W DOC AIRBUS | AMM A320F

Installation of the Alternate-Brake Servovalve Manifold


TASK 32-43-31-400-001-A
Installation of the Alternate-Brake Servovalve Manifold


WARNING: MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
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.
FIN: 2614GM ** ON A/C NOT FOR ALL
FIN: 2615GM ** ON A/C NOT FOR ALL
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)
No specific
AR
SAFETY BARRIER(S)
No specific
AR
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 20-21-11-911-001-A
Tightening Torques for Standard Threaded Fasteners
TASK 20-23-11-917-001-A
Tightening Practices for Hydraulic Connections
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 29-23-00-860-001-A
Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU)
TASK 29-23-00-860-002-A
Connection of the Isolation Coupling of the Power Transfer Unit (PTU)
TASK 32-00-00-481-001-A
Installation of the Safety Devices on the Landing Gears
TASK 32-43-00-710-001-A
Operational Check of Alternate Braking System
TASK 32-43-00-870-002-A
Bleeding of the High Pressure Alternate Braking System
3. Job Set-up
Subtask 32-43-31-941-052-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Make sure that the SAFETY BARRIER(S) are in position.
   (2) Make sure that the ground safety locks are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
   (3) On the panel 400VU:
  • make sure that the landing-gear control-lever 6GA is in the DOWN position
  • make sure that the WARNING NOTICE(S) is in position to tell persons not to operate the landing gear.
   (4) Make sure that the WARNING NOTICE(S) is in position to tell persons not to pressurize the Yellow hydraulic system.
Subtask 32-43-31-860-050-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable false spar at the alternate-brake servovalve manifold.
   (2) Make sure that the Yellow hydraulic system has been depressurized (Ref. AMM TASK 29-00-00-864-001).
   (3) Make sure that the pressure in the brake accumulator of the Yellow hydraulic system is at zero.
   (4) Make sure that the isolation coupling of the PTU is disconnected (Ref. AMM TASK 29-23-00-860-001).
Subtask 32-43-31-865-051-A ** ON A/C NOT FOR ALL
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR 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/HYD POWER/Y3803GXN30
123VUY HYD/ELEC/PUMP3802GXAB06
123VUY HYD/ELEC/ELEC PUMP/NORM3801GXAB03
4. Procedure
Subtask 32-43-31-420-051-A ** ON A/C NOT FOR ALL
A. Preparation for Installation
   (1) Clean the component interface and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (4) Remove the CAP - BLANKING from the hydraulic and the electrical connectors.
   (5) Make sure that the hydraulic line end-fittings are serviceable.
Subtask 32-43-31-420-050-A ** ON A/C NOT FOR ALL
B. Installation of the Alternate-Brake Servovalve Manifold

   (1) Install the manifold (2) with the four bolts (4).
   (2) Tighten the four bolts (4) (Ref. AMM TASK 20-21-11-911-001).
   (3) Connect the hydraulic connectors (3) and (5) (Ref. AMM TASK 20-23-11-917-001).
   (4) Connect the electrical connectors (1).
   (5) Make sure that the work area is clean and clear of tools and other items.
Subtask 32-43-31-865-052-A ** ON A/C NOT FOR ALL
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR 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/HYD POWER/Y3803GXN30
123VUY HYD/ELEC/PUMP3802GXAB06
123VUY HYD/ELEC/ELEC PUMP/NORM3801GXAB03
Subtask 32-43-31-860-052-A ** ON A/C NOT FOR ALL
D. Aircraft Configuration
   (1) Connect the isolation coupling of the PTU (Ref. AMM TASK 29-23-00-860-002).
Subtask 32-43-31-870-050-A ** ON A/C NOT FOR ALL
E. Bleed the Brake System
   (1) Bleed the alternate brake system (Ref. AMM TASK 32-43-00-870-002).
Subtask 32-43-31-710-050-A ** ON A/C NOT FOR ALL
F. Test
   (1) Do an operational test of the alternate brake system (Ref. AMM TASK 32-43-00-710-001).
   (2) Make sure that there are no hydraulic leaks at the hydraulic connectors (3) and (5).
5. Close-up
Subtask 32-43-31-942-050-A ** ON A/C NOT FOR ALL
A. Removal of Equipment
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the SAFETY BARRIER(S).
   (3) Remove the WARNING NOTICE(S).
   (4) Remove the access platform(s).
   (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 00:49:07 UTC