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- push the line key adjacent to  - the TEST page comes into view.
 the TEST indication.
 12. On the TEST page:  On the TEST page:
 - push the line key adjacent to  - the REQUEST indication goes out of
 the REQUEST VHF3 LINK  view
 indication.  - the IN PROGRESS indication comes into
 view
 - at the end of the test, the OK
 indication comes into view.
 13. On the MCDU 1:
 - push the line key adjacent to
 the RETURN indication until
 the ATSU DATALINK page comes
 into view.
 14. On the MCDU 1:  On the MCDU1:
 - push the MCDU MENU key.  - the MCDU MENU page comes into view. 

R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 5. Close-up
________
 Subtask 46-21-00-860-053

 A. Put the aircraft back to its initial configuration.
 (1) On the MCDU 1, fully decrease the brightness of the MCDU screen (display off).
 (2) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
 Subtask 46-21-00-862-050

 B. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

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 TASK 46-21-00-740-001

 BITE Test of the ATIMS
 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 31-32-00-860-003 Procedure to Get Access to the SYSTEM REPORT/TEST/COM Page 31-32-00-860-013 Procedure to Get Access to the SYSTEM
 REPORT/TEST/INFO SYS Page
 31-60-00-860-001 EIS Start Procedure
 31-60-00-860-002 EIS Stop Procedure

R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 Post SB 46-1013 For A/C 151-156,201-209,
 46-21-00-991-007 Fig. 505

R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 3. Job Set-up
__________
 Subtask 46-21-00-861-072

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

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 46-21-00Page 542 1401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,

 

 Subtask 46-21-00-860-050-A
 B. Aircraft Maintenance Configuration
 (1)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (2)
 Do the procedure to get the SYSTEM REPORT/TEST/INFO SYS page (Ref. TASK 31-32-00-860-013).

 **ON A/C 151-154, 201-207,
 Subtask 46-21-00-860-050
 B. Aircraft Maintenance Configuration
 (1)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (2)
 Do the procedure to get access to the SYSTEM REPORT/TEST/COM page (Ref. TASK 31-32-00-860-003).

 

R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 46-21-00-865-050
 C. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/MCDU/1 11CA1 B01 49VU SDAC/1/SPLY 3WV F04 49VU FWS/FWC1/SPLY 3WW F01 121VU CFDS/CFDIU/SPLY 2TW J18 121VU ATSU 1 3TX1 L16 121VU ATSU 1/SWTG 5TX1 L15 121VU COM NAV/VHF/3 2RC3 L05 121VU AUTO FLT/MCDU/2 11CA2 N20 121VU EIS/FWC2/SPLY 2WW Q07
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 46-21-00Page 543 1401-499, 1Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------**ON A/C 151-199, 201-210,
 121VU AIDS/DMU 4TV K15 R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 4. Procedure
_________
 **ON A/C 151-154, 201-207,

 Subtask 46-21-00-740-050
 A. BITE Test of the ATIMS
 NOTE : During the test, obey the instructions on the MCDU.

____
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
　
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