X LOADING Procedure of the DMC1 to the PFD CAPT, ND CAPT, the EWD or the SD

TASK 31-60-00-610-001-A
X LOADING Procedure of the DMC1 to the PFD CAPT, ND CAPT, the EWD or the SD

ZONE: 210
FIN: 1WT1 ** ON A/C NOT FOR ALL
FIN: 2WT1 ** ON A/C NOT FOR ALL
FIN: 3WT1 ** ON A/C NOT FOR ALL
FIN: 4WT1 ** ON A/C NOT FOR ALL

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
210	CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD

B. Referenced Information

REFERENCE	DESIGNATION
TASK 24-41-00-861-002-A	Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01	Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02	Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A	De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01	De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02	De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 31-32-00-860-008-A	Procedure to Get Access to the SYSTEM REPORT/TEST/INST Page
TASK 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure

3. Job Set-up
Subtask 31-60-00-869-065-A ** ON A/C NOT FOR ALL

A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002)
(2) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001)
(3) On one MCDU, get the SYSTEM REPORT/TEST INST menu page (Ref. AMM TASK 31-32-00-860-008)
(4) On the switching panel 8VU, make sure that all the switches are set to NORM.

Subtask 31-60-00-865-056-A ** ON A/C NOT FOR ALL

B. Make sure that this(these) circuit breaker(s) is(are) closed:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
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
** ON A/C NOT FOR ALL
49VU	EIS/DMC3/SWTG	21WT3	E07
** ON A/C NOT FOR ALL
49VU	EIS/ECAM/CTL/PNL	15WT	E11
49VU	EIS/DMC1/SPLY	10WT1	E10
49VU	EIS/DMC3/STBY/SPLY	14WT1	E09
49VU	EIS/DMC1/SWTG	21WT1	E08
** ON A/C NOT FOR ALL
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 ** ON A/C NOT FOR ALL

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:: Push the line key adjacent to the EIS1 indication.	On the MCDU: The DMC1 main menu page comes into view. On the CAPT PFD, CAPT ND, EWD and SD Display Units: The green MAINTENANCE MODE message comes into view.
2.On the MCDU: Push the line key adjacent to the PIN PROG/STATUS AND XLOAD indication.	On the MCDU: The page DMC1 PIN PROG/STATUS AND XLOAD comes into view.
3.On the MCDU: Push the line key adjacent to the DU XLOAD indication.	On the MCDU: The page DMC1 DU XLOAD comes into view. 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: Push the line key adjacent to ACCESS XLOAD.	On the MCDU: The page DMC1 DU XLOAD comes into view with initial conditions.
5.On the MCDU: Obey the instructions refered to as: INITIAL CONDITIONS and press the line key adjacent to START XLOAD.	On the MCDU: The page DMC1 DU XLOAD comes into view with the message TRANSFER IN PROGRESS DMC1 TO PFD CAPT DMC1 TO ND CAPT DMC1 TO EWD DMC1 TO SD MAX 20 MINUTES On the Captain's PFD DU (ND, SD or EWD DU): a large white L comes into view on the screen.
6.XLOAD process Wait for 20 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: Push the line key adjacent to the RETURN indication.	On the MCDU: The page DMC1 DU XLOAD comes into 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: Push 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 ** ON A/C NOT FOR ALL

A. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(2) Make sure that the work area is clean and clear of tools and other items.
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.01 00:37:39 UTC