W DOC AIRBUS | AMM A320F

Extension-Retraction of the Spoilers for Maintenance


TASK 27-60-00-866-002-A
Extension-Retraction of the Spoilers for Maintenance


NOTE: The procedure is the same for all spoilers
ZONE: 580
ZONE: 680
1. Reason for the Job
Self explanatory
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
1
ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
TOMMY BAR DIA 4 MM (0,157 IN) - METALLIC
98D27603002000
1
KEY-SPOILER MAINTENANCE
OR
OR
98D27603002001
1
KEY-SPOILER MAINTENANCE
98D27604000000
1
COLLAR-SAFETY, SPOILER
OR
OR
98D27604004000
1
COLLAR SAFETY SPOILER
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
580
LEFT WING FLAPS AND SPOILERS
680
RIGHT WING FLAPS AND SPOILERS
822
FOR [31CE1] (SERVO CTL-SPLR1, L G)
573BB
FOR [31CE10] (SERVO CTL-SPLR5, R G)
675GB
FOR [31CE2] (SERVO CTL-SPLR1, R G)
673BB
FOR [31CE3] (SERVO CTL-SPLR2, L Y)
575BB
FOR [31CE4] (SERVO CTL-SPLR2, R Y)
675BB
FOR [31CE5] (SERVO CTL-SPLR3, L B)
575DB
FOR [31CE6] (SERVO CTL-SPLR3, R B)
675DB
FOR [31CE7] (SERVO CTL-SPLR4, L Y)
575EB
FOR [31CE8] (SERVO CTL-SPLR4, R Y)
675EB
FOR [31CE9] (SERVO CTL-SPLR5, L G)
575GB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 27-00-00-080-002-A
Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
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 27-80-00-866-004-A
Extending the Slats on the Ground
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 [31CE10] (SERVO CTL-SPLR5, R G)
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 [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)
FOR [31CE5] (SERVO CTL-SPLR3, L B)
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 [31CE6] (SERVO CTL-SPLR3, R B)
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 [31CE7] (SERVO CTL-SPLR4, 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 [31CE8] (SERVO CTL-SPLR4, 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)
FOR [31CE9] (SERVO CTL-SPLR5, L G)
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 27-60-00-860-050-A
A. Aircraft Maintenance Configuration
   (1) Extend the slats and flaps (Ref. AMM TASK 27-50-00-866-008) (Ref. AMM TASK 27-80-00-866-004).
   (2) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is in position on the flap/slat control lever.
   (3) Put the warning notice on the HYD section of the panel 40VU to tell persons not to pressurize the aircraft hydraulic systems.
Subtask 27-60-00-010-051-A
B. Get Access
   (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 822.
   (2) Open the access door 822.
   (3) On the battery power center 105VU:
  • loosen the two screws and remove the protective cover.
   (4) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position :
     (a) at the zone 580 for the left spoilers.
     (b) at the zone 680 for the right spoilers.
   (5) Open the applicable access panels:
     (a) FOR [31CE1] (SERVO CTL-SPLR1, L G)
     (b) FOR [31CE2] (SERVO CTL-SPLR1, R G)
     (c) FOR [31CE3] (SERVO CTL-SPLR2, L Y)
     (d) FOR [31CE4] (SERVO CTL-SPLR2, R Y)
     (e) FOR [31CE5] (SERVO CTL-SPLR3, L B)
     (f) FOR [31CE6] (SERVO CTL-SPLR3, R B)
     (g) FOR [31CE7] (SERVO CTL-SPLR4, L Y)
     (h) FOR [31CE8] (SERVO CTL-SPLR4, R Y)
     (i) FOR [31CE9] (SERVO CTL-SPLR5, L G)
     (j) FOR [31CE10] (SERVO CTL-SPLR5, R G)
Subtask 27-60-00-865-053-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
** ON A/C ALL
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
4. Procedure
Subtask 27-60-00-866-054-B
A. Extension
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) If there is no plate with the 'O' and 'M' indications on the maintenance device (PRE GOODRICH VSB 31077-27-15):
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.
     (a) Install the 98D27603002000 KEY-SPOILER MAINTENANCE98D27603002001 KEY-SPOILER MAINTENANCE (2) on the servocontrol 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 enough 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 servocontrol and send it back to the supplier for analysis.
       1 If necessary, use a TOMMY BAR DIA 4 MM (0,157 IN) - METALLIC to turn the spoiler maintenance key.
     (b) Move the spoiler to the extended position with your hand.
CAUTION: WHILE THE SAFETY COLLAR IS INSTALLED, DO NOT PRESSURIZE THE SPOILER SERVO CONTROL TO MOVE THE SPOILER. ONLY MOVE THE SPOILER WITH YOUR HAND. IF YOU PRESSURIZE THE SPOILER SERVO CONTROL WITH THE SAFETY COLLAR INSTALLED, YOU CAN CAUSE DAMAGE TO LUGS MADE OF CFRP.
     (c) Put the 98D27604000000 COLLAR-SAFETY, SPOILER98D27604004000 COLLAR SAFETY SPOILER (3) on the rod (1) of the servocontrol.
     (d) Install the two pins of the safety collar (3).
NOTE: The COLLAR-SAFETY, SPOILER is used to prevent the spoiler movements with its own weight.
   (2) If there is a plate with the 'O' and 'M' indications on the maintenance device (POST GOODRICH VSB 31077-27-15):
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.
     (a) Install the 98D27603002000 KEY-SPOILER MAINTENANCE98D27603002001 KEY-SPOILER MAINTENANCE (2) on the servocontrol and turn it a quarter turn counterclockwise to the 'M' position (Maintenance).
