DOC AIRBUS | AMM A320FLubricate Spoiler No 1 to 5 Actuator Attachments
TASK 12-22-27-640-005-A
Lubricate Spoiler No 1 to 5 Actuator Attachments
Refer to the MPD TASK: 276400-01
LUBRICATE SPOILER NO 1 TO 5 ACTUATOR ATTACHMENTS
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 12-22-27-941-055-A
Subtask 12-22-27-640-054-A
Subtask 12-22-27-410-065-A
[Rev.10 from 2021]
2026.03.31 22:56:36 UTC
Lubricate Spoiler No 1 to 5 Actuator Attachments
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.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
1. Reason for the Job- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Refer to the MPD TASK: 276400-01
LUBRICATE SPOILER NO 1 TO 5 ACTUATOR ATTACHMENTS
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 1 | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.03GBC1) | Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - |
| (Material No.03GBD1) | Synthetic Oil base Grease-General Purpose Lithium Thickened - |
| (Material No.03HBD9) | Synthetic Ester base Grease-General Purpose Low Temp - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 575 | AFT OUTBD SE OF WING AND TE FIXED STRUCT |
| 675 | AFT OUTBD SE OF WING AND TE FIXED STRUCT |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 27-50-00-866-008-A | Extension of the Flaps on the Ground |
| TASK 27-50-00-866-008-A-01 | Extension of the Flaps/Slats on the Ground |
| TASK 27-50-00-866-009-A | Retraction of the Flaps on the Ground |
| TASK 27-50-00-866-009-A-01 | Retraction of the Flaps/Slats on the Ground |
| TASK 27-60-00-866-002-A | Extension-Retraction of the Spoilers for Maintenance |
| TASK 27-64-00-710-001-A | Operational Test of the Spoiler Hydraulic Actuation |
| TASK 12-22-00-00 | LUBRICATION - DESCRIPTION AND OPERATION |
Spoiler Servo Control Bearing - Lubrication PointSubtask 12-22-27-941-055-A
A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 12-22-27-866-054-A (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
B. Aircraft Maintenance Configuration
(1) Extend the flaps fully (Ref. AMM TASK 27-50-00-866-008).
(2) On panel 114VU, make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is installed on the flap/slat control lever.
(3) Put a WARNING NOTICE(S) on the flap/slat control lever (panel 114VU) to tell persons not to operate the flap system.
(4) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position under the applicable spoiler.
Subtask 12-22-27-865-058-A (1) Extend the flaps fully (Ref. AMM TASK 27-50-00-866-008).
(2) On panel 114VU, make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is installed on the flap/slat control lever.
(3) Put a WARNING NOTICE(S) on the flap/slat control lever (panel 114VU) to tell persons not to operate the flap system.
(4) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position under the applicable spoiler.
C. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C ALL | |||
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
Subtask 12-22-27-640-054-A
A. Lubrication of Spoiler No.1 to 5 Servo Control Bearings
(1) Clean the greasers with a clean Textile-Lint free Cotton - (Material No.14SBA1) .
(2) Lubricate the spoiler servo-control bearings through the greasers with one of the greases that follow:
1 If the grease comes out from the greaser, extend the related spoiler (Ref. AMM TASK 27-60-00-866-002).
2 Lubricate the spoiler servo-control bearings through the greaser until the grease comes out on each side of the spherical bearings.
(3) Remove the unwanted grease from the greasers and the spoiler servo-control bearings with a clean Textile-Lint free Cotton - (Material No.14SBA1) .
(4) After lubrication of the spoiler servo-control bearings, make sure that the greaser ball is installed correctly.
(5) If the spoiler is extended, retract it (Ref. AMM TASK 27-60-00-866-002).
5. Close-up(1) Clean the greasers with a clean Textile-Lint free Cotton - (Material No.14SBA1) .
(2) Lubricate the spoiler servo-control bearings through the greasers with one of the greases that follow:
- Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9)
- Synthetic Oil base Grease-General Purpose Lithium Thickened - (Material No.03GBD1)
- Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - (Material No.03GBC1) .
NOTE: For lubricant grease specification and lubrication requirements, refer to (Ref. AMM D/O 12-22-00-00).
(a) Make sure that the grease comes out on each side of the spherical bearings: 1 If the grease comes out from the greaser, extend the related spoiler (Ref. AMM TASK 27-60-00-866-002).
2 Lubricate the spoiler servo-control bearings through the greaser until the grease comes out on each side of the spherical bearings.
(3) Remove the unwanted grease from the greasers and the spoiler servo-control bearings with a clean Textile-Lint free Cotton - (Material No.14SBA1) .
(4) After lubrication of the spoiler servo-control bearings, make sure that the greaser ball is installed correctly.
(5) If the spoiler is extended, retract it (Ref. AMM TASK 27-60-00-866-002).
Subtask 12-22-27-410-065-A
A. Close Access
(1) Remove the access platform(s).
Subtask 12-22-27-865-059-A (1) Remove the access platform(s).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 12-22-27-710-055-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C ALL | |||
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
C. Operational Test
(1) Do the operational test of the spoiler hydraulic actuation (Ref. AMM TASK 27-64-00-710-001).
Subtask 12-22-27-866-055-A (1) Do the operational test of the spoiler hydraulic actuation (Ref. AMM TASK 27-64-00-710-001).
D. Aircraft Configuration
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Retract the flaps fully (Ref. AMM TASK 27-50-00-866-009).
Subtask 12-22-27-942-055-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Retract the flaps fully (Ref. AMM TASK 27-50-00-866-009).
E. Removal of the Equipment
(1) Remove the safety barriers.
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the safety barriers.
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.