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CES 4. Procedure
_________ Subtask 25-00-00-220-061
A. Identify the Damage Limits (Ref. TASK 25-00-00-200-001)
(1) Type of repair patch:
-GILLPATCH III Subtask 25-00-00-340-061
B. Do the Repair
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(Ref. Fig. 826/TASK 25-00-00-991-039)
(1)
Remove the damaged material from the lining.
(2)
Rework the contour of the damaged area in order to get a regular shape.
NOTE : This will let you to cut and install the inlay patch
____
correctly.
(3)
Remove the rough edges with emery cloth, grade 80-120.
(4)
Clean the area with CLEANING AGENTS (Material No. 11-010) and a lint free cotton cloth MISCELLANEOUS (Material No. 19-003)
(5)
Cut two repair patches (1) and (3) to the applicable dimensions. NOTE : The repair patches must be 38 mm (1.5 in.) larger than the
____
damaged area in all directions.
NOTE : Do not use the patch to overlap another repair.
____
(6) Deburr the edges of the two repair patches with emery cloth grade 80-120..
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CES
CC Honeycomb Linings, Three Patches - Damage Through Figure 826/TASK 25-00-00-991-039
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(7)
Remove the protective backing from the repair patch (1).
(8)
Put the patch (1) over the damaged area on the rear side of the panel and push it in position.
(9)
Cut an inlay patch (2) to the dimension of the damaged area.
(10)
Remove the protective backing from the inlay patch (2).
(11)
From the view (cargo compartment) side of the panel:
(a)
Bond the inlay patch (2) onto the adhesive side of the rear side patch (1)
(b)
Make sure that patch (2) fully covers the adhesive side of the rear side patch (1).
(12)
Remove the protective backing from the repair patch (3).
(13)
Put the repair patch (3) over the damaged area on the view side of the panel and push it in position.
5. Close-up
________ Subtask 25-00-00-410-057
A. Close Access
(Ref. TASK 25-00-00-200-001)
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CES TASK 25-00-00-340-015
Speed Patches (on View Side) Repair Method (Damage Through) - All Cargo Compartment Linings with Honeycomb Core, but not Ceiling Panels
1. Reason for the Job
__________________
Refer to the AMM task 25-00-00-200-001
2. Job Set-up Information
______________________
A. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
No specific emery cloth grade 80-120.
No specific emery cloth, grade 80-120
No specific AKRO FIREGUARD (AF 800 SERIES)
Material No. 08-114A AIB AIMS 08-07-001
REPAIR PATCH INTURNESCENT SELF ADHESIVE (Ref. 20-31-00) Material No. 11-010 USA TT-I-735 GRADE A ISOPROPYL ALCOHOL (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-00-00-200-001 Cargo Compartment Linings with Honeycomb Core -General Repair/Protection Information 25-00-00-991-043 Fig. 827
3. Job Set-up
__________
Subtask 25-00-00-010-078
A. Get Access
(Ref. TASK 25-00-00-200-001).
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CES Subtask 25-00-00-220-064
B. Identify the Damage Limits (Ref. TASK 25-00-00-200-001)
(1) Type of repair patch:
-BONDING AND ADHESIVE COMPOUNDS (Material No. 08-114A) or
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