Operational Check of Correct Operation of EFIS and ECAM DMC Automatic and Manual Transfer

TASK 31-60-00-710-005-A
Operational Check of Correct Operation of EFIS and ECAM DMC Automatic and Manual Transfer

ZONE: 210

1. Reason for the Job
Refer to the MPD TASK: 315000-02
OPERATIONAL CHECK OF CORRECT OPERATION OF EFIS AND ECAM DMC AUTOMATIC AND MANUAL TRANSFER
To make sure that these functions are correct:

Automatic PFD/ND Transfer
Manual PFD/ND Transfer
Manual ECAM/ND Transfer
Manual DMC1 and DMC2 to DMC3 Switching
Automatic SD/EWD Transfer

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 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure

3. Job Set-up
Subtask 31-60-00-860-092-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 the center pedestal, on SWITCHING panel 8VU, make sure that all the selector switches are in the NORM position.

Subtask 31-60-00-865-070-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
49VU	EIS/ECAM DU/UPPER/SWTG	24WT1	E06
49VU	EIS/ECAM DU/UPPER/SPLY	13WT1	E05
49VU	EIS/PFD CAPT/SWTG	22WT1	E04
49VU	EIS/PFD/CAPT/SPLY	11WT1	E03
49VU	EIS/ND CAPT/SWTG	23WT1	E02
49VU	EIS/ND CAPT/SPLY	12WT1	E01
** 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/ECAM DU/LOWER/SPLY	13WT2	R11
121VU	EIS/ECAM DU/LOWER/SWTG	24WT2	R10
121VU	EIS/DMC2/SWTG	21WT2	R08
121VU	EIS/ND/F/O/SWTG	23WT2	R06
121VU	EIS/PFD/F/O/SWTG	22WT2	R05
121VU	EIS/ND/F/O	12WT2	R04
121VU	EIS/PFD/F/O	11WT2	R03
122VU	ELEC/AC/BUS1/CTL	17XN1	V25

Subtask 31-60-00-869-073-A ** ON A/C NOT FOR ALL

C. On panels 301VU and 500VU and on the ECAM control panel:
- Set all the potentiometers to the center position.

4. Procedure
Subtask 31-60-00-710-059-A ** ON A/C NOT FOR ALL

A. Automatic PFD/ND Transfer

NOTE: This test is for the CAPT side. For the F/O side, you can use the indications between parentheses.

ACTION	RESULT
1.On panel 301VU (500VU):
Set the PFD potentiometer to OFF.	The PFD stops and the PFD image moves to the ND.
Set the PFD potentiometer to the center position.	The message SELF TEST IN PROGRESS (MAX 40 SECONDS) comes into view. The ND image then comes back on the PFD.

Subtask 31-60-00-710-060-A ** ON A/C NOT FOR ALL

B. Manual PFD/ND Transfer

NOTE: This test is for to the CAPT side. For the F/O side, you can use the indications between parentheses.

ACTION	RESULT
1.On panel 301VU (500VU):
Push and release the PFD/ND/XFR pushbutton switch.	On the PFD: * The ND image comes into view. On the ND: * The PFD image comes into view.
Push and release the PFD/ND/XFR pushbutton switch again.	The PFD and ND images go back to the initial positions.

Subtask 31-60-00-710-061-A ** ON A/C NOT FOR ALL

C. Manual ECAM/ND Transfer

ACTION	RESULT
1.On the center pedestal, on SWITCHING panel 8VU:
Set the ECAM/ND/XFR selector switch to CAPT.	On the lower ECAM DU, the message "ECAM ON ND" comes into view and the system page comes into view on the CAPT ND.
Set the ECAM/ND/XFR selector switch to F/O.	On the lower ECAM DU, the message "ECAM ON ND" comes into view and the system page comes into view on the F/O ND.
Set the ECAM/ND/XFR selector switch to NORM.	The DUs go back to the initial configurations.

