Access to the RAD/NAV Page on the MCDU 1 Inoperative
TASK 22-82-00-810-821-A
Access to the RAD/NAV Page on the MCDU 1 Inoperative
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 22-82-00-860-062-A
Subtask 22-82-00-810-078-A
Subtask 22-82-00-860-067-A
[Rev.8 from Aug 2018]
2026.04.04 04:25:28 UTC
Access to the RAD/NAV Page on the MCDU 1 Inoperative
1. Possible Causes
- FMGC-1 [1CA1]
wiring of the NAV CONTROL OWN and NAV CONTROL OPP discretes (from the FMGC 1 (1CA1) to the first terminal block)
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 22-83-34-000-001 | Removal of the FMGC |
| AMM 22-83-34-400-001 | Installation of the FMGC |
| ASM 228504 | |
| 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 22-82-00-860-062-A
A. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
Subtask 22-82-00-865-056-A (1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 22-82-00-710-090-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | AUTO FLT/FMGC/1 | 10CA1 | B02 |
| 49VU | AUTO FLT/MCDU/1 | 11CA1 | B01 |
| 49VU | COM/RMP/1 | 2RG1 | G10 |
| 121VU | COM NAV/RMP/2 | 2RG2 | L02 |
| 121VU | AUTO FLT/FMGC/2 | 10CA2 | M17 |
| 121VU | AUTO FLT/MCDU/2 | 11CA2 | N20 |
C. Test
4. Fault Isolation| ACTION | RESULT |
|---|---|
| 1.On the center pedestal, on the MCDU 1: | |
| |
|
|
Subtask 22-82-00-810-078-A
A. If the RAD/NAV page does not come into view:
Subtask 22-82-00-710-091-A - replace the FMGC-1 [1CA1] AMM 22-83-34-000-001 and AMM 22-83-34-400-001.
- do a check and repair the
wiring of the NAV CONTROL OWN and NAV CONTROL OPP discretes (from the FMGC 1 (1CA1) to the first terminal block) ASM 228504.
B. Do the test given in Para. 3.
5. Close-upSubtask 22-82-00-860-067-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.