Removal of the Normal-Brake Servovalve Manifold Filter
TASK 32-42-16-000-002-A
Removal of the Normal-Brake Servovalve Manifold Filter
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 32-42-16-941-052-A
Subtask 32-42-16-020-051-B
[Rev.10 from 2021]
2026.04.01 00:47:51 UTC
Removal of the Normal-Brake Servovalve Manifold Filter
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.
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.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 3M (10 FT) |
| No specific | 1 | CONTAINER 5 L (1.32 USGAL) |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 1 | WARNING NOTICE(S) |
| 89901 | 1 | SPATULA |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 29-00-00-864-001-A | Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action |
| TASK 29-14-00-614-001-A | Depressurization of the Hydraulic Reservoirs |
| TASK 29-23-00-860-001-A | Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU) |
| TASK 32-00-00-481-001-A | Installation of the Safety Devices on the Landing Gears |
Subtask 32-42-16-941-052-A
A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Make sure that the ground safety locks are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On the panel 400VU:
Subtask 32-42-16-860-053-A (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Make sure that the ground safety locks are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On the panel 400VU:
- make sure that the landing-gear control-lever 6GA is in the DOWN position
- put a WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the landing gear.
B. Aircraft Maintenance Configuration
(2) Depressurize the Green hydraulic reservoir (Ref. AMM TASK 29-14-00-614-001).
Subtask 32-42-16-865-053-A WARNING:
OBEY THE HYDRAULIC SAFETY PROCEDURES.
(1) Make sure that the Green hydraulic system is depressurized (Ref. AMM TASK 29-00-00-864-001). (2) Depressurize the Green hydraulic reservoir (Ref. AMM TASK 29-14-00-614-001).
C. Open, safety and tag this(these) circuit breaker(s):
Subtask 32-42-16-010-052-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/MONG | 1702GK | R34 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY | 4GG | M36 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS2/CTL | 3GG | M35 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS1/CTL | 1GG | M34 |
| 121VU | HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY | 2GG | M33 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/MONG | 1702GK | R33 |
D. Get Access
(1) Put an ACCESS PLATFORM 3M (10 FT) below the applicable normal-brake servovalve manifold assembly:
(a) FOR [2613GM] (MANIFOLD-NORM BRK SERVOVALVE,L)
below zone 731
(b) FOR [2612GM] (MANIFOLD-NORM BRK SERVOVALVE,R)
below zone 741.
(2) Put a CONTAINER 5 L (1.32 USGAL) below the applicable normal-brake servovalve manifold assembly.
(3) Disconnect the isolation coupling of the PTU (Ref. AMM TASK 29-23-00-860-001).
4. Procedure(1) Put an ACCESS PLATFORM 3M (10 FT) below the applicable normal-brake servovalve manifold assembly:
(a) FOR [2613GM] (MANIFOLD-NORM BRK SERVOVALVE,L)
below zone 731
(b) FOR [2612GM] (MANIFOLD-NORM BRK SERVOVALVE,R)
below zone 741.
(2) Put a CONTAINER 5 L (1.32 USGAL) below the applicable normal-brake servovalve manifold assembly.
(3) Disconnect the isolation coupling of the PTU (Ref. AMM TASK 29-23-00-860-001).
Subtask 32-42-16-020-051-B
A. Removal of the Normal-Brake Servovalve Manifold-Filter
(2) Remove the plug (1) from the filter (4).
(3) Use the 89901 SPATULA to remove the packing (3) and the retainer (2) from the plug (1).
(4) Discard the retainer (2) and the packing (3).
(5) Remove the filter (4) from the manifold (6).
(6) Use the 89901 SPATULA to remove the packing (5) from the filter (4).
(7) Discard the filter (4) and the packing (5).
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.
WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
CAUTION:
MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER.
(1) Cut, remove and discard the lockwire from the plug (1).(2) Remove the plug (1) from the filter (4).
(3) Use the 89901 SPATULA to remove the packing (3) and the retainer (2) from the plug (1).
(4) Discard the retainer (2) and the packing (3).
(5) Remove the filter (4) from the manifold (6).
(6) Use the 89901 SPATULA to remove the packing (5) from the filter (4).
(7) Discard the filter (4) and the packing (5).
Normal-Brake Servovalve Manifold - Filter Installation Detail