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Viewing 1 to 30 of 18135
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.
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
AMS6409E
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
2016-12-06
Standard
AMST81915B
This specification prescribes the requirements for Titanium and Titanium-alloy castings produced by the investment casting process.
2016-12-01
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
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.
CURRENT
2016-11-29
Standard
AMS2451/3B
This specification covers the requirements for brush plating of low-hardness, low-stress nickel by electrodeposition.
CURRENT
2016-11-29
Standard
AMS2636A
This specification covers procedures for ultrasonic immersion inspection of premium grade wrought titanium and titanium alloy forgings. Premium grade is a term used to describe titanium alloys used for critical rotating components in turbine engines. For details, see SAE AMS2380, the specification that covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.
CURRENT
2016-11-29
Standard
AMS6487L
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
CURRENT
2016-11-28
Standard
AMS4174E
This specification covers an aluminum alloy in the form of flash welded rings 0.062 to 4.499 inches, incl (1.57 to 114.27 mm incl) in radial thickness, with cross sectional areas up to 32 in2 (206 cm2) (see 8.5).
CURRENT
2016-11-28
Standard
AMS4212L
This specification covers an aluminum alloy in the form of castings.
CURRENT
2016-11-23
Standard
AMS6255F
This specification covers a premium aircraft quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
2016-11-23
Standard
AIR4069C
This SAE Aerospace Information Report (AIR) presents preferred design, assembly, and repair practices for sealing of aircraft integral fuel tanks, including rework of applied fuel tank seals. It addresses engineering designs for integral fuel tanks as they are currently found in practice; and discusses the most practical and conservative methods for producing a reliable, sealed system. Although this AIR presents practices for sealing of integral fuel tanks, the practices presented within this report are practices that are carried throughout sealing that include both pressure and environmental aircraft sealing. Design preferences for optimum sealing are not within the scope of this document. Such discussions can be found in the United States Air Force (USAF) sponsored report, entitled Aircraft Integral Fuel Tank Design Handbook, AFWAL-TR-87-3078.
CURRENT
2016-11-23
Standard
AMS5666J
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, extrusions, flash welded rings, and stock for forging, extruding, or flash welded rings up to 10 inches (254 mm) in diameter or least cross-sectional dimension (see 8.5).
CURRENT
2016-11-22
Standard
AMS5441B
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and flash welded rings 5 inches (127 mm) and under in nominal diameter or least distance between parallel sides and up to 50 in2 (323 cm2) in cross-sectional area, and stock of any size for forging, flash welded rings, or heading (see 8.5).
CURRENT
2016-11-22
Standard
AMS2817G
This specification covers procedures which will provide protection of elastomeric seals and seal assemblies such as O-rings, cap seal assemblies, and other designs from contamination by foreign materials and handling / transportation / storage damage prior to installation and ensure positive identification by part number of each piece until it is installed.
2016-11-21
WIP Standard
AMS4335A
This specification establishes requirements for 2xxx-series and 7xxx- series aluminum alloy forgings of any shape or form from which finished parts are to be made.

These forgings are used typically in the manufacture of high-performance parts when control of short-transverse tensile properties and fracture toughness is required, but usage is not limited to such applications.

CURRENT
2016-11-21
Standard
J430_201611
These specifications cover the mechanical and chemical requirements, and surface discontinuities limits for carbon steel solid rivets used in automotive and other related industries.
CURRENT
2016-11-18
Standard
AMS3613E
This specification covers a polyester resin in the form of a film clad on one or both sides with copper foil.
CURRENT
2016-11-18
Standard
AMS3753C
This specification covers carbon in the form of hollow microspheres.
CURRENT
2016-11-18
Standard
AMS3755/1B
This specification covers one type of silicon dioxide in the form of a white, anhydrous powder with high thickening efficiency.
CURRENT
2016-11-18
Standard
AMS3755D
This specification and its supplementary detail specifications cover silicon dioxide in the form of a white, amorphous powder.
2016-11-18
WIP Standard
AMS4959F
This specification covers a titanium alloy in the form of cold drawn wire.
CURRENT
2016-11-17
Standard
AMS3755/2B
The specification covers one type of silicon dioxide in the form of a white, anhydrous powder with moderate thickening efficiency.
Viewing 1 to 30 of 18135