Search Results

Standard

Sealing Compound Aircraft Firewall, Silicone

2023-05-22

CURRENT

AMS3374G

This specification covers six types of silicone sealing compounds as either one-part or two-part systems that cure at room temperature.

Standard

Sealing Compound, Polysulfide (T) Rubber, Fuel Resistant, Non-Chromated Corrosion Inhibiting for Intermittent Use to 360 °F (182 °C)

2020-09-09

CURRENT

AMS3265F

This specification covers polysulfide rubber sealing compounds containing only non-chromated corrosion inhibitors, supplied as a two-component system which cures at room temperature.

Standard

Sealing and Coating Compound, Polyurethane (PUR) Fuel Resistant High Tensile Strength / Elongation For Integral Fuel Tanks / Fuel Cavities / General Purpose

2016-10-24

HISTORICAL

AMS3278B

This specification covers polyurethane (PUR) in the form of two-component sealing compounds.

Standard

Sealing Compound, Polysulfide (T) Rubber, Fuel Resistant, Non-Chromated Corrosion Inhibiting For Intermittent Use to 360 °F (182 °C)

2015-12-02

HISTORICAL

AMS3265E

This specification covers polysulfide rubber sealing compounds containing only non-chromated corrosion inhibitors, supplied as a two component system which cures at room temperature.

Standard

Aerospace Standard Test Methods for Aerospace Sealants Two-Component Synthetic Rubber Compounds

2014-10-08

HISTORICAL

AS5127/1C

This SAE Aerospace Standard (AS) describes test methods to determine the application and performance properties of two-component sealing compounds. It shall be used in conjunction with AS5127 and the applicable material specification. When modifications to these test methods are called out in material specifications, the material specification shall take precedence.

Standard

Sealing Compound Aircraft Firewall, Silicone

2013-11-26

HISTORICAL

AMS3374D

This specification covers six (6) types of silicone sealing compounds curing to elastomeric materials.

Standard

Isolation and Corrosion Protection of Dissimilar Materials, Carbon Composite Structure Repair

2013-08-15

HISTORICAL

ARP4118A

This SAE Aerospace Recommended Practice (ARP) provides methods and guidelines for isolating dissimilar repair patch materials from carbon composite structure during a repair operation.

Standard

Sealing Compounds, Quick Repair, Low Temperature Curing Polysulfide, for Aircraft Structures

2011-09-23

CURRENT

AMSS85420A

This specification establishes requirements for two types and classes of a two component, low temperature curing, polysulfide, sealing compound for use as a quick-repair material for aircraft structure.

Standard

Sealing Compound, Polysulfide, Accelerator Required, For Aircraft Structures

2011-09-23

CURRENT

AMSS7124B

This specification covers compounds for sealing aircraft structure against the passage of air, liquids and vapors.

Standard

Aerospace Standard Test Methods for Aerospace Sealants Two-Component Synthetic Rubber Compounds

2009-09-28

HISTORICAL

AS5127/1B

This SAE Aerospace Standard (AS) describes test methods to determine the application and performance properties of two-component sealing compounds. It shall be used in conjunction with AS5127 and the applicable AMS material specifications.

Standard

Adhesion Promoter For Polysulfide Sealing Compounds Nonrestricted Solvent

2004-02-25

HISTORICAL

AMS3100/2A

This specification covers one type of adhesion promoter in the form of a liquid.

Standard

Aerospace Standard Test Methods for Aerospace Sealants Two-Component Synthetic Rubber Compounds

2002-03-29

HISTORICAL

AS5127/1A

This standard describes test methods to determine the application and performance properties of two-component polysulfide or polythioether sealing compounds. It shall be used in conjunction with AS5127.

Standard

Sealing Compound, Polysulfide, Accelerator Required, For Aircraft Structures

2001-08-01

HISTORICAL

AMSS7124A

This specification covers compounds for sealing aircraft structure against the passage of air, liquids and vapors.

Standard

Sealing Compound, Polythioether, for Aircraft Structures, Fuel and High Temperature Resistant, Fast Curing At Ambient and Low Temperatures

2001-07-01

HISTORICAL

AMSS29574

This specification establishes the requirements for two types and three classes of a two component, fast curing at low and ambient temperature, polythioether sealing compound for use in sealing integral fuel tanks and other aircraft structures. Temperature capabilities are identified in 1.2.1.

Standard

Sealing Compounds, Quick Repair, Low Temperature Curing Polysulfide, for Aircraft Structures

2001-06-01

HISTORICAL

AMSS85420

This specification establishes requirements for two types and classes of a two component, low temperature curing, polysulfide, sealing compound for use as a quick-repair material for aircraft structure.

Standard

Sealing Compound, Polysulfide, Accelerator Required, For Aircraft Structures

1999-07-01

HISTORICAL

AMSS7124

This specification covers compounds for sealing aircraft structure against the passage of air, liquids and vapors.

Standard

Sealing of Integral Fuel Tanks

1998-05-01

HISTORICAL

AIR4069A

This SAE Aerospace Information Report (AIR) presents preferred 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 this document discusses the most practical and conservative methods for producing a reliable, sealed system. Design preferences for optimum sealing are not within the scope of this document. Such discussions can be found in the Air Force sponsored handbook, 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 air vehicle.

Standard

SEALING COMPOUND, POLYSULFIDE (T) RUBBER Nonchromated, Corrosion Inhibiting for Intermittent Use to 340 °C (171 °F)

1996-03-01

HISTORICAL

AMS3265

This specification covers a polysulfide (T) rubber sealing compound with nonchromated corrosion inhibitors supplied as a two-component system which cures at room temperature.

Standard

ISOLATION AND CORROSION PROTECTION OF DISSIMILAR MATERIALS

1994-06-01

HISTORICAL

ARP4118

This SAE Aerospace Recommended Practice (ARP) provides methods and guidelines for isolating dissimilar repair patch materials from carbon composite structure during a repair operation.

Standard

SEALING INTEGRAL FUEL TANKS

1990-10-01

HISTORICAL

AIR4069

This Aerospace Information Report (AIR) presents preferred practices for sealing and repairing integral fuel tanks. It addresses several basic fuel tank designs as they are currently found in practice and discusses the most practical and conservative methods for producing a reliable, sealed system. Design preferences for optimum sealing are not within the scope of this document. Such discussions can be found in the Air Force sponsored handbook entitled Aircraft Integral Fuel Tank Design Handbook, AFWAL-TR-87-3078. The basic goal in sealing an integral fuel tank is to produce a system that is leak-free for the long term under the environmental and operational conditions expected.