(c)
Put the repair patch in position and align the surface structure.
(d)
Transfer the contour of the repair patch to the NTF with a MARKER
-FELT TIP.
(2)
Cut the Damaged NTF CAUTION: DO NOT DAMAGE THE SURFACE BELOW THE TOP LAYER.
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R NTF (PVC) Repair Figure 808/TASK 25-00-00-991-028- 12 (SHEET 1)
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R NTF (PVC) Repair Figure 808/TASK 25-00-00-991-028- 22 (SHEET 2)
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CES
(a)
Carefully cut through the top layer of the floor covering with a CUTTER - THIN BLADE.
(b)
Carefully remove the top layer with a CHISEL - NON FERROUS from the laminate.
(c)
Remove the unwanted adhesive from the laminate with a SPATULA -NON METALLIC.
(3) Install the Repair Patch.
(a)
Clean the repair area and the smooth side of the patch with CLEANING AGENTS (Material No. 11-010) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
(b)
Apply a thin layer of BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) to the laminate with a BRUSH - BRISTLED.
(c)
Carefully put the patch in position and push it down with a ROLLER - RUBBER.
(d)
Remove the redundant adhesive with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
(e)
If necessary clean the area of the repair with CLEANING AGENTS (Material No. 11-010) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
5. Close-up
________
Subtask 25-00-00-862-068
A. De-energize the ground service network
(Ref. TASK 24-42-00-862-001).
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CES TASK 25-00-00-350-009
Repair of Insert Nut Connections Installed in Components with Honeycomb Core
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 SYRINGE
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific emery cloth, grade 80-120
Material No. 08-001 USA DOD-A-82720
GENERAL PURPOSE ADHESIVE HONEYCOMB FILLER
(Ref. 20-31-00) Material No. 08-074
MASKING TAPE (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. 11-010 USA TT-I-735 GRADE A
ISOPROPYL ALCOHOL (Ref. 20-31-00) Material No. 16-053 D DAN 1282-02
FILLER FOR CORE AND EDGE (2 PARTS) (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 -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 25-00-00-350-001 Minor Repair to the Decor Foil of Flat Composite Components R 25-00-00-991-029 Fig. 809
3. Job Set-up
__________
Subtask 25-00-00-861-085
A. Energize the ground service network
(Ref. TASK 24-42-00-861-001).
4. Procedure
_________
Subtask 25-00-00-350-069
A. Repair of Standard Insert Nut Attachment R (Ref. Fig. 809/TASK 25-00-00-991-029)
CAUTION : SOME PLASTICS AND RUBBER-BASE MATERIALS ARE ATTACKED BY
_______
HYDROCARBON SOLVENTS.
CAUTION : DO NOT USE METHANOL OR ENGINE TITANIUM PARTS COULD BE DAMAGED.
_______
(1) Preparation for Installation
(a)
Carefully remove the damaged insert and/or the unwanted material from the component.
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