Deactivation of Spoiler Servo-Controls 1 and 2

TASK 27-64-00-040-002-A
Deactivation of Spoiler Servo-Controls 1 and 2

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: DO NOT DO THIS DEACTIVATION PROCEDURE IF THERE IS EXTERNAL LEAKAGE ON THE UNSERVICEABLE SERVOCONTROL.

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.

ZONE: 580
ZONE: 680
FIN: 31CE1
FIN: 31CE2
FIN: 31CE3
FIN: 31CE4

1. Reason for the Job
MMEL 27-64-04A
SPOILERS 1 AND 2
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific	AR	CAP - BLANKING
No specific	AR	TIE WRAP
No specific	AR	TOMMY BAR DIA 4 MM (0,157 IN) - METALLIC
No specific	AR	WARNING NOTICE(S)
98D27603002000	1	KEY-SPOILER MAINTENANCE
OR	OR
98D27603002001	1	KEY-SPOILER MAINTENANCE
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
FOR [31CE1] (SERVO CTL-SPLR1, L G)
573BB
FOR [31CE2] (SERVO CTL-SPLR1, R G)
673BB
FOR [31CE3] (SERVO CTL-SPLR2, L Y)
575BB
FOR [31CE4] (SERVO CTL-SPLR2, R Y)
675BB

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 27-64-00-710-001-A	Operational Test of the Spoiler Hydraulic Actuation
TASK 27-64-51-000-004-A	Removal of the Spoiler Servo Control
TASK 27-64-51-400-004-A	Installation of the Spoiler Servo Control
TASK 29-23-00-864-001-A	Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU
TASK 29-24-00-864-001-A	Depressurize the Yellow Hydraulic System
Deactivation and Reactivation of the Servo-Control
FOR [31CE1] (SERVO CTL-SPLR1, L G)
TASK 57-51-37-000-002-A	Removal of the Access Panels 571AB(671AB), 573AB(673AB), 573BB(673BB), 573CB(673CB), 573EB(673EB)
TASK 57-51-37-400-002-A	Installation of the Access Panels 571AB(671AB), 573AB(673AB), 573BB(673BB), 573CB(673CB), 573EB(673EB)
FOR [31CE2] (SERVO CTL-SPLR1, R G)
TASK 57-51-37-000-002-A	Removal of the Access Panels 571AB(671AB), 573AB(673AB), 573BB(673BB), 573CB(673CB), 573EB(673EB)
TASK 57-51-37-400-002-A	Installation of the Access Panels 571AB(671AB), 573AB(673AB), 573BB(673BB), 573CB(673CB), 573EB(673EB)
FOR [31CE3] (SERVO CTL-SPLR2, L Y)
TASK 57-51-37-000-004-A	Removal of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB)
TASK 57-51-37-400-004-A	Installation of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB)
FOR [31CE4] (SERVO CTL-SPLR2, R Y)
TASK 57-51-37-000-004-A	Removal of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB)
TASK 57-51-37-400-004-A	Installation of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB)

3. Job Set-up
Subtask 27-64-00-860-067-A

A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Extend the flaps (Ref. AMM TASK 27-50-00-866-008).
(3) On the overhead panel, on FLT CTL panel 24VU, release the SEC 3 pushbutton switch (the OFF legend comes on).
(4) Depressurize the hydraulic system related to the spoiler that you must deactivate:
(a) For spoiler 1, depressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-864-001).
(b) For spoiler 2, depressurize the Yellow hydraulic system (Ref. AMM TASK 29-24-00-864-001).
(5) Before you deactivate a servo-control, make sure that it has no external leaks.

Subtask 27-64-00-941-061-A

B. Safety Precautions
(1) On the CAPT and F/O side-stick assemblies:

Put the 98D27903500000 PIN-SIDE STICK LOCKING in position.
Put the WARNING NOTICE(S) in position to tell persons not to touch them.

