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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 a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips, and a viscous mixture (paste) of powder in a suitable binder
AMS D Nonferrous Alloys Committee
This specification covers a gold-palladium-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
AMS F Corrosion and Heat Resistant Alloys 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 an aluminum alloy in the form of bars and rods 0.500 inch (12.7 mm) to 8.000 inches (203.2 mm) in nominal diameter or least difference between parallel sides and up to 50 square inches (322.6 square centimeters) in cross-sectional area (see 8.7
AMS D Nonferrous Alloys Committee
This specification covers a cobalt alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips, and a viscous mixture (paste) of powder in a suitable binder
AMS D Nonferrous Alloys Committee
This specification establishes requirements for a temporary protective coating (TPC) intended to protect aluminum surfaces from damage and corrosion. This specification also establishes requirements for an alkaline remover used to strip the specified TPCs
AMS G8 Aerospace Organic Coatings Committee
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and extrusions 7.00 inches (177.8 mm) and under in nominal diameter or least distance between parallel sides, and stock of any size for forging, flash welded rings, or extruding (see 8.8
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a silicone (VMQ) rubber in the form of molded rings. These rings have been used typically as sealing rings for service from -65 to +260 °C (-85 to +500 °F) in contact with air, but usage is not limited to such applications. The cross-section of such rings is usually not over 0.275 inch (6.98 mm) in diameter or thickness
AMS CE Elastomers Committee
This specification covers the requirements for removers used on amine-cured epoxy coating systems (see 6.1
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers an aluminum alloy in the form of sheet from 0.063 to 0.249 inches (1.60 to 6.30 mm) in nominal thickness (see 8.7
AMS D Nonferrous Alloys Committee
This specification covers a fluorosilicone (FVM) rubber sponge in the form of sheet, strip, extrusions, and molded shapes
AMS CE Elastomers Committee
This specification covers a premium aircraft-quality, 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
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion and heat-resistant nickel alloy in the form of plate nominally 2.00 inches (50.8 mm) and under in thickness, inclusive
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers molded or extruded bar, rod, and shapes produced from a polyamide-imide (PAI) polymer filled with 20% graphite and 3% polytetrafluoroethylene (PTFE). This is designated as Grade 2 material per AMS3670
AMS P Polymeric Materials Committee
This specification covers a cobalt alloy in the form of powder
AMS F Corrosion and Heat Resistant Alloys Committee
The intent of this specification is for the procurement of the material listed on the QPL and, therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the quality assurance section of this base specification, AMS6891
AMS P17 Polymer Matrix Composites Committee
This specification covers a corrosion-resistant nickel-copper alloy in the form of wire and ribbon
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers established manufacturing tolerances applicable to titanium and titanium alloy tubing. These tolerances apply to all conditions, unless otherwise noted. The term "excl" is used to apply only to the higher figure of the specified range
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of bars, rods, and wire
AMS D Nonferrous Alloys Committee
This specification covers a silicone (VMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7XXX specification
AMS CE Elastomers Committee
This specification and its supplementary detail specifications cover molded or extruded bar, rod, and shapes made from filled and unfilled polyamide-imide (PAI) polymer
AMS P Polymeric Materials Committee
This specification covers the specific requirements for 7075 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy (7075) core with thin layers of an aluminum alloy (7072) anodic to the core and of approximately equal thickness bonded to both surfaces
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat resistant steel in the form of wire
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a titanium alloy in the form of sheet, strip, and plate up to 4.000 inches (101.60 mm), inclusive, in thickness
AMS G Titanium and Refractory Metals Committee
This specification covers a permanently mastic, non-curing fluorosilicone sealing compound in the form of a paste
AMS G9 Aerospace Sealing Committee
This specification covers a manganese alloy in the form of powder, preforms, and a viscous mixture (paste) of the powder in a suitable binder
AMS F Corrosion and Heat Resistant Alloys Committee
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of low-alloy steel parts to minimum ultimate tensile strengths of 220 ksi (1517 MPa) and higher. Parts are defined in AMS2759. The requirements for heat treatment of alloy Aermet100 are no longer part of this specification and can be found in AMS2759/3. Due to the limited hardenability of these materials, size limits have been added to this specification
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a copper alloy in the form of strip
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of die forgings up to 6 inches in thickness and forging stock of any size ordered to inch/pound units (see 8.8
AMS D Nonferrous Alloys Committee
This specification covers particle size classifications and corresponding particle size distribution requirements for metal powder feedstock conforming to a classification
AMS AM Additive Manufacturing Metals
This specification covers an aluminum alloy in the form of sheet, clad on two sides
AMS D Nonferrous Alloys Committee
This specification covers one type of one-component, air-drying protective coating which cures at room temperature
AMS G9 Aerospace Sealing Committee
This specification covers a corrosion-resistant steel in the form of investment castings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion and heat-resistant steel alloy in the form of pre-alloyed powder
AMS AM Additive Manufacturing Metals
This specification covers a manganese bronze alloy in the form of sand and centrifugal castings
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet and strip up to 0.1874 inch (4.76 mm) thick, inclusive, and plate up to 4.000 inches (101.6 mm) thick, inclusive (see 8.6
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy procured in the form of extruded profiles (shapes) with cross-sections up to 7.75 square inches (5000 mm2
AMS D Nonferrous Alloys Committee
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (see 8.6.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (see 1.3 and 8.5). It covers the following aluminum alloys: 1100, 2004, 2014, 2017, 2024, 2098, 2117, 2124, 2195, 2219, 2224, 3003, 5052, 6013, 6061, 6063, 6066, 6951, 7049, 7050, 7075, 7149, 7178, 7249, and 7475
AMS D Nonferrous 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 for forging and flash welded rings of any size
AMS G Titanium and Refractory Metals Committee
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings up to 8.0 inches (203 mm) in diameter or least distance between parallel sides in the solution heat treated condition (see 8.4), and stock of any size for forging, flash welded rings, or heading (see 8.8
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of plate 0.250 to 3.000 inches (6.35 to 76.20 mm) in nominal thickness (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of plate 1.000 to 6.000 inches (25.40 to 152.40 mm), inclusive, in nominal thickness (see 8.4
AMS D Nonferrous Alloys Committee
This specification covers a premium aircraft-quality steel in the form of bars, forgings, mechanical tubing, and flash-welded rings up to 5.000 inches (127.00 mm), inclusive, in diameter or least distance between parallel sides, and stock of any size for forging or flash-welded rings
AMS E Carbon and Low Alloy Steels Committee
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