W DOC AIRBUS | AMM A320F

Special Detailed Inspection of Splice Plate at Circumferential Skin Splice at FR64, from Stringer 10, LH/RH to Crown Centerline

TASK 53-41-00-220-010-A
Special Detailed Inspection of Splice Plate at Circumferential Skin Splice at FR64, from Stringer 10, LH/RH to Crown Centerline

ZONE: 200
1. Reason for the Job
Refer to the MPD TASK: 534121-01
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 64, FROM STRINGER 10, LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE
No specific
1
CLOTH-EMERY (GRADE 280)
 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
200
UPPER HALF FUSELAGE
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 51-75-12-300-001-A
Repair of Major Paint Damage on Light Alloy and Composite Material
TASK 51-75-12-300-003-A
Repair of Minor Paint Damage (Topcoat Only)
SRM 511100
SRM 512200
SRM 534111
NTM 534121
SRM 51730000
 (for corrective action)
SRM 51740000
 (for corrective action)
F Circumferential Skin Splice at FR64, from STGR10 LH/RH to Crown Centerline
3. Job Set-up
Subtask 53-41-00-010-121-A
A. Get Access
   (1) Put the ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE in position adjacent to FR64.
Subtask 53-41-00-860-057-A
B. Preparation of the Inspection Areas
F Circumferential Skin Splice at FR64, from STGR10 LH/RH to Crown Centerline
   (1) Make sure that the outer surface of the inspection area is clean and smooth.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
   (2) If necessary, clean the outer surface of the inspection area with the Non Aqueous Cleaner-General - - (Material No.08BAA9) and a Textile-Lint free Cotton - (Material No.14SBA1) . Make sure the inspection area is dry before you continue.
   (3) If necessary, make the outer surface of the inspection area smooth with the CLOTH-EMERY (GRADE 280).
   (4) Do a visual inspection of the outer surface of the inspection area. Look for damage, and defects in the shape of the external surface.
   (5) If you find damage :
     (a) Refer to the ASRM SRM 511100 for the classification of the damage.
     (b) If you find corrosion damage:
  • refer to the ASRM SRM 512200 for the general corrosion data
  • refer to the ASRM SRM 51740000 for the repair of the corroded areas.
     (c) If you find other types of damage:
  • Refer to the ASRM SRM 51730000 for the repair of the minor damage.
4. Procedure
Subtask 53-41-00-220-058-A
A. Special Detailed Inspection Procedure
   (1) Do the special detailed inspection NTM 534121 of the splice plates at the circumferential skin splice at FR64. Do this externally from the STGR10 LH/RH positions, to the crown centerline.
   (2) Write a report about the damage you find during the inspection procedure.
NOTE: No repair data is given in the ASRM SRM 534111 for the splice plates of the circumferential skin splice at FR64. If a splice plate is damaged:
  • you must contact AIRBUS INDUSTRIE for the necessary corrective action procedure.
5. Close-up
Subtask 53-41-00-370-054-A
A. Repair of the Surface Protection
   (1) If necessary, repair the paint coatings in the inspection areas (Ref. AMM TASK 51-75-12-300-003) or (Ref. AMM TASK 51-75-12-300-001).
Subtask 53-41-00-410-118-A
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the access platform(s).
   (3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.02 06:29:19 UTC
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