Search
Advanced Search
of the following are true

Results

Items (207,327)
This SAE Aerospace Recommended Practice (ARP) provides recommendations for: The audit process in general A list of specific areas of attention to be audited Maintaining the test facility in such a manner that it meets audit requirements
EG-1E Gas Turbine Test Facilities and Equipment
This document provides background information, rationale, and data (both physical testing and computer simulations) used in defining the component test methods and similarity criteria described in SAE Aerospace Recommended Practice (ARP) 6330. ARP6330 defines multiple test methods used to assess the effect of seat back mounted IFE monitor changes on blunt trauma to the head and post-impact sharp edge generation. The data generated is based on seat and IFE components installed on type A-T (transport airplane) certified aircraft. While not within the scope of ARP6330, generated test data for the possible future development of surrogate target evaluation methods is also included
Aircraft Seat Committee
This specification covers the specific requirements for aluminum alloy 5086, plate and sheet for applications requiring a weldable moderate strength alloy having comparatively and corrosive resistance
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of cold rolled sheet and strip up to 0.100 inch (2.540 mm), inclusive, in thickness
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of prealloyed powder
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and stock of any size for forging or flash welded rings (see 8.8
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion and heat-resistant steel in the form of thin-wall seamless tubing
AMS F Corrosion and Heat Resistant Alloys Committee
This specification is to prescribe process requirements for production (from raw materials through preparation for shipment, see 8.6) of metal powder feedstock for use in additive manufacturing of aerospace parts. This specification covers requirements for the production of metal powder for use as feedstock in additive manufacturing. Such powders may be pre-alloyed or commercially pure. This specification is not limited to a specific powder production method. It is intended to define those procedures and requirements necessary to achieve required cleanliness and performance of metal powder feedstock to be used in the manufacture of aerospace parts. This specification is intended to be used in conjunction with AMS powder specifications for additive manufacturing
AMS AM Additive Manufacturing Metals
This specification covers steel in the form of laminated sheet
AMS E Carbon and Low Alloy Steels Committee
This specification covers a lead alloy in the form of sheet and extrusions
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings 10 inches (254 mm) and under in nominal diameter or maximum cross-sectional dimension, and forging stock
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a titanium alloy in the form of pre-alloyed powder
AMS AM Additive Manufacturing Metals
This specification establishes maximum permissible limits for elements not normally specified but which may occur in trace amounts in wrought nickel, cobalt, and iron alloy products
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the specific requirements for 2014 aluminum alloy bar, rod, wire and special shapes produced by rolling, drawing or cold finishing
AMS D Nonferrous Alloys Committee
This specification covers one type of a biodegradable, deactant-type deodorizer in the form of an aerosol-packaged liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers vulcanized sheet made of granulated cork uniformly dispersed in a synthetic rubber compound, for use in gaskets where aromatic fuel or oil resistance is required (See 6.2
AMS CE Elastomers Committee
This specification covers a high-strength, corrosion-resistant alloy in the form of bars up to 1.75 inches (44.4 mm) in diameter (see 8.2 and 8.7
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers interior aircraft cabin coatings, which when tested under specified conditions exhibit low heat release and smoke release properties
AMS G8 Aerospace Organic Coatings Committee
Aluminum Alloy Plate 4.3Zn - 3.3Mg - o.6Cu - o.2Mn - 0.17Cr (7o79-T651) Stress-Relief Stretched
AMS D Nonferrous Alloys Committee
This specification covers a low-alloy steel in the form of welding wire
AMS E Carbon and Low Alloy Steels Committee
This specification covers a petroleum-based reference oil
AMS CE Elastomers Committee
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings
AMS E Carbon and Low Alloy Steels Committee
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 AMS2980/1 and AMS2980/2. Unless otherwise specified by the drawing, the order or the inspection schedule, the present specification shall be used in conjunction with the referenced documents
AMS CACRC Commercial Aircraft Composite Repair Committee
This specification has been "Cancelled" by the Aerospace Materials Division, SAE, as of January 1997
AMS CE Elastomers Committee
AMS B Finishes Processes and Fluids Committee
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing produced with cross sectional area of 32 in2 (206 cm2) maximum
AMS D Nonferrous Alloys Committee
No scope available
AMS P17 Polymer Matrix Composites Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of June, 1996
AMS P Polymeric Materials Committee
This specification covers a standard phosphonitrilic fluoroelastomer (FZ) rubber stock in the form of molded test slabs
AMS CE Elastomers Committee
This specification covers a process for removal of aluminide protective coatings from cobalt alloys
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers the procedure for through-hardening and related heat treatments of carbon, low-alloy, and specialty steel parts to produce specified mechanical properties within the capability of each respective steel. Heat treating processes such as induction hardening, flame hardening, carburizing, nitriding, austempering, and martempering are recognized processes but are not covered by this specification
AMS E Carbon and Low Alloy Steels Committee
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
This specification covers an aluminum-lithium alloy in the form of extruded profiles 0.040 to 1.000 inch, incl in thickness (see 8.5
AMS D Nonferrous Alloys Committee
This specification establishes acceptance criteria for discontinuities revealed by magnetic particle inspection of parts made from wrought, ferromagnetic materials
AMS B Finishes Processes and Fluids Committee
This specification establishes the requirements for heat treatment of wrought copper beryllium parts (See 1.2.2 and 8.2.1) by users or by their vendors or subcontractors
AMS D Nonferrous Alloys Committee
This specification covers a carbon steel in the form of wire supplied as coils, spools, or cut lengths (see 8.2
AMS E Carbon and Low Alloy Steels Committee
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, forgings, and forging stock
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an alclad aluminum alloy in the form of sheet and plate
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of welding wire
AMS G Titanium and Refractory Metals Committee
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
Items per page:
1 – 50 of 207327