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Viewing 1 to 30 of 18167
2017-01-19
WIP Standard
AS7469B
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable, nickel base alloy of the type identified under the Unified Numbering System as UNS N07041 and of 155 ksi tensile strength at room temperature, with maximum test temperature of parts at 1400 °F.
CURRENT
2017-01-19
Standard
AMS5639J
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
2017-01-18
WIP Standard
AIR6190A
This document provides information on provisions for passengers with disabilities on board commercial aircraft. In this context the term "provision of medical oxygen" shall be understood as application of oxygen on board an aircraft not linked to (post) decompression in the sense of Airworthiness Requirements FAR/CS 25 and Operational Regulations of FAR 121/135. Information about available equipment and physiological treatment in clinical practice will be provided in this document. It covers the use of oxygen concentrators according to guidance of FAR Advisory Circular AC120-95.
2017-01-18
WIP Standard
AMS1424N
This foundation specification (AMS1424M) and its associated detail specifications (AMS1424/1 and AMS1424/2) cover a deicing/anti-icing material in the form of a fluid.
CURRENT
2017-01-18
Standard
AMS5618J
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
CURRENT
2017-01-18
Standard
AMS6431P
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2017-01-16
WIP Standard
AMSQQA225/4A
This specification covers the specific requirements for 2014 aluminum alloy bar, rod, wire and special shapes produced by rolling, drawing or cold finishing.
2017-01-12
WIP Standard
AMS2451/14
This specification covers the requirements for brush plating of nickel-tungsten by electrodeposition. This process has been used as a chromium alternative for repair and OEM applications that require exceptionaly hard elcectroplated deposits. It’s typically used in aerospace, automotive and oil and gas to improve hardness and wearability and to repair damaged or worn parts, but usage is not limited to such applications.
2017-01-12
WIP Standard
AIR1412D
This document lists those guidelines recognized as being essential for consideration by the designer who is preparing to select an elastomer as part of an aerospace design.
2017-01-12
WIP Standard
AMS3713E
This specification covers honeycomb core made of polymide paper sheets in a non-hexagonal, flexible cell configuration and supplied in the form of blocks, slices, and ordered shapes. This honeycomb core has been used tyipcally in sandwich structures in single or compound curvature parts requiring high strength and corrosion resistance in the temperature range -55 to +82 degrees C (-67 to +180 degrees F) but usage is not limited to such applications.
CURRENT
2017-01-12
Standard
AMS3415E
This specification covers the requirements for an aluminum brazing flux in granular form.
CURRENT
2017-01-12
Standard
ARP5429A
This SAE Aerospace Recommended Practice (ARP) applies to fatigue testing of landing gear and landing gear components.
CURRENT
2017-01-11
Standard
AMS2821
This specification covers the procurement of granular heat-treating salts suitable for use in the molten state.
2017-01-10
WIP Standard
AMS5047G
This specification covers an aluminum-killed carbon steel in the form of sheet and strip.
2017-01-06
WIP Standard
AMS4575F
This specification covers a corrosion-resistant nickel-copper alloy in the form of copper-furnace-brazed tubing.
CURRENT
2017-01-05
Standard
AMS4291J
This specification covers an aluminum alloy in the form of die castings.
CURRENT
2017-01-05
Standard
AMSDTL22499/2B
SCOPE IS UNAVAILABLE.
CURRENT
2017-01-05
Standard
AMS4121J
This specification covers an aluminum alloy in the form of bars, rods, and wire.
CURRENT
2017-01-05
Standard
AMS4787G
This specification covers a gold-nickel alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, chips, preforms and a viscous mixture (paste) of the powder in a suitable binder.
CURRENT
2017-01-05
Standard
AMS6435G
This specification covers a premium aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
CURRENT
2017-01-04
Standard
AS1303B
This SAE Aerospace Standard (AS) applies to a portable chemical oxygen generator assembly intended for the following uses: a. First aid treatment of aircraft occupants after an emergency descent following a decompression or other emergency condition. b. Use by cabin attendants to maintain their mobility after a decompression.
CURRENT
2017-01-04
Standard
GEIASTD0003A
This document provides an industry standard for Long Term Storage (LTS) of electronic devices by drawing from the best long term storage practices currently known. LTS is defined as any device storage for more than 12 months but typically allows for much longer (years). While intended to address the storage of unpackaged semiconductors and packaged electronic devices, nothing in this standard precludes the storage of other items under the storage levels defined herein. This standard is not intended to address built-in failure mechanisms (e.g., tin whiskers, plating diffusion, and intermetallics) that would take place regardless of storage conditions
CURRENT
2017-01-04
Standard
AMS4544H
This specification covers a corrosion-resistant nickel-copper alloy in the form of sheet, strip, and plate.
CURRENT
2017-01-04
Standard
AMS4675E
This specification covers a corrosion-resistant nickel-copper alloy in the form of bars 0.093 to 4.000 inches (2.35 to 100.00 mm) in diameter or distance between parallel sides, and forgings and forging stock of any size (see 8.5).
CURRENT
2017-01-04
Standard
AS6070/3A
SCOPE IS UNAVAILABLE.
CURRENT
2017-01-04
Standard
AS6070/4A
SCOPE IS UNAVAILABLE.
Viewing 1 to 30 of 18167