(4)
Use the removed panel as a template and transfer all the holes from the removed panel to the replacement panel.
(5)
Drill and deburr the holes.
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(6) Remove the honeycomb-core to a minimum depth of 6 mm (0.24 in.) from along the edges you have cut.
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______
THIS/THESE MATERIAL/S.
USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
(7) Clean the replacement panel with CLEANING AGENTS (Material No. 11-010) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______
THIS/THESE MATERIAL/S.
USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
(8)
Apply filler STRUCTURE PAINTS (Material No. 16-053) into the edges and let the filler harden.
(9)
Smooth and deburr the edges with emery cloth, 80-120 grade .
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(10) Install all the removed anchor-nuts, clip-nuts and other items to the
replacement panel. ________
5. Close-up
Subtask 25-00-00-410-076
A. Close Access (Ref. TASK 25-00-00-200-001)
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CES TASK 25-00-00-340-020
Patches and Filler Repair Method (Damage 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 Material No. 08-075 D WA-10016
QUICK SETTING EPOXY ADHESIVE KIT (Ref. 20-31-00) Material No. 08-076 D WA-10016
QUICK SETTING EPOXY ADHESIVE KIT (Ref. 20-31-00) Material No. 08-077 D WA-10016
QUICK SETTING EPOXY ADHESIVE KIT (Ref. 20-31-00) Material No. 08-115 AIB AIMS 08-08-001
CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 08-115A AIB AIMS 08-08-001
CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 08-115B AIB AIMS 08-08-001
CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 08-115C D DAN 1282
CORE FILLER AMBIENTTEMPERATURE CURING (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 25-00-00-991-040 Fig. 828
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CES 3. Job Set-up
__________
Subtask 25-00-00-010-092
A. Get Access
(Ref. TASK 25-00-00-200-001)
4. Procedure
_________
Subtask 25-00-00-220-065
A. Identify the Damage Limits (Ref. TASK 25-00-00-200-001)
(1) Select the appropriate repair kit.
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-075) or
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