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2017-06-23
WIP Standard
D17AB
This revises the Identification section of the General Agreement on Marking.
CURRENT
2017-06-22
Standard
AMS5568H
This specification covers a corrosion and heat resistant steel in the form of welded tubing.
2017-06-22
WIP Standard
AMS2451/4D
This specification establishes the requirements for brush plating of cadmium by electrodeposition.
2017-06-22
WIP Standard
AMS2451/3C
This specification covers the requirements for brush plating of low-hardness, low-stress nickel by electrodeposition.
CURRENT
2017-06-22
Standard
AMS6512H
This specification covers a premium aircraft-quality, maraging alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings up through 10.000 inches (254.00 mm) inclusive in diameter or least distance between parallel sides and stock for forging or flash welded rings.
CURRENT
2017-06-21
Standard
AMS4443H
This specification covers a magnesium alloy in the form of sand castings.
CURRENT
2017-06-21
Standard
AMS2249H
This specification defines limits of variation for determining acceptability of the composition of cast or wrought titanium and titanium alloy parts and material acquired from a producer.
CURRENT
2017-06-21
Standard
AS43021AR-3
No Scope available.
CURRENT
2017-06-21
Standard
AS43021-3
No Scope available.
CURRENT
2017-06-20
Standard
AIR4844C
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures. The purpose of this AIR is to provide terminology that should be used when developing CACRC repair documents or repair documents produced by airlines or airframe and engine manufacturers. It is intended to develop this AIR into an AS.
CURRENT
2017-06-20
Standard
AMS4315A
This specification covers an aluminum alloy in the form of sheet and plate up to 2.000 inch (54.80 mm) inclusive, in thickness (see 8.5).
CURRENT
2017-06-19
Standard
AMS6514J
This specification covers a premium aircraft-quality steel in the form of bars, forgings, mechanical tubing, flash welded rings up through 10.000 inches (254.00 mm) inclusive in diameter or least distance between parallel sides, and stock for forging or flash welded rings.
CURRENT
2017-06-19
Standard
AS7112/3A
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/3. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7112/3. Cancelled specifications are available from SAE.
CURRENT
2017-06-16
Standard
AMS4200C
This specification covers an aluminum alloy in the form of plate.
CURRENT
2017-06-16
Standard
AMS2380G
This specification covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.
CURRENT
2017-06-16
Standard
AMS4300D
This specification covers boron filaments and 6061-0 aluminum alloy foil laminated and bonded into a composite sheet.
CURRENT
2017-06-16
Standard
ARP584D
This SAE Aerospace Recommended Practice (ARP) addresses the design, installation, and testing of coiled tube assemblies ranging from 1/4 inch (6.3 mm) to 1.0 inch (25 mm) diameter using CRES tubing per AMS-T-6845, unless otherwise approved by the Procuring Activity. This ARP specifically details three different configurations of coiled tubing. These configurations should be compatible with pressure levels up to 3000 psi (20.7 MPa) upon the completion of the analysis for the actual stress and life requirement of the intended application. However, formal qualification tests are recommended to verify the satisfactory installation, clamping, and the life of each unique design. NOTE: Refer to ARP4146 for information on design of coiled tube assemblies using Titanium tubing.
CURRENT
2017-06-15
Standard
AMS4046G
This specification covers an aluminum alloy in the form of sheet and plate clad on one side.
CURRENT
2017-06-15
Standard
AMS4084E
This specification covers an aluminum alloy in the form of sheet.
2017-06-15
WIP Standard
AMS2428
This specification covers an electrodeposited nanocrystalline cobalt-phosphorus alloy on metal surfaces. It is generally applied to steel alloys but may be applied to other metals such as, but not limited to, aluminum, copper, stainless steel, nickel, cobalt and their alloys. Nanocrystalline Cobalt-Phosphorus Electroplating as an alternative to hard chrome electroplating.
2017-06-15
WIP Standard
AMS6407K
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
2017-06-13
Standard
AMS5707N
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, 3.25 inches (82.6 mm) and under and stock of any size for forging and for flash welded rings. (see 8.5).
CURRENT
2017-06-13
Standard
AMSA21180C
This specification covers the requirements for six alloy compositions, four inspection classes, four radiographic quality grades and six classes of mechanical properties of high strength aluminum-alloy castings.
CURRENT
2017-06-13
Standard
AMS5826E
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
2017-06-13
WIP Standard
B17AD
Specification to cover the technical requirements for a high density ceramic peening media.
CURRENT
2017-06-09
Standard
AMS4352J
This specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles up to 40 in2 (258 cm2) in cross-sectional area (solids) and up to 8.5 inches (216 mm) OD by 1.188 inches (30.18 mm) wall thickness (tubing) (see 8.4).
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.
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.
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