W DOC AIRBUS | AMM A320F

Servicing of the HP-Filter


TASK 29-13-45-610-001-A
Servicing of the HP-Filter


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.
WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
ZONE: 196
FIN: 3048GM
1. Reason for the Job
  • Replace the filter element.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
CONTAINER 3 L(3/4 USGAL)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
1
WARNING NOTICE(S)
ALT29000001
1
HYD GRND PWR UNIT3000
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.02ABA1)
Phosphate Ester Hydraulic Fluid-General Power - -
No specific
lockwire 0.8 mm (0.032 in.)
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
196
HYDRAULIC COMPT AND FAIRINGS
196BB
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
FILTER ELEMENT
AIPC 29-13-45-01-020
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 12-12-29-611-001-A
Fill the Hydraulic Fluid Reservoir with a Hand Pump
TASK 29-00-00-280-006-A
Check of the Green or Yellow Hydraulic System after Engine Pump Failure or Operation in a Possible Cavitation Condition - with Ground Cart Available
TASK 29-00-00-280-006-A-01
Check of the Green or Yellow Hydraulic System after Engine Pump Failure or Operation in a Possible Cavitation Condition - Ground Cart not Available
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 29-10-00-863-002-A
Pressurize the Yellow Hydraulic System with a Hydraulic Ground Power-Cart
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 29-14-00-614-002-A
Pressurization of the Hydraulic Reservoirs through the Ground Connector
TASK 29-14-00-614-002-A-01
Pressurization of the Hydraulic Reservoirs with the Auxiliary Power Unit (APU)
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)
3. Job Set-up
Subtask 29-13-45-865-050-A
A. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN30
** 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 29-13-45-941-050-A
B. Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Yellow hydraulic system:
  • in the cockpit on the hydraulic section 40VU of the overhead panel
  • on the ground service panel of the Yellow hydraulic system.
Subtask 29-13-45-010-050-A
C. Open the access panel 196BB.
Subtask 29-13-45-860-050-A
D. Aircraft Maintenance Configuration
WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.
   (1) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002).
   (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
   (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. AMM TASK 29-14-00-614-001).
   (4) Disconnect the isolation coupling of the Power Transfer Unit (PTU) (Ref. AMM TASK 29-23-00-860-001).
   (5) Put the CONTAINER 3 L(3/4 USGAL) below the filter to collect any hydraulic fluid.
4. Procedure
Subtask 29-13-45-020-050-A
A. Removal of the Filter Element
   (1) Cut and remove the lockwire between the filter bowl (1) and the filter head (3).
   (2) Remove the filter bowl (1) together with the filter element (2).
   (3) Remove the filter element (2) from the filter bowl (1). Discard the filter element (2).
NOTE: It is possible that the filter element (2) will stay in the filter head (3). If it does, pull it out.
   (4) Examine the filter element in order to find the causes of contamination:
     (a) If you find metal particles in the filter element you must check the associated hydraulic system after operation of the engine pump in possible cavitation condition (Ref. AMM TASK 29-00-00-280-006).
NOTE: It is not necessary to do the check of the associated hydraulic systems if you find non-metalic particles.
Subtask 29-13-45-560-050-A
B. Preparation for Installation
   (1) Do a check of the correct condition and installation of the O-ring (5).
NOTE: The O-ring (5) is part of the filter element (2).
   (2) Lubricate the O-ring (5) of the new AIPC 29-13-45-01-020 FILTER ELEMENT (2) with Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) .
   (3) Lubricate the threads of the filter bowl (1) with Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) .
   (4) If the red clogging indicator (4) is out, push it in to set it again.
Subtask 29-13-45-420-050-A
C. Installation of the Filter Element
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Do a check of the filter element (2) and make sure that it is clean and not damaged.
   (4) Install the new filter element (2), together with its O-ring (5), in the filter bowl (1).
   (5) Engage the filter bowl (1) in the filter head (3) and tighten it with your hands.
NOTE: If it is not possible to tighten the filter bowl (1), caught pressure upstream of the filter bowl may be the cause. Connect a ALT29000001 HYD GRND PWR UNIT3000 to the aircraft connectors 3006GM and 3008GM to release this pressure.
Subtask 29-13-45-942-050-A
D. Remove the WARNING NOTICE(S).
Subtask 29-13-45-865-051-A
E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN30
** 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 29-13-45-790-050-A
F. Test of the Filter Assembly
   (1) Pressurize the reservoir of the Yellow hydraulic system (Ref. AMM TASK 29-14-00-614-002).
   (2) Pressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-863-002).
   (3) Make sure that the clogging indicator stays in.
   (4) Make sure that no hydraulic fluid comes out of the filter assembly.
   (5) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002).
5. Close-up
Subtask 29-13-45-860-052-A
A. Put the aircraft back to the serviceable condition.
   (1) Safety the filter bowl (1) to the filter head (3) with lockwire 0.8 mm (0.032 in.).
   (2) Make sure that the fluid level in the Yellow reservoir is correct. Add fluid as necessary (Ref. AMM TASK 12-12-29-611-001).
   (3) Remove the container from below the filter.
   (4) Connect the PTU isolation coupling (Ref. AMM TASK 29-23-00-860-002).
   (5) Make sure that the work area is clean and clear of tools and other items.
Subtask 29-13-45-410-050-A
B. Close the access panel 196BB.
[Rev.10 from 2021] 2026.04.01 00:21:51 UTC