Page 231 201-210, Config-2 Aug 01/05
 CES  Subtask 49-00-00-860-135
 C. Aircraft Maintenance Configuration
 (1)
 On C/B panel 121VU, pull the circuit breaker AIDS/DMU 4TV (K15).
 (2)
 On the overhead panel push the APU MASTER SW p/bsw (the blue ON legend comes on).
 (3)
 Do the procedure to get the SYSTEM/REPORT TEST item APU (Ref. TASK 31-32-00-860-001).
 4. Procedure
_________ Subtask 49-00-00-970-050
 A. Get access to the DMM data
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:  On the MCDU display:
 -
push the line key adjacent to  - the APU page comes on.
 the APU indication.
 -
push the NEXT page p/bsw.
 -
push the line key adjacent to  - the SERVICE DATA page comes on.
 the SERVICE DATA indication.
 -
push the line key adjacent to  - the DMM DATA page comes on.
 the DMM indication.
 5. Close-up
________ Subtask 49-00-00-860-136
 A. Aircraft Maintenance Configuration
 (1)
 On the overhead panel push the APU MASTER SW p/bsw (the blue ON legend goes off).
 (2)
 On C/B panel 121VU, push the circuit breaker AIDS/DMU 4TV (K15).
R EFF : 001-049, 101-105, 107-107, 151-199, 49-00-00Page 232 201-210, Config-2 Aug 01/05 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 机载辅助动力 AIRBORNE AUXILIARY POWER1(106)