Reclamation of the Hydraulic Fluid in the Blue Hydraulic System
TASK 12-36-29-600-006-A
Reclamation of the Hydraulic Fluid in the Blue Hydraulic System
1. Reason for the Job
To decrease the particle contamination of the hydraulic fluid in the Blue hydraulic system if it is more than NSA307110 class 9.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 12-36-29-860-119-A Subtask 12-36-29-010-082-A Subtask 12-36-29-860-118-A
Subtask 12-36-29-960-065-A
Subtask 12-36-29-860-117-A
[Rev.10 from 2021]
2026.04.02 06:10:40 UTC
Reclamation of the Hydraulic Fluid in the Blue Hydraulic System
1. Reason for the Job
To decrease the particle contamination of the hydraulic fluid in the Blue hydraulic system if it is more than NSA307110 class 9.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| ALT29000001 | 1 | HYD GRND PWR UNIT3000 |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 195BB, 197EB, 197FB |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-32-29-281-001-A | Analyze Hydraulic Fluid |
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| 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 29-12-43-610-001-A | Servicing of the Electric-Pump Case-Drain Filter |
| TASK 29-12-44-610-001-A | Servicing of the LP-Filter |
| TASK 29-12-45-610-001-A | Servicing of the HP-Filter |
Subtask 12-36-29-860-119-A Subtask 12-36-29-010-082-A Subtask 12-36-29-860-118-A
C. Preparation for the Reclamation Procedure
(1) Connect the pressure hose of the ALT29000001 HYD GRND PWR UNIT3000 to the delivery connector 2008GM.
(2) Connect the return hose of the hydraulic power cart to the suction connector 2006GM.
4. Procedure(1) Connect the pressure hose of the ALT29000001 HYD GRND PWR UNIT3000 to the delivery connector 2008GM.
(2) Connect the return hose of the hydraulic power cart to the suction connector 2006GM.
Subtask 12-36-29-960-065-A
A. Replacement of the Filter Elements
(1) Replace the element in the LP filter 2002GM (Ref. AMM TASK 29-12-44-610-001).
(2) Replace the element in the HP filter 2048GM (Ref. AMM TASK 29-12-45-610-001).
(3) Replace the element in the case drain filter 2084GM (Ref. AMM TASK 29-12-43-610-001).
Subtask 12-36-29-869-078-A (1) Replace the element in the LP filter 2002GM (Ref. AMM TASK 29-12-44-610-001).
(2) Replace the element in the HP filter 2048GM (Ref. AMM TASK 29-12-45-610-001).
(3) Replace the element in the case drain filter 2084GM (Ref. AMM TASK 29-12-43-610-001).
B. Reclamation Procedure
(2) Operate the hydraulic power cart.
(3) In the cockpit, operate the flight controls.
(a) On the panel 11VU, move the GND SPLRS ARMED lever to the FULL position and then to the RET position. Do this step 3 times.
Subtask 12-36-29-281-052-A 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.
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002). (2) Operate the hydraulic power cart.
(3) In the cockpit, operate the flight controls.
(a) On the panel 11VU, move the GND SPLRS ARMED lever to the FULL position and then to the RET position. Do this step 3 times.
NOTE: The spoilers 3 LH and RH operate.
(b) On the panel 18VU or 19VU, move the side stick fully to the left and then fully to the right. Do this step 3 times. NOTE: The ailerons and spoilers 3 LH and RH operate.
(c) On the panel 18VU or 19VU, move the side stick fully forward and then fully rearward. Do this step 3 times. NOTE: The elevators operate.
(d) At the captain or first officer position, push the LH pedal fully forward and then the RH pedal fully forward. Do this step 3 times. NOTE: The rudder operates.
(e) On the panel 114VU, move the flap/slat lever to the FULL position and then to the 0 deg. position. Do this step 2 times. NOTE: The slats operate.
(4) Stop the hydraulic power cart. C. Sampling Procedure
(1) Take a sample from the Blue hydraulic system and make an analysis (Ref. AMM TASK 12-32-29-281-001).
(2) If the particle contamination is more than NSA307110 class 9, do the procedure again.
Subtask 12-36-29-010-083-A Subtask 12-36-29-869-073-A (1) Take a sample from the Blue hydraulic system and make an analysis (Ref. AMM TASK 12-32-29-281-001).
(2) If the particle contamination is more than NSA307110 class 9, do the procedure again.
E. Make sure that the clogging indicators on the filters 2002GM, 2048GM and 2084GM are in (the filter is not clogged).
5. Close-upSubtask 12-36-29-860-117-A
A. Put the system back to the serviceable condition.
(1) Disconnect the pressure hose of the hydraulic power cart from the delivery connector 2008GM.
(2) Disconnect the return hose of the hydraulic power cart from the suction connector 2006GM.
Subtask 12-36-29-410-070-A (1) Disconnect the pressure hose of the hydraulic power cart from the delivery connector 2008GM.
(2) Disconnect the return hose of the hydraulic power cart from the suction connector 2006GM.
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access panel/doors 195BB 197FB 197EB.
Subtask 12-36-29-860-120-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access panel/doors 195BB 197FB 197EB.
C. Put the aircraft back to the serviceable condition.
(1) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(2) Remove the warning notices and safety barriers.
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(2) Remove the warning notices and safety barriers.
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.