Removal of the Yellow Hydraulic Reservoir
TASK 29-13-41-000-002-A
Removal of the Yellow Hydraulic Reservoir
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 29-13-41-865-053-A
Subtask 29-13-41-020-054-B
[Rev.10 from 2021]
2026.04.01 00:21:08 UTC
Removal of the Yellow Hydraulic Reservoir
WARNING:
MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | CAP - BLANKING |
| No specific | 1 | CONTAINER - HYDRAULIC FLUID RESISTANT |
| No specific | AR | PLUG - BLANKING |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 2 | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 196 | HYDRAULIC COMPT AND FAIRINGS |
| 196AB, 196BB |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 29-00-00-864-001-A | Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action |
| TASK 29-00-00-910-002-A | Safety Procedures of the Hydraulic System |
| TASK 29-10-00-680-002-A | Drainage of the Reservoir of the Yellow 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) |
Subtask 29-13-41-865-053-A
A. Open, safety and tag this(these) circuit breaker(s):
Subtask 29-13-41-941-053-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N30 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LOW/LVL/IND | 1832GQ | N32 |
| 121VU | HYDRAULIC/HYD/QTY/IND | 1831GQ | P35 |
| 121VU | HYDRAULIC/Y HYD/PUMP ENG2/MONG | 3700GD | Q37 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N31 |
| ** ON A/C ALL | |||
| 123VU | Y HYD/ELEC/PUMP | 3802GX | AB06 |
| 123VU | Y HYD/ELEC/ELEC PUMP/NORM | 3801GX | AB03 |
B. Safety Precautions
(2) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system:
Subtask 29-13-41-010-053-A Subtask 29-13-41-860-058-A WARNING:
OBEY THE HYDRAULIC SAFETY PROCEDURES.
(1) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002). (2) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system:
- in the cockpit on the hydraulic section 40VU of the overhead panel,
- on the ground service panel of the Yellow hydraulic system.
D. Aircraft Maintenance Configuration
(1) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
(2) Depressurize the reservoir of the Yellow hydraulic system (Ref. AMM TASK 29-14-00-614-001).
(3) Disconnect the isolation coupling of the Power Transfer Unit (PTU) (Ref. AMM TASK 29-23-00-860-001).
(4) Put a CONTAINER - HYDRAULIC FLUID RESISTANT below the reservoir.
(5) Drain the reservoir of the Yellow hydraulic system (Ref. AMM TASK 29-10-00-680-002).
4. Procedure(1) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
(2) Depressurize the reservoir of the Yellow hydraulic system (Ref. AMM TASK 29-14-00-614-001).
(3) Disconnect the isolation coupling of the Power Transfer Unit (PTU) (Ref. AMM TASK 29-23-00-860-001).
(4) Put a CONTAINER - HYDRAULIC FLUID RESISTANT below the reservoir.
(5) Drain the reservoir of the Yellow hydraulic system (Ref. AMM TASK 29-10-00-680-002).
Subtask 29-13-41-020-054-B
A. Removal of the Reservoir
(2) Install a CAP - BLANKING on the electrical connectors and on the electrical receptacles on the reservoir (1).
(3) Temporarily attach the electrical leads to the aircraft structure.
(4) Remove the nut (30), the bolt (26) and the washer (29) and disconnect the bonding jumpers (27),(28) from the reservoir (1).
(5) Loosen the union nut (36) and disconnect the air pipe (37) from the reservoir (1).
(6) Loosen the union nut (38) and remove the air pipe (37).
(7) Loosen the union nut (16) and disconnect the air bleed pipe (15) from the reducer (17).
(8) Remove the bolt (40), the washer (41) and the distance bush (43) which attach the P-clip (42) to the structure.
(9) Loosen the union nut (24) and disconnect the seal drain pipe (25) from the air pressure relief valve (23).
(10) Remove the two bolts (44), the washers (45) and the clamp block halves (46).
(11) Loosen the union nut (6) and disconnect the suction pipe (5) from the structure attachment.
(12) Loosen the union nut (8) and remove the suction pipe (5).
(13) Loosen the union nut (9) and disconnect the return pipe (10) from the reservoir (1).
(14) Loosen the union nut (12) and disconnect the suction pipe (11) from the reservoir (1).
(15) Cut and remove the lockwire from the two strap bolts (4).
(16) Hold the reservoir (1) and loosen the two reservoir strap bolts (4).
(17) Disconnect the ends of the reservoir straps (3) and remove the reservoir (1) from the aircraft.
(18) Install a PLUG - BLANKING in all open pipe ends, unions and the reservoir ports.
CAUTION:
USE A SECOND WRENCH TO APPLY COUNTERTORQUE TO THE UNION WHEN YOU DISCONNECT/CONNECT HYDRAULIC LINES ON UNIONS. IF YOU DO NOT USE THE SECOND WRENCH, THERE IS A RISK THAT YOU WILL LOOSEN OR TIGHTEN THE UNION TOO MUCH.
(1) Disconnect the electrical connectors (2),(7),(33). (2) Install a CAP - BLANKING on the electrical connectors and on the electrical receptacles on the reservoir (1).
(3) Temporarily attach the electrical leads to the aircraft structure.
(4) Remove the nut (30), the bolt (26) and the washer (29) and disconnect the bonding jumpers (27),(28) from the reservoir (1).
(5) Loosen the union nut (36) and disconnect the air pipe (37) from the reservoir (1).
(6) Loosen the union nut (38) and remove the air pipe (37).
(7) Loosen the union nut (16) and disconnect the air bleed pipe (15) from the reducer (17).
(8) Remove the bolt (40), the washer (41) and the distance bush (43) which attach the P-clip (42) to the structure.
(9) Loosen the union nut (24) and disconnect the seal drain pipe (25) from the air pressure relief valve (23).
(10) Remove the two bolts (44), the washers (45) and the clamp block halves (46).
(11) Loosen the union nut (6) and disconnect the suction pipe (5) from the structure attachment.
(12) Loosen the union nut (8) and remove the suction pipe (5).
(13) Loosen the union nut (9) and disconnect the return pipe (10) from the reservoir (1).
(14) Loosen the union nut (12) and disconnect the suction pipe (11) from the reservoir (1).
(15) Cut and remove the lockwire from the two strap bolts (4).
(16) Hold the reservoir (1) and loosen the two reservoir strap bolts (4).
(17) Disconnect the ends of the reservoir straps (3) and remove the reservoir (1) from the aircraft.
(18) Install a PLUG - BLANKING in all open pipe ends, unions and the reservoir ports.
Reservoir of the Yellow Hydraulic System (Sheet 1)