Subtask 25-00-00-340-057
B. Repair of Cargo Compartment Lining(s) with Patch and Filler.
(Ref. Fig. 825/TASK 25-00-00-991-036)
Use
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-075)
or
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-076)
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CC Honeycomb Linings, Filler and Patches (AKRO 300) - Damage Not Through Figure 825/TASK 25-00-00-991-036
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or
-BONDING AND ADHESIVE COMPOUNDS (Material No. 08-077).
NOTE : If the damage exceeds the dimension of the biggest repair patch,
____ it is allowed to overlap patches in one direction only. Make sure that the minimum overlap width is 6.4 mm (0.25 in.).
(1)
Carefully remove the damaged material from the lining panel.
(2)
If necessary remove a portion of the layers of Tedlar film from the repair area at least as large as the used patch(es).
NOTE : The lining panel has a Tedlar film if the resin below the
____
white film is of a different color.
(3)
Smooth the repair area with emery cloth, grade 80-120 and make sure that all the gloss finish is removed.
(4)
Remove the grit and dust from the repair area with the towel supplied in the repair kit(s).
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
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.
(5) Clean the repair area with CLEANING AGENTS (Material No. 11-010) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
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(6)
Fill the
-
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115) or
-
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) it into the prepared area.
(7)
Perform the further work-steps necessary to complete the repair according to the manufacturer's instructions delivered with the repair kit(s).
(8)
Make sure that:
-
the repair patch(es) overlap the damaged area 25.4 mm (1.00 in.) minimum in all directions
-
the reinforcement scrim(s) overlap the repair patch(es) 25.4 mm
(1.00 in.) minimum in all directions.
5. Close-up
________
Subtask 25-00-00-410-056
A. Close Access
(Ref. TASK 25-00-00-200-001)
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Speed Patches (on Both Sides) 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. No specific emery cloth, grade 80-120 No specific GILLPATCH III 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 25-00-00-991-039 Fig. 826
3. Job Set-up
__________
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