W DOC AIRBUS | AMM A320F

Removal of the Hydraulic Brake Filter

TASK 32-42-12-000-001-A
Removal of the Hydraulic Brake Filter

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.
FIN: 2584GM
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)
No specific
1
CONTAINER 5 L (1.32 USGAL)
No specific
AR
PLUG - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. 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 32-00-00-860-001-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
F Hydraulic Brake Filter 2584GM
3. Job Set-up
Subtask 32-42-12-860-052-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 32-42-12-010-050-A
B. Get Access
   (1) Open the left or the right MLG door (Ref. AMM TASK 32-12-00-010-001).
Subtask 32-42-12-869-051-A
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).
   (4) Put the ACCESS PLATFORM 2M (6 FT) in position.
   (5) Put the CONTAINER 5 L (1.32 USGAL) below the hydraulic brake filter 2584GM to collect the hydraulic fluid leakage.
Subtask 32-42-12-865-050-A
D. 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/BRAKING AND STEERING/SYS2/SPLY4GGM36
121VUHYDRAULIC/BRAKING AND STEERING/SYS2/CTL3GGM35
121VUHYDRAULIC/BRAKING AND STEERING/SYS1/CTL1GGM34
121VUHYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY2GGM33
** ON A/C NOT FOR ALL
121VUHYDRAULIC/G HYD/PUMP ENG1/MONG1702GKR33
Subtask 32-42-12-941-050-A
E. Safety Precautions
   (1) 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.
4. Procedure
Subtask 32-42-12-020-051-A
A. Removal of the Hydraulic Brake Filter (4)
   (1) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002).
   (2) Disconnect the connectors (1) from the unions (2).
   (3) Put the PLUG-BLANKING in each disconnected line end.
   (4) Remove the bolts (6), the washers (5) and the hydraulic brake filter (4).
[Rev.10 from 2021] 2026.04.01 00:47:45 UTC
"Aviabrain" 2025