Subtask 27-64-00-010-061-A

C. Get Access
(1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position in:
(a) Zone 580 for the left spoilers
(b) Zone 680 for the right spoilers.
(2) Open the applicable access panels:
(a) FOR [31CE1] (SERVO CTL-SPLR1, L G)
Access panel 573BB (Ref. AMM TASK 57-51-37-000-002)
(b) FOR [31CE2] (SERVO CTL-SPLR1, R G)
Access panel 673BB (Ref. AMM TASK 57-51-37-000-002)
(c) FOR [31CE3] (SERVO CTL-SPLR2, L Y)
Access panel 575BB (Ref. AMM TASK 57-51-37-000-004)
(d) FOR [31CE4] (SERVO CTL-SPLR2, R Y)
Access panel 675BB (Ref. AMM TASK 57-51-37-000-004).

4. Procedure
Subtask 27-64-00-040-053-B

A. Deactivation of the Spoiler Servo-Control

NOTE: When you deactivate a spoiler servo-control, it is not necessary to deactivate the symmetrical spoiler servo-control on the other wing (the Spoiler Elevator Computer (SEC) deactivates the symmetrical spoiler servo-control automatically).

(1) If there is no plate with the 'O' and 'M' indications on the maintenance device (PRE VSB 31077-27-15 or PRE VSB 31077-27-08):
(a) Put the servo-control in the Maintenance position:

CAUTION: DO NOT APPLY A HIGH TORQUE LOAD ON THE KEY SPOILER MAINTENANCE TOOL WHEN YOU SET THE SERVOCONTROL TO OPERATIONAL MODE OR MAINTENANCE MODE. IF YOU APPLY A HIGH TORQUE LOAD, IT CAN CAUSE DAMAGE TO THE TOOL AND/OR TO THE SERVOCONTROL.

1 Install the 98D27603002000 KEY-SPOILER MAINTENANCE98D27603002001 KEY-SPOILER MAINTENANCE (3) on the servo-control and turn it a quarter turn counterclockwise.

NOTE: The necessary torque to operate the maintenance device is 0.350 m.daN (30.97 lbf.in). If 0.350 m.daN (30.97 lbf.in) is not sufficient to turn the KEY-SPOILER MAINTENANCE, it is possible that the maintenance device is damaged. To prevent more damage to the maintenance device, remove the spoiler servo-control and send it back to the supplier for analysis.

2 If you cannot turn the spoiler maintenance key, use the TOMMY BAR DIA 4 MM (0,157 IN) - METALLIC.
(b) Disconnect the electrical connector (2) from the receptacle (1) of the servo-control.
(c) Put the CAP - BLANKING on the electrical connector (2) and the receptacle (1).
(d) Attach the electrical connector (2) to a hydraulic line with the TIE WRAP.
(e) Make sure that the spoiler is in the fully retracted position.
(f) Make sure that the defective servo-control stays hydraulically connected to the aircraft hydraulic system.
(g) Put the servo-control in the Operation position:

1 Turn the 98D27603002000 KEY-SPOILER MAINTENANCE98D27603002001 KEY-SPOILER MAINTENANCE (3) a quarter turn clockwise and remove it.

2 If you cannot turn the spoiler maintenance key, use the TOMMY BAR DIA 4 MM (0,157 IN) - METALLIC.
(h) Make sure that the work area is clean and clear of tools and other items.
(i) Make sure that you cannot move the spoiler manually:

CAUTION: MAKE SURE THAT NO SPOILER MAINTENANCE KEY STAYS ENGAGED IN THE MAINTENANCE DEVICE HOUSING. AERODYNAMIC FORCES WILL CAUSE UNWANTED MOVEMENT OF THE SPOILER IF THE MAINTENANCE KEY STAYS IN ITS HOUSING.

