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,
R 1EFF : 401-499, 1 31-60-00Page 311 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
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.
R 1EFF : 401-499, 1 31-60-00Page 312 1 1 Aug 01/05 1 1 1CES 1 TASK 31-60-00-610-009
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.
R 1EFF : 401-499, 1 31-60-00Page 313 1 1 Aug 01/05 1 1 1CES 1 Subtask 31-60-00-865-068
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 -------------------------------------------------------------------------------
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 指示/记录系统 7(69)
