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时间:2011-03-25 12:26来源:蓝天飞行翻译 作者:admin
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R 1EFF : 401-499, 1 31-60-00Page 301 1 1 Aug 01/05 1 1 1CES 1 Subtask 31-60-00-865-056


 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 31-60-00-610-050
 A. Crossloading of the DMC1 data to the CAPT PFD, CAPT ND, EWD or SD
 NOTE : The procedure is for the Captain's PFD. For the Captain's ND, for
____ the ECAM SD or EWD, use the information between parentheses.
 NOTE : Crossloading is possible only if the target DU's (DU to which you
____ crossload data) have an EIS software P/N different than the source DMC. You can crossload data to all DUs at the same time.
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU::
-press the line key adjacent to the EIS1 indication
2. On the MCDU:
-press the line key adjacent to the PIN PROG/STATUS AND XLOAD indication On the MCDU:
-
the DMC1 main menu page comes intoview. On the CAPT PFD, CAPT ND, EWD and SD Display Units:

 -
the green MAINTENANCE MODE message comes into view.

On the MCDU:

-
the page DMC1 PIN PROG/STATUS ANDXLOAD comes into view


R 1EFF : 401-499, 1 31-60-00Page 302 1 1 Aug 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
3. On the MCDU:  On the MCDU:
 - press the line key adjacent to the DU XLOAD indication  - the page DMC1 DU XLOAD comes intoview
 - make sure that on the CAPT PFD DU
 (ND, EWD,SD DU): the EIS software P/N is amber or empty
 4. On the MCDU:  On the MCDU:
 - press the line key adjacent to ACCESS XLOAD  - the page DMC1 DU XLOAD comes intoview with initial conditions
 5. On the MCDU:  On the MCDU:
 - obey the instructions refered to as: INITIAL CONDITIONS and press the line key adjacent to START XLOAD  - the page DMC1 DU X LOAD comes intoview with the message TRANSFER INPROGRESSDMC1 TO PFD CAPT
 DMC1 TO ND CAPT
 DMC1 TO EWD
 DMC1 TO SD
 MAX 10 MINUTES
 On the Captain's PFD DU (ND, SD or EWD DU): a large white L comes into view on the screen
 6. X LOAD process - wait for 10 minutes maximum  On the MCDU:- DMC1 DU XLOAD comes into view with
 INTEGRITY CHECK
 PFD CAPT
 ND CAPT
 EWD
 SD
 MAX 60 SECONDS
 On the PFD CAPT (ND CAPT, SD or EWD) display unit: - the message SELF TEST IN PROGRESS (MAX 40 SECONDS) comes into view - make sure that the message MAINTENANCE MODE comes into view
 On the MCDU:
 - the message PFD CAPT (ND CAPT, SD or EWD): XLOAD COMPLETED is displayed in
 green
 7. On the MCDU:  On the MCDU: 

R 1EFF : 401-499, 1 31-60-00Page 303 1 1 Aug 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-press the line key adjacent to - the page DMC1 DU X LOAD comes into
 the RETURN indication  view with, on the same line as the PFD CAPT (ND CAPT, SD or EWD) DU, the EIS software P/N is displayed in green
 8. On the MCDU:
 -press the line key adjacent to
 RETURN 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) XLOAD ABORTED, then
 try again once from step

 1. If the new result is
 XLOAD 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 31-60-00-860-085
 A. Put the aircraft back to its initial configuration.
 (1)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (2)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (3)
 De-energize the aircraft electrical circuits
 
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