W DOC AIRBUS | AMM A320F

Installation of the Side Rollers - Slat Tracks 5 thru 12


TASK 27-84-62-400-002-A
Installation of the Side Rollers - Slat Tracks 5 thru 12


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.
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
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
1
MICROMETER - EXTERNAL
No specific
AR
SAFETY BARRIER(S)
No specific
AR
WARNING NOTICE(S)
98D27804021000
1
GAUGE-SLAT TRACK SETTING
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.03GBD1)
Synthetic Oil base Grease-General Purpose Lithium Thickened -
(Material No.06AEA1)
Polysulfide Sealant-Low Adhesion Brushable -
(Material No.06AEB2)
Polysulfide Sealant-Low Adhesion Fillet Structure
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.12ACC1)
Corrosion Preventive Compound-Heavy Duty Soft Film -
(Material No.14QFB1)
Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 20-28-00-869-002-A
Table of the Maximum Permitted Resistance-Values
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
TASK 27-84-49-000-001-A
Removal of the Type B Actuators
TASK 27-84-49-000-002-A
Removal of the Type B Actuators
TASK 27-84-49-400-001-A
Installation of the Type B Actuators
TASK 27-84-49-400-002-A
Installation of the Type B Actuators
TASK 27-84-61-000-002-A
Removal of the Side-Rollers - Slat Tracks 1 thru 4
TASK 27-84-62-400-001-A
Installation of the Slat Tracks 5 thru 12
TASK 27-84-64-000-001-A
Removal of the No. 2 Slat
TASK 27-84-64-400-002-A
Installation of the No. 2 Slat
TASK 27-84-65-000-001-A
Removal of the No 3 Slat
TASK 27-84-65-400-002-A
Installation of the No 3 Slat
TASK 27-84-66-000-001-A
Removal of the No. 4 Slat
TASK 27-84-66-400-002-A
Installation of the No. 4 Slat
TASK 27-84-67-000-001-A
Removal of the No. 5 Slat
TASK 27-84-67-400-002-A
Installation of the No. 5 Slat
3. Job Set-up
Subtask 27-84-62-941-056-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 the cockpit to tell persons not to operate the slat controls.
   (3) Make sure that the 98D27803500001 LOCKING TOOL ZERO POS or 98D27803500002 LOCKING TOOL ZERO POS is on the slat/flap control lever.
Subtask 27-84-62-865-051-A
B. 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
Subtask 27-84-62-860-052-A
C. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is below the applicable zone 510 or 610.
   (2) Make sure that the applicable slats have been removed:
   (3) Make sure that the applicable actuators have been removed:
   (4) Make sure that the applicable side rollers have been removed (Ref. AMM TASK 27-84-61-000-002).
4. Procedure
Subtask 27-84-62-420-057-A
A. Preparation for Installation
   (1) Clean the component interface and/or the adjacent area with a 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) Set the Track Datum use the 98D27804021000 GAUGE-SLAT TRACK SETTING as follows:
NOTE: This procedure is only necessary where all the side rollers are removed.
     (a) Install the applicable setting track (35).
     (b) Install and lock the two clamp assemblies (36) at the locations of the non-datum side-rollers.
     (c) Turn the thumb screws (37) equally until they stop.
     (d) Install the gage assembly (40) with the washers (22) and the bolts (21) at the location of the aft datum side-roller.
     (e) Turn the torque screw (38) on the gage assembly (40) until it stops. Lock it in position with the thumb screw (39).
   (5) To calculate the thickness of the datum side-roller shims (23):
NOTE: This procedure is only necessary where all the side rollers are removed.
     (a) Remove the bolts (21), the washers (22) and the gage assembly (40) from the location of the aft datum side-roller.
     (b) Set the micrometer (42) on the gage block (44) to zero.
     (c) Install the gage assembly (40) on the gage block (44) and lock it in position with the clamps (41).
     (d) Move the micrometer (42) in the gage block (44) until it touches the gage assembly (40). Lock the micrometer (42) in position with the screw (43).
     (e) Remove the gage assembly (40) from the gage block (44).
     (f) Install the serviceable datum side-roller (20) on the gage block (44) and lock it in position with the clamps (41).
