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Standard

Test Method for Aerospace Firewall Sealant Flame Penetration

2018-10-15
WIP
AS5127/2C
This SAE Aerospace Standard (AS) describes the procedures for the flammability testing of aircraft firewall sealants in accordance with the requirements of FAR Part 25 Sections 25.865, 25.867, 25.1191, and 25.1193. This test method is intended to determine the capability of sealant materials to control the passage of and effects from fire.
Standard

Test Method for Aerospace Firewall Sealant Flame Penetration

2014-05-06
CURRENT
AS5127/2B
This SAE Aerospace Standard (AS) describes the procedures for the flammability testing of aircraft firewall sealants in accordance with the requirements of FAR Part 25 Sections 25.865, 25.867, 25.1191, and 25.1193. This test method is intended to determine the capability of sealant materials to control the passage of and effects from fire.
Standard

Test Method for Aerospace Firewall Sealant Flame Penetration

2013-03-20
HISTORICAL
AS5127/2A
This SAE Aerospace Standard (AS) describes the procedures for the flammability testing of aircraft firewall sealants in accordance with the requirements of FAR Part 25 Sections 25.865, 25.867, 25.1191, and 25.1193. This test method is intended to determine the capability of sealant materials to control the passage of and effects from fire.
Standard

Swabs and Applicators

2019-06-20
WIP
G919AA
This specification covers both cotton and foam style swabs and applicators for solvent cleaning processes applications.
Standard

Solvents, Cleaning, Cleaning Prior to Application of Sealing Compounds

2014-01-10
CURRENT
AMS3166C
This specification covers cleaning solvents. These solvents are used typically for cleaning aircraft primary and secondary structural surfaces prior to application of adhesion promoters and/or sealing materials, but usage is not limited to such applications.
Standard

Solvents, Cleaning, Cleaning Prior to Application of Sealing Compounds

1994-02-01
HISTORICAL
AMS3166
This specification covers cleaning solvents. These solvents are used typically for cleaning aircraft primary and secondary structural surfaces prior to application of adhesion promoters and/or sealing materials, but usage is not limited to such applications.
Standard

Silicone Rubber Compound Room Temperature Vulcanizing, 50,000 Centipoise Viscosity Short Application Life, Durometer 35-55

1964-01-01
HISTORICAL
AMS3364
This specification covers a silicone rubber in the form of a two-component liquid compound. Primarily for potting or encasement of electrical and electronic components with an elastomeric medium or for production of mechanical rubber parts in low-pressure tooling. Elastomeric properties are retained in operation from -55 to +230 degrees C (-67 to +446 degrees F). For mechanical applications where compression set resistance is important, elevated temperature post-curing of parts may be required.
Standard

Silicone Rubber Compound Room Temperature Vulcanizing, 50,000 Centipoise Viscosity Short Application Life, Durometer 35-55

1965-02-01
HISTORICAL
AMS3364A
This specification covers a silicone rubber in the form of a two-component liquid compound. Primarily for potting or encasement of electrical and electronic components with an elastomeric medium or for production of mechanical rubber parts in low-pressure tooling. Elastomeric properties are retained in operation from -55 to +230 degrees C (-67 to +446 degrees F). For mechanical applications where compression set resistance is important, elevated temperature post-curing of parts may be required.
Standard

Silicone Rubber Compound Room Temperature Vulcanizing, 15,000 Centipoise Viscosity Durometer 35-55

1965-02-01
HISTORICAL
AMS3362A
This specification covers a silicone rubber in the form of a two-component liquid compound. Primarily for potting or encasement of electrical and electronic components with an elastomeric medium or for production of mechanical rubber parts in low-pressure tooling. Elastomeric properties are retained in operation from -55 to +230 degrees C (-67 to +446 degrees F). For mechanical applications where compression set resistance is important, elevated temperature post-curing of parts may be required.
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