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CURRENT
2016-12-07
Standard
J1677_201612
This SAE Standard is intended to establish uniform methods for testing certain types of carbon steel and high strength, low alloy steel tubing as listed in section 2.1.1. The specified test and performance criteria applicable to each variety of tubing are set forth in the respective SAE J Specifications.
CURRENT
2016-12-07
Standard
AMS6304M
This specification covers an aircraft quality, low alloy, heat resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
2016-12-07
Standard
AMS6415U
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2016-12-06
WIP Standard
AMS7489
This document standardizes the knowledge, skills, and abilities inherent of all formally certified Aerospace Coatings Technicians. It shall provide clear guidelines for academic and other accredited organizations to teach a common language and critical core knowledge reflecting aircraft-specific coatings processes for complete aircraft and/or aircraft components.
2016-12-06
WIP Standard
AS31831A
Scope unavailable
2016-12-06
WIP Standard
AS35051A
No scope available.
CURRENT
2016-12-06
Standard
J1939/11_201612
This document defines a physical layer having a robust immunity to EMI and physical properties suitable for harsh environments. CAN controllers are available which support the CAN Flexible Data Rate Frame Format. These controllers, when used on SAE J1939-11 networks, must be restricted to use only the Classical Frame Format compliant to ISO 11898-1:2015. These SAE Recommended Practices are intended for light- and heavy-duty vehicles on- or off-road as well as appropriate stationary applications which use vehicle derived components (e.g., generator sets). Vehicles of interest include but are not limited to: on- and off-highway trucks and their trailers; construction equipment; and agricultural equipment and implements.
CURRENT
2016-12-06
Standard
AMS4909K
This specification covers a titanium alloy in the form of sheet, strip, and plate up to 1.000 inch (25.40 mm) inclusive.
CURRENT
2016-12-06
Standard
AMS4962B
This specification covers a premium grade titanium alloy in the form of investment castings.
CURRENT
2016-12-06
Standard
AMST81915B
This specification prescribes the requirements for Titanium and Titanium-alloy castings produced by the investment casting process.
2016-12-06
WIP Standard
AS31821B
SCOPE IS UNAVAILABLE.
CURRENT
2016-12-06
Standard
J2601_201612
SAE J2601 establishes the protocol and process limits for hydrogen fueling of light duty vehicles. These process limits (including the fuel delivery temperature, the maximum fuel flow rate, the rate of pressure increase and the ending pressure) are affected by factors such as ambient temperature, fuel delivery temperature and initial pressure in the vehicle’s compressed hydrogen storage system. SAE J2601 establishes standard fueling protocols based on either a look-up table approach utilizing a fixed pressure ramp rate, or a formula based approach utilizing a dynamic pressure ramp rate continuously calculated throughout the fill. Both protocols allow for fueling with communications or without communications. The table-based protocol provides a fixed end-of-fill pressure target, whereas the formula-based protocol calculates the end-of-fill pressure target continuously.
CURRENT
2016-12-06
Standard
AMS6409E
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2016-12-02
WIP Standard
AS4726A
This specification establishes the requirements for self-locking nuts, wrenching type (i.e., hexagon, double hexagon, and spline drive), made of a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286. Classification: a. 220 ksi minimum tensile strength at room temperature and b. 850 degrees F maximum test temperature of parts. Primarily for use in aerospace propulsion systems in temperatures up to approximately 850 degrees were nuts are used with bolts capable of developing 220 ksi axial tensile strength at room temperature, and having UNJ thread form.
CURRENT
2016-12-02
Standard
J2911_201612
This SAE Standard provides manufacturers, testing facilities and providers of technician training with a procedure for certifying compliance with the applicable standard. Manufacturers or seller who advertise their products as Certified to an SAE J standard shall follow this procedure. Certification of a product is voluntary; however, this certification process is mandatory for those advertising meeting SAE Standard(s) requirements. Only certifying to this standard allows those claiming compliance to advertise that their product (unit), component, or service technician training meets all requirements of the applicable SAE standard. Certification of compliance to this and the appropriate standard and use of the SAE label on the product shall only be permitted after all the required information has been submitted to SAE International and it has been posted on the SAE web site.
2016-12-01
WIP Standard
AMS3400
This fluid has been used typically to evaluate the ability of elastomeric and other polymeric compounds to conform to designated requirements after immersion in the fluid at a specific temperature and time, as required by an applicable specification, and its use is limited to such applications. This fluid is not intended for operational use in hydraulic systems. Each application should be considered separately.
2016-12-01
WIP Standard
ARP5429A
This SAE Aerospace Recommended Practice (ARP) applies to fatigue testing of landing gear and landing gear components.
CURRENT
2016-12-01
Standard
ARP1821B
This SAE Aerospace Recommended Practice (ARP) includes recommended ground flotation analysis methods for both paved and unpaved airfields with application to both commercial and military aircraft.
CURRENT
2016-12-01
Standard
ARP5369B
These guidelines have been written to provide process information regarding the hot stamp method of marking wire identification directly on aerospace wires and cables. This document is not intended to encourage the use of hot stamp marking or to endorse the related process. This method of marking wire identification may be prohibited on any aerospace vehicle wiring that is required to conform to the provisions of MIL-W-5088L or AS 50881. Methods which do not deform wire or cable insulation, such as Ink Jet, Dot Matrix or UV Laser marking are encouraged as a means of minimizing the possibility of insulation damage, particularly on insulation constructions of less than 0.010 in wall thickness. In recognition that the present use of hot stamp wire marking is widespread and may continue for an extended period, the guidelines provided in this document are intended to provide process control information necessary to minimize the possibility of insulation damage.
2016-12-01
WIP Standard
AMSDTL22499/2B
SCOPE IS UNAVAILABLE.
2016-12-01
WIP Standard
AS81714/10A
Scope not available.
2016-12-01
WIP Standard
AS81714/5A
No scope available.
Viewing 1 to 30 of 43546