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Sealing Compound, Polysulfide Type, Low Temperature Curing, Quick Repair, Integral Fuel Tanks and Fuel Cell Cavities

2003-01-16
HISTORICAL
AMSS83318A
This specification covers two-component polysulfide sealing compounds, temperature resistant, for use from -65 to +250 °F (-54 to 121 °C), low temperature curing to 20 °F (-13 °C) minimum, for quick repair of integral fuel tanks and fuel cell cavities. During application, the sealing compound shall exhibit suitable, fluid consistency.
Standard

Sealing Compound, Polysulfide Type, Low Temperature Curing, Quick Repair, Integral Fuel Tanks and Fuel Cell Cavities

2011-04-04
HISTORICAL
AMSS83318B
This specification covers two-component polysulfide sealing compounds, temperature resistant, for use from −65 to 250 °F (−54 to 121 °C), low temperature curing to 20 °F (−13 °C) minimum, for quick repair of integral fuel tanks and fuel cell cavities. During application, the sealing compound shall exhibit suitable, fluid consistency.
Standard

Sealing Compound, Polysulfide Type, Low Temperature Curing, Quick Repair, Integral Fuel Tanks and Fuel Cell Cavities

1999-05-01
HISTORICAL
AMSS83318
This specification covers two-component polysulfide sealing compounds, temperature resistant, for use from -65 to +250 °F (-54 to 121 °C), low temperature curing from 20 °F (-13 °C) minimum, for quick repair of integral fuel tanks and fuel cell cavities. During application, the sealing compound shall exhibit suitable, fluid consistency.
Standard

Sealing Compound, Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities High Strength, for Intermittent Use to 360°F (182°C)

1993-10-01
HISTORICAL
AMS3269
This specification covers three class of fuel-resistant polysulfide (T) sealing compound with high strength and temperature characteristics, 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)

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).
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