Loss of Communication with the AIDS through the MCDU 2
TASK 22-82-00-810-818-A
Loss of Communication with the AIDS through the MCDU 2
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 22-82-00-860-056-A
Subtask 22-82-00-810-075-A
Subtask 22-82-00-860-057-A
[Rev.8 from Aug 2018]
2026.04.04 04:25:28 UTC
Loss of Communication with the AIDS through the MCDU 2
1. Possible Causes
- MCDU-2 [3CA2]
wiring of the AIDS DATA IN bus from the MCDU 2 (3CA2) to the first terminal block
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 22-82-12-000-001 | Removal of the MCDU |
| AMM 22-82-12-400-002 | Installation of the MCDU |
| ASM 228604 | |
| AMM 24-41-00-861-002 | Energize the Aircraft Electrical Circuits from the External Power |
| AMM 24-41-00-862-002 | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
Subtask 22-82-00-860-056-A
A. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Make sure that the ventilation of the electronics racks is in operation.
Subtask 22-82-00-865-053-A (1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Make sure that the ventilation of the electronics racks is in operation.
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 22-82-00-710-084-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | AIDS/DMU | 4TV | K15 |
| ** ON A/C ALL | |||
| 121VU | AUTO FLT/MCDU/2 | 11CA2 | N20 |
C. Test
4. Fault Isolation| ACTION | RESULT |
|---|---|
| 1.On the center pedestal, on the MCDU 2: | On the center pedestal, on the MCDU 2: |
| The MCDU MENU page comes into view. |
| The AIDS MENU page comes into view. |
Subtask 22-82-00-810-075-A
A. If the AIDS MENU page does not come into view:
Subtask 22-82-00-710-085-A - replace the MCDU-2 [3CA2] AMM 22-82-12-000-001 and AMM 22-82-12-400-002.
- do a check and repair the
wiring of the AIDS DATA IN bus from the MCDU 2 (3CA2) to the first terminal block ASM 228604.
B. Do the test given in Para. 3.C.
5. Close-upSubtask 22-82-00-860-057-A
A. Put the aircraft back to its initial configuration.
(1) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
(1) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.