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Aerospace Standard Test Methods for Aerospace Sealants Methods for Preparing Aerospace Sealant Test Specimens

AMS G9 Aerospace Sealing Committee
  • Aerospace Standard
  • AS5127C
  • Current
Published 2018-11-14 by SAE International in United States

This standard describes the accepted methods used for preparing aerospace sealant test specimens for qualification and quality conformance or acceptance testing. AS5127/1 and AS5127/2 are to be used in conjunction with this document and the applicable AMS specifications.

Sealing Compound Aircraft Firewall, Silicone

AMS G9 Aerospace Sealing Committee
  • Aerospace Material Specification
  • AMS3374E
  • Current
Published 2018-10-15 by SAE International in United States
This specification covers six types of silicone sealing compounds curing to elastomeric materials.
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Sealing Compound, Polysulfide Rubber Preformed Strips for Sealing Removable Doors, Skins, and Panels

AMS G9 Aerospace Sealing Committee
  • Aerospace Material Specification
  • AMS3379
  • Current
Published 2018-07-23 by SAE International in United States
This specification establishes the requirements for a polysulfide sealing compound in putty consistency to be used for form-in-place sealing of removable doors, skins, and panels.
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Sealing Compound, Low Adhesion, for Removable Panels and Fuel Tank Inspection Plates

AMS G9 Aerospace Sealing Committee
  • Aerospace Material Specification
  • AMS3284C
  • Current
Published 2017-11-16 by SAE International in United States
This specification covers a polysulfide sealing compound with low adhesive strength. This elastomeric compound shall be supplied as a two-component system which cures at room temperature.
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Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant

AMS G9 Aerospace Sealing Committee
  • Aerospace Material Specification
  • AMS3255B
  • Current
Published 2017-07-17 by SAE International in United States
This specification establishes the requirements for an expanded polytetrafluoroethylene (EPTFE) in the form of sealing tape, gaskets, or sheets requiring no mixing or curing.
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Sealing Compound, Polythioether Elastomeric Two-Part Electrically Conductive

AMS G9 Aerospace Sealing Committee
  • Aerospace Material Specification
  • AMS3266A
  • Current
Published 2017-02-23 by SAE International in United States
This specification covers two types of electrically conductive, elastomeric polythioether sealing compounds that cure at room temperature. The sealing compound is supplied as either a two-component system or as premixed and frozen.
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Sealing Compound, Polythioether Rubber Fast Curing, Light Weight (Specific Gravity 0.78, max.) for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C)

AMS G9 Aerospace Sealing Committee
  • Aerospace Material Specification
  • AMS3102
  • Current
Published 2017-02-22 by SAE International in United States
This specification covers a fuel-resistant polythioether sealing compound with low specific gravity, supplied as a two-component system which cures at room temperature.
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Fluid, Jet Reference

AMS G9 Aerospace Sealing Committee
  • Aerospace Material Specification
  • AMS2629E
  • Current
Published 2017-02-08 by SAE International in United States
This specification covers a mixture of liquid hydrocarbons and soluble additives.
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Sealing of Integral Fuel Tanks

AMS G9 Aerospace Sealing Committee
  • Aerospace Standard
  • AIR4069C
  • Current
Published 2016-11-23 by SAE International in United States
This SAE Aerospace Information Report (AIR) presents preferred design, assembly, and repair practices for sealing of aircraft integral fuel tanks, including rework of applied fuel tank seals. It addresses engineering designs for integral fuel tanks as they are currently found in practice; and discusses the most practical and conservative methods for producing a reliable, sealed system. Although this AIR presents practices for sealing of integral fuel tanks, the practices presented within this report are practices that are carried throughout sealing that include both pressure and environmental aircraft sealing. Design preferences for optimum sealing are not within the scope of this document. Such discussions can be found in the United States Air Force (USAF) sponsored report, entitled Aircraft Integral Fuel Tank Design Handbook, AFWAL-TR-87-3078. Key objectives of the fuel tank sealing process are to produce a sealing plane that is leak-free and corrosion resistant, especially at fastener locations, at environmental and operational conditions expected for the life of each aircraft. Factors that can influence the outcome of this process are: a How well the basic design…
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Sealing Compound, Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C)

AMS G9 Aerospace Sealing Committee
  • Aerospace Material Specification
  • AMS3276G
  • Current
Published 2016-10-25 by SAE International in United States
This specification covers fuel-resistant polysulfide (T) sealing compounds supplied as a two-component system.
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