Procedure to Update the DIU Database Software
TASK 23-34-00-610-001-A
Procedure to Update the DIU Database Software
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 23-34-00-010-054-A ** ON A/C NOT FOR ALL
Subtask 23-34-00-970-050-B ** ON A/C NOT FOR ALL
Subtask 23-34-00-280-053-A ** ON A/C NOT FOR ALL
Subtask 23-34-00-860-055-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:12:08 UTC
Procedure to Update the DIU Database Software
FIN: 190MH ** ON A/C NOT FOR ALL
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 824 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 23-36-00-710-001-A | Operational Test of the Passenger Entertainment (Video) |
| TASK 23-73-00-861-001-A | Energize the Cabin Intercommunication Data System (CIDS) |
| TASK 23-73-00-862-001-A | De-energize the Cabin Intercommunication Data System (CIDS) |
| 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 |
| TASK 34-10-00-860-002-A | ADIRS Start Procedure |
| TASK 34-10-00-860-004-A | Inertial Reference (IR) Alignment-Procedure |
| TASK 34-10-00-860-004-A-02 | Inertial Reference (IR) Alignment-Procedure to do a Check of the Links between each Flight Management and Guidance Computer (FMGC) and the three Air Data/Inertial Reference Units (ADIRUs) |
| TASK 34-10-00-860-005-A | ADIRS Stop Procedure |
| TASK 52-41-00-010-002-A | Open the Avionics Compartment Doors for Access |
| TASK 52-41-00-410-002-A | Close the Avionics Compartment Doors after Access |
Subtask 23-34-00-010-054-A ** ON A/C NOT FOR ALL
A. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the access door 824.
(2) Open the access door 824 (Ref. AMM TASK 52-41-00-010-002).
Subtask 23-34-00-860-054-A ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the access door 824.
(2) Open the access door 824 (Ref. AMM TASK 52-41-00-010-002).
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) Do the ADIRS Start Procedure (Ref. AMM TASK 34-10-00-860-002).
(4) Do the IR Alignment Procedure (Ref. AMM TASK 34-10-00-860-004).
(6) Make sure that the Passenger Entertainment System (PES) (Video) is energized (Ref. AMM TASK 23-36-00-710-001).
(7) Make sure that the CD-ROM DIU (190MH1) is in the Digital Interface Unit (DIU) (190MH).
Subtask 23-34-00-865-074-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) Do the ADIRS Start Procedure (Ref. AMM TASK 34-10-00-860-002).
(4) Do the IR Alignment Procedure (Ref. AMM TASK 34-10-00-860-004).
NOTE: For the alignment procedure, make sure that the correct values for the longitude and latitude of the A/C position are shown.
NOTE: During the alignment procedure, make sure that a point of departure and a destination (airport identification) are put in on the MCDU. The point of departure must be where the A/C location is now.
(5) Make sure that the Cabin Intercommunication Data System (CIDS) is energized (Ref. AMM TASK 23-73-00-861-001). (6) Make sure that the Passenger Entertainment System (PES) (Video) is energized (Ref. AMM TASK 23-36-00-710-001).
(7) Make sure that the CD-ROM DIU (190MH1) is in the Digital Interface Unit (DIU) (190MH).
C. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FCU/1 | 9CA1 | B05 |
| 49VU | AUTO FLT/FMGC/1 | 10CA1 | B02 |
| 121VU | AUTO FLT/FCU/2 | 9CA2 | M21 |
| 121VU | AUTO FLT/FMGC/2 | 10CA2 | M17 |
| 2000VU | PES PFIS | 189MH | C07 |
| 2000VU | PES-VIDEO-CABIN-RH AFT | 25MH | C06 |
| 2000VU | PES-VIDEO-CABIN-LH | 23MH | C05 |
| 2000VU | PES-VIDEO-CABIN-RH FWD | 24MH | C04 |
| 2000VU | PES-VIDEO-CABIN-LH FWD | 22MH | C03 |
| 2000VU | PES-VIDEO-CONTROL-VCC | 21MH | C02 |
| 2000VU | PES-VIDEO-CONTROL-MAIN | 20MH | C01 |
Subtask 23-34-00-970-050-B ** ON A/C NOT FOR ALL
CAUTION:
DO NOT REMOVE THE POWER WHILE THE AIRSHOW DATA TRANSFER PROGRAM (ADTP) OPERATES. WHEN THE ADTP IS COMPLETED, THE COPYRIGHT PAGE SHOWS ON THE DISPLAY. IF YOU REMOVE THE POWER BEFORE THE ADTP IS COMPLETED, DAMAGE TO THE DIU 190MH WILL OCCUR.
