L/G - NLG Shock Absorber Fault
TASK 32-31-00-810-851-A
L/G - NLG Shock Absorber Fault
A. Referenced Information
3. Fault Confirmation
Subtask 32-31-00-700-050-A
Subtask 32-31-00-810-109-B
[Rev.8 from Aug 2018]
2026.04.04 04:31:23 UTC
L/G - NLG Shock Absorber Fault
WARNING:
MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. MOVEMENT OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
1. Possible Causes- NLG shock absorber is not aligned correctly
- damage to the NLG linkage
- PROX SNSR-NLG EXT, SYS 1 [24GA]
- PROX SNSR-NLG EXT, SYS 2 [25GA]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 32-21-00-200-002 | General Visual Inspection of the Nose Landing Gear |
| AMM 32-31-00-720-003 | Functional Test of the Normal Extension and Retraction of the Nose Landing Gear |
| AMM 32-31-73-000-005 | Removal of the NLG Proximity-Sensors |
| AMM 32-31-73-200-002 | Inspection of the NLG Proximity Sensor and Target Clearances |
| AMM 32-31-73-400-005 | Installation of the NLG Proximity-Sensors |
| AMM 32-31-73-820-006 | Adjustment of the NLG Extension/Steering Proximity Sensors |
Subtask 32-31-00-700-050-A
A. Analysis
(1) If the Post Flight Report (PFR) shows the ECAM Warning SHOCK ABSORBER FAULT with the the CFDS message AFS: LGCIU1(2)-FAC1(2) CKT, do the fault isolation procedure in Para.4.A.
4. Fault Isolation(1) If the Post Flight Report (PFR) shows the ECAM Warning SHOCK ABSORBER FAULT with the the CFDS message AFS: LGCIU1(2)-FAC1(2) CKT, do the fault isolation procedure in Para.4.A.
Subtask 32-31-00-810-109-B
A. Procedure
(3) Do the Inspection of the NLG Proximity Sensor and Target Clearances for the applicable proximity sensor AMM 32-31-73-200-002:
(a) Do the test in step (6).
(5) Do the adjustment of the applicable proximity sensor AMM 32-31-73-820-006.
(6) Do the Functional Test of the Normal Extension and Retraction of the NLG AMM 32-31-00-720-003.
NOTE: The maintenance message AFS:LGCIU1(2)-FAC1(2) CKT shows when the related NLG proximity sensors 24GA (25GA) sense that the NLG shock absorber is not aligned correctly and damage to the NLG linkage can have occurred. Usually the two messages are shown, one from each LGCIU, but it is possible that only one message is shown on the PFR.
(1) Do a General Visual inspection of the Nose Landing Gear AMM 32-21-00-200-002 and look for damage to the proximity switches, the NLG structure and its linkages: - if you do not find damage, do step (3)
- if you find damage, do step (2)
(3) Do the Inspection of the NLG Proximity Sensor and Target Clearances for the applicable proximity sensor AMM 32-31-73-200-002:
- if the proximity sensor/target clearances are not correct, do step (5)
- if the proximity sensor/target clearances are correct, do step (4).
(a) Do the test in step (6).
(5) Do the adjustment of the applicable proximity sensor AMM 32-31-73-820-006.
(6) Do the Functional Test of the Normal Extension and Retraction of the NLG AMM 32-31-00-720-003.