Check of the Position of the Fluid-Reserve Piston of the Elevator Servo Control with the Hydraulic Reservoirs Depressurized
TASK 27-34-00-220-001-A
Check of the Position of the Fluid-Reserve Piston of the Elevator Servo Control with the Hydraulic Reservoirs Depressurized
Refer to the MPD TASK: 273400-03
CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC RESERVOIR DEPRESSURIZED.
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 27-34-00-010-057-A
Subtask 27-34-00-220-054-A
Subtask 27-34-00-410-057-A
[Rev.10 from 2021]
2026.03.31 23:50:11 UTC
Check of the Position of the Fluid-Reserve Piston of the Elevator Servo Control with the Hydraulic Reservoirs Depressurized
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 JobRefer to the MPD TASK: 273400-03
CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC RESERVOIR DEPRESSURIZED.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 6M (20 FT) - ADJUSTABLE |
| No specific | AR | RULE |
| No specific | AR | WARNING NOTICE(S) |
| 98D27903500000 | 2 | PIN-SIDE STICK LOCKING |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 334 | THS TRAILING EDGE |
| 344 | THS TRAILING EDGE |
| 334DB, 344DB |
| REFERENCE | DESIGNATION |
|---|---|
| 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 29-10-00-863-003-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) |
| TASK 29-23-00-863-001-A | Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump |
| TASK 29-23-00-864-001-A | Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU |
| TASK 29-24-00-863-001-A | Pressurize the Yellow Hydraulic System with the Electric Pump |
| TASK 29-24-00-864-001-A | Depressurize the Yellow Hydraulic System |
| TASK 55-13-11-000-001-A | Remove/Open of the Trimmable Horizontal Stabilizer (THS) Trailing-Edge Access-Panels |
| TASK 55-13-11-400-001-A | Install/Close of the Trimmable Horizontal Stabilizer (THS) Trailing-Edge Access-Panels |
Subtask 27-34-00-010-057-A
A. Get Access
(1) Put the ACCESS PLATFORM 6M (20 FT) - ADJUSTABLE in position.
(2) Open the THS trailing edge access panels 334DB 344DB (Ref. AMM TASK 55-13-11-000-001).
Subtask 27-34-00-865-063-A (1) Put the ACCESS PLATFORM 6M (20 FT) - ADJUSTABLE in position.
(2) Open the THS trailing edge access panels 334DB 344DB (Ref. AMM TASK 55-13-11-000-001).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 27-34-00-860-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | L/G/LGCIU/SYS1/NORM | 1GA | C09 |
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| 121VU | HYDRAULIC/LGCIU/SYS1/GRND SPLY | 52GA | Q34 |
C. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 20VU, make sure that:
(4) Pressurize the aircraft hydraulic systems (Ref. AMM TASK 29-23-00-863-001) (Ref. AMM TASK 29-24-00-863-001) (Ref. AMM TASK 29-10-00-863-003).
(5) On each servo control (1), make sure that the indicator of the fluid-reserve (2) piston is in the maximum extended position.
(6) Depressurize the aircraft hydraulic systems (Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001) (Ref. AMM TASK 29-10-00-864-003).
(7) Depressurize the hydraulic reservoirs (Ref. AMM TASK 29-14-00-614-001).
(8) Put WARNING NOTICE(S) in position to tell persons not to pressurize the hydraulic systems:
(10) Install the 98D27903500000 PIN-SIDE STICK LOCKING on the CAPT and F/O side sticks.
(11) Put a WARNING NOTICE(S) on the CAPT and F/O side sticks to tell persons not to touch the side sticks.
(12) Put a WARNING NOTICE(S) on the pitch-trim control wheels to tell persons, not to use the pitch trim.
4. Procedure(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 20VU, make sure that:
- the 3 OFF/NAV/ATT selector switches are in OFF position.
(4) Pressurize the aircraft hydraulic systems (Ref. AMM TASK 29-23-00-863-001) (Ref. AMM TASK 29-24-00-863-001) (Ref. AMM TASK 29-10-00-863-003).
(5) On each servo control (1), make sure that the indicator of the fluid-reserve (2) piston is in the maximum extended position.
(6) Depressurize the aircraft hydraulic systems (Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001) (Ref. AMM TASK 29-10-00-864-003).
(7) Depressurize the hydraulic reservoirs (Ref. AMM TASK 29-14-00-614-001).
(8) Put WARNING NOTICE(S) in position to tell persons not to pressurize the hydraulic systems:
- in the cockpit, on the HYD overhead panel 40VU,
- on the ground service panels.
(10) Install the 98D27903500000 PIN-SIDE STICK LOCKING on the CAPT and F/O side sticks.
(11) Put a WARNING NOTICE(S) on the CAPT and F/O side sticks to tell persons not to touch the side sticks.
(12) Put a WARNING NOTICE(S) on the pitch-trim control wheels to tell persons, not to use the pitch trim.
Subtask 27-34-00-220-054-A
A. Check of the Position of the Fluid-Reserve Piston of the Elevator Servo Control with the Hydraulic Reservoirs Depressurized
(1) After three hours, on the fluid reserve (2), with a RULE make sure that the indicator does not retract more than 32 mm (1,2598 in.).
5. Close-up(1) After three hours, on the fluid reserve (2), with a RULE make sure that the indicator does not retract more than 32 mm (1,2598 in.).
- If the indicator retracts more than 32 mm (1.2598 in.), the pressure and return line closing valves are not sealed. You must remove the servo control (1) for repair.
Subtask 27-34-00-410-057-A
A. Close Access
(1) Close the THS trailing edge access panels 334DB 344DB (Ref. AMM TASK 55-13-11-400-001).
(2) Remove the access platform(s).
Subtask 27-34-00-860-051-A (1) Close the THS trailing edge access panels 334DB 344DB (Ref. AMM TASK 55-13-11-400-001).
(2) Remove the access platform(s).
B. Put the Aircraft Back to its Initial Configuration
(1) Remove the 98D27903500000 PIN-SIDE STICK LOCKING from the CAPT and F/O side sticks.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Remove the WARNING NOTICE(S).
(4) Pressurize the hydraulic reservoirs (Ref. AMM TASK 29-14-00-614-002).
(5) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(1) Remove the 98D27903500000 PIN-SIDE STICK LOCKING from the CAPT and F/O side sticks.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Remove the WARNING NOTICE(S).
(4) Pressurize the hydraulic reservoirs (Ref. AMM TASK 29-14-00-614-002).
(5) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Elevator Servo Control