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 enough 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 servocontrol and send it back to the supplier for analysis.
       1 If necessary, use a TOMMY BAR DIA 4 MM (0,157 IN) - METALLIC to turn the spoiler maintenance key.
     (b) Move the spoiler to the extended position with your hand.
CAUTION: WHILE THE SAFETY COLLAR IS INSTALLED, DO NOT PRESSURIZE THE SPOILER SERVO CONTROL TO MOVE THE SPOILER. ONLY MOVE THE SPOILER WITH YOUR HAND. IF YOU PRESSURIZE THE SPOILER SERVO CONTROL WITH THE SAFETY COLLAR INSTALLED, YOU CAN CAUSE DAMAGE TO LUGS MADE OF CFRP.
     (c) Put the 98D27604000000 COLLAR-SAFETY, SPOILER98D27604004000 COLLAR SAFETY SPOILER (3) on the rod (1) of the servocontrol.
     (d) Install the two pins of the safety collar (3).
NOTE: The COLLAR-SAFETY, SPOILER is used to prevent the spoiler movements with its own weight.
Subtask 27-60-00-866-056-B
B. Retraction
   (1) Make sure that the warning notice is in position on the panel 40VU to tell persons not to pressurize the hydraulic systems.
   (2) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is in position on the flap/slat control lever.
   (3) Remove the two pins of the safety collar (3).
   (4) Remove the safety collar (3) of the servocontrol.
   (5) Move the spoiler to the retracted position with your hand.
NOTE: The spoiler can move with his own weight.
   (6) Make sure that the spoiler is in the fully retracted position.
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.
   (7) If there is no plate with the 'O' and 'M' indications on the maintenance device (PRE GOODRICH VSB 31077-27-15):
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.
     (a) Turn the 98D27603002000 KEY-SPOILER MAINTENANCE98D27603002001 KEY-SPOILER MAINTENANCE (2) a quarter turn clockwise and remove it.
The servocontrol is in operational position.
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 enough 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 servocontrol and send it back to the supplier for analysis.
       1 If necessary, use a TOMMY BAR DIA 4 MM (0,157 IN) - METALLIC to turn the spoiler maintenance key.
     (b) Make sure that the work area is clean and clear of tool(s) and other items.
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.
     (c) Gradually apply a manual force to the spoiler surface trailing-edge and make sure that you cannot extend the spoiler.
NOTE: If you can extend the spoiler manually with the servocontrol in the operational position:
- It is necessary to replace the spoiler servocontrol.
   (8) If there is a plate with the 'O' and 'M' indications on the maintenance device (POST GOODRICH VSB 31077-27-15):
CAUTION: MAKE SURE THAT THE STOP OF THE HEXAGONAL HEAD OF THE SPOILER MAINTENANCE KEY 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.
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.
     (a) Turn the 98D27603002000 KEY-SPOILER MAINTENANCE98D27603002001 KEY-SPOILER MAINTENANCE (2) a quarter turn clockwise to the 'O' position (Operation) and remove it.
The servocontrol is in operational position.
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 enough 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 servocontrol and send it back to the supplier for analysis.
       1 If necessary, use a TOMMY BAR DIA 4 MM (0,157 IN) - METALLIC to turn the spoiler maintenance key.
     (b) Make sure that the work area is clean and clear of tool(s) and other items.
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.
     (c) Gradually apply a manual force to the spoiler surface trailing-edge and make sure that you cannot extend the spoiler.
NOTE: If you can extend the spoiler manually with the servocontrol in the operational position:
- It is necessary to replace the spoiler servocontrol.
5. Close-up
Subtask 27-60-00-860-051-A
A. Put the aircraft back to its initial configuration.
   (1) Make sure that the work area is clean and clear of tools and other items.
Subtask 27-60-00-710-051-A
B. Do the operational test of the spoiler hydraulic actuation (Ref. AMM TASK 27-64-00-710-001).
Subtask 27-60-00-410-051-A
C. Close Access
   (1) Install the protective cover on the battery power center 105VU.
   (2) Tighten the two screws.
   (3) Close the access door 822.
   (4) Close the applicable access panels:
     (a) FOR [31CE1] (SERVO CTL-SPLR1, L G)
     (b) FOR [31CE2] (SERVO CTL-SPLR1, R G)
     (c) FOR [31CE3] (SERVO CTL-SPLR2, L Y)
     (d) FOR [31CE4] (SERVO CTL-SPLR2, R Y)
     (e) FOR [31CE5] (SERVO CTL-SPLR3, L B)
     (f) FOR [31CE6] (SERVO CTL-SPLR3, R B)
     (g) FOR [31CE7] (SERVO CTL-SPLR4, L Y)
     (h) FOR [31CE8] (SERVO CTL-SPLR4, R Y)
     (i) FOR [31CE9] (SERVO CTL-SPLR5, L G)
     (j) FOR [31CE10] (SERVO CTL-SPLR5, R G)
   (5) Remove the access platform(s).
Subtask 27-60-00-865-054-A
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
** ON A/C ALL
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
Subtask 27-60-00-866-055-A
E. Retraction of the flaps
   (1) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the FLAPS panel 114VU (Ref. AMM TASK 27-00-00-080-002).
   (2) Retract the flaps (Ref. AMM TASK 27-50-00-866-009).
[Rev.10 from 2021] 2026.03.31 23:55:13 UTC