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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 an aluminum alloy in the form of rolled or forged rings up to 8 inches (203 mm), inclusive, in nominal thickness at the time of heat treatment, and having an OD to wall thickness ratio of 10 or greater (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aluminum alloy in the form of hand forgings up to 8 inches, incl (203 mm, incl) in nominal thickness, and rolled rings up to 3.5 inches, incl (89 mm, incl) in nominal thickness (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers a dilute aluminum/TiB2 metal matrix composite in the form of sand castings
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of bars and forgings up through 3.000 inches (76.20 mm), inclusive, in diameter or least distance between parallel sides with a maximum cross-sectional area of 10 in2 (64.5 cm2), and forging stock of any size (see 8.7
AMS G Titanium and Refractory Metals Committee
This specification covers a discontinuously reinforced aluminum alloy (DRA) made by mechanical alloying 2124A aluminum powder and SiC particulate. It is produced in the form of extruded bar, rod, wire and shapes with cross section inclusive of 1 inch (25.4 mm) diameter or less
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness (see 8.6
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers two methods for determining the percentage of delta ferrite in steels and other iron alloys. When applicable, this specification will be invoked by the material specification
AMS F Corrosion and Heat Resistant Alloys Committee
This specification establishes the requirements for chemical-film (conversion) coatings on aluminum alloys
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of alclad sheet 0.040 to 0.187 inch (1.02 to 4.75 mm) inclusive in nominal thickness (see 8.6
AMS D Nonferrous Alloys Committee
This specification establishes requirements for steel forgings of any shape or form from which finished parts are to be made (See 8.2, 8.3, & 8.4). This specification covers steel forgings suitable for use in the construction of aircraft/aerospace equipment
AMS E Carbon and Low Alloy Steels Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996
AMS P Polymeric Materials Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of June 1996
AMS P Polymeric Materials Committee
This specification covers the engineering requirements for selective (brush) electrodeposition of nickel and the properties of the deposit. This process has been used typically to provide moderate corrosion and oxidation resistance and dimensional build-up and restoration of parts which may operate in service up to 700 degrees F (371 degrees C), where low tensile stress in the deposit is required to avoid marked reduction of fatigue strength, but usage is not limited to such applications
AMS B Finishes Processes and Fluids Committee
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of May, 1990
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion and heat resistant steel in the form of covered welding electrodes
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers procedures for identifying wrought products of aluminum and magnesium alloys
AMS D Nonferrous Alloys Committee
To establish the issue of specifications, standards, and recommended practices published by standardizing agencies other than divisions and committees of the Aerospace Council of SAE approved for use in determining conformance to requirements of Aerospace Material Specifications (AMS) and other specifications in which this specification is referenced
AMS B Finishes Processes and Fluids Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
AMS P Polymeric Materials Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
AMS P Polymeric Materials Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. Primarily for parts, such as turbine blades, bolts, and fittings, requiring high strength up to 1600 degrees F (870 degrees Centigrade) and oxidation resistance up to 1800 degrees F (980 degrees C). This specification has been declared "Noncurrent" by the Aerospace materials Division, SAE, as of October 16, 1987. It is recommended, therefore, that this specification not be specified for new designs
AMS F Corrosion and Heat Resistant Alloys Committee
This specification is declared "CANCELLED" by the Aerospace Materials Division, SAE, as of 1-1-82. By this action, subject specification number and title will be deleted from the active specification index of Aerospace Material Specifications. This fabric style is no longer manufactured. See the latest issue of AMS 3824 for other glass cloth styles
AMS P Polymeric Materials Committee
This specification was declared "NONCURRENT"^by the Aerospace Materials Division, SAE, as of 2-1-56. It was recommended that this specification not be specified for new designs. This cover sheet should be attached to the initial issue of the subject specification. This specification is declared J/CANCELLED" by the Aerospace Materials Division, SAE, as of 1-1-82. By this acfflWP^Wfft^c^^pecification number and title will be deleted from the active specification index of Aerospace Material Specifications. This fabric style is no longer manufactured. See the latest issue of AMS 3824 for other glass cloth styles
AMS P Polymeric Materials Committee
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
AMS F Corrosion and Heat Resistant Alloys Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
AMS P Polymeric Materials Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of September 1996
AMS CE Elastomers Committee
This specification has been 'Cancelled' by the Aerospace Materials Division, SAE, as of September 1996
AMS D Nonferrous Alloys Committee
This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system
AMS G9 Aerospace Sealing Committee
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing hose with textile reinforcement
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers the specific requirements for seamless tube drawn from aluminum alloy 5086
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of extruded profiles (shapes) 0.063 to 0.375 inch (1.6 to 10 mm), inclusive, in nominal thickness (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers phosphonitrilic fluoroelastomer (FZ) in the form of molded rings. Primarily for use in aircraft fuel systems operating from -55 to +150 degrees C (-67 to +302 degrees F
AMS CE Elastomers Committee
The purpose of this document is to provide minimum requirements for weld filler materials, workmanship, inspection and record requirements for fusion welding of alloys applicable to aircraft, missiles, other aerospace equipment, their parts and accessories
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion and heat resistant steel in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
This standard establishes the procedure for qualification of welders and welding operators engaged in the welding of aircraft, missiles, other aerospace equipment, and their parts and accessories by fusion welding processes. This standard is applicable to aircraft, missile, and aerospace ground support equipment or other welding, when included in the contracting documents or when invoked in the absence of a specified welder qualification document
AMS B Finishes Processes and Fluids Committee
This specification covers a magnesium alloy in the form of sand castings. Primarily for parts operating in service in the range 300 degrees - 500 degrees F (150 degrees - 260 degrees C
AMS D Nonferrous Alloys Committee
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996. Alloy: LA141A UNS Number: M14141
AMS D Nonferrous Alloys Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of August, 1992
AMS G Titanium and Refractory Metals Committee
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