R 1EFF : 401-499, 1 31-60-00Page 314 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-press the line key adjacent to the DU X LOAD indication
4. On the MCDU:
-press the line key adjacent to ACCESS X LOAD
5.
On the MCDU:
- obey the instructions refered to as: INITIAL CONDITIONS and press the line key adjacent to START X LOAD
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
-the page DMC3 DU X LOAD comes intoview
-make sure that on the F/O PFD DU (F/O ND 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 First Officer's PFD DU (ND DU): a large white L comes into view on the screen
On the PFD F/O (ND F/O) display unit:
-
the message SELF TEST IN PROGRESS comes into view and remains 40s On the MCDU:
-
the message PFD F/O (ND F/O): X LOAD COMPLETED is displayed in green On the PFD F/O (ND F/O) 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 F/O (ND F/O) 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 F/O (ND F/O) X LOAD ABORTED, then try again once from step 1. If the new result is X LOAD ABORTED, remove the PFD DU (the ND DU) and return it to the shop for repair.
R 1EFF : 401-499, 1 31-60-00Page 315 1 1 Aug 01/05 1 1 1CES 1
5. Close-up
________ Subtask 31-60-00-860-091
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 316 1 1 Aug 01/05 1 1 1CES 1 TASK 31-60-00-610-003
1. Reason for the Job
X LOADING Procedure of the DMC1 __________________ 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 31-60-00-869-067
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)
R 1EFF : 401-499, 1 31-60-00Page 317 1 1 Aug 01/05 1 1 1CES 1 Subtask 31-60-00-865-058
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
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM 指示/記錄系統(tǒng) 7(70)
