Check Spoiler Servocontrol Bearing and Hinge Bearings for Excessive Play and Condition

TASK 27-64-00-200-001-A
Check Spoiler Servocontrol Bearing and Hinge Bearings for Excessive Play and Condition

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: 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: 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.

WARNING: MAKE SURE THERE ARE NO PERSONS OR EQUIPMENT NEAR THE SLATS. THE SLATS WILL MOVE WITH THE FLAPS.

ZONE: 580
ZONE: 680

1. Reason for the Job
Refer to the MPD TASK: 276400-02
CHECK SPOILER SERVOCONTROL BEARING AND HINGE BEARINGS FOR EXCESSIVE PLAY AND CONDITION
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific	AR	PLATE - CORNER
No specific	1	SCALE - GRADUATED
No specific	AR	WARNING NOTICE(S)
97A27003000005	1	GAGE,ASSY - PUSH-PULL
OR	OR
97A27003000007	1	GAGE,ASSY-PUSH-PULL
98D27603001000	1	LOAD APPLICATION TOOL - SPOILER
98D27803000000	1	LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
98D27903500000	2	PIN-SIDE STICK LOCKING

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
580	LEFT WING FLAPS AND SPOILERS
680	RIGHT WING FLAPS AND SPOILERS

C. Referenced Information

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 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 27-64-41-200-001-A	Inspection/Check of the Spoiler 1
TASK 27-64-41-400-001-A	Installation of the Spoiler 1
TASK 27-64-42-200-001-A	Inspection/Check of the Spoiler 2
TASK 27-64-42-400-001-A	Installation of the Spoiler 2
TASK 27-64-43-200-001-A	Inspection/check of the Spoiler 3
TASK 27-64-43-400-001-A	Installation of the Spoiler 3
TASK 27-64-44-200-001-A	Inspection/Check of the Spoiler 4
TASK 27-64-44-400-001-A	Installation of Spoiler 4
TASK 27-64-45-200-001-A	Inspection/Check of the Spoiler 5
TASK 27-64-45-400-001-A	Installation of the Spoiler 5
TASK 27-64-51-960-801-A	Replacement of the Spoiler Servo-Control Eye-End
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 29-23-00-863-001-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 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure
Location of the Tools

3. Job Set-up
Subtask 27-64-00-860-054-A

A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 23VU, make sure that the FLT CTL/SEC1 pushbutton switch is pushed (the FAULT and OFF legends are off).
(3) On the overhead panel 24VU, make sure that the FLT CTL/SEC2 and FLT CTL/SEC3 pushbutton switches are pushed (the FAULT and OFF legends are off).
(4) On the center pedestal, make sure that the SPEED BRAKE lever is in the RET position.
(5) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
(6) On the center pedestal, on the ECAM control panel, push the F/CTL pushbutton switch (on the lower ECAM display unit, the F/CTL page comes into view).
(7) Extend the flaps (lever in the FULL position ) (Ref. AMM TASK 27-50-00-866-008).

Subtask 27-64-00-875-058-A

B. Make sure that this(these) circuit breaker(s) is(are) closed:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/SEC1/NORM/SPLY	21CE1	B08
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/SEC1/NORM/SPLY	21CE1	B03
** ON A/C ALL
121VU	FLIGHT CONTROLS/SEC3/SPLY	21CE3	Q19
121VU	FLIGHT CONTROLS/SEC2/SPLY	21CE2	Q18

Subtask 27-64-00-865-053-A

DELETED

Subtask 27-64-00-010-055-A

D. Get Access
(1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position:
(a) At zone 580 for the spoilers 1,2,3,4,5 left side.
(b) At zone 680 for the spoilers 1,2,3,4,5 right side.

