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Viewing 1 to 15 of 15
HISTORICAL
1995-05-01
Standard
AIR4279
An analysis was made of the effects of various surface conditions on the heat up time of steel bars which are heated in atmosphere furnaces to the temperature range used for steel hardening or normalizing. The purpose was to examine whether a standard heating time for a given section thickness is acceptable.
CURRENT
2012-05-09
Standard
AIR4279A
An analysis was made of the effects of various surface conditions on the heat up time of steel bars which are heated in atmosphere furnaces to the temperature range used for steel hardening or normalizing. The purpose was to examine whether a standard heating time for a given section thickness is acceptable.
HISTORICAL
1996-09-01
Standard
AMS2431/8
The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS 2431.
2016-04-20
WIP Standard
AMEC-16AA
This ARP addresses the general procedure for the best practices for minimizing uncertainty when calibrating thermal conductivity and cold cathode vacuum gauges, which includes the vacuum sensor(s) and accompanying electronics necessary for a pressure measurement to be made. It also includes the best practices for an in process verification where limitations make it impossible to follow the best practices for minimizing uncertainty.
HISTORICAL
1999-08-01
Standard
AIR5065
Performed tensile and fatigue tests on bolts to determine if cutting of materials flow lines at the bolt underhead would degrade bolt integrity. Five different alloys used in aerospace industry fatigue critical applications were employed to fabricate 5/16 to 1/2 inch diameter bolts. These bolts were machined from bar stock producing fully cut material flow lines under their heads. Tensile testing with and without underhead washers was performed along with industry standard fatigue testing.
CURRENT
2012-05-09
Standard
AIR5065A
Performed tensile and fatigue tests on bolts to determine if cutting of materials flow lines at the bolt underhead would degrade bolt integrity. Five different alloys used in aerospace industry fatigue critical applications were employed to fabricate 5/16 to 1/2 inch diameter bolts. These bolts were machined from bar stock producing fully cut material flow lines under their heads. Tensile testing with and without underhead washers was performed along with industry standard fatigue testing.
2014-09-03
WIP Standard
AMEC14AC
This appendix establishes the procedures, guidelines and requirements for qualification and quenching of parts produced from the alloys listed in AMS2759/2, Table 2 using inert pressure gas in vacuum furnaces.
HISTORICAL
1993-04-01
Standard
AIR4498
The objective of this program is to compare the properties of aus-bay quenched 300M steel with the properties of 300M steel oil quenched in the conventional manner.
CURRENT
2012-05-09
Standard
AIR4498A
The objective of this program is to compare the properties of aus-bay quenched 300M steel with the properties of 300M steel oil quenched in the conventional manner.
CURRENT
2008-07-30
Standard
AS7117A
This Aerospace Standard (AS) establishes the requirements for suppliers of Shot Peening Services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). NADCAP accreditation is granted in accordance with SAE AS7003 after demonstration of compliance with the requirements herein. The requirements may be supplemented by additional requirements specified by the NADCAP Nonconventional Machining and Surface Enhancement (NMSE) Task Group. Using the corresponding Audit Criteria (PRI AC7117) will ensure that accredited Shot Peening suppliers meet all of the requirements in this standard and all applicable supplementary standards. The purpose of this audit program is to assess a supplier's ability to consistently provide a product or service that conforms to the technical specifications and customer requirements.
HISTORICAL
2002-06-25
Standard
AS7117
This Aerospace Standard (AS) establishes the requirements for suppliers of Shot Peening Services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). NADCAP accreditation is granted in accordance with SAE AS7003 after demonstration of compliance with the requirements herein. The requirements may be supplemented by additional requirements specified by the NADCAP Nonconventional Machining and Surface Enhancement (NMSE) Task Group. Using the corresponding Audit Criteria (PRI AC7117) will ensure that accredited Shot Peening suppliers meet all of the requirements in this standard and all applicable supplementary standards. The purpose of this audit program is to assess a supplier's ability to consistently provide a product or service that conforms to the technical specifications and customer requirements.
2014-01-31
WIP Standard
AS6293
This SAE Aerospace Standard (AS) defines and clarifies terms used in SAE Aerospace Metals Division materials and process specifications, standards and recommended practices. Mandatory definitions are shown in bold, italic text. A definition may have additional clarifying information in standard text. The terms defined or clarified in this ARP are not intended to supersede those terms for which definition or clarification is already provided in existing specifications.
2017-10-09
WIP Standard
TEMPBALAMS2801
Ballot of AMS2801 to AMEC members only.
2017-08-23
WIP Standard
TEMPBALAMS2769
This is a temporary project for the purposes of balloting AMS2769 to AMEC only.
HISTORICAL
1993-07-01
Standard
AMS2430L
This specification covers the engineering requirements for peening surfaces of parts by impingement of metallic shot, glass beads, and ceramic shot. To induce residual compressive stress in surface layers of parts, thereby increasing fatigue strength and resistance to stress corrosion cracking.
Viewing 1 to 15 of 15

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