A320飞机维护手册 AMM 指示/记录系统 3(120)

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R  The procedure is as follows: 
R  - select '<LRU IDENT' on the DMU Menu, 
R  - the DMU LRU Identification Page comes on. 
R 
R  In line # 3 the aircraft identification, the date and the time is 
R  presented. 
R  In line # 5 the DMU part number is presented. 
R 
R  (4) Class 3 Faults 
R  (Ref. Fig. 079A) 
R  The operator may get Class 3 Fault information from the AIDS. 
R  The procedure is as follows: 
R  - select '<CLASS 3 FAULTS' on the DMU Menu, 
R  - the DMU Class III Faults Page comes on. 
R 
R  The class 3 faults from the previous 64 flights including the present 
R  flight are displayed. If more than 4 faults have occured, scrolling 
R  will display the rest of the faults. 
R 
R  (5) DMU Test Functions The operator may initiate test functions via the 
R  MCDU. 
R  (a) Result Power Up Test 
R  (Ref. Fig. 080A) 
R  The procedure is as follows: 
R  - select 'TEST>' on the DMU Menu, 
R  - select '<RESULT POWER UP TEST' on the DMU Test Menu, 
R  - the DMU POR BIT Result Page displays the message 'ALL PASSED' 
R  or the registered failure during initialisation of AIDS DMU.

 1EFF : 151-199, 201-210, 1 31-36-00Page B71 1 1 Config-2 May 01/05 1 1 1CES 1 1EFF : 151-199, 201-210, 1 31-36-00Page B72 1 1 Config-2 May 01/05 1 1 1CES 1 AIDS INTERCONNECTION ((FDIMU, DAR)) - MAINTENANCE PRACTICES

R 
R  (b) Create Test 
R  (Ref. Fig. 081A) 
R  The procedure is as follows: 
R  - select 'TEST>' on the DMU Menu, 
R  - select '<CREATE TEST' on the DMU Test Menu, 
R  - the DMU POR BIT Result Page displays the message 'POR BIT 
R  UNDERWAY WAIT FOR RESULTS'. 
R  The CFDS creates an actual POR BIT Test. The actual results are 
R  displayed on the MCDU. The message 'ALL PASSED' or the actual 
R  failures are displayed. 
R  (6) Not Applicable 
R  (7) Not Applicable 
R  (8) Not Applicable 
R  (9) Not Applicable

 

___________________________________________________________ R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
 TASK 31-36-00-740-004 Update of the APU Hours and Cycles in the DMU after APU, ECB or DMU Replacement NOTE : BEFORE UPDATE OF APU HOURS AND CYCLES THE ECB MUST BE ENERGIZED (C/B
____
 PUSHED AND GROUND POWER SWITCHED ON).

 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
 3. Job Set-up
__________
 Subtask 31-36-00-860-052

 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002)

 (2)
 On the Overhead Panel 25VU push the APU MASTER SW button (the blue light indicator ON comes on).

 1EFF : ALL 1 31-36-00Page 201 1 1 May 01/05 1 1 1CES 1 Subtask 31-36-00-865-058

 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU AIDS/DMU 4TV K15 121VU APU/ECB/SPLY 1KD L41
 4. Procedure
_________

R **ON A/C 001-049, 051-099, 101-105,
 Subtask 31-36-00-740-052
 A. Enter the APU hours and cycles data into the DMU.
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the MCDU:  On the MCDU display:
 -
Push the MCDU MENU mode key. - The MCDU MENU page comes into view.

 -
Push the line key adjacent to the  - The AIDS page comes into view.
 < AIDS indication.

 -
Push the line key adjacent to the  - The AIDS DMU PROGRAMMING page comes < PROGRAMMING indication. into view.
　
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