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Standard

Sealing Compound, Polythioether Rubber Fuel Resistant, Fast Curing Intermittent Use to 360°F (182°C)

2010-08-18
HISTORICAL
AMS3277E
This specification coverspolythioether rubber sealing compound that is fuel resistant, supplied as a two component system which cures at room temperature. This product has been used typically for contact with fuel, but usage is not limited to such applications. Each application should be considered separately. Polythioether rubber has a service temperature range of -65 to +320 degrees F (-54 to +160 degrees C), with short-term recurring exposures (approximately 6 hours) to 360 degrees F (182 degrees C). It can be used for faying surface and fillet sealing and fastener overcoating. This product is not recommended for use in aerofairing, on aircraft windshields, on canopies or other applications directly exposed to weather. Sealing compound must be applied at temperatures above 50 degrees F (10 degress C), but will cure at lower temperatures.
Standard

Silicone Resin, Elastomeric, Opaque, Room Temperature Cure

2009-06-16
CURRENT
AMS3371A
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED". Cancelled specifications are available from SAE.
Standard

Sealing Compound, Polysulfide (T) Rubber, Fuel Resistant, Nonchromated Corrosion Inhibiting for Intermittent Use to 360°F (182°C)

2002-08-05
HISTORICAL
AMS3265B
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 product has been used typically for contact with air pressures, fuels and water, but usage is not limited to such applications. Each application should be considered separately. Polysulfide (T) rubber has a service temperature range of -65 to +250 degrees F (-54 to +121 degrees C), with short term recurring exposures (approximately 6 hours) to 360 degrees F (182 degrees C). It can be used for aerodynamic smoothing, cabin pressure and fillet sealing and fastener overcoating.
Standard

Sealing Compound, Polythioether Rubber Fuel Resistant, Fast Curing Intermittent Use to 360°F (182°C)

2002-07-30
HISTORICAL
AMS3277B
This specification coverspolythioether rubber sealing compound that is fuel resistant, supplied as a two component system which cures at room temperature. This product has been used typically for contact with fuel, but usage is not limited to such applications. Each application should be considered separately. Polythioether rubber has a service temperature range of -65 to +320 degrees F (-54 to +160 degrees C), with short-term recurring exposures (approximately 6 hours) to 360 degrees F (182 degrees C). It can be used for faying surface and fillet sealing and fastener overcoating. This product is not recommended for use in aerofairing, on aircraft windshields, on canopies or other applications directly exposed to weather. Sealing compound must be applied at temperatures above 50 degrees F (10 degress C), but will cure at lower temperatures.
Standard

Sealing Compound, Polysulfide (T) Rubber Nonchromated, Corrosion Inhibiting for Intermittent Use to 360°C (182°F)

2001-07-01
HISTORICAL
AMS3265A
This specification covers a polysulfide (T) rubber sealing compound with nonchromated corrosion inhibitors supplied as a two-component system which cures at room temperature. The compound has been used typically for faying surface sealing and for wet-installation of fasteners in aircraft structural joints, but usage is not limited to such applications. It can be used in non-fuel areas for fillet sealing and overcoating fasteners, for sealing joints and seams, cabin pressure sealing, and aerodynamic smoothing. AMS 3100 adhesion promoter can be applied prior to application of the sealant. This material is usable for continuous service from -65 to 248 degrees F (-55 to 120 degrees C), with short-term exposure (approximately 6 hours to 360 degrees F (182 degrees C).
Standard

Sealing Compound, Polysulfide (T) Synthetic Rubber For Integral Fuel Tank and Fuel Cell Cavities Low Density (1.20 to 1.35 sp gr), for Intermittent Use to 360°F (182°C)

1999-03-01
HISTORICAL
AMS3281B
This specification covers three classes of fuel-resistant polysulfide (T) sealing compound with low specific gravity, supplied as a two-component system which cures at room temperature. This sealing compound has been used typically in sealing aircraft integral fuel tanks, fuel tank fillets and faying surfaces, pressure barriers and moldline surfaces, but usage is not limited to such applications. The sealing compound is resistant to jet fuels and is capable of withstanding long-term exposure from -65 to +250 degrees F (-54 to +121 degrees C) and short-term exposure (six hours) to 360 degrees F (182 degrees C).
Standard

Sealing Compound, Polysulfide (T) Synthetic Rubber For Integral Fuel Tank and Fuel Cell Cavities Low Density (1.20 to 1.35 sp gr), for Intermittent Use to 360°F (182°C)

1996-11-01
HISTORICAL
AMS3281A
This specification covers three classes of fuel-resistant polysulfide (T) sealing compound with low specific gravity, supplied as a two-component system which cures at room temperature. This sealing compound has been used typically in sealing aircraft integral fuel tanks, fuel tank fillets and faying surfaces, pressure barriers and moldline surfaces, but usage is not limited to such applications. The sealing compound is resistant to jet fuels and is capable of withstanding long-term exposure from -65 to +250 degrees F (-54 to +121 degrees C) and short-term exposure (six hours) to 360 degrees F (182 degrees C).
Standard

Sealing Compound, Polysulfide (T) Rubber Nonchromated, Corrosion Inhibiting for Intermittent Use to 360°C (182°F)

1996-03-01
HISTORICAL
AMS3265
This specification covers a polysulfide (T) rubber sealing compound with nonchromated corrosion inhibitors supplied as a two-component system which cures at room temperature. The compound has been used typically for faying surface sealing and for wet-installation of fasteners in aircraft structural joints, but usage is not limited to such applications. It can be used in non-fuel areas for fillet sealing and overcoating fasteners, for sealing joints and seams, cabin pressure sealing, and aerodynamic smoothing. AMS 3100 adhesion promoter can be applied prior to application of the sealant. This material is usable for continuous service from -65 to 248 degrees F (-55 to 120 degrees C), with short-term exposure (approximately 6 hours to 360 degrees F (182 degrees C).
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