Subtask 31-60-00-710-062-A ** ON A/C NOT FOR ALL

D. Manual Switching of DMC1 and DMC2 to DMC3

ACTION	RESULT
1.On overhead C/B panel 49VU:
Open circuit breaker 10WT1.	On the CAPT PFD and ND, the INVALID DATA message comes into view. On the upper ECAM DU, the EIS DMC 1 FAULT indication comes into view. On the glareshield, the MASTER CAUT lights come on. You can hear a chime.
2.On the center pedestal, on SWITCHING panel 8VU:
Set the EIS DMC selector switch to CAPT 3.	On the CAPT PFD and ND, the INVALID DATA message goes out of view and the DUs show the initial images.
3.On the main instrument panel, on panel 301VU:
Push and release the PFD/ND XFR pushbutton switch.	On the PFD: * The ND image comes into view. On the ND: * The PFD image comes into view.
Push and release the PFD/ND XFR pushbutton switch again.	The DUs go back to the initial configuration.
4.On rear C/B panel 121VU:
Open circuit breaker 10WT3.	On the CAPT ND and PFD, the INVALID DATA message comes into view. On the upper ECAM DU, the indications that follow come into view: * EIS DMC 1 FAULT * --- DMC 3 FAULT.
5.On rear C/B panel 122VU:
Open circuit breaker 17XN1.	On the CAPT PFD and ND: * After approximately 35 seconds, the INVALID DATA message goes out of view and the DUs show the images. On the upper ECAM DU: * The ELEC AC BUS 1 FAULT indication comes into view. * The EIS DMC 1 FAULT indication stays in view. * The DMC 3 FAULT indication goes out of view.
6.On rear C/B panels 121VU and 122VU:
Close circuit breaker 10WT3 and 17XN1.	On the DUs, the related image of each DU stays in view. On the upper ECAM DU, the ELEC AC BUS 1 FAULT indication goes out of view.
7.On overhead C/B panel 49VU:
Close circuit breaker 10WT1.	On the upper ECAM DU: * After approximately 35 seconds, the EIS DMC 1 FAULT indication goes out of view. On the glareshield, the MASTER CAUT lights go off.
8.On SWITCHING panel 8VU:
Set the EIS DMC selector switch to NORM.	There is no change.
9.On rear C/B panel 121VU:
Open circuit breaker 10WT2.	On the F/O PFD and ND, the INVALID DATA message comes into view. On the upper ECAM DU, the EIS DMC 2 FAULT indication comes into view. On the glareshield, the MASTER CAUT lights come on. You can hear a chime.
10.On SWITCHING panel 8VU:
Set the EIS DMC selector switch to F/O 3.	On the F/O PFD and ND, the INVALID DATA message goes out of view and the DUs show the images.
11.On rear C/B panel 121VU:
Close circuit breaker 10WT2.	On the upper ECAM DU: * After approximately 35 seconds, the EIS DMC 2 FAULT indication goes out of view. On the glareshield, the MASTER CAUT lights go off.
12.On the central pedestal, on SWITCHING panel 8VU:
Set the EIS DMC selector switch to NORM.	There is no change.
13.On ELEC panel 35VU: Release the AC ESS FEED pushbutton switch. Push the AC ESS FEED pushbutton switch.	On ELEC panel 35VU: The ALTN legend of the AC ESS FEED pushbutton switch comes on. The ALTN legend of the AC ESS FEED pushbutton switch goes off.
14.On the ECAM control panel: Push the ELEC key to get the ELEC page.	On the lower ECAM DU: The essential transformer rectifier does not supply the DC essential busbar (the normal configuration comes into view).
15.If the essential transformer rectifier continues to supply the DC essential busbar, on the aircraft power center, on rear C/B panel 123VU: Open and close circuit breaker 1XC. Make sure that the essential transformer rectifier does not supply the DC essential busbar.

Subtask 31-60-00-710-063-A ** ON A/C NOT FOR ALL

E. Automatic Upper DU/Lower DU Transfer

ACTION	RESULT
1.On the center pedestal, on the ECAM control panel:
Set the upper display potentiometer to OFF.	The upper ECAM DU stops. The ENGINE/WARNING image goes to the lower ECAM DU.
2.On the center pedestal, on the ECAM control panel:
Set the upper display potentiometer to ON.	The DUs go back to the initial configurations.

5. Close-up
Subtask 31-60-00-869-074-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) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.01 00:37:58 UTC