W DOC AIRBUS | AMM A320F

Flushing of the Blue Hydraulic System of the Constant Speed Motor/Generator (CSM/G)


TASK 12-36-29-170-011-A
Flushing of the Blue Hydraulic System of the Constant Speed Motor/Generator (CSM/G)


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.
WARNING: DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO:
  • FLUSH IT AWAY WITH CLEAN WATER
  • GET MEDICAL AID.
FIN: 8XE
1. Reason for the Job
To flush the Blue hydraulic System after a failure in the CSM/G 8XE.
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
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
1
CONTAINER 5 L (1.32 USGAL)
No specific
1
LOCALLY MANUFACTURED - ADAPTER
No specific
AR
PLUG - BLANKING
No specific
AR
SAFETY BARRIER(S)
No specific
1
WARNING NOTICE(S)
ALT29000001
1
HYD GRND PWR UNIT3000
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
197EB, 197FB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
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 29-12-44-610-001-A
Servicing of the LP-Filter
TASK 29-14-00-614-001-A
Depressurization of the Hydraulic Reservoirs
TASK 32-12-00-010-001-A
Open the Main Gear Doors for Access
TASK 32-12-00-410-001-A
Close the Main Gear Doors after Access
3. Job Set-up
Subtask 12-36-29-860-080-A
A. Aircraft Maintenance Configuration
   (1) Obey the hydraulic safety procedure (Ref. AMM TASK 29-00-00-910-002).
   (2) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
   (3) Depressurize the reservoir of the Blue hydraulic system (Ref. AMM TASK 29-14-00-614-001).
   (4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 12-36-29-010-094-A
B. Get Access
   (1) Open the left MLG door (Ref. AMM TASK 32-12-00-010-001).
   (2) Open the access doors 197EB 197FB.
Subtask 12-36-29-860-081-A
C. Preparation for the Flushing Procedure
   (1) Put the WARNING NOTICE(S) in position.
   (2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
   (3) Put an ACCESS PLATFORM 2M (6 FT) in position at the Zone 147.
   (4) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the Zone 197.
   (5) Put a CONTAINER 5 L (1.32 USGAL) in position to collect the hydraulic fluid below:
  • the CSM/G 8XE,
  • the LP filter 2002GM.
   (6) Disconnect the case drain line from the LP filter 2002GM.
   (7) Disconnect the pressure line from the CSM/G 8XE.
   (8) Disconnect the case drain line from the CSM/G 8XE.
   (9) Connect the pressure line to the case drain line at the CSM/G 8XE with a union.
CAUTION: MAKE SURE THAT THE FLOW RATE AND THE SUPPLY PRESSURE ON THE GROUND HYDRAULIC CART ARE SET TO A MINIMUM.
   (10) Put the ALT29000001 HYD GRND PWR UNIT3000 in position as necessary.
   (11) Connect the pressure hose of the ALT29000001 HYD GRND PWR UNIT3000 to the delivery connector 2008GM with an LOCALLY MANUFACTURED - ADAPTER.
   (12) Connect the return hose of the ALT29000001 HYD GRND PWR UNIT3000 to the case drain line at the LP filter 2002GM with an LOCALLY MANUFACTURED - ADAPTER.
   (13) Put the PLUG-BLANKING in each disconnected line end.
4. Procedure
Subtask 12-36-29-170-060-A
A. Flush the Blue hydraulic system.
   (1) Operate the hydraulic power cart for 20 s at 20 bar (290.0754 psi).
   (2) Stop the hydraulic power cart.
Subtask 12-36-29-960-060-A
B. Replace the LP filter element (Ref. AMM TASK 29-12-44-610-001).
5. Close-up
Subtask 12-36-29-860-082-A
A. Put the system back to the serviceable condition.
   (1) Disconnect the pressure hose of the hydraulic power cart and the adaptor from the delivery connector 2008GM.
   (2) Disconnect the return hose of the hydraulic power cart and the adaptor from the case drain line.
   (3) Disconnect and remove the union from the case drain line and the pressure line at the CSM/G 8XE.
   (4) Remove the hydraulic power cart.
   (5) Remove the blanking plugs.
   (6) Connect the case drain line to the LP filter 2002GM.
   (7) Connect the case drain line to the CSM/G 8XE.
   (8) Connect the pressure line to the CSM/G 8XE.
Subtask 12-36-29-790-060-A
B. Leak Test of the Components which were Disconnected
   (1) Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
   (2) Make sure that there is no hydraulic fluid leakage.
   (3) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
Subtask 12-36-29-942-099-A
C. Put the aircraft back to its initial configuration.
   (1) Remove the containers.
   (2) Remove the safety barriers.
   (3) Remove the access platform(s).
   (4) Remove the WARNING NOTICE(S).
Subtask 12-36-29-410-081-A
D. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the left MLG door (Ref. AMM TASK 32-12-00-410-001).
   (3) Close the access door 197EB 197FB.
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.02 06:10:39 UTC