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Viewing 1 to 30 of 9259
2014-11-25
Standard
ARP1313D
This SAE Aerospace Recommended Practice (ARP) describes procedures for the determination of trace elements listed in AMS2280 for Nickel, Cobalt, and Iron-based high temperature alloys.
2014-11-25
Standard
AS1260A
Primarily to provide the aerospace industry with approximate standards for comparing various shaped sections to round bars, in determining the response to hardening characteristics when heat treating low-alloy and marensitic corrosion-resistant steels.
2014-11-18
Standard
AMS4130N
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those materials which may have been widely used previously and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
2014-11-14
Standard
AMS4125L
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those materials which may have been widely used previously and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
2014-11-13
Standard
AMS2472G
This specification establishes the requirements for dyed anodic coatings on aluminum alloys.
2014-11-13
Standard
AS6500
This standard is applicable to all phases of the system acquisition life cycle. It is intended for use on all programs with manufacturing content. It requires proven manufacturing management practices with the goal of delivering affordable and capable systems to the extent that it is invoked contractually. The term “organization” as used in this document refers to the company or facility that is implementing this standard, such as when imposed contractually by the customer. NOTE: The term “shall” is used wherever the criterion for conformance with the specific recommendation requires that there be no deviation. The term “should” is used wherever noncompliance with the specific recommendation is permissible.
2014-11-07
Standard
AMSQQA591B
This specification covers aluminum alloy die castings.
2014-11-07
Standard
AMS4025M
This specification covers an aluminum alloy in the form of sheet and plate.
2014-11-06
WIP Standard
J2129
This SAE Information Report lists the method which outside sources will follow when submitting documents for origination or review by the SAE CONAG Council.
2014-11-04
WIP Standard
AMS4479
This specification covers an aluminum alloy in the form of extruded profiles.
2014-11-04
WIP Standard
AMS4480
This specification covers an aluminum alloy in the form of seamless, drawn tubing.
2014-10-30
Standard
AS90387C
Scope is unavailable.
2014-10-30
Standard
AS9116
The aviation, space, and defense industries rely on the development and manufacture of complex products comprised of multiple systems, subsystems, and components each designed by individual designers (design activities) at various levels within the supply chain. Each design activity controls various aspects of the configuration and specifications related to the product. When a change to design information is requested or required, the change has to be evaluated against the impacts to the higher-level system. Proposed changes to design information that the design activity identifies to be minor and have no effect on their product requirements or specifications have the potential to be concurrently implemented and approved, where authorized to do so. Changes that affect customer mandated requirements or specifications shall be approved prior to implementation.
2014-10-30
Standard
ARP5316D
This SAE Aerospace Recommended Practice (ARP) addresses the general requirements for data recording procedures, packaging, and storing of elastomeric seals and seal assemblies which include an elastomeric element prior to the seal being assembled into hardware components. It applies specifically to those elastomeric seals and seal assemblies packaged shortly after manufacture. The storage period prior to installation of the elastomeric seals and seal assemblies into hardware components is commonly referred to as shelf life. The information contained in this ARP is intended to be utilized by those organizations who do not have specific requirements or recommendations already in place for the control of elastomeric seals and seal assemblies. This ARP can be specified in control, storage, and procurement documents.
2014-10-28
WIP Standard
AMS4366
This specification would cover an aluminum-lithium alloy in the extruded profiles form. These extrusions are typically used for parts where low density, high mechanical properties and good dimensional stability during the machining process are desired but is not limited in usage to such applications.
2014-10-28
WIP Standard
AMS4353
This specification would cover an aluminum-lithium alloy in the extruded form. These extrusions are typically used for parts where low density, high mechanical properties and good stress-corrosion resistance are desired but is not limited in usage to such applications.
2014-10-28
Standard
AMS4900P
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate.
2014-10-27
Standard
AMS4937D
This specification covers a titanium alloy in the form of extruded bars, tubes, and shapes, and of flash welded rings and stock for flash welded rings.
2014-10-27
Standard
AMS4918N
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm), inclusive.
2014-10-24
WIP Standard
GAD14AC
This is a general agreement ballot to define the statistical procedure for determination of specification property minima for small (30) data sample sizes.
2014-10-23
WIP Standard
AMS4863
This new specification covers a copper-nickel-tin alloy in the form of investment castings. These castings are for wear-resistnat, anti-corrosion and high strength intricate parts cast to approximate final dimensions for use in bearings, bushings and fluid conveyance parts, but usage is not limited to such applications.
2014-10-22
WIP Standard
AIR1351J

This SAE Aerospace Information Report (AIR) covers the general requirements for and the listing of manufacturers identification that appear on electrical/electronic wiring devices and accessories as required by individual product specifications. Supplier markings from previous submitted listings are maintained for component traceability.

2014-10-21
WIP Standard
GA-F14AC
This general agreement proposes standard wording for the condition paragraph of bar and wire specifications under the cognizance of Committee F
2014-10-21
Standard
J2417_201410
This SAE Standard provides a uniform method to calculate the lift capacity of knuckle-boom log loaders and certain forestry equipment. It establishes definitions and specifies machine conditions for calculations. This document applies to knuckle-boom log loaders as defined in ISO 6814 and ISO 17591 and certain forestry equipment defined in ISO 6814 that have a rotating upper-structure such as feller bunchers, forwarders, harvesters, and behind the cab or rear-mounted knuckle-boom log loaders not having their own power supply. It does not apply to harvesters that are incapable of lifting a tree or log completely off the ground. This document applies to those machines that are crawler, rubber-tired, and pedestal or stationary mounted.
2014-10-17
WIP Standard
AMS2771F
This specification covers the engineering requirements for heat treatment of aluminum alloy castings and for parts machined from castings.
2014-10-17
WIP Standard
AMS4236D
This specification covers an aluminum alloy in the form of sand, investment, permanent mold, and composite mold castings.
2014-10-12
WIP Standard
AMS5772E
This specification covers a corrosion and heat resistant cobalt alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.

These products have been used typically for parts requiring high strength up to 1800 degrees F (982 degrees C) and oxidation resistance up to 2000 degrees F (1093 degrees C), but usage is not limited to such applications.

2014-10-09
Standard
ARP4925B
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a commercial transport rotorcraft hydraulic system, including the applicable airworthiness regulations that affect the hydraulic system. This ARP also provides information and guidelines on the many factors that arise in the design process to provide cost effectiveness, reliability, maintainability and accepted design and installation practices.
2014-10-08
WIP Standard
GAD14AB
This is a General Agreement for Committee D, and if adopted it will rescind the actions implemented by GA D12AA.
Viewing 1 to 30 of 9259