Removal of the MLG Slave Link Assembly
TASK 32-11-12-000-802-A
Removal of the MLG Slave Link Assembly
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 32-11-12-941-055-A
Subtask 32-11-12-020-054-B ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 00:40:06 UTC
Removal of the MLG Slave Link Assembly
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 731 | L.H MAIN GEAR |
| 741 | R.H MAIN GEAR |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 07-11-00-581-001-A | Lifting for Aircraft Maintenance Operations |
| TASK 07-12-00-582-002-A | Jacking of the Main Landing Gear |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 29-00-00-864-001-A | Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action |
| TASK 29-14-00-614-001-A | Depressurization of the Hydraulic Reservoirs |
| TASK 32-00-00-481-001-A | Installation of the Safety Devices on the Landing Gears |
| TASK 32-00-00-860-001-A | Flight Configuration Precautions with Electrical Power |
| TASK 32-00-00-860-001-A-01 | Flight Configuration Precautions without Electrical Power |
| TASK 32-11-12-000-001-A | Removal of the MLG Hydraulic Dressings |
| TASK 32-11-43-000-001-A | Removal of the 1M and 2M Harnesses from the MLG Leg |
| TASK 32-11-43-000-003-A | Removal of the 1M and 2M Harnesses from the MLG Axle |
| TASK 32-31-73-000-001-A | Removal of the MLG Proximity-Sensors |
| TASK 32-42-27-000-001-A | Removal of the Brake |
Subtask 32-11-12-941-055-A
A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Make sure that the safety devices are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
(a) Make sure that landing-gear control lever 6GA is in the DOWN position.
(b) Put the WARNING NOTICE(S) in position to tell persons not to operate the landing gear.
(4) Put the WARNING NOTICE(S) in position to tell persons not to operate the brakes.
(5) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the hydraulic systems.
Subtask 32-11-12-582-050-A (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Make sure that the safety devices are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
(a) Make sure that landing-gear control lever 6GA is in the DOWN position.
(b) Put the WARNING NOTICE(S) in position to tell persons not to operate the landing gear.
(4) Put the WARNING NOTICE(S) in position to tell persons not to operate the brakes.
(5) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the hydraulic systems.
B. Jacking
(1) Lift the applicable MLG (Ref. AMM TASK 07-12-00-582-002) or lift the aircraft on jacks (Ref. AMM TASK 07-11-00-581-001).
Subtask 32-11-12-860-058-A (1) Lift the applicable MLG (Ref. AMM TASK 07-12-00-582-002) or lift the aircraft on jacks (Ref. AMM TASK 07-11-00-581-001).
C. Aircraft Maintenance Configuration
(1) Make sure that the Yellow and Green hydraulic systems are depressurized (Ref. AMM TASK 29-00-00-864-001).
(2) Make sure that the Yellow and the Green hydraulic reservoirs are depressurized (Ref. AMM TASK 29-14-00-614-001).
Subtask 32-11-12-869-061-A (1) Make sure that the Yellow and Green hydraulic systems are depressurized (Ref. AMM TASK 29-00-00-864-001).
(2) Make sure that the Yellow and the Green hydraulic reservoirs are depressurized (Ref. AMM TASK 29-14-00-614-001).
D. Flight Configuration Precautions
(1) If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.
(2) If the electrical power is necessary, do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.
Subtask 32-11-12-865-055-A (1) If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.
(2) If the electrical power is necessary, do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.
E. Open, safety and tag this(these) circuit breaker(s):
Subtask 32-11-12-010-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R32 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
| 121VU | LGCIU/BAT SPLY/SYS1 | 58GA | R31 |
F. Get Access
(1) Remove the applicable brake (Ref. AMM TASK 32-42-27-000-001).
(2) Release the electrical harnesses from the applicable slave link assembly (Ref. AMM TASK 32-11-43-000-001).
(3) Remove the applicable proximity sensor 21GA(20GA) (Ref. AMM TASK 32-31-73-000-001).
(4) If necessary, release the 1M electrical harness from the MLG axle for access (Ref. AMM TASK 32-11-43-000-003).
4. Procedure(1) Remove the applicable brake (Ref. AMM TASK 32-42-27-000-001).
(2) Release the electrical harnesses from the applicable slave link assembly (Ref. AMM TASK 32-11-43-000-001).
(3) Remove the applicable proximity sensor 21GA(20GA) (Ref. AMM TASK 32-31-73-000-001).
