(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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 CES

 (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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