AMSS83318C: Sealing Compound, Polysulfide Type, Low Temperature Curing, Quick Repair, Integral Fuel Tanks and Fuel Cell Cavities - Material Specification

Features

Issuing Committee: AMS G9 Aerospace Sealing Committee

Scope

Content: This specification covers two-component polysulfide sealing compounds for quick repair of integral fuel tanks and fuel cell cavities. The sealing compound shall be capable of being cured as low as 20 °F (-7 °C), and be resistant to long term exposures from -65 to 250 °F (-54 to 121 °C).

Rationale

Content: 5-year update. Removed Air Content and Minimum Flow requirements. Removed Chalking as an Initial Acceptance Test. Added a fuel exposure requirement prior to testing for Low Temperature Flexibility. Additional formatting, editorial corrections and clarifications were offered.

Meta Tags

Topics: Materials properties
Adhesives and sealants
Fuel tanks
Titanium alloys
Aluminum alloys
Fuel cells
Heat treatment
Tensile strength
Drying
Test procedures

Details

DOI: https://doi.org/10.4271/AMSS83318C

Pages: 11

Citation: SAE International Material Specification, Sealing Compound, Polysulfide Type, Low Temperature Curing, Quick Repair, Integral Fuel Tanks and Fuel Cell Cavities, SAE Standard AMSS83318C, Revised July 2016, Issued May 1999, https://doi.org/10.4271/AMSS83318C.

Additional Details

Publisher: SAE International

Published: Jul 12, 2016

Product Code: AMSS83318C

Content Type: Material Specification

Status: Revised

Language: English

Historical