Aug 01/05
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CES 3. Job Set-up
__________
Subtask 25-00-00-010-089
A. Get Access
(Ref. TASK 25-00-00-200-001)
4. Procedure
_________
Subtask 25-00-00-220-059
A. Identify the Damage Limits (Ref. TASK 25-00-00-200-001)
(1)
If the length of a damaged area is more than 25 mm (0.98 in.):
-the minimum distance to another damaged area or repaired area in the same panel is 50 mm (1.97 in.)
-If the distance to another damaged area is less than 50 mm (1.97 in.), both damaged areas should be considered as a single damage.
(2)
Types of repair patch
-
GILLFAB 1367P-013 and double side adhesive tape BONDING AND ADHESIVE COMPOUNDS (Material No. 08-066)
-
GILLFAB 1367P-013
-GILLPATCH III
Subtask 25-00-00-340-094
B. Do the Repair
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
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. 832/TASK 25-00-00-991-044)
NOTE : Do not use the patch to overlap another repair.
____
EFF : ALL 25-00-00Page A864
Aug 01/05
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CES
CC Honeycomb Linings, Filler/Patch - Damage Not Through Figure 832/TASK 25-00-00-991-044
R EFF : CES ALL 25-00-00 Page A865 Aug 01/05
(1)
Remove the damaged area from the panel.
(2)
Smooth and deburr the repair with emery cloth grade 80-120.
(3)
Clean the repair area with CLEANING AGENTS (Material No. 11-010) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003)
(4)
Make sure that the repair area is dry.
(5)
Cut a patch to the applicable dimensions. NOTE : The repair patch must be 38 mm (1.5 in.) larger than the
____
damaged area in all directions.
(6)
Deburr the edges of the patch with emery cloth grade 80-120.
(7)
Fill the
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115) or
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115A) or
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115B) or
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115C) into the prepared area.
NOTE : Obey the manufacturers instructions.
____
(8)
Make sure that the repair area is dry.
(9)
Remove the protective backing from the patch.
NOTE : Obey the manufacturers instructions.
____
(10) Put the patch over the damaged area on the view side of the panel and push it into position.
5. Close-up
________ Subtask 25-00-00-410-083
A. Close Access
(Ref. TASK 25-00-00-200-001)
EFF : ALL 25-00-00Page A866
Aug 01/05
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CES TASK 25-00-00-340-026
Stainless Steel-Patch Repair Method (Damage not Through) - All Cargo Compartment Linings with Honeycomb Core
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 sheet of Stainless Steel 0.6 mm (0.024 in.) to 2 mm
(0.08 in.)
Material No. 08-001 USA DOD-A-82720 GENERAL PURPOSE ADHESIVE HONEYCOMB FILLER (Ref. 20-31-00)
Material No. 08-010A D DAN 1199-01 EPOXY RESIN AND HARDENER ADHESIVE (Ref. 20-31-00)
Material No. 08-066 D DAN 319, DAN 1202 ACRYLIC PRESSURE SENSITIVE ADHESIVE FILM (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 -------------------------------------------------------------------------------
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