W DOC AIRBUS | AMM A320F

Removal of the Green Hydraulic Reservoir


TASK 29-11-41-000-001-A
Removal of the Green 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.
ZONE: 147
FIN: 1000GQ
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 3M (10 FT)- ADJUSTABLE
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)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
147
MAIN GEAR WELL AND HYDRAULIC COMPARTMENT
 C. Referenced Information
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 29-10-00-680-001-A
Drainage of the Reservoir of 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 32-12-00-010-001-A
Open the Main Gear Doors for Access
3. Job Set-up
Subtask 29-11-41-865-050-A
A. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUHYDRAULIC/G HYD/PUMP ENG1/CTL1701GKH12
** ON A/C NOT FOR ALL
121VUHYDRAULIC/G HYD/PUMP ENG1/CTL1701GKR35
** ON A/C NOT FOR ALL
121VUHYDRAULIC/G HYD/PUMP ENG1/MONG1702GKR34
** ON A/C ALL
121VUHYDRAULIC/LOW/LVL/IND1832GQN32
121VUHYDRAULIC/HYD/QTY/IND1831GQP35
** ON A/C NOT FOR ALL
121VUHYDRAULIC/G HYD/PUMP ENG1/MONG1702GKR33
Subtask 29-11-41-860-050-A
B. Aircraft Maintenance Configuration
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 Green hydraulic system:
  • in the cockpit on the hydraulic section 40VU of the overhead panel,
  • on the ground service panel of the Green hydraulic system.
   (3) Open the main doors of the main gear (Ref. AMM TASK 32-12-00-010-001).
   (4) Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
   (5) Depressurize the reservoir of the Green hydraulic system (Ref. AMM TASK 29-14-00-614-001).
   (6) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the main doors of the main gear.
   (7) Put a CONTAINER - HYDRAULIC FLUID RESISTANT below the reservoir.
   (8) Disconnect the isolation coupling of the Power Transfer Unit (PTU) (Ref. AMM TASK 29-23-00-860-001).
   (9) Drain the reservoir of the Green hydraulic system (Ref. AMM TASK 29-10-00-680-001).
4. Procedure
Subtask 29-11-41-020-055-B
A. Removal of the Reservoir
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 (40),(41),(15).
   (2) Install a CAP - BLANKING on the electrical connector and on the electrical receptacle on the reservoir (16).
   (3) Remove the nut (14), the bolt (10) and the washer (13) and disconnect the bonding jumpers (11),(12) from the reservoir.
   (4) Loosen the union nut (20) and disconnect the air pipe (19) from the reservoir (16).
   (5) Loosen the union nut (2) and disconnect the air pipe (1) from the reducer (24).
   (6) Loosen the union nut (8) and disconnect the seal drain pipe (9) from the pressure relief valve (7).
   (7) Loosen the union nut (36) and disconnect the suction pipe (35) from the elbow (37).
   (8) Loosen the union nut (42) and disconnect the return pipe (43) from the reservoir (16).
   (9) Loosen the union nut (44) and disconnect the suction pipe (45) from the reservoir (16).
   (10) Loosen and remove the two nuts (50).
   (11) Remove the two bolts (46) and the washers (47).
   (12) Remove the pipe clamp halves (48),(49).
   (13) Remove and discard the lockwire from the reservoir strap bolts (39).
   (14) Hold the reservoir (16) and loosen the two reservoir strap bolts (39).
   (15) Disconnect the ends of the reservoir straps (38) and remove the reservoir (16) from the aircraft.
   (16) Install a PLUG - BLANKING in all open pipe ends and unions and in the reservoir ports.
[Rev.10 from 2021] 2026.04.01 00:15:46 UTC