W DOC AIRBUS | AMM A320F

Installation of the Check Valve of the Blue Electric Pump


TASK 29-12-36-400-001-A
Installation of the Check Valve of the Blue Electric Pump


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: 2050GM ** 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
CONTAINER 5 L (1.32 USGAL)
No specific
2
WARNING NOTICE(S)
No specific
Torque wrench: range to between 4.61 and 4.32 m.daN (34.00 and 31.86 lbf.ft ) T
No specific
Torque wrench: range to between 5.9 and 5.4 m.daN (43.51 and 39.82 lbf.ft ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.02ABA1)
Phosphate Ester Hydraulic Fluid-General Power - -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
195BB
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
4
O-RING
AIPC 29-12-03-12-070
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 12-12-29-611-001-A
Fill the Hydraulic Fluid Reservoir with a Hand Pump
TASK 12-12-29-611-002-A
Fill the Hydraulic Fluid Reservoir with a Hydraulic Service Cart
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 29-12-36-860-051-A ** ON A/C NOT FOR ALL
A. 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 Blue hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
   (3) Make sure that the reservoir of the Blue hydraulic system is depressurized.
(Ref. AMM TASK 29-14-00-614-001).
   (4) Make sure that the access door 195BB is open.
   (5) Make sure that the CONTAINER 5 L (1.32 USGAL) is in position below the HP manifold.
   (6) Make sure that the WARNING NOTICE(S) are 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.
Subtask 29-12-36-865-051-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUHYD/HYD PWR/B WARN/& CTL2702GJC12
123VUB HYD/ELEC PUMP2701GJAB09
4. Procedure
Subtask 29-12-36-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Check Valve
CAUTION: USE A SECOND WRENCH TO APPLY COUNTERTORQUE TO THE UNION WHEN YOU DISCONNECT/CONNECT HYDRAULIC LINES ON UNIONS. IF YOU DO NOT USE THE SECOND WRENCH, THERE IS A RISK THAT YOU WILL LOOSEN OR TIGHTEN THE UNION TOO MUCH.
CAUTION: YOU MUST INSTALL HYDRAULIC TUBES WITH HYDRAULIC FLUID AS LUBRICANT.
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Make sure that the hydraulic line end-fittings are serviceable.
   (4) Remove the blanking plugs.
   (5) Lubricate the new AIPC 29-12-03-12-070 O-RING (4) with Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) .
   (6) Put the O-ring (4) in position on the check valve (3).
   (7) Install the check valve on the Tee-fitting (5).
   (8) Hold the Tee-fitting (5) and TORQUE the check valve (3) to between 4.61 and 4.32 m.daN (34.00 and 31.86 lbf.ft ) T.
   (9) Apply Phosphate Ester Hydraulic Fluid-General Power - - (Material No.
02ABA1) to the end fitting (2).
   (10) Connect the pipe (1) to the check valve (3).
   (11) Hold the check valve (3) and TORQUE the end fitting (2) to between 5.9 and 5.4 m.daN (43.51 and 39.82 lbf.ft ) T.
Subtask 29-12-36-865-052-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUHYD/HYD PWR/B WARN/& CTL2702GJC12
123VUB HYD/ELEC PUMP2701GJAB09
Subtask 29-12-36-790-050-A ** ON A/C NOT FOR ALL
C. Test
   (1) Pressurize the reservoir of the Blue hydraulic system (
Ref. AMM TASK 29-14-00-614-002).
   (2) Make sure that the level of fluid in the reservoir of the Blue hydraulic system is correct. Add fluid as necessary (Ref. AMM TASK 12-12-29-611-001) or (Ref. AMM TASK 12-12-29-611-002).
   (3) Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
   (4) Examine the connections of the check valve (3) and make sure that there are no leaks.
   (5) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
5. Close-up
Subtask 29-12-36-942-050-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to the serviceable condition.
   (1) Remove the container.
   (2) Remove the WARNING NOTICE(S).
Subtask 29-12-36-410-050-A ** ON A/C NOT FOR ALL
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the access door 195BB.
[Rev.10 from 2021] 2026.04.01 00:19:12 UTC