6.
 X LOAD process

-wait for 10 minutes
7. On the MCDU:
-press the line key adjacent to the RETURN indication
8. On the MCDU:
-press the line key adjacent to RETURN
On the MCDU:
-the page DMC3 DU X LOAD comes intoview
 -make sure that on the CAPT PFD DU (ND, EWD,SD DU): the EIS software P/N is amber or empty
On the MCDU:
-
the page DMC3 DU X LOAD comes intoview

On the MCDU:

-
the page DMC3 DU X LOAD comes intoview with the message TRANSFER INPROGRESSOn the Captain's PFD DU (ND, SD or EWD DU): a large white L comes into view on the screen

On the PFD CAPT (ND CAPT, SD or EWD)display unit:

 -
the message SELF TEST IN PROGRESS comes into view and remains 40s On the MCDU:

 -
the message PFD CAPT (ND CAPT, SD or EWD): X LOAD COMPLETEDis displayed in green On the PFD CAPT (ND CAPT, SD or EWD) display unit:

 -make sure that the message MAINTENANCE MODE comes into view
On the MCDU:
-the page DMC3 DU X LOAD comes intoview with, on the same line as the PFD CAPT (ND CAPT, SD or EWD) DU, the EIS software P/N is displayed in green
-to get back to the main menu page
NOTE : If the result of the test gives
____ the amber message PFD CAPT (ND CAPT, SD or EWD) X LOAD ABORTED,
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 -------------------------------------------------------------------------------
ACTION RESULT
 -------------------------------------------------------------------------------then try again once from step 1. If the new result is X LOAD ABORTED, remove the PFD DU (the ND DU, the SD DU or EWD DU) and return it to the shop for repair.
 5. Close-up________
 Subtask 31-60-00-860-090
 A. Put the aircraft back to its initial configuration.
 (1)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (2)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

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 1. Reason for the Job
 XLOADING Procedure of the DMC3 to the PFD F/O and ND F/O __________________ 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
 31-32-00-860-008  Procedure to Get Access to the SYSTEM
 REPORT/TEST/INST Page 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
 3. Job Set-up
__________ Subtask 31-60-00-869-072
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002)

 (2)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001)

 (3)
 On one MCDU, get the SYSTEM REPORT/TEST INST menu page (Ref. TASK 31-32-00-860-008)

 (4)
 On the switching panel 8VU, put the EIS DMC selector switch to F/O 3.

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 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU EIS/ECAM/CTL/PNL 15WT E12 49VU EIS/DMC1/SPLY 10WT1 E11 49VU EIS/DMC3/STBY/SPLY 14WT1 E10 49VU EIS/DMC1/SWTG 21WT1 E09 49VU EIS/DMC3/SWTG 21WT3 E07 121VU EIS/DMC3/SPLY 10WT3 Q09 121VU EIS/DMC2/SPLY 10WT2 Q08 121VU EIS/DMC2/SWTG 21WT2 R08
 4. Procedure
_________
 Subtask 31-60-00-610-059
 A. Crossloading of the DMC3 to the F/O PFD (ND)
 NOTE : The procedure is for the FO PFD. For the FO ND, use the
____
 indications between parentheses.

 NOTE : Crossloading is possible only if the target DUs (DUs to which you
____ crossload data) have an EIS software PN different than that of the source DMC. You can crossload data to all the DUs at the same time.
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
　
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