A. Load the DIU Database Software. | ACTION | RESULT |
|---|---|
| 1.On the circuit breaker panel 2000VU: | |
| The Passenger Visual Information System (PVIS) energizes. |
| 2.On the System Control Unit (SCU) 11MH: | On the SCU 11MH: |
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| | On the SCU 11MH, on the monitor:
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| 3.On the SCU 11MH, on the MODE SELECT area: | On the SCU 11MH, on the monitor: |
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| 4.On the SCU 11MH: | On the SCU 11MH: |
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| 5.On the SCU 11MH, the MANUAL CONTROL board, ALL ZONES: | On the SCU 11MH, the MANUAL CONTROL board, ALL ZONES: |
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| 6.On the SCU 11MH, the MANUAL CONTROL board, ALL ZONES: | On the SCU 11MH, the MANUAL CONTROL board, ALL ZONES: |
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| | On the SCU 11MH, on the monitor:
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| 7.On the DIU 190MH: | On the DIU 190MH: |
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| 8.On the DIU 190MH: | On the DIU 190MH: |
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| 9.On the DIU 190MH: | On the DIU 190MH: |
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NOTE: When you remove or install a DVD-ROM or CD-ROM disk, make sure that you do not scratch or put fingerprints on the surfaces of the disk. NOTE: Do not push the front of the disk tray to retract it. This can damage the mechanism. |
| 10.On the DIU 190MH: | On the DIU 190MH: |
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| 11.On the DIU 190MH, on the modification plate: | On the DIU 190MH, on the modification plate: |
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NOTE: You can find the modification data on the modification plate on the front panel of the DIU 190MH. |
| 12.On the circuit breaker panel 2000VU: | |
| The PVIS de-energizes. |
| 13.On the circuit breaker panel 2000VU: | |
| The PVIS energizes. |
| 14.Obey the rules that follow: | |
NOTE: IF THE OPERATION OF THE ADTP STOPS BEFORE THE COPYRIGHT PAGE COMES INTO VIEW, YOU MUST WAIT FOR A MINIMUM OF 10 MINUTES BEFORE YOU CAN REMOVE THE POWER. | |
| 15.On the SCU 11MH, on the monitor: | On the SCU 11MH, on the monitor: |
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| 16.On the SCU 11MH, on the monitor: | On the SCU 11MH, on the monitor: |
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| 17.On the SCU 11MH, on the monitor: | On the SCU 11MH, on the monitor: |
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NOTE: The subsequent step 18 is only for the ADTP with the revision status REV A. |
| 18.On the SCU 11MH, on the monitor: | On the SCU 11MH, on the monitor: |
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NOTE: The subsequent step 19 is only for the ADTP with the revision status REV B. |
| 19.On the SCU 11MH, on the monitor: | On the SCU 11MH, on the monitor: |
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B. Do a Check of the new loaded DIU Database Software.
(1) Open and then close the circuit breaker 189MH to do a reset of the PVIS.
(2) Do this check.
5. Close-up(1) Open and then close the circuit breaker 189MH to do a reset of the PVIS.
(2) Do this check.
| ACTION | RESULT |
|---|---|
| 1.On the SCU 11MH, on the monitor: | On the SCU 11MH, on the monitor: |
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| 2.On the SCU 11MH, on the monitor: | On the SCU 11MH, on the monitor: |
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| 3.On the SCU 11MH: | On the SCU 11MH: |
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| 4.On the circuit breaker panel 2000VU: | |
| The PVIS de-energizes. |
Subtask 23-34-00-860-055-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) De-energize the Cabin Intercommunication Data System (CIDS) (Ref. AMM TASK 23-73-00-862-001).
(2) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(4) Make sure that the work area is clean and clear of tools and other items.
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 23-34-00-410-054-A ** ON A/C NOT FOR ALL (1) De-energize the Cabin Intercommunication Data System (CIDS) (Ref. AMM TASK 23-73-00-862-001).
(2) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(4) Make sure that the work area is clean and clear of tools and other items.
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
B. Close Access
(1) Close the access door 824 (Ref. AMM TASK 52-41-00-410-002).
(2) Remove the access platform(s).
(1) Close the access door 824 (Ref. AMM TASK 52-41-00-410-002).
(2) Remove the access platform(s).