Removal of the NLG Shock Absorber Assy
TASK 32-21-13-000-001-B
Removal of the NLG Shock Absorber Assy
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 32-21-13-941-055-A ** ON A/C NOT FOR ALL
Subtask 32-21-13-020-056-A ** ON A/C NOT FOR ALL
[Rev.9 from 2019]
2026.04.01 00:42:09 UTC
Removal of the NLG Shock Absorber Assy
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| No specific | 1 | DRIFT - PLASTIC |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 1 | TROLLEY - LIFTING |
| No specific | AR | WARNING NOTICE(S) |
| J47564 | 1 | ADAPTOR |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 07-11-00-581-001-A | Lifting for Aircraft Maintenance Operations |
| TASK 32-21-27-000-002-A | Removal of the Torque-Link Center Hinge |
| TASK 32-21-41-000-001-A | Removal of the NLG TOWING attachment |
| TASK 32-22-00-010-001-A | Nose Gear Doors - Ground Doors Opening |
| TASK 32-41-12-000-001-A | Removal of the NLG Wheel |
Subtask 32-21-13-941-055-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) In the cockpit, on the panel 400VU put WARNING NOTICE(S) in position to tell persons not to operate the landing gear control lever.
(2) On the steering handwheel (CAPT and F/O) and on the brake pedals, put WARNING NOTICE(S) in position to tell persons not to operate them .
(3) Put the SAFETY BARRIER(S) in position.
Subtask 32-21-13-860-055-A ** ON A/C NOT FOR ALL (1) In the cockpit, on the panel 400VU put WARNING NOTICE(S) in position to tell persons not to operate the landing gear control lever.
(2) On the steering handwheel (CAPT and F/O) and on the brake pedals, put WARNING NOTICE(S) in position to tell persons not to operate them .
(3) Put the SAFETY BARRIER(S) in position.
B. Aircraft Maintenance Configuration
(1) Lift the aircraft with jacks until the wheels are off the ground (Ref. AMM TASK 07-11-00-581-001).
Subtask 32-21-13-010-052-A ** ON A/C NOT FOR ALL (1) Lift the aircraft with jacks until the wheels are off the ground (Ref. AMM TASK 07-11-00-581-001).
C. Get Access
(1) Open the doors of the nose landing gear (Ref. AMM TASK 32-22-00-010-001).
(2) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position in zone 123.
Subtask 32-21-13-865-056-A ** ON A/C NOT FOR ALL (1) Open the doors of the nose landing gear (Ref. AMM TASK 32-22-00-010-001).
(2) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position in zone 123.
D. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY | 4GG | M36 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS2/CTL | 3GG | M35 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS1/CTL | 1GG | M34 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY | 2GG | M33 |
Subtask 32-21-13-020-056-A ** ON A/C NOT FOR ALL
A. Preparation before Removal
(1) Remove the wheels of the nose landing gear. (Ref. AMM TASK 32-41-12-000-001)
(2) Remove the towing fitting (Ref. AMM TASK 32-21-41-000-001).
Subtask 32-21-13-020-057-F ** ON A/C NOT FOR ALL (1) Remove the wheels of the nose landing gear. (Ref. AMM TASK 32-41-12-000-001)
(2) Remove the towing fitting (Ref. AMM TASK 32-21-41-000-001).
B. Removal of the NLG Shock Absorber Assy
(1) Lightly loosen the valve (1) and let the nitrogen go out of the shock absorber (10).
(2) Remove and discard the cotter pin (22) and remove the nut (23) and the bolt (20).
(4) Disconnect the center hinge (Ref. AMM TASK 32-21-27-000-002).
(5) Remove the nuts (60), the bolts (64) and the washers (61) and (63).
(6) Remove the stop (62).
(7) Lift the aircraft with jacks so as to get a clearance higher than 1.50 m (4.92 ft.) between the bottom of the shock absorber and the ground (Ref. AMM TASK 07-11-00-581-001).
(8) Install the TROLLEY - LIFTING and attach the shock absorber (10).
(9) Open the valve (1) and fully compress the shock absorber (10).
(10) Remove the bolt (2) and the washer (3).
(11) Cut and discard the lockwire between the valve (1) and the stop plate (4).
(12) Remove the stop plate (4), then remove the valve (1).
(13) Remove the nut (6) with the J47564 ADAPTOR.
(14) Slowly remove the shock absorber (10). Be careful not to hit the inner part of the shock strut (7) with the sliding tube.
(15) Remove the shock absorber (10).
(1) Lightly loosen the valve (1) and let the nitrogen go out of the shock absorber (10).
(2) Remove and discard the cotter pin (22) and remove the nut (23) and the bolt (20).
NOTE: Remove the bolt (20) with a DRIFT - PLASTIC.
(3) Remove the support (21). (4) Disconnect the center hinge (Ref. AMM TASK 32-21-27-000-002).
(5) Remove the nuts (60), the bolts (64) and the washers (61) and (63).
(6) Remove the stop (62).
(7) Lift the aircraft with jacks so as to get a clearance higher than 1.50 m (4.92 ft.) between the bottom of the shock absorber and the ground (Ref. AMM TASK 07-11-00-581-001).
(8) Install the TROLLEY - LIFTING and attach the shock absorber (10).
(9) Open the valve (1) and fully compress the shock absorber (10).
(10) Remove the bolt (2) and the washer (3).
(11) Cut and discard the lockwire between the valve (1) and the stop plate (4).
(12) Remove the stop plate (4), then remove the valve (1).
(13) Remove the nut (6) with the J47564 ADAPTOR.
(14) Slowly remove the shock absorber (10). Be careful not to hit the inner part of the shock strut (7) with the sliding tube.
(15) Remove the shock absorber (10).
Nose Gear Shock Absorber