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Viewing 1 to 30 of 16972
2014-12-17
Standard
AMS3277H
This specification covers polythioether rubber fuel resistant sealing compounds supplied as a two-component system which cures at room temperature.
2014-12-12
Standard
AS83248/2
Scope is unavailable.
2014-12-12
Standard
AS83248/1
Scope is unavailable.
2014-12-12
Standard
AS3075E
SCOPE IS UNAVAILABLE.
2014-12-11
Standard
AMS4111E
This specification covers an aluminum alloy in the form of die forgings, hand forgings, and forging stock.
2014-12-11
Standard
AMS4140K
This specification covers an aluminum alloy in the form of die forgings and forging stock.
2014-12-11
Standard
AMS5629/H1000
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, flash welded rings, and extrusions in the solution and precipitation heat treated (H1000) condition. These products have been used typically for parts requiring corrosion resistance, stress-corrosion resistance, high strength up to 600 °F (316 °C), and good ductility and strength in the transverse direction in large section sizes, but usage is not limited to such applications.
2014-12-11
Standard
AMS5675H
This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire.
2014-12-11
Standard
AMS4783G
This specification covers a cobalt alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of powder in a suitable binder. This filler metal has been used typically for joining cobalt alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications.
2014-12-11
Standard
AMS5544K
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
2014-12-08
WIP Standard
AS12500
Establish minimum requirements for procedures, materials and systems for protecting electronic components and assemblies from adverse environments in commercial and government applications.
2014-12-08
Standard
MA1565C
This SAE Metric Aerospace Standard defines the requirements for corrosion resistant steel helical coil metric series screw thread inserts made from formed wire, the inner surfaces of which, after assembly, provide internal threads of the diameter and pitch specified on the drawing.
2014-12-06
WIP Standard
AS7220A
This procurement specification covers rivets fabricated from an aluminum alloy designated as 1100-H14, strain hardened. Primarily for joining aluminum parts where a low shear strength is adequate.
2014-12-01
Standard
AS5756/4B
SCOPE IS UNAVAILABLE.
2014-12-01
Standard
ARP6265
This document describes a recommended test procedure to assess the burst characteristics of tires used on 14CFR Part 25 or similar transport airplanes.
2014-11-25
Standard
AS1260A
Primarily to provide the aerospace industry with approximate standards for comparing various shaped sections to round bars, in determining the response to hardening characteristics when heat treating low-alloy and marensitic corrosion-resistant steels.
2014-11-25
Standard
ARP1313D
This SAE Aerospace Recommended Practice (ARP) describes procedures for the determination of trace elements listed in AMS2280 for Nickel, Cobalt, and Iron-based high temperature alloys.
2014-11-20
Standard
AS5860B
This SAE Aerospace Standard (AS) covers scarf-cut polytetrafluoroethylene (PTFE) retainers (back-up rings) for use in static glands in accordance with AS5857. They are for use in hydraulic and pneumatic system components as anti-extrusion devices in conjunction with O-rings, packings and other elastomeric seals. Because of the construction of groove dimensions, back-ups specific to rod applications are designated “R” - Rod (Female), back-ups specific to piston applications are designated “P” - Piston (Male). Retainers specified herein have been designed for a temperature range of -65 to 275 °F (-54 to 135 °C) and a nominal operating pressure of 3000 psi (20.7 MPa) for code 09 material and 5000 psi (34.5 MPa) for code 10 material. Material codes are based on AMS3678 material types.
2014-11-18
Standard
AMS4130N
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those materials which may have been widely used previously and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
2014-11-16
WIP Standard
AMSP83461/2B
The purpose of this specification sheet is to set up a standardized part numbering system for O-rings procured to MIL-P-83461 for use in straight thread tube boss fittings.
2014-11-14
Standard
AMS4125L
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those materials which may have been widely used previously and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
2014-11-14
Standard
AMS5934A
This specification covers an extra high toughness, corrosion-resistant steel in the form of bars, wire, forgings, flash welded rings, extrusions 12 inches (305 mm) and under, and stock of any size for forging, flash welded rings, or extrusion.
2014-11-13
Standard
AMS2472G
This specification establishes the requirements for dyed anodic coatings on aluminum alloys.
2014-11-07
Standard
AMSQQA591B
This specification covers aluminum alloy die castings.
2014-11-07
Standard
AMS4025M
This specification covers an aluminum alloy in the form of sheet and plate.
2014-11-07
Standard
AMS3305J
This specification covers a silicone rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. Primarily for parts required to operate or seal from -65 to +205 degrees C (-85 to +401 degrees F). Silicone elastomer is resistant to deterioration by weathering and petroleum-base lubricating oil and remains flexible over the temperature range noted. These products are not normally suitable for use in contact with gasoline or aromtic fuels and low-aniline-point petroleum-base fluids due to excessive swelling of the elastomer.
Viewing 1 to 30 of 16972