W DOC AIRBUS | AMM A320F

Removal of the Manifold Assembly


TASK 32-31-36-000-802-A
Removal of the Manifold Assembly


WARNING: MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.
ZONE: 734
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 1M(3 FT)
No specific
AR
CONTAINER - HYDRAULIC FLUID RESISTANT
No specific
1
PLUG - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
734
MAIN DOOR
 C. Referenced Information
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 29-00-00-910-002-A
Safety Procedures of the Hydraulic System
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 32-00-00-481-002-A
Installation of the Safety Devices on the Landing Gear Doors
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
TASK 32-31-36-000-001-A
Removal of the MLG Check Valves
3. Job Set-up
Subtask 32-31-36-860-053-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 32-31-36-010-052-A
B. Get Access
   (1) Open the left MLG door (Ref. AMM TASK 32-12-00-010-001).
   (2) Install the safety devices on the left MLG door (Ref. AMM TASK 32-00-00-481-002).
Subtask 32-31-36-869-053-A
C. Aircraft Maintenance Configuration
   (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) Put the WARNING NOTICE(S) in the position to tell persons not to pressurize the Green hydraulic system:
  • On panel 40VU in the cockpit
  • On the ground service panel of the Green hydraulic system.
   (4) Obey the flight configuration precautions (Ref. AMM TASK 32-00-00-860-001).
   (5) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002).
   (6) Put the ACCESS PLATFORM 1M(3 FT) in position at zone 734.
   (7) Put the CONTAINER - HYDRAULIC FLUID RESISTANT below the check valves (7) and (8) and the reducer (2) to collect unwanted hydraulic fluid.
Subtask 32-31-36-865-053-A
D. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUL/G/LGCIU/SYS1/NORM1GAC09
** 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
121VULGCIU/BAT SPLY/SYS259GAR33
121VULGCIU/BAT SPLY/SYS158GAR32
** ON A/C ALL
121VUHYDRAULIC/LGCIU/SYS22GAQ35
121VUHYDRAULIC/LGCIU/SYS1/GRND SPLY52GAQ34
** ON A/C NOT FOR ALL
121VUHYDRAULIC/G HYD/PUMP ENG1/MONG1702GKR33
121VULGCIU/BAT SPLY/SYS259GAR32
121VULGCIU/BAT SPLY/SYS158GAR31
4. Procedure
Subtask 32-31-36-020-054-A
A. Removal of the Manifold Assembly
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) Remove the MLG check valves (7) and (8) (Ref. AMM TASK 32-31-36-000-001).
   (2) Loosen the nut of the hydraulic line (1) and disconnect the hydraulic line (1) from the reducer (2).
   (3) Put the PLUG - BLANKING in the disconnected end of the hydraulic line (1).
   (4) Remove the reducer (2).
   (5) Remove and discard the packing (3).
   (6) Remove the bolts (6) and the washers (5).
   (7) Remove the manifold (4) from the bracket (9).
[Rev.10 from 2021] 2026.04.01 00:45:09 UTC