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Standard

Anodic Treatment of Aluminum and Aluminum Alloys, Brush General Requirements

2021-01-15

WIP

B21AA

Create a base AMS for brush application of anodic treatment of aluminum and aluminum alloys. Multiple slash AMS's to be created for different types.

Standard

Compound, Corrosion-Preventive, Soft Film, Hot Application

2011-10-03

AMS3079B

Standard

Compound, Corrosion-Preventive, Soft Film, Hot Application

2017-09-19

AMS3079C

Standard

COMPOUND, CORROSION-PREVENTIVE Soft Film - Hot Application

1949-02-01

AMS3079

Standard

COMPOUND, CORROSION-PREVENTIVE Soft Film, Hot Application

1951-12-01

AMS3079A

Standard

Anodize Treatment of Titanium and Titanium Alloys pH 12.4 Maximum

2000-10-01

ARP1932A

This recommended practice describes the engineering requirements for producing a voltage-resistant, non-powdery anodic coating on titanium and titanium alloys and the properties of such coatings. Primarily to increase resistance to galvanic and high temperature corrosion and high voltages and to form a receptive base for the application of lubricants and paints on titanium and titanium alloys.

Standard

ANODIZE TREATMENT OF TITANIUM AND TITANIUM ALLOYS pH 12.4 maximum

1994-07-01

ARP1932

This recommended practice describes the engineering requirements for producing a voltage-resistant, non-powdery anodic coating on titanium and titanium alloys and the properties of such coatings.

Standard

TEST METHODS EVALUATION OF NONFLAMMABLE, CHLOROTRIFLUOROETHYLENE BASE HYDRAULIC FLUID

1994-12-01

AS4707

This SAE Aerospace Standard (AS) covers laboratory test methods required to evaluate nonflammable hydraulic fluids. The methods of testing and description of the equipment have been used typically for evaluating chlorotrifluoroethylene (CTFE) base hydraulic fluids.

Standard

INSTRUMENTAL METHODS OF DETERMINING SURFACE CLEANLINESS

1995-05-01

ARP4252

This Aerospace Recommended Practice is intended as a guide toward standard practices for the determination of surface cleanliness that are applicable to field operation. Some of these methods can also be used to determine quality assurance that a surface has been properly prepared and maintained. The instrumental methods are: Wettability, Surface Potential Difference (SPD), Ellipsometry, and Optically Stimulated Electron Emission (OSEE). Each instrument is described with respect to measurement techniques, limitations, and advantages and types of available instruments. Elementary theoretical principles and examples of the use of each instrument are also given.

Standard

Instrumental Methods of Determining Surface Cleanliness

2017-01-04

ARP4252A

This Aerospace Recommended Practice is intended as a guide toward standard practices for the determination of surface cleanliness that are applicable to field operation. Some of these methods can also be used to determine quality assurance that a surface has been properly prepared and maintained. The instrumental methods are: Wettability, Surface Potential Difference (SPD), Ellipsometry, and Optically Stimulated Electron Emission (OSEE). Each instrument is described with respect to measurement techniques, limitations, and advantages and types of available instruments. Elementary theoretical principles and examples of the use of each instrument are also given.

Standard

Instrumental Methods of Determining Surface Cleanliness

2017-09-20

ARP4252B

This Aerospace Recommended Practice is intended as a guide toward standard practices for the determination of surface cleanliness that are applicable to field operation. Some of these methods can also be used to determine quality assurance that a surface has been properly prepared and maintained. The instrumental methods are: Wettability, Surface Potential Difference (SPD), Ellipsometry, and Optically Stimulated Electron Emission (OSEE). Each instrument is described with respect to measurement techniques, limitations, and advantages and types of available instruments. Elementary theoretical principles and examples of the use of each instrument are also given.

Standard

Qualification of Aerospace Personnel Performing Special Processes

2021-07-23

AS7767

Standard

Material Safety Data Sheets

2010-01-05

AMS2825B

This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of xxxx and has been superseded by ANSI Z400.1, Material Safety Data Sheets -Preparation. The requirements of the latest issue of ANSI Z400.1 shall be fulfilled whenever reference is made to the cancelled AMS2825. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by ANSI Z400.1.

Standard

PRESSURE TESTING, GASEOUS MEDIA 40 psi

1994-07-01

AMS2604F

This specification provides requirements and procedures for gas-pressure leak testing of parts.

Standard

Flux, Brazing High Temperature

2002-02-28

AMS3417B

This specification covers a high temperature brazing flux in the form of paste or powder.

Standard

FLUX, BRAZING High Temperature

1997-04-01

AMS3417A

This specification covers a high temperature brazing flux in the form of paste or powder.

Standard

Flux, Brazing, High Temperature

2007-10-31

AMS3417C

This specification covers a high temperature brazing flux in the form of paste or powder.

Standard

FLUX, BRAZING High Temperature

1987-10-01

AMS3417

This specification covers a high temperature brazing flux in the form of paste or powder.

Standard

Peening of Metals

2001-04-01

AMSP81985

This specification covers procedures and requirements for dry peening the surfaces of metals by impingement of metallic shot or glass beads for the purpose of increasing the fatigue strength and resistance to stress corrosion cracking by inducing residual compressive stresses in specified surfaces.

Standard

Peening of Metals

2004-12-15

AMSP81985A

This specification covers procedures and requirements for dry peening the surfaces of metals by impingement of metallic shot or glass beads for the purpose of increasing the fatigue strength and resistance to stress corrosion cracking by inducing residual compressive stresses in specified surfaces.