W DOC AIRBUS | AMM A320F

Lubricate all Track Rollers and Pinions


TASK 12-22-27-640-006-A
Lubricate all Track Rollers and Pinions


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 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.
ZONE: 510
ZONE: 520
ZONE: 610
ZONE: 620
1. Reason for the Job
Refer to the MPD TASK: 278468-01
LUBRICATE ALL TRACK ROLLERS AND PINIONS
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific
1
BRUSH - BRISTLED
No specific
1
GUN - GREASE
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
1
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.03GBC1)
Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. -
(Material No.03GBD1)
Synthetic Oil base Grease-General Purpose Lithium Thickened -
(Material No.03HBD9)
Synthetic Ester base Grease-General Purpose Low Temp -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
510
LEFT WING SLATS
520
LEFT WING FIXED LEADING EDGE
610
RIGHT WING SLATS
620
RIGHT WING FIXED LEADING EDGE
521AB, 521CB, 521EB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB
522AB, 622AB
522XB, 522YB, 622XB, 622YB
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 27-80-00-866-004-A
Extending the Slats on the Ground
TASK 27-80-00-866-005-A
Retracting the Slats on the Ground
TASK 57-41-37-000-004-A
Removal of the Pressure Relief Panels
TASK 57-41-37-000-006-A
Removal of the Access Panels
TASK 57-41-37-400-002-A
Installation of the Pressure Relief Panels
TASK 57-41-37-400-006-A
Installation of the Access Panels
TASK 12-22-00-00
LUBRICATION - DESCRIPTION AND OPERATION
3. Job Set-up
Subtask 12-22-27-941-056-A
A. Safety Precautions
   (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 12-22-27-866-056-A
B. Aircraft Maintenance Configuration
   (1) Fully extend the slats (Ref. AMM TASK 27-80-00-866-004).
   (2) Put a WARNING NOTICE(S) on the flap/slat control lever to tell persons not to operate the slats.
Subtask 12-22-27-865-060-A
C. 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 12-22-27-010-054-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below the applicable slat track.
   (2) Remove the applicable access panels (Ref. AMM TASK 57-41-37-000-004) and (Ref. AMM TASK 57-41-37-000-006):
Subtask 12-22-27-010-054-B ** ON A/C NOT FOR ALL
D. Get Access
   (1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below the applicable slat track.
   (2) Remove the applicable access panels (Ref. AMM TASK 57-41-37-000-004) and (Ref. AMM TASK 57-41-37-000-006):
4. Procedure
Subtask 12-22-27-640-055-A
A. Lubricate the Slat-Track Pinion Bearings, Slat Track Rollers, Pinions and Rack Teeth
NOTE: For grease specification and lubrication requirements, refer to (Ref. AMM D/O 12-22-00-00).
   (1) Use a GUN - GREASE to lubricate the slat-track pinion bearings and the slat track rollers with a Synthetic Oil base Grease-General Purpose Lithium Thickened - (Material No.03GBD1) or Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) or Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - (Material No.03GBC1) as follows:
     (a) Clean the grease nipples with a Textile-Lint free Cotton - (Material No.14SBA1) .
CAUTION: IF YOU USE POWER-OPERATED LUBRICATION EQUIPMENT, DO NOT USE AN AIR SUPPLY PRESSURE OF MORE THAN 3 BARS (43.5 PSI). THE AIR PRESSURE CAUSES THE GREASE TO COME OUT OF THE EQUIPMENT WITH MORE FORCE THAN IF YOU USE MANUALLY-OPERATED EQUIPMENT. THUS IF THE AIR PRESSURE IS TOO HIGH, THE GREASE WILL POSSIBLY CAUSE DAMAGE TO THE PINION BEARING SEALS.
     (b) If you use power-operated lubrication equipment:
       1 Lubricate the slat-track pinion bearings and the slat track rollers through the grease nipples at a maximum pressure of 3 bar (43.5 psi).
     (c) If you use manually-operated lubrication equipment:
       1 Lubricate the slat-track pinion bearings and the slat track rollers through the grease nipples.
     (d) Lubricate until the new grease comes out.
     (e) Remove the unwanted grease from the grease nipples, the slat track rollers and the slat-track pinion bearings with a Textile-Lint free Cotton - (Material No.14SBA1) .
     (f) Make sure that the grease nipple balls are in the correct position against their seats after lubrication.
   (2) Use a BRUSH - BRISTLED to lubricate the pinions and the rack teeth as follows:
     (a) Lightly apply Synthetic Oil base Grease-General Purpose Lithium Thickened - (Material No.03GBD1) or Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) or Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - (Material No.03GBC1) on the pinions and on the rack teeth as far as possible.
5. Close-up
Subtask 12-22-27-410-054-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Install the applicable access panels (Ref. AMM TASK 57-41-37-400-002) and (Ref. AMM TASK 57-41-37-400-006):
   (2) Remove the access platform(s).
Subtask 12-22-27-410-054-B ** ON A/C NOT FOR ALL
A. Close Access
   (1) Install the applicable access panels (Ref. AMM TASK 57-41-37-400-002) and (Ref. AMM TASK 57-41-37-400-006):
   (2) Remove the access platform(s).
Subtask 12-22-27-865-061-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 12-22-27-866-057-A
C. Aircraft Configuration
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Retract the slats fully (Ref. AMM TASK 27-80-00-866-005).
Subtask 12-22-27-942-056-A
D. Removal of Equipment
   (1) Remove the safety barriers.
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 04:23:19 UTC