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Viewing 151 to 180 of 20352
CURRENT
2017-06-07
Standard
J811_201706
This SAE Information Report covers applications of mechanical prestressing, improving fatigue resistance, theory of surface rolling for fatigue improvement, calculations for the surface rolling process, tooling for surface rolling, control and inspection, effect of surface rolling on properties other than fatigue, and other methods for mechanical prestressing.
CURRENT
2017-06-07
Standard
AS7109/1B
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/1. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7109/1. Cancelled specifications are available from SAE.
2017-06-07
WIP Standard
AS8010D
This document defines the minimum degree of purity and maximum levels of certain deleterious impurities allowable for aviator's breathing oxygen at the point of manufacture or generation. It covers gaseous, liquid, and chemically generated oxygen, and oxygen supplied by in situ concentration and in situ electrolysis. Different limits are established for oxygen from different sources, in recognition of differences in the ways the oxygen is stored, dispensed, and utilized, taking into account the safety of the user. These limits are not intended to specifically reflect upon the relative capabilities or merits of various technologies. Procurement documents may specify more stringent limits, where required for specific applications. Medical oxygen is not covered by this standard. In the United States, medical oxygen is a prescription drug.
CURRENT
2017-06-07
Standard
AS7109/2B
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7109/2. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7109/2. Cancelled specifications are available from SAE.
CURRENT
2017-06-07
Standard
J948_201706
These methods of test are applicable for determining the resistance to snagging and abrasion of automotive bodycloth, vinyl, and leather.
2017-06-06
WIP Standard
GA-E17AB
General Agreement to give guidance on utility of previous revision material in stock.
CURRENT
2017-06-05
Standard
AMS4966R
This specification covers a titanium alloy in the form of forgings and forging stock. These forgings have been used typically for parts requiring strength up to 800 °F (427 °C) and that may be welded during fabrication, but usage is not limited to such applications.
CURRENT
2017-06-05
Standard
AIR4938B
This is a general curriculum that has been developed to identify the minimum knowledge and skill requirements of a composite and/or metal bond repair technician/specialist. This revision changes the document from an all-inclusive curriculum into a modular set of curricula. Teaching levels have been assigned to the curriculum to define the knowledge, skills and abilities graduates will need to make composite repairs. Minimum hours of instruction have been provided to ensure adequate coverage of all subject matter - lecture and laboratory. These minimums may be exceeded, and may include an increase in the total number of training hours and/or increases in the teaching levels.
CURRENT
2017-06-05
Standard
AMS5802E
This specification covers a corrosion and heat-resistant iron-nickel alloy in the form of welding wire.
CURRENT
2017-06-05
Standard
AMS7445E
This specification covers balls made of high-carbon corrosion-resistant steel of three carbon ranges.

These products have been used typically for bearing balls, but usage is not limited to such applications.

CURRENT
2017-06-05
Standard
AS14227D
SCOPE IS UNAVAILABLE.
CURRENT
2017-06-05
Standard
AS5620B
This SAE Aerospace Standard (AS) shall be used in conjunction with AMS 4946 to provide requirements for qualification testing and for Qualified Products Listing (QPL) and Qualified Manufacturer Listing (QML) for Ti-3Al-2.5V cold worked and stress relieved hydraulic system tubing. The basic tubing shall comply with the requirements of AMS 4946.
CURRENT
2017-06-01
Standard
AS20218B
SCOPE IS UNAVAILABLE.
CURRENT
2017-06-01
Standard
AMS7510/2C
This specification covers one type of samarium-cobalt permanent magnets.
CURRENT
2017-06-01
Standard
AS1005H
SCOPE IS UNAVAILABLE.
CURRENT
2017-06-01
Standard
AMS5357D
This specification covers a corrosion-resistant steel in the form of investment castings.
CURRENT
2017-06-01
Standard
AMS1548B
This specification covers a solvent-emulsion cleaner in the form of a solvent-base liquid concentrate.
CURRENT
2017-05-31
Standard
AMS7510C
This specification and its supplementary detail specifications cover commonly-available rare-earth/cobalt permanent magnets produced by powder metallurgy.
CURRENT
2017-05-30
Standard
AMS4021H
This specification covers an alclad aluminum alloy in the form of sheet and plate.
2017-05-30
WIP Standard
AMS4467B

This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T861 temper.

CURRENT
2017-05-30
Standard
AMS4416B
This specification covers an aluminum-lithium alloy in the form of extruded profiles 0.040 to 1.000 inch, incl in thickness (see 8.5).
CURRENT
2017-05-30
Standard
AMS4490K
This specification covers a magnesium alloy in the form of die castings.
2017-05-30
WIP Standard
AMS4478A
This specification covers an aluminum alloy in the form of Alclad sheet and plate supplied in the –T81/-T851 temper. These products have been used typically for high strength parts requiring higher yield strength than is afforded by naturally aged tempers of this alloy and maximum corrosion resistance and whose fabrication does not involve welding, but usage is not limited to such applications.
CURRENT
2017-05-30
Standard
AMS4009C
This specification covers an aluminum alloy in the form of foil.
2017-05-26
WIP Standard
ARP4977A
This SAE Aerospace Recommended Practice (ARP) describes standard methods for drying commercial aircraft composite structures prior to repair and gives general guidelines on use and applicability. It addresses the removal of liquids that have collected inside the structures through open damage, microcracks, or porosity and the removal of absorbed moisture from the composite material. The methods described in this document shall only be used when specified in an approved repair document or with the agreement of the original equipment manufacturer (OEM) or regulatory authority. If this document is used for the drying of materials other than thermosetting composite materials, the fitness for this purpose must be determined by the user. The purpose of this document is to provide a set of standard drying methods that may be referenced in repair documents produced by airlines or airframe and engine manufacturers.
CURRENT
2017-05-25
Standard
AMS4254C
This specification covers aluminum alloy sheet laminated with one or more layers of unidirectional aramid fiber/epoxy prepreg. The outer layers are always aluminum alloy.
CURRENT
2017-05-25
Standard
AMS4258B
This specification covers an aluminum alloy in the form of sheet laminated with two or more layers of unidirectional aramid fiber/epoxy prepreg.
CURRENT
2017-05-25
Standard
AMS4425D
This specification covers a magnesium alloy in the form of sand castings.
CURRENT
2017-05-25
Standard
AMS6529D
This specification covers a special aircraft-quality, low-alloy steel in the form of bars.
CURRENT
2017-05-25
Standard
AMS4148F
This specification covers an aluminum alloy in the form of die forgings and forging stock.
Viewing 151 to 180 of 20352