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SAE International - ARP4118A

Isolation and Corrosion Protection of Dissimilar Materials, Carbon Composite Structure Repair

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Organization: SAE International
Publication Date: 15 August 2013
Status: active
description:

This SAE Aerospace Recommended Practice (ARP) provides methods and guidelines for isolating dissimilar repair patch materials from carbon composite structure during a repair operation.

Document History

ARP4118A
August 15, 2013
Isolation and Corrosion Protection of Dissimilar Materials, Carbon Composite Structure Repair
This SAE Aerospace Recommended Practice (ARP) provides methods and guidelines for isolating dissimilar repair patch materials from carbon composite structure during a repair operation.

References

This document references:
AMS2825 - MATERIAL SAFETY DATA SHEETS
Published by SAE International on January 1, 1979
This specification establishes requirements for the preparation of Material Safety Data Sheets which will provide information concerning the harmful or hazardous nature of materials to facilitate...
This document references:
AMS3265 - SEALING COMPOUND, POLYSULFIDE (T) RUBBER Nonchromated, Corrosion Inhibiting for Intermittent Use to 340 °C (171 °F)
Published by SAE International on March 1, 1996
This specification covers a polysulfide (T) rubber sealing compound with nonchromated corrosion inhibitors supplied as a two-component system which cures at room temperature.
This document references:
AMS3277 - SEALING COMPOUND, POLYTHIOETHER Integral Fuel Tanks and General Purpose, Fast Curing Intermittent Use to 360 °F (182 °C)
Published by SAE International on April 1, 1995
This specification covers two types and three classes of a fuel resistant polythioether sealing compound supplied as a two-component system.
This document references:
AMS3284 - Sealing Compound, Low Adhesion, for Removable Panels and Fuel Tank Inspection Plates
Published by SAE International on January 1, 1999
This specification covers a polysulfide sealing compound with low adhesive strength. This elastomeric compound shall be supplied as a two-component system which cures at room temperature.
This document references:
AMS3373 - COMPOUND, SILICONE RUBBER, INSULATING AND SEALING 35 - 55
Published by SAE International on January 1, 1981
This specification and its supplementary detail specifications cover elastomeric silicone insulating and sealing compounds supplied as two-component systems which cure at room temperature.
This document references:
AMSS8802 - Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion
Published by SAE International on May 1, 1999
This specification covers temperature resistant, two component synthetic rubber compounds of the polysulfide type for sealing and repairing integral fuel tanks and fuel cell cavities, for continuous...
This document references:
AS5502 - Standard Requirements for Aerospace Sealants
Published by SAE International on November 1, 2000
This document establishes standard requirements for aerospace sealants, which may be incorporated as part of Aerospace Material Specifications (AMS) for such products. This document provides for...
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