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)

Standard:
Revised:
  • 2008-03-26
 
  • HISTORICAL Access the latest revision: AMS3281F
Publisher:
  • SAE International
Pages:
15
Scope:

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).

Rationale:

Added types to differentiate by specific gravity.

History:
Standard Published Revision Status
AMS3281F 2016-03-08 Latest Revised
2010-12-02 Historical Revised
2008-03-26 Historical Revised
2003-01-24 Historical Revised
1999-03-01 Historical Revised
1996-11-01 Historical Revised
1994-11-01 Historical Issued
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