W DOC AIRBUS | AMM A320F

Detailed Inspection of Outer Wing, Flap Track 2, Aft Attachment Fittings on Wing Bottom Skin at False Rear Spar and Flap Track 3 & 4 Aft Attachment ....

TASK 57-26-00-200-001-A
Detailed Inspection of Outer Wing, Flap Track 2, Aft Attachment Fittings on Wing Bottom Skin at False Rear Spar and Flap Track 3 & 4 Aft Attachment ....

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: 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: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
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.
CAUTION: DO NOT APPLY TEMPORARY PROTECTION SYSTEM (TPS) ON THE INSPECTION AREA. IF YOU APPLY TPS ON THE INSPECTION AREA, YOU CAN CAUSE DAMAGE TO THE AIRCRAFT.
ZONE: 570
ZONE: 670
1. Reason for the Job
Refer to the MPD TASK: 572653-01
DETAILED INSPECTION OF OUTER WING, FLAP TRACK 2, AFT ATTACHMENT FITTINGS ON WING BOTTOM SKIN AT FALSE REAR SPAR, AND FLAP TRACK 3 & 4, AFT ATTACHMENT FITTINGS AT REAR SPAR
NOTE: The effectivity of this task is ALL. To know if this task is applicable for your aircraft, refer to the MPD task applicability and the weight variant data given in the SRM introduction.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 3M (10 FT)
No specific
1
LIGHT SOURCE - INSPECTION
No specific
1
MIRROR - INSPECTION
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 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
570
AFT SECTION OF L WING & TE FIXED STRUCT
670
AFT SECTION OF R WING & TE FIXED STRUCT
531CB, 532CB, 533CB, 631CB, 632CB, 633CB
531AB, 531BB, 532AB, 532BB, 533AB, 533BB, 631AB, 631BB, 632AB, 632BB, 633AB, 633BB
531EB, 532EB, 533EB, 631EB, 632EB, 633EB
 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 51-78-00-916-001-A
Application of Temporary Protection System (TPS)
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
TASK 57-55-11-400-001-A
Installation of the Flap Track Fairings Nos. 2, 3 and 4
TASK 57-55-11-400-004-A
Installation of the Flap Track Fairings Nos. 2, 3 and 4
SRM 572600
 (for corrective action)
F Flap Tracks 2, 3 and 4 - Aft Attachment Fittings
3. Job Set-up
Subtask 57-26-00-941-064-A
A. Safety Precautions
   (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
   (2) Put the WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-26-00-866-050-A
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 on the flap/slat control lever.
Subtask 57-26-00-865-050-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
Subtask 57-26-00-010-050-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Put the ACCESS PLATFORM 3M (10 FT) below the applicable flap track fairings, zones 531 (631) 532 (632) and 533 (633).
   (2) Remove the applicable flap track fairing: (Ref. AMM TASK 57-55-11-000-001)
Subtask 57-26-00-010-050-B ** ON A/C NOT FOR ALL
D. Get Access
   (1) Put the ACCESS PLATFORM 3M (10 FT) below the applicable flap track fairings, zones 531 (631) 532 (632) and 533 (633).
   (2) Remove the applicable flap track fairing: (Ref. AMM TASK 57-55-11-000-004)
Subtask 57-26-00-110-050-A
E. Preparation for Inspection
   (1) Make sure that the inspection area is sufficiently clean to do the inspection of the area.
   (2) Use a Textile-Lint free Cotton - (Material No.14SBA1) , made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean:
  • the aft attachment of the flap track 2 on the wing bottom skin at the false rear spar
  • the aft attachment fittings of the flap tracks 3 and 4 at the rear spar.
   (3) Make sure that there is no TPS layer and if there is a TPS layer, remove it (Ref. AMM TASK 51-78-00-916-001).
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 57-26-00-210-050-A
A. Detailed Inspection of Outer Wing, Flap Track 2, Aft Attachment Fittings on Wing Bottom Skin at False Rear Spar and Flap Track 3 & 4 Aft Attachment Fittings at Rear Spar
   (1) Examine the aft attachment fittings of the flap track 2 on the wing bottom skin at the false rear spar. Use a MIRROR - INSPECTION and a LIGHT SOURCE - INSPECTION to make sure that:
  • there is no corrosion
  • there are no cracks
  • the nuts and safety devices are in the correct condition
  • the protective treatment is in the correct condition.
   (2) Examine the aft attachment fittings of the flap tracks 3 and 4 at the rear spar. Use a MIRROR - INSPECTION and a LIGHT SOURCE - INSPECTION to make sure that:
  • there is no corrosion
  • there are no cracks
  • the nuts and safety devices are in the correct condition
  • the protective treatment is in the correct condition.
NOTE: If necessary, refer to the SRM 572600 for the correct repair procedure.
5. Close-up
Subtask 57-26-00-410-051-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 applicable flap track fairing: (Ref. AMM TASK 57-55-11-400-001)
Subtask 57-26-00-410-051-B ** 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 applicable flap track fairing: (Ref. AMM TASK 57-55-11-400-004)
Subtask 57-26-00-865-051-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/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
Subtask 57-26-00-866-051-A
C. Aircraft Configuration
   (1) Retract the flaps (Ref. AMM TASK 27-50-00-866-009).
Subtask 57-26-00-942-051-A
D. Removal of Equipment
   (1) Remove the safety barriers.
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 02:11:14 UTC
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