Removal of the MLG Uplock - Support Struts
TASK 32-31-44-000-002-A
Removal of the MLG Uplock - Support Struts
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 32-31-44-860-053-A
Subtask 32-31-44-020-052-A
[Rev.10 from 2021]
2026.04.01 00:45:23 UTC
Removal of the MLG Uplock - Support Struts
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| No specific | 1 | CONTAINER 5 L (1.32 USGAL) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 29-10-00-864-001-A | Depressurize the Green Hydraulic System |
| TASK 29-14-00-614-001-A | Depressurization of the Hydraulic Reservoirs |
| TASK 29-23-00-860-001-A | Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU) |
| 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 32-12-00-010-001-A | Open the Main Gear Doors for Access |
Subtask 32-31-44-860-053-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001).
Subtask 32-31-44-010-052-A Subtask 32-31-44-869-053-A (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001).
C. Disconnection of the PTU Isolation Coupling
(1) Depressurize the reservoir of the Green hydraulic system (Ref. AMM TASK 29-14-00-614-001).
(2) Disconnect the PTU isolation coupling (Ref. AMM TASK 29-23-00-860-001).
(3) Obey the flight configuration precautions (Ref. AMM TASK 32-00-00-860-001).
Subtask 32-31-44-865-053-A (1) Depressurize the reservoir of the Green hydraulic system (Ref. AMM TASK 29-14-00-614-001).
(2) Disconnect the PTU isolation coupling (Ref. AMM TASK 29-23-00-860-001).
(3) Obey the flight configuration precautions (Ref. AMM TASK 32-00-00-860-001).
D. Open, safety and tag this(these) circuit breaker(s):
Subtask 32-31-44-941-053-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | HYDRAULIC/G HYD/PUMP ENG1/CTL | 1701GK | H12 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/CTL | 1701GK | R35 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/MONG | 1702GK | R34 |
| ** 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 | HYDRAULIC/G HYD/PUMP ENG1/MONG | 1702GK | R33 |
E. Safety Precautions
(1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position.
(2) Put the CONTAINER 5 L (1.32 USGAL) below the uplock assembly 2509GM (2510GM) to collect the hydraulic fluid leakage.
(3) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Green hydraulic system:
4. Procedure(1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position.
(2) Put the CONTAINER 5 L (1.32 USGAL) below the uplock assembly 2509GM (2510GM) to collect the hydraulic fluid leakage.
(3) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Green hydraulic system:
- On the panel 40VU in the cockpit
- On the ground service panel of the Green hydraulic system.
Subtask 32-31-44-020-052-A
A. Removal of MLG Uplock-Support Struts
(1) Remove the support strut "A":
(a) Make a note of the dimension "Y".
(c) Remove the nut (4) and the washer (3).
(d) Remove the bolt (1) and the bush (2).
(e) Remove the nut (12) and the washers (9) and (10).
(f) Pull the bolt (6) out and remove the washer assembly (7).
(g) Remove the support strut "A" (8).
(2) Remove the support strut "B":
(a) Make a note of the dimension "Z"
(c) Remove the nut (20) and the washer (22).
(d) Remove the bolt (24) and the bush (23).
(e) Remove the nut (18) and the washers (16) and (17).
(f) Pull the bolt (13) out and remove the washer assembly (14).
(g) Remove the support strut "B" (15).
(1) Remove the support strut "A":
(a) Make a note of the dimension "Y".
NOTE: This dimension is necessary for the installation of the new component.
(b) Remove and discard the cotter pins (5) and (11). (c) Remove the nut (4) and the washer (3).
(d) Remove the bolt (1) and the bush (2).
(e) Remove the nut (12) and the washers (9) and (10).
(f) Pull the bolt (6) out and remove the washer assembly (7).
(g) Remove the support strut "A" (8).
(2) Remove the support strut "B":
(a) Make a note of the dimension "Z"
NOTE: This dimension is necessary for the installation of the new component.
(b) Remove and discard the cotter pins (19) and (21). (c) Remove the nut (20) and the washer (22).
(d) Remove the bolt (24) and the bush (23).
(e) Remove the nut (18) and the washers (16) and (17).
(f) Pull the bolt (13) out and remove the washer assembly (14).
(g) Remove the support strut "B" (15).
MLG Uplock-Support Struts