W DOC AIRBUS | AMM A320F

Removal of the Leading Edge Panels 2 and 5 on the Outboard Flap


TASK 27-54-62-000-003-A
Removal of the Leading Edge Panels 2 and 5 on the Outboard Flap


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.
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: 587
ZONE: 687
1. Reason for the Job
To get visual access for internal structure.
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
SPATULA - PLASTIC
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
587
FLAP N° 2
687
FLAP N° 2
 C. 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
3. Job Set-up
Subtask 27-54-62-941-057-A
A. Safety Precautions
   (1) Put the SAFETY BARRIER(S) in position.
   (2) Put the WARNING NOTICE(S) on the HYD section of the panel 430VU to tell persons not to pressurize the aircraft hydraulic system.
   (3) Put a WARNING NOTICE(S) in position to tell persons not to operate the flight controls.
   (4) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable flap.
Subtask 27-54-62-860-057-A
B. Aircraft Maintenance Configuration
WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
   (1) Extend the flaps fully (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.
Subtask 27-54-62-865-057-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 27-54-62-020-055-B ** ON A/C NOT FOR ALL
A. Removal of the Leading Edge Panels 2 and 5 on the Outboard Flap
NOTE: The leading edge panel 2 is attached to the outboard flap with rivets.
   (1) Remove the leading edge panel 2 from the flap.
   (2) Use a SPATULA - PLASTIC to remove the sealant between the leading edge panel 5 (2) and the outboard flap.
   (3) Remove the screws (1) and carefully remove the leading edge panel 5 (2) from the flap.
Subtask 27-54-62-020-055-C ** ON A/C NOT FOR ALL
A. Removal of the Leading Edge Panels 2 and 5 on the Outboard Flap
   (1) Remove the rivets from the leading edge panels 2 and 5.
[Rev.10 from 2021] 2026.03.31 23:54:57 UTC