Loss of the LGCIU 1 or the LGCIU 2
TASK 30-31-00-810-856-A
Loss of the LGCIU 1 or the LGCIU 2
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 30-31-00-860-050-A
Subtask 30-31-00-810-105-A
[Rev.8 from Aug 2018]
2026.04.04 04:29:38 UTC
Loss of the LGCIU 1 or the LGCIU 2
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| ASM 301003 | |
| ASM 303101 | |
| ASM 303102 | |
| AMM 32-31-71-000-001 | Removal of the LGCIU |
| AMM 32-31-71-400-001 | Installation of the LGCIU |
| AMM 32-31-73-000-001 | Removal of the MLG Proximity-Sensors |
| AMM 32-31-73-000-005 | Removal of the NLG Proximity-Sensors |
| AMM 32-31-73-400-001 | Installation of the MLG Proximity-Sensors |
| AMM 32-31-73-400-005 | Installation of the NLG Proximity-Sensors |
| AMM 32-69-00-740-001 | BITE Check of Landing-Gear Control Interface-Unit (LGCIU) With Use of MCDU to Ensure that Continuous BITE is Operative |
Subtask 30-31-00-860-050-A
A. Get the CFDS MENU page as follows:
(1) Push in the line key adjacent to the CFDS indication. Make sure that the CFDS menu page comes into view.
(2) Push in the line key adjacent to the LAST LEG REPORT.
(a) If there are CFDS messages related to ATA chapter 32:
4. Fault Isolation(1) Push in the line key adjacent to the CFDS indication. Make sure that the CFDS menu page comes into view.
(2) Push in the line key adjacent to the LAST LEG REPORT.
(a) If there are CFDS messages related to ATA chapter 32:
- Refer to the para. 4.A.
- Refer to the para. 4.B.
- Refer to the para. 4.C.
Subtask 30-31-00-810-105-A
A. If the fault symptom is identified by the ECAM warnings:
. ANTI ICE CAPT PROBES
. ANTI ICE F/O PITOT
. ANTI ICE STBY PITOT
and the CFDS messages related to ATA chapter 32:
Subtask 30-31-00-810-111-A . ANTI ICE CAPT PROBES
. ANTI ICE F/O PITOT
. ANTI ICE STBY PITOT
and the CFDS messages related to ATA chapter 32:
- Do the bite test of the landing gear AMM 32-69-00-740-001.
- replace the defective LGCIU-1 [5GA1] or LGCIU-2 [5GA2] AMM 32-31-71-000-001 AMM 32-31-71-400-001.
B. If the fault symptom is identified by the ECAM warnings:
. ANTI ICE CAPT PROBES
. ANTI ICE F/O PITOT
. ANTI ICE STBY PITOT
and CFDS messages related to ATA chapter 30.31:
Subtask 30-31-00-810-112-A . ANTI ICE CAPT PROBES
. ANTI ICE F/O PITOT
. ANTI ICE STBY PITOT
and CFDS messages related to ATA chapter 30.31:
- Refer to the related trouble shooting.
C. If the fault symptom is identified by the ECAM warnings:
. ANTI ICE CAPT PROBES
. ANTI ICE F/O PITOT
. ANTI ICE STBY PITOT
(1) Do a check of the wiring from:
. ANTI ICE CAPT PROBES
. ANTI ICE F/O PITOT
. ANTI ICE STBY PITOT
(1) Do a check of the wiring from:
- The PHC 1 (6DA1) pin A/<E to the LGCIU 1 (5GA1) pin AB/14A ASM 303101
- The PHC 1 (6DA1) pin A/<D to the LGCIU 2 (5GA2) pin AB/14A
- The PHC 2 (6DA2) pin E/<E to the LGCIU 1 (5GA1) pin AB/14E ASM 303102
- The PHC 2 (6DA2) pin E/<D to the LGCIU 2 (5GA2) pin AB/14E
- The PHC 3 (6DA3) pin A/<E to the LGCIU 1 (5GA1) pin AB/15A ASM 301003
- The PHC 3 (6DA3) pin A/<D to the LGCIU 2 (5GA2) pin AB/15A.
- Repair the wiring.
- Do the bite test of the landing gear AMM 32-69-00-740-001.
- Replace the defective LGCIU-1 (5GA1) or LGCIU-2 (5GA2) AMM 32-31-71-000-001 and AMM 32-31-71-400-001.
- Replace the proximity sensors AMM 32-31-73-000-001 and AMM 32-31-73-400-001 or AMM 32-31-73-000-005 and AMM 32-31-73-400-005.