W DOC AIRBUS | AMM A320F

Adjustment of the Spoilers

TASK 27-64-00-820-001-C
Adjustment of the Spoilers

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 THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM. UNWANTED MOVEMENT OF HYDRAULICALLY OPERATED ITEMS CAN CAUSE SERIOUS INJURY AND/OR DAMAGE.
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.
ZONE: 580
ZONE: 680
1. Reason for the Job
NOTE: This task can contribute to fuel savings.
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
GAGE - FEELER
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 3.15 and 2.85 m.daN (23.23 and 21.02 lbf.ft ) T
No specific
Torque wrench: range to between 9 and 8 m.daN (66.37 and 59.00 lbf.ft ) T
98D27603000001
1
SPOILER POSITION CHECK TOOL
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
98D27903500000
2
PIN-SIDE STICK LOCKING
 B. Consumable Materials
REFERENCE
DESIGNATION
No specific
lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)
 C. 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
 D. 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 27-60-00-866-002-A
Extension-Retraction of the Spoilers for Maintenance
TASK 27-64-00-710-001-A
Operational Test of the Spoiler Hydraulic Actuation
TASK 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
F Adjustment of the Spoilers
F Adjustment of the Spoilers
F Measurement of Negative Clearance Between Spoiler and Flap
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 27-64-00-860-060-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
   (2) Make sure that the flaps are in the fully retracted position (Ref. AMM TASK 27-50-00-866-009).
   (3) On the center pedestal, make sure that the SPEED BRAKE control lever is set to RET.
   (4) Install the 98D27903500000 PIN-SIDE STICK LOCKING on each side stick controller.
   (5) Put the WARNING NOTICE(S) on the CAPT and F/O side sticks to tell persons not to touch the side sticks.
   (6) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap and slat control lever.
   (7) Put a WARNING NOTICE(S) on the center pedestal to tell persons not to operate the SPEED BRAKE control lever.
Subtask 27-64-00-010-057-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 822.
     (a) Open the access door 822.
     (b) On the battery power center 105VU:
  • loosen the two screws and remove the protective cover.
   (2) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position at:
     (a) the zone 580 for the left spoilers.
     (b) the zone 680 for the right spoilers.
   (3) 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 27-64-00-865-059-A ** ON A/C NOT FOR ALL
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
Subtask 27-64-00-863-056-A ** ON A/C NOT FOR ALL
D. Pressurize the hydraulic system that relates to the spoiler you adjust.
   (1) For the spoiler 1 or 5, pressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-863-001).
   (2) For the spoiler 2 or 4, pressurize the Yellow hydraulic system (Ref. AMM TASK 29-24-00-863-001).
   (3) For the spoiler 3, pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
4. Procedure
Subtask 27-64-00-220-052-B ** ON A/C NOT FOR ALL
A. Measure the clearance or the interference U between the underside of the spoiler trailing edge and the upper surface of the flap.
   (1) For the spoiler 1, measure the clearance U with a GAGE - FEELER.
  • the clearance must be:
    U = 0 +0 mm or +0.5 mm (0.0000 +0.0000 in. or +0.0197 in.).
NOTE: You must do this measurement at the outboard end of the spoiler.
     (a) If necessary, adjust the servocontrol (Ref. Para. B).
       1 Initially adjust the servocontrol in order to measure:
U = 4 +0 mm or +0.5 mm (0.1575 +0.0000 in. or +0.0197 in.).
       2 Then adjust the servocontrol again by half a turn clockwise in order to get the clearance.
   (2) For the spoilers 2, 3 and 4, measure the interference U:
  • the interference must be:
    U = -2 +0.5 mm or -0.5 mm (-0.0787 +0.0197 in. or -0.0197 in.)

