Sealing Compound, Polysulfide, Accelerator Required, For Aircraft Structures
- Aerospace Material Specification
- AMSS7124A
- Noncurrent
Scope
Recommended Content
Aerospace Material Specification | Sealing Compound, Polysulfide, Accelerator Required, For Aircraft Structures |
Aerospace Material Specification | Sealing Compound Aircraft Firewall, Silicone |
Aerospace Material Specification | Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
Topic
Data Sets - Support Documents
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TABLE I | Application life. | |
TABLE II | Tack free time. | |
TABLE III | Properties after cure. | |
TABLE IV | Qualification tests. | |
TABLE V | Quality conformance tests. | |
TABLE VI | Packaging examination. | |
TABLE VII | Formulation of cleaner. | |
TABLE VIII | Curing cycles. | |
TABLE IX | Adhesion panel materials and specimens required. | |
TABLE X | Immersion fluids. | |
Unnamed Dataset 16 | ||
Unnamed Dataset 17 |
Issuing Committee
AMS G9 Aerospace Sealing Committee
AMS Committee G9, Aerospace Sealing, is primarily responsible for the preparation, revision, and review of documents related to the sealing of aerospace vehicles for fluid containment and environmental protection by the use of sealants which are applied and cured to solid materials or are permanently mastic. Common sealant application examples include the sealing of integral fuel tanks, fuel bladder cavities, crew and passenger areas, access doors, fasteners, avionics compartments, windshields, and firewalls. The committee shall discuss sealing material and process developments, material property requirements, test methods, the effect of the environment on cured and uncured sealant materials and their containers, and emerging sealant industry challenges. The committee has dedicated subcommittees to address elastomeric aircraft fuel bladders, new sealant specification requirements, surface preparation for sealing, and sealant application and removal technologies.