Subtask 27-64-00-480-051-A

E. Installation of the Tools
(1) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap and slat control lever.
(2) Install the 98D27903500000 PIN-SIDE STICK LOCKING on each side stick controller.
(3) Put the WARNING NOTICE(S) on the CAPT and F/O side stick and on the SPEED BRAKE control lever to tell persons not to touch them.
(4) Install the 98D27603001000 LOAD APPLICATION TOOL - SPOILER at the trailing edge of the spoiler, at the level of the servocontrol.
(5) Install the pointer of the 98D27603001000 LOAD APPLICATION TOOL - SPOILER on the trailing edge of the spoiler.
(6) Install a PLATE - CORNER on the adjacent structure.
(7) Install a SCALE - GRADUATED on the corner plate.

Subtask 27-64-00-863-051-A

F. 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).

4. Procedure
Subtask 27-64-00-210-053-A

A. Check of the Spoiler Servo-controls and Hinge Bearings for General Condition
(1) Do a visual check of the servo control bearings on surface side.
(2) Do a visual check of the spoiler hinge bearings.

Subtask 27-64-00-220-051-A

B. Check of the Spoiler Servocontrol Bearing and Hinge Bearings for too Much Play

Location of the Tools

NOTE: This check is for one surface only.
The same check is applicable to the other surfaces.

(1) On the 98D27603001000 LOAD APPLICATION TOOL - SPOILER, connect the 97A27003000007 GAGE,ASSY-PUSH-PULL97A27003000005 GAGE,ASSY - PUSH-PULL (or equivalent).
(2) Apply a force of 30 lbf (13.3447 daN) on the trailing edge, in the up direction.
(3) Make a mark of the pointer position on the SCALE - GRADUATED.
(4) Apply a force of 30 lbf (13.3447 daN) on the trailing edge, in the down direction.
(5) Make a mark of the pointer position on the SCALE - GRADUATED.
(6) Make sure that the play between the two limit positions is not more than 1.2 mm (0.0472 in.).
(7) If the measured play is more than the maximum permitted value:

Do the inspection/check of the bearings that attach the control surface to the structure, and
Do the inspection/check of the servocontrol bearings.

NOTE: The worn or damaged parts that you must replace are identified in the inspection/check AMM tasks applicable to the bearings (Ref. AMM TASK 27-64-41-200-001) (Ref. AMM TASK 27-64-42-200-001) (Ref. AMM TASK 27-64-43-200-001) (Ref. AMM TASK 27-64-44-200-001) (Ref. AMM TASK 27-64-45-200-001).

(a) If the defective bearing is a part of a spoiler, send the spoiler to the workshop to replace the bearing.
(b) If the defective bearing is the servocontrol eye-end-fitting bearing, replace the spoiler servocontrol eye-end (Ref. AMM TASK 27-64-51-960-801).
(c) Install the removed spoiler (Ref. AMM TASK 27-64-41-400-001) or (Ref. AMM TASK 27-64-42-400-001) or (Ref. AMM TASK 27-64-43-400-001) or (Ref. AMM TASK 27-64-44-400-001) or (Ref. AMM TASK 27-64-45-400-001).
(d) Go to Para. 4.B. to make sure that the measured play is not more than the maximum permitted value.

5. Close-up
Subtask 27-64-00-080-050-A

A. Removal of the Tools
(1) Remove the GAGE ASSY - PUSH-PULL TOOL 97A27003000007 GAGE,ASSY-PUSH-PULL97A27003000005 GAGE,ASSY - PUSH-PULL, the SCALE - GRADUATED, the plate, the pointer and the 98D27603001000 LOAD APPLICATION TOOL - SPOILER.
(2) Remove the 98D27903500000 PIN-SIDE STICK LOCKING from each side stick and the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap and slat control lever.
(3) Remove the WARNING NOTICE(S).

Subtask 27-64-00-860-055-A

B. Put the aircraft back to its initial configuration.
(1) Retract the FLAPS (lever in the 0 position) (Ref. AMM TASK 27-50-00-866-009).
(2) 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).
(3) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(4) Make sure that the work area is clean and clear of tools and other items.
(5) Remove the access platform(s).
(6) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.01 07:05:35 UTC