(4) If necessary, release the 1M electrical harness from the MLG axle for access (Ref. AMM TASK 32-11-43-000-003).
NOTE: To correctly release the 1M electrical harness, you must remove the cable clamp from the lower-surface of the support bracket.
(5) Release the hydraulic dressings from the applicable slave link assembly (Ref. AMM TASK 32-11-12-000-001). Subtask 32-11-12-020-054-B ** ON A/C NOT FOR ALL
A. Removal of the MLG Slave Link Assembly
(2) Remove the bolts (3), the washers (4) and the bracket (2) from the upper slave-link assembly (8).
(3) Remove the cotter pin (10) from the nut (9) and discard it.
(4) Remove the nut (9), the washer (11), the bolt (18) and the spacer (19).
(5) Disconnect the upper slave-link assembly (8) from the lower slave-link assembly (12).
(6) Remove the cotter pin (7) from the nut (6) and discard it.
(7) Remove the nut (6), the washer (5) and the pin (1).
(8) Remove the upper slave-link assembly (8) from the main fitting lug.
(9) Remove the cotter pin (14) from the nut (13) and discard it.
(10) Remove the nut (13), the washer (15), the bolt (17) and the spacer (16).
(11) Remove the lower slave-link assembly (12) from the sliding piston lug.
Subtask 32-11-12-020-054-D ** ON A/C NOT FOR ALL WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
WARNING:
USE PROTECTIVE GOGGLES WHEN YOU REMOVE OR INSTALL A COTTER PIN. EACH TIME YOU REMOVE A COTTER PIN DURING THE TASK, DISCARD IT IMMEDIATELY. A LOOSE COTTER PIN CAN CUT YOU OR MAKE YOU BLIND.
(1) Cut, remove and discard the lockwire from the bolts (3). (2) Remove the bolts (3), the washers (4) and the bracket (2) from the upper slave-link assembly (8).
(3) Remove the cotter pin (10) from the nut (9) and discard it.
(4) Remove the nut (9), the washer (11), the bolt (18) and the spacer (19).
(5) Disconnect the upper slave-link assembly (8) from the lower slave-link assembly (12).
(6) Remove the cotter pin (7) from the nut (6) and discard it.
(7) Remove the nut (6), the washer (5) and the pin (1).
(8) Remove the upper slave-link assembly (8) from the main fitting lug.
(9) Remove the cotter pin (14) from the nut (13) and discard it.
(10) Remove the nut (13), the washer (15), the bolt (17) and the spacer (16).
(11) Remove the lower slave-link assembly (12) from the sliding piston lug.
A. Removal of the MLG Slave Link Assembly
(2) Remove the bolts (3), the washers (4) and the bracket (2) from the upper slave-link assembly (9).
(3) Remove the cotter pin (11) from the nut (10) and discard it.
(4) Remove the nut (10), the washer (12), the bolt (19) and the spacer (20).
(5) Disconnect the upper slave-link assembly (9) from the lower slave-link assembly (13).
(6) Remove the cotter pin (8) from the nut (7) and discard it.
(7) Remove the nut (7), the washer (6), the washer(s) (5) (if installed) and the pin (1).
(8) Remove the upper slave-link assembly (9) from the main fitting lug.
(9) Remove the cotter pin (15) from the nut (14) and discard it.
(10) Remove the nut (14), the washer (16), the bolt (18) and the spacer (17).
(11) Remove the lower slave-link assembly (13) from the sliding piston lug.
WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(1) Cut, remove and discard the lockwire from the bolts (3). (2) Remove the bolts (3), the washers (4) and the bracket (2) from the upper slave-link assembly (9).
(3) Remove the cotter pin (11) from the nut (10) and discard it.
(4) Remove the nut (10), the washer (12), the bolt (19) and the spacer (20).
(5) Disconnect the upper slave-link assembly (9) from the lower slave-link assembly (13).
(6) Remove the cotter pin (8) from the nut (7) and discard it.
(7) Remove the nut (7), the washer (6), the washer(s) (5) (if installed) and the pin (1).
(8) Remove the upper slave-link assembly (9) from the main fitting lug.
(9) Remove the cotter pin (15) from the nut (14) and discard it.
(10) Remove the nut (14), the washer (16), the bolt (18) and the spacer (17).
(11) Remove the lower slave-link assembly (13) from the sliding piston lug.
MLG Slave Link Assembly - Location and Details