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Standard

Aluminum Alloy Tempers

1999-04-01
HISTORICAL
AS1990B
The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from different sources for the benefit of the user.
Standard

ALUMINUM ALLOY TEMPERS

1998-05-01
HISTORICAL
AS1990A
The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from different sources for the benefit of the user.
Standard

Aluminum Alloy Tempers

2003-01-23
HISTORICAL
AS1990C
The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from different sources for the benefit of the user.
Standard

Aluminum Alloy Tempers

1990-01-01
HISTORICAL
AS1990
The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from different sources for the benefit of the user.
Standard

Aluminum Alloy Tempers

2016-01-02
CURRENT
AS1990D
The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from different sources for the benefit of the user.
Standard

Copper-Beryllium Alloy (Copper Alloy Numbers C17500 and C17510), Strip

2016-05-24
CURRENT
AS81021B
This specification covers the requirements for the acquisition of two alloys of copper-beryllium alloy strip, having higher electrical conductivity than copper-beryllium alloy strip normally used (see 6.1). All sizes of strip are covered by this specification.
Standard

Copper-Beryllium Alloy (Copper Alloy Numbers C17500 and C17510), Strip

2002-03-01
HISTORICAL
AS81021
This specification covers the requirements for the acquisition of two alloys of Copper-Beryllium alloy strip, having higher electrical conductivity than Copper-Beryllium alloy strip normally used (see 6.1). All sizes of strip are covered by this specification.
Standard

Copper-Beryllium Alloy (Copper Alloy Numbers C17500 and C17510), Strip

2007-11-21
HISTORICAL
AS81021A
This specification covers the requirements for the acquisition of two alloys of copper-beryllium alloy strip, having higher electrical conductivity than copper-beryllium alloy strip normally used (see 6.1). All sizes of strip are covered by this specification.
Standard

Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of

2013-04-01
WIP
ARP1947C
This document covers the recommended practice for determining the acceptability of the dendrite arm spacing (DAS) of D357-T6 aluminum alloy castings required to have tensile strength not lower than 50,000 psi (345 MPa). To apply this method, at least two coupons used for DAS measurement and tensile testing shall be attached to the casting in locations as defined by the cognizant engineering organization. Areas of the casting which require DAS control must be accessible for surface DAS measurements.
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