W DOC AIRBUS | AMM A320F

Special Detailed Inspection (US) of Centre Wing Box and Outer Wing Box, Lower Splice and Panel between Stiffener 6 and FR 42, LH/RH


TASK 57-10-00-270-807-A
Special Detailed Inspection (US) of Centre Wing Box and Outer Wing Box, Lower Splice and Panel between Stiffener 6 and FR 42, 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: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 191
ZONE: 192
ZONE: 195
ZONE: 196
1. Reason for the Job
Refer to the ALI TASK: 571204-01
SPECIAL DETAILED INSPECTION (US) OF CENTRE WING BOX AND OUTER WING BOX, LOWER SPLICE AND PANEL BETWEEN STIFFENER 6 AND FR 42, LH/RH.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT)
 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
191
AIR CONDITIONING COMPT AND FAIRINGS
192
AIR CONDITIONING COMPT AND FAIRINGS
195
HYDRAULIC COMPT AND FAIRINGS
196
HYDRAULIC COMPT AND FAIRINGS
147CB, 148DB, 191LB, 192LB, 734, 744
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 28-00-00-910-001-A
Fuel Safety Procedures
TASK 32-12-00-010-001-A
Open the Main Gear Doors for Access
TASK 32-12-00-410-001-A
Close the Main Gear Doors after Access
TASK 53-35-11-000-001-A
Removal of the Wing-to-Fuselage Fairings
TASK 53-35-11-400-001-A
Installation of the Wing-to-Fuselage Fairings
SRM 512300
SRM 512400
NTM 571204
SRM 511100
(for corrective action)
SRM 512200
(for corrective action)
3. Job Set-up
Subtask 57-10-00-941-077-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Obey the fuel safety precautions (Ref. AMM TASK 28-00-00-910-001).
Subtask 57-10-00-010-105-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Open MLG door 734 ( 744) (Ref. AMM TASK 32-12-00-010-001).
   (2) Put the ACCESS PLATFORM 2M (6 FT) in position at zone 191 (192).
   (3) Remove wing-to-fuselage fairings 147CB, 148DB, 191LB and 192LB (Ref. AMM TASK 53-35-11-000-001).
Subtask 57-10-00-110-093-A ** ON A/C NOT FOR ALL
C. Preparation of the Inspection Area
   (1) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection of the area.
   (2) If not, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and the Textile-Lint free Cotton - (Material No.14SBA1) .
   (3) Remove the sealant and/or paint from the inspection area if this is necessary for the Nondestructive Testing Manual (NTM) task.
4. Procedure
Subtask 57-10-00-270-063-A ** ON A/C NOT FOR ALL
A. Inspection
   (1) Do a special detailed inspection of the left and right sides of the center and outer wing boxes (and of the lower splice and panel) for damage or discontinuities. This inspection includes the area between stiffener 6 and FR42. Refer to NTM 571204.
   (2) Make a report of the damage after the NTM inspection:
     (a) Corrosion damage:
If you find corrosion, refer to the Structural Repair Manual (Ref. SRM 512200) for the corrosion types, inspection, removal and subsequent corrosion protection.
     (b) Other damage (scratches, cracks, gouges, dents, creases):
If you find this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100) for the damage types, classification and corrective action.
Subtask 57-10-00-390-062-A ** ON A/C NOT FOR ALL
B. Sealant or Paint Application
   (1) If the NTM procedure told to remove the sealant and/or paint from the inspection area, apply sealant (refer to SRM 512400) or paint (refer to SRM 512300) on the inspection area.
5. Close-up
Subtask 57-10-00-410-106-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 wing-to-fuselage fairings 147CB, 148DB, 191LB and 192LB (Ref. AMM TASK 53-35-11-400-001).
   (3) Remove the access platform(s).
   (4) Close MLG door 734 ( 744) (Ref. AMM TASK 32-12-00-410-001).
[Rev.10 from 2021] 2026.04.02 06:30:32 UTC