W DOC AIRBUS | AMM A320F

Installation of the Torque Shafts

TASK 27-84-45-400-008-A
Installation of the Torque Shafts

WARNING: MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
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.
FIN: 6016CM
FIN: 6020CM
FIN: 6026CM
FIN: 6030CM
FIN: 6066CM
FIN: 6070CM
FIN: 6076CM
FIN: 6080CM
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 1.24 and 1.02 m.daN (109.73 and 90.27 lbf.in ) T
98D27504030001
2
LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.03FDB1)
Mineral Oil base Grease-Anti-Fretting Paste -
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.12ACC1)
Corrosion Preventive Compound-Heavy Duty Soft Film -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [6016CM] (SLAT XMSN TORQUE SHAFT)
521EB
FOR [6020CM] (SLAT XMSN TORQUE SHAFT)
521EB
FOR [6026CM] (SLAT XMSN TORQUE SHAFT)
522AB
FOR [6030CM] (SLAT XMSN TORQUE SHAFT)
522CB
FOR [6066CM] (SLAT XMSN TORQUE SHAFT)
621EB
FOR [6070CM] (SLAT XMSN TORQUE SHAFT)
621EB
FOR [6076CM] (SLAT XMSN TORQUE SHAFT)
622AB
FOR [6080CM] (SLAT XMSN TORQUE SHAFT)
622CB
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 27-50-00-000-003-A
Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)
TASK 27-50-00-400-003-A
Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)
TASK 27-80-00-866-005-A
Retracting the Slats on the Ground
TASK 27-84-00-710-001-A
Operational Test of the Slat System
F Torque shafts - Slat Power Transmission
F Torque Shafts - Slat Power Transmission
FOR [6080CM] (SLAT XMSN TORQUE SHAFT)
TASK 57-41-37-000-004-A
Removal of the Pressure Relief Panels
TASK 57-41-37-400-002-A
Installation of the Pressure Relief Panels
3. Job Set-up
Subtask 27-84-45-941-064-A
A. Safety Precautions
   (1) Make sure that the SAFETY BARRIER(S) are in position.
   (2) Make sure that the WARNING NOTICE(S) is in position to tell persons not to operate the slat controls.
Subtask 27-84-45-860-057-A
B. Aircraft Maintenance Configuration
   (1) Make sure that the slats are retracted fully (Ref. AMM TASK 27-80-00-866-005).
   (2) Make sure that the 98D27803500001 LOCKING TOOL ZERO POS or 98D27803500002 LOCKING TOOL ZERO POS is installed on the flap/slat control lever on panel 114VU.
   (3) Make sure that a 98D27504030001 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed (Ref. AMM TASK 27-50-00-400-003):
  • on the torque shaft, inboard of the applicable components
  • on the torque shaft, outboard of the applicable components.
   (4) Make sure that the adjustable access platform is in position below the applicable access panel.
   (5) Make sure that the applicable access panel has been removed:
     (a) FOR [6016CM] (SLAT XMSN TORQUE SHAFT)
panel 521EB
     (b) FOR [6020CM] (SLAT XMSN TORQUE SHAFT)
panel 521EB
     (c) FOR [6026CM] (SLAT XMSN TORQUE SHAFT)
panel 522AB
     (d) FOR [6030CM] (SLAT XMSN TORQUE SHAFT)
panel 522CB
     (e) FOR [6066CM] (SLAT XMSN TORQUE SHAFT)
panel 621EB
     (f) FOR [6070CM] (SLAT XMSN TORQUE SHAFT)
panel 621EB
     (g) FOR [6076CM] (SLAT XMSN TORQUE SHAFT)
panel 622AB
     (h) FOR [6080CM] (SLAT XMSN TORQUE SHAFT)
panel 622CB
(Ref. AMM TASK 57-41-37-000-004).
Subtask 27-84-45-865-076-A
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
4. Procedure
Subtask 27-84-45-420-076-A
A. Preparation for Installation
   (1) Clean the component interface and/or the adjacent area with Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (4) Apply a thin layer of Mineral Oil base Grease-Anti-Fretting Paste - (Material No.03FDB1) to the torque shaft splines.
Subtask 27-84-45-420-077-A
B. Installation of the Torque Shafts
   (1) Install the universal joint (8).
   (2) Install the shaft (9) and attach it with the bolts (11) and the nuts (10).
   (3) TORQUE the nuts (10) to between 1.24 and 1.02 m.daN (109.73 and 90.27 lbf.in ) T.
   (4) Apply Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to the:
  • nuts (10)
  • bolts (11)
  • flange of the universal joint (8)
  • flanges of the shaft (9).
   (5) Remove the 98D27504030001 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. AMM TASK 27-50-00-000-003):
  • from the torque shaft, inboard of the applicable component
  • from the torque shaft, outboard of the applicable component.
Subtask 27-84-45-210-067-A
C. Dimensional/Visual Checks
F Torque Shafts - Slat Power Transmission
   (1) Make sure that:
  • you cannot see the spline engagement groove at the movable joint
  • the dimension A is a minimum of 6.5 mm (0.2559 in.) at the movable joint.
Subtask 27-84-45-865-077-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/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 27-84-45-710-055-A
E. Test
   (1) Do an operational test of the slat power-transmission system (Ref. AMM TASK 27-84-00-710-001). Make sure that the rotation of the torque shafts does not cause damage.
5. Close-up
Subtask 27-84-45-865-078-A
A. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 27-84-45-410-055-A
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the applicable access panel:
     (a) FOR [6016CM] (SLAT XMSN TORQUE SHAFT)
install 521EB
     (b) FOR [6020CM] (SLAT XMSN TORQUE SHAFT)
install 521EB
     (c) FOR [6026CM] (SLAT XMSN TORQUE SHAFT)
install 522AB
     (d) FOR [6030CM] (SLAT XMSN TORQUE SHAFT)
install 522CB
     (e) FOR [6066CM] (SLAT XMSN TORQUE SHAFT)
install 621EB
     (f) FOR [6070CM] (SLAT XMSN TORQUE SHAFT)
install 621EB
     (g) FOR [6076CM] (SLAT XMSN TORQUE SHAFT)
install 622AB
     (h) FOR [6080CM] (SLAT XMSN TORQUE SHAFT)
install 622CB
(Ref. AMM TASK 57-41-37-400-002).
Subtask 27-84-45-865-079-A
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/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 27-84-45-942-056-A
D. Removal of Equipment
   (1) Remove the safety barriers.
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.03.31 23:57:16 UTC
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