(3)
If necessary, make the outer surface of the inspection area smooth with the abrasive cloth, grade 280. Make sure the inspection area is dry before you continue.
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Internal Doubler of the Cutout at the Waste Service Panel Figure 659/TASK 53-41-00-991-022
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(4)
Do a visual inspection of the outer surface of the inspection area. Look for damage, and defects in the shape of the surface.
(5)
If you find damage :
(a)
Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification of the damage.
(b)
If you find corrosion damage:
-
refer to the ASRM (Ref. ASRM 51-22-00-001) for the general corrosion data
-
refer to the ASRM (Ref. ASRM 51-74-00-001) for the repair of the corroded areas.
(c)
If you find other types of damage:
-Refer to the ASRM (Ref. ASRM 51-73-00-001) for the repair of the minor damage.
4. Procedure
_________
(Ref. Fig. 659/TASK 53-41-00-991-022)
Subtask 53-41-00-220-055
A. Special Detailed Inspection Procedure
(1)
Do the special detailed inspection (Ref. NTM 534137-Part.6) of the internal doubler, FWD and AFT of the cutout for the waste service panel. Do this externally between the STGR35 and the STGR39 positions, RH only.
(2)
Write a report about the damage you find during the inspection procedure.
NOTE : No repair data is given in the ASRM (Ref. ASRM 53-41-11-001)
____ for the doubler of the cutout for the waste service panel. If the doubler is damaged:
-you must contact AIRBUS INDUSTRIE for the necessary corrective action procedure.
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5. Close-up
________
Subtask 53-41-00-370-056
A. Repair of the Surface Protection
(1) If necessary, repair the paint coating in the inspection area (Ref. TASK 51-75-12-300-003) or (Ref. TASK 51-75-12-300-001).
Subtask 53-41-00-410-096
B. Put the aircraft back to the serviceable condition.
(1)
Make sure that the work area is clean and clear of tool(s) 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.
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CES TASK 53-41-00-220-010
special Detailed Inspection of Splice Plate at Circumferential Skin Splice at FR64, from Stringer 10, LH/RH, to Crown Centerline
1. Reason for the Job
__________________
Refer to the MPD TASK: 534121-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific abrasive cloth, grade 280
No specific access platform 5.5 m (18 ft. 1 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-75-12-300-001 Repair of Major Paint Damage on Light Alloy and
Composite Material 51-75-12-300-003 Repair of Minor Paint Damage (Topcoat Only) ASRM 51-11-00-001 ASRM 51-22-00-001 ASRM 53-41-11-001 NTM 534121-Part.6 ASRM 51-73-00-001 (for corrective action) ASRM 51-74-00-001 (for corrective action)
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