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Emissions Electrical, Electronics, and Avionics Energy conservation AMS G9 Aerospace Sealing Committee

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Standard

Aircraft Sealant Removal Techniques
2012-01-17
CURRENT
AIR3270A
This SAE Aerospace Information Report (AIR) provides information on the possible methods of sealant removal. The discussion will focus on the methods of sealant removal and give the strengths and weaknesses of each method.
Standard

Aircraft Sealant Removal Techniques
2008-01-16
HISTORICAL
AIR3270
This SAE Aerospace Information Report (AIR) provides information on the possible methods of sealant removal. The discussion will focus on the methods of sealant removal and give the strengths and weaknesses of each method.
Standard

COATING MATERIALS, FLUOROCARBON (FKM) ELASTOMERIC
1990-07-01
HISTORICAL
AMS3138B
This specification and its supplementary detail specifications cover fluorocarbon (FKM) elastomeric coating materials for fiber-reinforced-resin composite structures in the form of two-component brushable or sprayable liquids.
Standard

Insulating Compound, Electrical, Embedding, Reversion Resistant Silicone
2021-03-05
CURRENT
AS81550B
This specification covers the requirements for two types of a two-part, transparent, reversion resistant flexible insulating compound, to provide resilient, environmental, and electrical insulation of components in systems in temperature range -85 to 392 °F (-65 to 200 °C). These insulating compounds are intended for embedding, potting or encapsulation of electrical and electronic components in systems where tear resistance is not critical, but their use is not limited to such applications. These transparent compounds allow visual circuit and part identification and facilitate part replacement and repairs. The insulating compound shall cure in sections of unlimited thickness, either exposed to air or completely sealed.
Standard

SEALING INTEGRAL FUEL TANKS
1990-10-01
HISTORICAL
AIR4069
This Aerospace Information Report (AIR) presents preferred practices for sealing and repairing integral fuel tanks. It addresses several basic fuel tank designs as they are currently found in practice and discusses the most practical and conservative methods for producing a reliable, sealed system. Design preferences for optimum sealing are not within the scope of this document. Such discussions can be found in the Air Force sponsored handbook entitled Aircraft Integral Fuel Tank Design Handbook, AFWAL-TR-87-3078. The basic goal in sealing an integral fuel tank is to produce a system that is leak-free for the long term under the environmental and operational conditions expected.
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