NOTE: You must do this measurement at the closest point (point where the gap between the spoiler and the flap is the smallest).
     (a) With the 98D27603000001 SPOILER POSITION CHECK TOOL.
       1 Install the 98D27603000001 SPOILER POSITION CHECK TOOL as follows:
  • on the upper surface of the wing
  • on the trailing edge of the spoiler
  • at the closest point of the spoiler.
       2 Set the needle of the dial gauge to the zero position.
       3 Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION.
       4 Extend the flaps (Ref. AMM TASK 27-50-00-866-008).
NOTE: Put the flap and slat control lever to the position 1.
       5 Read the new position of the needle of the dial gauge.
The difference of positions gives the negative clearance U.
       6 Retract the flaps (Ref. AMM TASK 27-50-00-866-009).
       7 Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION.
       8 If necessary, adjust the servocontrol (Ref. Para. B).
     (b) If the 98D27603000001 SPOILER POSITION CHECK TOOL is not available, do the adjustment (Ref Para.B) to get the negative clearance as follow:
       1 Initially adjust the servocontrol in order to measure:
U = 2 +0.5 mm or -0.5 mm (0.0787 +0.0197 in. or -0.0197 in.).
       2 Then adjust the servocontrol again by half a turn clockwise in order to get the negative clearance.
   (3) For the spoiler 5, measure the clearance U with a GAGE - FEELER.
  • the clearance must be:
    U = 0 +0 mm or +0.5 mm (0.0000 +0.0000 in. or +0.0197 in.).
NOTE: You must do this measurement at the closest point (point where the gap between the spoiler and the flap is the smallest).
     (a) If necessary, adjust the servocontrol (Ref. Para. B).
       1 Initially adjust the servocontrol in order to measure:
U = 4 +0 mm or +0.5 mm (0.1575 +0.0000 in. or +0.0197 in.).
       2 Then adjust the servocontrol again by half a turn clockwise in order to get the clearance.
Subtask 27-64-00-820-052-B ** ON A/C NOT FOR ALL
B. If the clearance or the interference U is not correct, do this adjustment:
   (1) Write the clearance or interference U.
   (2) Depressurize the hydraulic system that relates to the spoiler you adjust.
     (a) For the spoiler 1 or 5, depressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-864-001).
     (b) For the spoiler 2 or 4, depressurize the Yellow hydraulic system (Ref. AMM TASK 29-24-00-864-001).
     (c) For the spoiler 3, depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
   (3) Extend the related spoiler by hand (Ref. AMM TASK 27-60-00-866-002).
   (4) On the servocontrol (1), remove the lockwire from the nut (3) and discard it.
   (5) Loosen the nut (3) and release the lockwashers (2).
   (6) Turn the rod (4) in the related direction (Refer to the NOTE below to find the number of turns of the rod (4)).
NOTE: If you do one turn of the rod (4), this moves the trailing edge of the spoiler 8 mm (0.3150 in.).
   (7) Install the lockwashers (2) and TORQUE the nut (3) to between 3.15 and 2.85 m.daN (23.23 and 21.02 lbf.ft ) T. Do not safety the nut at this time.
   (8) Retract the related spoiler by hand (Ref. AMM TASK 27-60-00-866-002).
   (9) Pressurize the hydraulic system that relates to the spoiler you adjust.
     (a) For the spoiler 1 or 5, pressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-863-001).
     (b) For the spoiler 2 or 4, pressurize the Yellow hydraulic system (Ref. AMM TASK 29-24-00-863-001).
     (c) For the spoiler 3, pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
   (10) Make sure that the clearance or the interference U is correct.
   (11) Depressurize the hydraulic system that relates to the spoiler you adjust.
     (a) For the spoiler 1 or 5, depressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-864-001).
     (b) For the spoiler 2 or 4, depressurize the Yellow hydraulic system (Ref. AMM TASK 29-24-00-864-001).
     (c) For the spoiler 3, depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
   (12) Extend the related spoiler by hand (Ref. AMM TASK 27-60-00-866-002).
   (13) TORQUE the nut (3) to between 9 and 8 m.daN (66.37 and 59.00 lbf.ft ) T and safety it with lockwire corrosion resistant steel dia 0.8 mm (0.03 in.).
   (14) Retract the related spoiler by hand (Ref. AMM TASK 27-60-00-866-002).
   (15) Pressurize the hydraulic system that relates to the spoiler you adjust.
     (a) For the spoiler 1 or 5, pressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-863-001).
     (b) For the spoiler 2 or 4, pressurize the Yellow hydraulic system (Ref. AMM TASK 29-24-00-863-001).
     (c) For the spoiler 3, pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
   (16) Make sure that the clearance or the interference U is correct.
   (17) Remove the 98D27903500000 PIN-SIDE STICK LOCKING from each sidestick controller.
   (18) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap and slat control lever.
Subtask 27-64-00-865-058-A ** ON A/C NOT FOR ALL
C. 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
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
Subtask 27-64-00-710-055-A ** ON A/C NOT FOR ALL
D. Do the operational test of the spoiler hydraulic actuation (Ref. AMM TASK 27-64-00-710-001).
5. Close-up
Subtask 27-64-00-860-061-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Depressurize the hydraulic system that relates to the spoiler you adjust:
     (a) For the spoiler 1 or 5, depressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-864-001).
     (b) For the spoiler 2 or 4, depressurize the Yellow hydraulic system (Ref. AMM TASK 29-24-00-864-001).
     (c) For the spoiler 3, depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
   (2) Remove the WARNING NOTICE(S).
   (3) Make sure that the work area is clean and clear of tools and other items.
Subtask 27-64-00-410-056-A ** ON A/C NOT FOR ALL
B. 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 27-64-00-862-058-A ** ON A/C NOT FOR ALL
C. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.03.31 23:55:21 UTC
"Aviabrain" 2025