W DOC AIRBUS | AMM A320F

Removal of the Accumulator

TASK 32-44-11-000-001-A
Removal of the Accumulator

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: 744
FIN: 2582GM
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. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
744
MAIN DOOR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 29-00-00-910-002-A
Safety Procedures of the Hydraulic System
TASK 29-10-00-864-002-A
Depressurize 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)
TASK 32-12-00-010-001-A
Open the Main Gear Doors for Access
TASK 32-44-11-200-001-A
Functional Check of Parking/Emergency Brake Accumulator by Reading the Charge Pressure on the Accumulator Gauge
F Accumulator 2582GM
3. Job Set-up
Subtask 32-44-11-010-050-A
A. Get Access
   (1) Open the right MLG door (Ref. AMM TASK 32-12-00-010-001).
Subtask 32-44-11-860-050-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002).
   (2) Push the pressure release button on pressure relief valve 3067GM to depressurize the alternate brake system.
   (3) Make sure that the pressure on gage 2585GM decreases until accumulator 2582GM pressure has fully stopped (Ref. AMM TASK 32-44-11-200-001).
Subtask 32-44-11-860-050-B ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002).
   (2) Set the Anti-skid and Nose Wheel switch to OFF.
   (3) Push the pressure release button on pressure relief valve 3067GM to depressurize the alternate brake system.
   (4) Make sure that the pressure on gage 2585GM decreases until accumulator 2582GM pressure has fully stopped (Ref. AMM TASK 32-44-11-200-001).
Subtask 32-44-11-869-050-A
C. Disconnection of the PTU Isolation Coupling
   (1) Depressurize the reservoir of the Yellow 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 ACCESS PLATFORM 2M (6 FT) in position.
   (4) Put the CONTAINER 5 L (1.32 USGAL) below the accumulator 2582GM to collect the hydraulic fluid leakage.
Subtask 32-44-11-865-052-A
D. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUL/G/Y BRK/PRESS/IND61GGC10
** ON A/C NOT FOR ALL
49VUABCU &/Y BRK/PRESS IND61GGC10
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN30
** 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
121VUHYDRAULIC/PARK BRK/CTL/STBY71GGN37
121VUHYDRAULIC/PARK BRK/CTL/NORM70GGN36
121VUHYDRAULIC/Y HYD/PUMP ENG2/MONG3700GDQ37
121VUHYDRAULIC/Y HYD/PUMP ENG2/CTL3701GDQ36
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN31
** ON A/C ALL
123VUY HYD/ELEC/PUMP3802GXAB06
123VUY HYD/ELEC/ELEC PUMP/NORM3801GXAB03
Subtask 32-44-11-941-051-A
E. Safety Precautions
   (1) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system:
  • on the panel 40VU in the cockpit,
  • on the ground service panel of the Yellow hydraulic system.
4. Procedure
Subtask 32-44-11-020-050-A
A. Removal of the Accumulator 2582GM
   (1) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002).
   (2) Remove the cap (10) and carefully turn the charging valve (11) to the open position to depressurize the accumulator (1).
   (3) Disconnect the connector (4) from the reducer (3).
   (4) Remove the nut (5) and the washer (6) from the reducer (3).
   (5) Remove the nuts (9), the washers (8) and release the clamps (7).
   (6) Remove the accumulator (1) from the aircraft structure.
   (7) Put the PLUG-BLANKING in each disconnected line end.
[Rev.10 from 2021] 2026.04.01 07:51:13 UTC
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