____
damaged
area in all directions.
(9)
For Isovolta RHM Patch BONDING AND ADHESIVE COMPOUNDS (Material No. 08-083) only:
(a) Use a heat blanket between 100 DEG.C (212 DEG.F) and 110 DEG.C (230 DEG.F) with a soft force to bond the repair patch to the panel.
5. Close-up
________ Subtask 25-00-00-410-079
A. Close Access
(Ref. TASK 25-00-00-200-001)
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CES TASK 25-00-00-340-022
Speed Patches and Filler 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 No specific No specific Material No. 08-066
Material No. 08-114A
Material No. 08-115 Material No. 08-115A Material No. 08-115B Material No. 08-115C Material No. 11-010 Material No. 19-003
emery cloth grade 80-120.GILLFAB 1367A-013GILLFAB 1367P-013D DAN 319, DAN 1202 ACRYLIC PRESSURE SENSITIVE ADHESIVE FILM (Ref. 20-31-00)AIB AIMS 08-07-001 REPAIR PATCH INTURNESCENT SELF ADHESIVE (Ref. 20-31-00)AIB AIMS 08-08-001 CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00)AIB AIMS 08-08-001 CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00)AIB AIMS 08-08-001 CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00)D DAN 1282 CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00)USA TT-I-735 GRADE A ISOPROPYL ALCOHOL (Ref. 20-31-00)USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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CES B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-00-00-200-001 Cargo Compartment Linings with Honeycomb Core -General Repair/Protection Information 25-00-00-991-037 Fig. 830
3. Job Set-up
__________ Subtask 25-00-00-010-086
A. Get Access
(Ref. TASK 25-00-00-200-001)
4. Procedure
_________ Subtask 25-00-00-220-057
A. Identify the Damage Limits (Ref. TASK 25-00-00-200-001)
(1) Types of repair patch
-
GILLFAB 1367P-013
-
GILLFAB 1367P-013 and double side adhesive tape BONDING AND ADHESIVE COMPOUNDS (Material No. 08-066)
-
GILLFAB 1367A-013 and double side adhesive tape BONDING AND ADHESIVE COMPOUNDS (Material No. 08-066)
-BONDING AND ADHESIVE COMPOUNDS (Material No. 08-114A) Subtask 25-00-00-340-091
B. Do the Repair WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
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CES 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. 830/TASK 25-00-00-991-037)
NOTE : Do not use the patch to overlap another repair.
____
(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.
NOTE : The overlap of patches is not allowed.
____
(6)
Deburr the edges of the patch with emery cloth grade 80-120..
(7)
Remove the protective backing from the repair patch.
NOTE : Obey the manufacturers instructions.
____
(8)
Put the patch over the damaged area on the rear side and push it into position.
(9)
Fill the
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115)
or
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