Aug 01/05
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CES
CC Honeycomb Linings, Filler - Damage Not Through Figure 824/TASK 25-00-00-991-038
R EFF : CES ALL 25-00-00 Page A825 Aug 01/05
(4) Fill the
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BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115) or
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BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115A) or
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BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115B) or
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BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115C) into the prepared area.
NOTE : Obey the manufacturers instructions.
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(5) Make the cured repaired area smooth with emery cloth, grade 80-120
5. Close-up
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Subtask 25-00-00-410-063
A. Close Access
(Ref. TASK 25-00-00-200-001)
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CES TASK 25-00-00-340-005
Patch and Filler Repair Method (Damage not Through) - All Cargo Compartment Linings with Honeycomb Core
1. Reason for the Job
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Refer to the AMM task 25-00-00-200-001
2. Job Set-up Information
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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 25-00-00-991-036 Fig. 825
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Aug 01/05
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CES 3. Job Set-up
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Subtask 25-00-00-010-060
A. Get Access
(Ref. TASK 25-00-00-200-001)
4. Procedure
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Subtask 25-00-00-220-062
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)
Select the appropriate repair kit.
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BONDING AND ADHESIVE COMPOUNDS (Material No. 08-075) or
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BONDING AND ADHESIVE COMPOUNDS (Material No. 08-076) or
-BONDING AND ADHESIVE COMPOUNDS (Material No. 08-077) |------------------------------------|---------------------------------------| | Mat.-No.: | Damage length: | Damage width: | |------------------------------------|---------------------------------------| |08-075(Akro Fireguard Patch, small) | 50.8 mm (2.0 in.) | 50.8 mm (2.0 in.) | |------------------------------------|---------------------------------------| |08-076(Akro Fireguard Patch, medium)| 50.8 mm (2.0 in.) | 152 mm (6.0 in.) | |------------------------------------|---------------------------------------| |08-077(Akro Fireguard Patch, large) | 152 mm (6.0 in.) | 152 mm (6.0 in.) | |------------------------------------|---------------------------------------|
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