     (g) Adjust the micrometer (42) until it touches the datum side-roller (20). Write down the dimension shown on the micrometer (42).
     (h) Use an MICROMETER - EXTERNAL to calculate the dimensions for the shims (23) from the data written down.
     (i) Remove the datum side-roller (20) from the gage block (44).
     (j) Keep the side-roller (20) and its shims (23) together.
     (k) Do the procedure again for the forward datum side-roller.
   (6) Remove the clamp assemblies (36) and the setting track (35).
Subtask 27-84-62-420-051-B
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
B. Installation of the Datum Side-Rollers
NOTE: This procedure is only necessary where all the side-rollers are removed.
   (1) For tracks 5 and 11, prepare the aft datum side-roller (20) for electrical bonding (Ref. AMM TASK 20-28-00-912-802).
   (2) For tracks 6, 7, 8, 9, 10 and 12, apply a thin layer of Synthetic Oil base Grease-General Purpose Lithium Thickened - (Material No.03GBD1) to the interface of the datum side-rollers (20) and the shims (23).
   (3) Apply a layer of Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the shanks of the bolts (21).
   (4) Put the necessary thickness of shims (23) and the aft datum side-roller (20) in position.
   (5) Install the shims (23) and the aft datum side-roller (20) with the washers (22) and the bolts (21).
   (6) For tracks 8 and 11, where applicable, safety the bolts (21) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
   (7) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to the bolts (21), the washers (22) and the shims (23).
   (8) Do the procedure again for the front datum side-roller (20).
   (9) If removed, install the applicable slat track (2) (Ref. AMM TASK 27-84-62-400-001).
Subtask 27-84-62-420-052-A
C. Installation of One Side-Roller or a Pair on the Same Side
   (1) For tracks 5 and 11, prepare the side-roller(s) (20) for electrical bonding (Ref. AMM TASK 20-28-00-912-802).
   (2) For tracks 6, 7, 8, 9, 10 and 12, apply a thin layer of Synthetic Oil base Grease-General Purpose Lithium Thickened - (Material No.03GBD1) to the interface of the side-roller(s) (20) and the shims (23).
   (3) Apply a layer of Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the shanks of the bolts (21).
   (4) Put the shims (23) and the side-roller(s) (20) in position.
   (5) Install the shims (23) and the side roller(s) (20) with the washers (22) and the bolts (21).
Subtask 27-84-62-820-059-A
D. Adjustment of the Side Rollers
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
   (1) Move the applicable track (2) through its full range of travel and make sure that:
  • the side-roller(s) (20) touch the track (2) at some point of its travel
  • the points that touch do not stop the smooth travel of the track (2).
   (2) To adjust the side-roller(s):
     (a) Remove the bolts (21), the washers (22), the side-roller(s) (20) and the shims (23).
     (b) Adjust the thickness of the shims (23):
  • to reduce the friction, increase the thickness of the shims (23)
  • to make sure that the side-roller(s) (20) touch the track (2) at some point of its travel, decrease the thickness of the shims (23) as necessary.
   (3) Install the shims (23) and the side-rollers (20) with the washers (22) and bolts (21).
   (4) Do the procedure again, as necessary, until the side-roller(s) (20) adjustment is correct.
   (5) For tracks 8 and 11, where applicable, safety the bolts (21) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
   (6) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to the bolts (21), the washers (22) and the shims (23).
Subtask 27-84-62-912-057-A
E. Electrical Bonding Test
   (1) For track 5 and 11, do the electrical bonding test (Ref. AMM TASK 20-28-00-869-002).
5. Close-up
Subtask 27-84-62-410-051-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the applicable actuators:
   (3) Install the applicable slat:
Subtask 27-84-62-865-055-A
B. 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 27-84-62-942-051-A
C. Removal of Equipment
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the safety barriers.
   (3) Remove the WARNING NOTICE(S).
   (4) Remove the access platform(s).
   (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.03.31 23:58:03 UTC