Search Results

Standard

Test Method for Aerospace Firewall Sealant Flame Penetration

2000-09-01

HISTORICAL

AS5127/2

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

Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant

2010-08-18

HISTORICAL

AMS3255A

This specification establishes the requirements for an expanded polytetrafluoroethylene (EPTFE) in the form of sealing tape, gaskets, or sheets requiring no mixing or curing.

Standard

Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant

2017-07-17

CURRENT

AMS3255B

This specification establishes the requirements for an expanded polytetrafluoroethylene (EPTFE) in the form of sealing tape, gaskets, or sheets requiring no mixing or curing.

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 Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 400 °F (204 °C)

2004-10-18

HISTORICAL

AMS3277C

This specification covers polythioether rubber fuel resistant sealing compounds supplied as a two-component system which cures at room temperature.

Standard

Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 400 °F (204 °C)

2007-07-19

HISTORICAL

AMS3277D

This specification covers polythioether rubber fuel resistant sealing compounds supplied as a two-component system which cures at room temperature.

Standard

Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C)

2010-08-18

HISTORICAL

AMS3277E

This specification covers polythioether rubber fuel resistant sealing compounds supplied as a two-component system which cures at room temperature.

Standard

Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C)

2010-12-29

HISTORICAL

AMS3277F

This specification covers polythioether rubber fuel resistant sealing compounds supplied as a two-component system which cures at room temperature.

Standard

Putty, General Purpose, Non-Hardening, Corrosion-Inhibiting

2022-09-08

CURRENT

AMS1321

This specification covers a general purpose, non-curing, corrosion-inhibiting putty compounds with non-hexavalent chromium corrosion inhibitors.

Standard

Methods for Testing Aerospace Sealants

2002-03-29

HISTORICAL

AS5127A

This standard describes the accepted methods used for testing aerospace sealants for qualification and for quality conformance or acceptance testing.

Standard

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

2020-03-18

CURRENT

AS5127/1D

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

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

2018-11-14

CURRENT

AS5127C

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.

Standard

Aerodynamic Smoothing Compound, Flexible −55° to +130°C (−65° to +270°F)

2012-01-17

CURRENT

AMS3694B

This specification covers a two-component air-curing resin-baue material in the form of a paste or putty, suitable for application by spatula or putty knife.

Standard

Aerodynamic Fairing Compound −55° to +85°C (−65° to +185°F)

2012-01-17

CURRENT

AMS3696C

This specification covers a two-component air-curing, aluminum-powder-filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife.

Standard

Aerodynamic Fairing Compound −55° to +150°C (−65° to +300°F)

2012-01-17

CURRENT

AMS3697C

This specification covers a two-component air-curing, aluminum-powder-filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife.

Standard

AERODYNAMIC SMOOTHING COMPOUND, FLEXIBLE -55° to +130°C (-65° to +270°F)

2004-02-25

HISTORICAL

AMS3694A

This specification covers a two-component air-curing resin-baue material in the form of a paste or putty, suitable for application by spatula or putty knife.

Standard

AERODYNAMIC SMOOTHING COMPOUND, FLEXIBLE -55° to +130°C (-65° to +270°F)

1983-07-01

HISTORICAL

AMS3694

This specification covers a two-component air-curing resin-base material in the form of a paste or putty, suitable for application by spatula or putty knife.

Standard

AERODYNAMIC FAIRING COMPOUND −55° to +85° C −67° to +185° F)

1974-03-01

HISTORICAL

AMS3696

This specification covers a two-component, air-curing, aluminum-powder-filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife.

Standard

AERODYNAMIC FAIRING COMPOUND −55° to +150° C (−67° to +302° F)

1974-03-01

HISTORICAL

AMS3697

This specification covers a two-component, air-curing, aluminum-powder-filled, epoxy- resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife.

Standard

AERODYNAMIC FAIRING COMPOUND -55° to +85°C (-65° to +185°F)

2004-02-25

HISTORICAL

AMS3696B

This specification covers a two-component air-curing, aluminum-powder-filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife.