SAE AMS3269
Sealing Compound, Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities High Strength, for Intermittent Use to 360°F (182°C).
Standard:
AKA:
- AMS3269
- 1993-10-01
- Historical. Access the latest revision: AMS3269C
- Ams G9 Aerospace Sealing Committee
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).
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS3269C | 2011-09-23 | Latest | |
| AMS3269B | 2008-03-17 | Historical | |
| AMS3269A | 2003-01-13 | Historical | |
| AMS3269 | 1993-10-01 | Historical |
- SAE AMS 3269
- Aerospace
- Adhesives and Sealants
- Elastomers
- Plastics
- Materials properties
- Fuel tanks