W DOC AIRBUS | AMM A320F

Removal of the Flap-Tracks Attachment-Bracket Bearing


TASK 57-26-15-000-001-A
Removal of the Flap-Tracks Attachment-Bracket Bearing


CAUTION: BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
  • DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
  • DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
  • MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
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)
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98D27803500001
1
LOCKING TOOL ZERO POS
98D57004033000
1
REM.-INST. TOOL - FLAP BEARING
98D57004034000
1
REM-INST. TOOL - FLAP BEARING
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
531AB, 531BB, 532AB, 532BB, 533AB, 533BB, 631AB, 631BB, 632AB, 632BB, 633AB, 633BB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 27-54-61-000-001-A
Removal of the Inboard Flap
TASK 27-54-61-000-003-A
Removal of the Inboard Double-Slotted Flap
TASK 27-54-62-000-001-A
Removal of the Outboard Flap
TASK 27-54-62-000-002-A
Removal of the Outboard Double-Slotted Flap
TASK 57-51-33-000-002-A
Removal of the No.2 Flap Track Beam
TASK 57-51-33-000-003-A
Removal of the No.3 Flap Track Beam
TASK 57-51-33-000-004-A
Removal of the No.4 Flap Track Beam
TASK 57-55-11-000-001-A
Removal of the Flap Track Fairings Nos. 2, 3 and 4
TASK 57-55-11-000-004-A
Removal of the Flap Track Fairings Nos. 2, 3 and 4
3. Job Set-up
Subtask 57-26-15-941-050-A
A. Safety Precautions
   (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
   (2) Install the 98D27803500001 LOCKING TOOL ZERO POS on the slat/flap control lever.
   (3) Put the WARNING NOTICE(S) in position to tell persons not to operate the slat/flap system.
Subtask 57-26-15-010-050-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) For the flap track beam 2:
     (a) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable inboard flap at zone 531(631).
     (b) Remove the applicable inboard flap (Ref. AMM TASK 27-54-61-000-001).
   (2) For the flap track beams 3 and 4:
     (a) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable outboard flap at zone 533(633).
     (b) Remove the applicable outboard flap (Ref. AMM TASK 27-54-62-000-001).
   (3) Put the ACCESS PLATFORM 3M (10 FT) below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
   (4) Remove the applicable fixed fairing access panels (Ref. AMM TASK 57-55-11-000-001):
   (5) Remove the applicable flap track beam:
Subtask 57-26-15-010-050-B ** ON A/C NOT FOR ALL
B. Get Access
   (1) For the flap track beam 2:
     (a) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable inboard flap at zone 531(631).
     (b) Remove the applicable inboard flap (Ref. AMM TASK 27-54-61-000-003).
   (2) For the flap track beams 3 and 4:
     (a) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable outboard flap at zone 533(633).
     (b) Remove the applicable outboard flap (Ref. AMM TASK 27-54-62-000-002).
   (3) Put the ACCESS PLATFORM 3M (10 FT) below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
   (4) Remove the applicable fixed fairing access panels (Ref. AMM TASK 57-55-11-000-004):
   (5) Remove the applicable flap track beam:
Subtask 57-26-15-865-050-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB07
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
** ON A/C ALL
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
4. Procedure
CAUTION: BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
  • DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
  • DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
  • MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 57-26-15-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the Flap Beam Attachment-Bracket Bearing
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) Remove and discard the lockwire from the outer ring (1) and the inner ring (5).
   (2) Remove the outer ring (1) and the inner ring (5), using the applicable tool as follows:
  • for the flap track beams 2 and 3, use the 98D57004033000 REM.-INST. TOOL - FLAP BEARING.
  • for the flap track beam 4, use the 98D57004034000 REM-INST. TOOL - FLAP BEARING.
   (3) Remove the spherical bearing (4) and carefully remove the sleeve bearing (3).
Subtask 57-26-15-020-050-B ** ON A/C NOT FOR ALL
A. Removal of the Flap Beam Attachment-Bracket Bearing
   (1) Release the washer (3).
   (2) Remove the nut (4), using the applicable tool as follows:
  • for the flap track beams 2 and 3, use the 98D57004033000 REM.-INST. TOOL - FLAP BEARING
  • for the flap track beam 4, use the 98D57004034000 REM-INST. TOOL - FLAP BEARING.
   (3) Remove the nut (4).
   (4) Remove and discard the washer (3).
   (5) Carefully remove the bearing assembly (1).
[Rev.10 from 2021] 2026.04.01 02:11:42 UTC