W DOC AIRBUS | AMM A320F

Servicing of the Electric-Pump Case-Drain Filter


TASK 29-12-43-610-001-A
Servicing of the Electric-Pump Case-Drain 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.
FIN: 2084GM
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
2
CONTAINER 2 L (0.53 USGAL)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
2
WARNING NOTICE(S)
 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
195BB
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
FILTER ELEMENT
AIPC 29-12-43-01-020
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 12-12-29-611-001-A
Fill the Hydraulic Fluid Reservoir with a Hand Pump
TASK 29-00-00-864-001-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 29-10-00-863-003-A
Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart
TASK 29-10-00-863-003-A-01
Pressurize the Blue Hydraulic System with the Blue Electric Pump
TASK 29-10-00-864-003-A
Depressurize the Blue 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)
3. Job Set-up
Subtask 29-12-43-865-050-A
A. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUHYD/HYD PWR/B WARN/& CTL2702GJC12
123VUB HYD/ELEC PUMP2701GJAB09
Subtask 29-12-43-860-052-A
B. Aircraft Maintenance Configuration
WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.
   (1) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002).
   (2) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Blue hydraulic system:
  • In the cockpit on the hydraulic section 40VU of the overhead panel.
  • On the ground service panel of the Blue hydraulic system.
   (3) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
   (4) Depressurize the reservoir of the Blue hydraulic system (Ref. AMM TASK 29-14-00-614-001).
   (5) Put the CONTAINER 2 L (0.53 USGAL) below the filter to collect any hydraulic fluid.
Subtask 29-12-43-010-050-A
C. Open the access panel 195BB
4. Procedure
Subtask 29-12-43-020-050-A
A. Removal of the Filter Element
   (1) Cut and remove the lockwire between the filter bowl (3) and the filter head (1).
   (2) Remove the filter bowl (3) together with the filter element (2).
   (3) Remove the spring (9) and the filter element (2) from the filter bowl (3).
   (4) Discard the filter element (2).
NOTE: It is possible that the filter element (2) stays in the filter head (1) and it is necessary to pull it out.
Subtask 29-12-43-560-050-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) in the new AIPC 29-12-43-01-020 FILTER ELEMENT (2) with Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) .
   (3) Lubricate the threads of the filter bowl (3) 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 29-12-43-420-050-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 filter element (2), together with its O-ring (5) and the spring (9) in the filter bowl (3).
   (5) Engage the filter bowl (3) in the filter head (1) and tighten it.
NOTE: Tighten the filter bowl with your hands only.
Subtask 29-12-43-865-051-A
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUHYD/HYD PWR/B WARN/& CTL2702GJC12
123VUB HYD/ELEC PUMP2701GJAB09
Subtask 29-12-43-790-050-A
E. Test of the Filter
   (1) Remove the warning notice from the ground service panel of the Blue hydraulic system.
   (2) Remove the warning notice from the overhead panel.
   (3) Pressurize the Blue hydraulic reservoir (Ref. AMM TASK 29-14-00-614-002).
   (4) Pressurize the Blue hydraulic system. (Ref. AMM TASK 29-10-00-863-003)
   (5) Make sure that no hydraulic fluid comes out of the filter assembly.
   (6) Make sure that the red clogging indicator stays in.
   (7) Depressurize the Blue hydraulic system. (Ref. AMM TASK 29-10-00-864-003)
5. Close-up
Subtask 29-12-43-860-051-A
A. Put the aircraft back to the serviceable condition.
   (1) Safety the filter bowl (3) to the filter head (1) with lockwire 0.8 mm (0.032 in.).
   (2) Make sure that the fluid level in the reservoir of the Blue hydraulic system is correct. Add fluid as necessary (Ref. AMM TASK 12-12-29-611-001).
   (3) Remove the CONTAINER 2 L (0.53 USGAL) from below the filter.
Subtask 29-12-43-410-050-A
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the access panel 195BB.
[Rev.10 from 2021] 2026.04.01 04:43:57 UTC