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Viewing 1 to 30 of 18298
WIP Standard
2014-04-17
Form: This specification covers an aluminum alloy in the form of an extrusion. Application: This product has been used in aerospace applications requiring a combination of high strength and compressive properties and with good corrosion resistance, but usage is not limited to such applications.
WIP Standard
2014-04-15
1.1 This specification is used to indicate the resistance to distortion of bare and two-side Alclad, flat sheet aluminum that will be chemically milled (often in the manufacture of aircraft skin panels). 1.2 This specification is intended for bare and two-side Alclad aluminum alloy in the T temper, which is the form of flat sheet having a thickness between 0.032 to 0.249 in. (0.8 to 6.3 mm). 1.3 Product having the capability prescribed by this specification is available in limited quantities and tempers because of the special processing required.
WIP Standard
2014-04-14
This specification would cover an aluminum-lithium alloy in the extruded form. These extrusions are typically used for parts where low density, high mechanical properties and good stress-corrosion resistance are desired but is not limited in usage to such applications.
Standard
2014-04-14
Scope is unavailable.
Standard
2014-04-11
This Material Specification defines the requirements of carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures, qualified according to AMS 2980/1 and 2980/2.
WIP Standard
2014-04-11
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate.
WIP Standard
2014-04-11
This specification covers a titanium alloy in the form of extruded bars, tubes, and shapes, and of flash welded rings and stock for flash welded rings.
WIP Standard
2014-04-11
This specification covers powdered metal products consolidated by hot isostatic pressing (HIP) of titanium alloy powder compacts.
WIP Standard
2014-04-11
This specification covers a corrosion and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
WIP Standard
2014-04-10
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.

These products have been used typically for parts, 0.750 inch (19.05 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 50 HRC when properly hardened and tempered and also parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.

WIP Standard
2014-04-10
This specification covers an aircraft-quality, low-alloy steel in the form of seamless tubing.

This tubing has been used typically for thin wall-thickness sections where minimum tensile strength up to 160 ksi (1103 MPa) is required and where parts may be welded during fabrication, but usage is not limited to such applications.

WIP Standard
2014-04-10
This specification covers a free-machining, low-alloy steel in the form of round bars 3.50 inches (88.9 mm) and under in nominal diameter.

These bars have been used typically for parts, such as shafts, axles, pins, fasteners, gears, and screw machine parts, which are normally used at hardness of 30 to 36 HRC and which do not require a high degree of ductility, but usage is not limited to such applications.

WIP Standard
2014-04-10
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
WIP Standard
2014-04-10
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
WIP Standard
2014-04-10
This specification covers a low-alloy steel in the form of welding wire.

This wire has been used typically as filler metal for gas-tungsten-arc and gas-metal-arc welding of low-alloy steels where the joint is capable of being heat treated to a minimum tensile strength up to 180 ksi (1241 MPa), but usage is not limited to such applications.

WIP Standard
2014-04-10
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
WIP Standard
2014-04-10
This specification covers a low-alloy steel in the form of welding wire.

This wire has been used typically for use as filler metal for gas-tungsten-arc and gas-metal-arc welding of low-alloy steels of similar composition where the weld area is required to have strength comparable to that of the parent metal, but usage is not limited to such applications.

WIP Standard
2014-04-10
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.

These products have been used typically for bearing component requiring a through-hardening steel usually with hardness of approximately 60 HRC and section thickness under 0.50 in. (12.7 mm).

WIP Standard
2014-04-10
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
WIP Standard
2014-04-10
A steel grade with improved properties compared to 300M (UTS>300ksi)
Standard
2014-04-09
AMS 2980/2 gives specific information about the qualification program for carbon fiber fabric, epoxy systems and the material combination used for wet lay-up repair of carbon fiber reinforced epoxy structures.
WIP Standard
2014-04-09
SAE Metallic Materials Testing Laboratories, is a technical Subcommittee in SAE’s Aerospace Materials Systems Group with the responsibility to develop and maintain material specifications and other SAE technical reports for Aerospace Metallic Materials Testing Requirements. The Subcommittee works in conjunction with related bodies such as the Performance Review Institute (PRI), and regulatory authorities such as FAA and EASA. The objectives of MTL are to: • Develop Aerospace Specifications (AS) for the control of materials testing specific to aerospace applications. • Provide a forum for the exchange of technical information related to aerospace materials testing. • Further the adaptation of industry sponsored material specifications through coordination with PRI and associated organizations. • Establish a system to ensure aerospace specifications are controlled.
Standard
2014-04-08
AMS 2980/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures.
Standard
2014-04-08
The PS specifies the batch release and delivery requirements for carbon fiber and carbon fabric used for wet lay-up repair purposes.
Standard
2014-04-08
This recommended practice provides general recommendations for welding structural assemblies for aerospace ground support equipment. The recommendations are based on practical engineering experience and reflect design practices and fabricating procedures that have been found to be effective in providing good strength and structural rigidity.
Standard
2014-04-08
This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inches in thickness. These products have been used typically in applications requiring high strength-to-weight ratio and stability up to 550 °F (288 °C), but usage is not limited to such applications. Parts are typically formed in the solution heat treated condition and subsequently precipitation heat treated to final condition.
Standard
2014-04-03
This PS specifies the batch release and delivery requirements for epoxy resin systems (base resin and curing agent) used for wet lay-up repair purposes. This specification relates to qualified epoxy resin systems listed in the associated QPL.
Viewing 1 to 30 of 18298