1 Gradually apply a manual force on the spoiler surface trailing-edge.
a If you can extend the spoiler manually with the servo-control in the Operation position, replace the spoiler servo-control (Ref. AMM TASK 27-64-51-000-004) and (Ref. AMM TASK 27-64-51-400-004).
(2) If there is a plate with the 'O' and 'M' indications on the maintenance device (POST GOODRICH VSB 31077-27-15):
(a) Put the servo-control in the Maintenance position:

1 Install the 98D27603002000 KEY-SPOILER MAINTENANCE98D27603002001 KEY-SPOILER MAINTENANCE (3) on the servo-control and turn it a quarter turn counterclockwise to the 'M' position (Maintenance).

1 Turn the 98D27603002000 KEY-SPOILER MAINTENANCE98D27603002001 KEY-SPOILER MAINTENANCE (3) a quarter turn clockwise to the 'O' position (Operation) and remove it.

CAUTION: MAKE SURE THAT THE STOP OF THE HEXAGONAL-HEAD CONTROL SWITCH IS AGAINST THE LETTER 'O' ON THE HOUSING. IF IT IS AGAINST THE LETTER 'M', AERODYNAMIC FORCES WILL CAUSE UNWANTED MOVEMENT OF THE SPOILER AND POSSIBLE DAMAGE TO EQUIPMENT.

1 Gradually apply a manual force on the spoiler surface trailing-edge and make sure that you cannot extend the spoiler.
a If you can extend the spoiler manually with the servo-control in the Operation position, replace the spoiler servo-control (Ref. AMM TASK 27-64-51-000-004) and (Ref. AMM TASK 27-64-51-400-004).

Subtask 27-64-00-410-063-A

B. Preparation of the Test
(1) On the overhead panel, on FLT CTL panel 24VU, push the SEC 3 pushbutton switch (the OFF legend goes off).
(2) On the ECAM control panel, push the F/CTL key.
(a) On the lower ECAM Display Unit (DU), the F/CTL page comes into view.
(3) Retract the flaps (Ref. AMM TASK 27-50-00-866-009).
(4) Remove the 98D27903500000 PIN-SIDE STICK LOCKING and the WARNING NOTICE(S) from each side stick assembly.

Subtask 27-64-00-710-058-A

C. Operational Test of the Spoiler
(1) During the operational test:
(a) Do a visual check from the ground:

Make sure that the spoiler that has the deactivated servo-control and its symmetrical spoiler on the other wing do not extend when you operate them.
Make sure that the spoilers are in the fully retracted position.

(b) In the cockpit, on the SD, make sure that :

The spoiler that has the deactivated servo-control and its symmetrical spoiler on the other wing stay amber.
The amber F/CTL SPOILER FAULT message is shown on the Engine/Warning Display (EWD).

(2) Do the operational test of the spoilers (Ref. AMM TASK 27-64-00-710-001).

5. Close-up
Subtask 27-64-00-410-065-A

A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the applicable access panels:
(a) FOR [31CE1] (SERVO CTL-SPLR1, L G)
Access panel 573BB (Ref. AMM TASK 57-51-37-400-002)
(b) FOR [31CE2] (SERVO CTL-SPLR1, R G)
Access panel 673BB (Ref. AMM TASK 57-51-37-400-002)
(c) FOR [31CE3] (SERVO CTL-SPLR2, L Y)
Access panel 575BB (Ref. AMM TASK 57-51-37-400-004)
(d) FOR [31CE4] (SERVO CTL-SPLR2, R Y)
Access panel 675BB (Ref. AMM TASK 57-51-37-400-004).
(3) Remove the access platform(s).

Subtask 27-64-00-865-068-A

B. Open this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
121VU	FLIGHT CONTROLS/SEC3/SPLY	21CE3	Q19

Subtask 27-64-00-860-068-A

C. Put the aircraft back to its initial configuration.
(1) On the overhead panel, on FLT CTL panel 24VU, release the SEC 3 pushbutton switch (the OFF legend comes on).
(2) Depressurize the aircraft hydraulic systems (Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001).
(3) Make an entry in the log book and record the defective servo-control.
(4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.03.31 23:55:15 UTC