W DOC AIRBUS | AMM A320F

Detailed Inspection of Inboard Flap, End Rib including Roller and Interconnection Strut Attachment Bracket LH/RH


TASK 57-52-00-200-004-A
Detailed Inspection of Inboard Flap, End Rib including Roller and Interconnection Strut Attachment Bracket LH/RH


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.
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.
ZONE: 581
ZONE: 681
1. Reason for the Job
Refer to the MPD TASK: 575211-01
DETAILED INSPECTION OF INBOARD FLAP, END RIB, INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT BRACKET, LH/RH
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
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
581
FLAP N° 1
681
FLAP N° 1
 D. Referenced Information
REFERENCE
DESIGNATION
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 27-54-61-000-002-A
Removal of the Flap Kink-Seals and Cushion-Seals
TASK 27-54-61-400-006-A
Installation of the Flap Kink-Seals and Cushion-Seals
SRM 575100
(for corrective action)
3. Job Set-up
Subtask 57-52-00-941-057-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
   (2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 57-52-00-860-083-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Fully extend the flaps (Ref. AMM TASK 27-50-00-866-008).
   (2) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is installed on the flap/slat control lever.
   (3) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable wing at the inboard flap, zone 581(681).
Subtask 57-52-00-865-062-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/FLP/CTL AND MONG/SYS16CVB07
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
Subtask 57-52-00-010-079-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Remove the flap kink-seals (Ref. AMM TASK 27-54-61-000-002).
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 57-52-00-110-056-A ** ON A/C NOT FOR ALL
A. Preparation for Inspection
   (1) Use a Textile-Lint free Cotton - (Material No.14SBA1) , made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean the:
  • end rib
  • roller
  • interconnecting strut attachment bracket.
Subtask 57-52-00-210-052-A ** ON A/C NOT FOR ALL
B. Detailed Inspection of Inboard Flap, End Rib including Roller and Interconnection Strut Attachment Bracket LH/RH
   (1) Examine the end rib and the interconnection strut attachment bracket on the inboard flap. Make sure that:
  • there is no damage
  • there are no loose or damaged fasteners
  • the protective finish is in the correct condition.
   (2) Examine the roller to make sure that:
  • there is no corrosion
  • there are no cracks
  • the roller is correctly attached
  • the roller is symmetrical
  • there is no distortion of the roller or the attachment pivot bolt
  • the protective finish of the roller is correct
  • there is not too much play of the roller.
    F End Rib - Inboard Flap ** ON A/C NOT FOR ALL
NOTE: If the AXIAL PLAY "X" or the RADIAL PLAY "Y" is more than 0.25 mm (0.0098 in.), do a check of the liner for damage and wear.
NOTE: If necessary, refer to the SRM 575100 for the correct repair procedure.
5. Close-up
Subtask 57-52-00-410-082-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the kink-seals (Ref. AMM TASK 27-54-61-400-006).
Subtask 57-52-00-865-063-A ** ON A/C NOT FOR ALL
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/FLP/CTL AND MONG/SYS16CVB07
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
Subtask 57-52-00-860-084-A ** ON A/C NOT FOR ALL
C. Aircraft Configuration
   (1) Retract the flaps (Ref. AMM TASK 27-50-00-866-009).
Subtask 57-52-00-942-056-A ** ON A/C NOT FOR ALL
D. Removal of Equipment
   (1) Remove the access platform(s).
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the safety barriers.
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.02 06:31:16 UTC