-
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)
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CC Honeycomb Linings, Filler/Patch - Damage Through Figure 830/TASK 25-00-00-991-037
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it into the prepared area.
NOTE : Obey the manufacturers instructions.
____
(10)
Make sure that the repair area is dry.
(11)
Cut another 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.
____
(12)
Deburr the edges of the patch with emery cloth grade 80-120..
(13)
Remove the protective backing from the repair patch.
NOTE : Obey the manufacturers instructions.
____
(14)
Put the patch over the damaged area on the view side of the panel and push it into position.
5. Close-up
________ Subtask 25-00-00-410-080
A. Close Access
(Ref. TASK 25-00-00-200-001)
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Patches, Filler and Rivets 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. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 GUN - FASTENER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
No specific emery cloth grade 80-120.
No specific heat blanket
No specific CRES rivets (NAS 1919 C 04 S 06 U)
No specific CRES rivets (NAS 1919 C 04 S 07 U)
No specific Monel Rivet (NAS 1919 M 04 S 06 U)
No specific Monel Rivet (NAS 1919 M 04 S 07 U)
No specific 3.3 mm (0.128 in.) to 3.5 mm (0.137 in.) drill.
Material No. 08-083
RAPID HOT-MELT PATCH (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)
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CES C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-00-00-200-001 Cargo Compartment Linings with Honeycomb Core -General Repair/Protection Information 25-00-00-991-045 Fig. 831
3. Job Set-up
__________ Subtask 25-00-00-010-087
A. Get Access
(Ref. TASK 25-00-00-200-001)
4. Procedure
_________ Subtask 25-00-00-220-058
A. Identify the Damage Limits (Ref. TASK 25-00-00-200-001)
(1) Type of repair patch:
-BONDING AND ADHESIVE COMPOUNDS (Material No. 08-083) Subtask 25-00-00-340-092
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. 831/TASK 25-00-00-991-045)
(1) Remove the damaged material from the panel.
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