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This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
This SAE Recommend Practice establishes for passenger cars, light trucks, and multipurpose vehicles with GVW of 4500 kg (10000 pounds) or less, as defined by the EPA, and M1 category vehicles, as defined by the European Commission:
Interior Climate Control Vehicle OEM Committee
This specification covers a low-alloy steel in the form of sheet, strip, and plate 4.00 inches (101.6 mm) and under in thickness.
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aluminum alloy in the form of sheet from 0.063 to 0.249 inch (1.60 to 6.30 mm) in nominal thickness (see 8.6).
AMS D Nonferrous Alloys Committee
This SAE Aerospace Recommended Practice (ARP) provides the user with standardized guidelines for the measurement of effective intensity of short pulse width strobe anticollision lights for aircraft in the laboratory, in maintenance facilities, and in the field. A common source of traceability for calibration of the measurement systems, compensation for known causes of variation in light output such as the use of colored lenses, and recommendations which minimize sources of errors and uncertainties are included in this document. Estimates of uncertainty and error sources for each class of measurement are discussed.
A-20B Exterior Lighting Committee
This specification covers a magnesium alloy in the form of investment castings (see 8.6).
AMS D Nonferrous Alloys Committee
This procedure describes a method of measuring the resistance to wet color transfer of materials such as textiles, leather, and composites.
Textile and Flexible Plastics Committee
This document provides a comprehensive compilation of currently available practices, standards, regulations, and guidance material that have been considered relevant for developing an electrified propulsion system (independently or as part of an aircraft) and that may also help the applicants in the process of building their own certification approach with their Authority. It also covers unique considerations for electrified propulsion development and aircraft integration. It focuses on the particularities introduced by the new technology. This document is not intended to represent a proposed Means of Compliance (MoC) with any particular certification regulation.
E-40 Electrified Propulsion Committee
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers a copper-zinc alloy (brass) in the form of sheet, strip, and plate (see 8.6).
AMS D Nonferrous Alloys Committee
This SAE Aerospace Recommended Practice (ARP) establishes methods and identifies opportunities to sample used powder feedstock circulating within closed loop equipment of an additive manufacturing (AM) process for the purpose of showing conformance to a powder specification. Powder within the entirety of closed loop equipment cannot be represented by sampling and testing of discrete, in-process lots. Because powder processing (i.e., reconditioning, conveyance, and storage) is asynchronous with a build cycle, individual samples and their associated tests do not represent the totality of powder committed to a machine. Powder consumed as part of an individual build cycle may only represent a subset of feedstock in circulation within such equipment. Therefore, regular testing to substantiate conformance to a powder specification is required to assert conforming feedstock was consumed during individual build cycles of the AM workflow to fabricate parts or preforms. Operation of some
AMS AM Additive Manufacturing Metals
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
The purpose of this SAE Recommended Practice is to establish a uniform laboratory procedure for securing and reporting the friction and wear characteristics of brake linings. The performance data obtained can be used for in-plant quality control by brake lining manufacturers and for the quality assessment of incoming shipments by the purchasers of brake linings.
Brake Linings Standards Committee
This specification covers a dilute aluminum/TiB2 metal matrix composite in the form of investment castings.
AMS D Nonferrous Alloys Committee
This specification covers two types of refined hydrocarbon compounds in the form of liquids. This specification only covers newly manufactured materials.
AMS K Non Destructive Methods and Processes Committee
This specification covers an aluminum alloy in the form of castings (see 8.11).
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, and drawn shapes up through 10.000 inches (254.00 mm), inclusive, in diameter or least distance between parallel sides and stock of any size for forgings or flash-welded rings. Bar over 6.000 inches (152.40 mm) in nominal thickness has a maximum cross-sectional area of 288 square inches (1858 cm2). Forgings and flash-welded rings with nominal thicknesses over 6.000 inches (152.40 mm) have a maximum cross-sectional area of 79 square inches (509 cm2) (see 8.6).
AMS G Titanium and Refractory Metals Committee
This specification covers an 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 the requirements for electrodeposited zinc-nickel on metal parts, including fasteners and other standard parts.
AMS B Finishes Processes and Fluids Committee
This document describes the materials, equipment, and processing techniques utilized in the fabrication of polyimide printed wiring boards. Included are recommendations for both double-sided and multilayer boards.
AMS P17 Polymer Matrix Composites Committee
This specification covers an aluminum alloy in the form of bars, rods, and wire, in the sizes shown in 3.3.3, in the “as-fabricated (F) temper.” When specified, product shall be supplied in the annealed (O) condition (see 8.6).
AMS D Nonferrous Alloys Committee
This SAE Standard defines the general requirements and provides a system for the control of quality for conformal coatings suitable for application to printed circuit assemblies.
AMS G8 Aerospace Organic Coatings Committee
This specification covers the requirements for gold deposited on metal surfaces and the properties of the deposit.
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum alloy in the form of sheet and plate 0.010 to 1.750 inch (0.25 to 44.45 mm) in thickness, supplied in the annealed (O temper) condition. When specified, product shall be supplied in the “as fabricated” (F) temper (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal diameter or least distance between parallel sides and 9 square inches (58 cm2) and under in cross-sectional area, and forging stock of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
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.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of plate 4.000 to 10.000 inches (101.60 to 254.00 mm), inclusive, in nominal thickness.
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of castings with nominal wall thickness up to 1.0 inch (25 mm) (see 8.8).
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm), inclusive, in nominal diameter or least distance between parallel sides and 32 square inches (206.46 cm2) maximum cross-sectional area and stock for forging of any size (see 8.7).
AMS G Titanium and Refractory Metals Committee
This document (Technical Specification) gives information about qualification rules and the relation between the different specification parts involved, such as the Technical Specification (TS), the Material Specification (MS), and the Purchasing Specifications (PS).
AMS CACRC Commercial Aircraft Composite Repair Committee
This test method covers procedures to qualitatively determine the visual and physical condition of a liquid organic coating component (pigmented base, base without pigment, curing solution, or thinner) in a container. Also covered is evaluation of the component container to determine any degradation.
AMS G8 Aerospace Organic Coatings Committee
This specification covers a shampoo type carpet cleaner in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers tungsten carbide-cobalt in the form of powder.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a titanium alloy in the form of bars, forgings, and flash-welded rings up to 4.500 inches (114.30 mm), inclusive, in nominal diameter or least distance between parallel sides and stock of any size for forging and flash-welded rings (see 8.6).
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion-resistant steel product in the solution and precipitation heat-treated (H1150) condition, 12 inches (305 mm) and under in nominal diameter, thickness, or, for hexagons, least distance between parallel sides.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant nickel-iron alloy in the form of bars and forgings 5 inches (127 mm) and under in nominal diameter or least distance between parallel sides and forging stock of any size.
AMS F Corrosion and Heat Resistant Alloys 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 specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, flash-welded rings, and stock for forging, flash-welded rings, or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant iron alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a silicone (PVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel product 12 inches (305 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides, and having a maximum cross-sectional area of 144 square inches (930 cm2) in the solution and precipitation heat treated (H1100) condition.
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Aerospace Recommended Practice (ARP) describes training and approval of personnel performing certain thermal processing and associated operations that could have a material impact on the properties of materials being processed. It also recommends that only approved personnel perform or monitor the functions listed in Table 1.
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion-resistant steel product 12 inches (305 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides, and having a maximum cross-sectional area of 144 square inches (930 cm2) in the solution and precipitation heat treated (H1075) condition.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a copper-beryllium alloy in the form of bars and rods (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a tin bronze in the form of sand and centrifugal castings (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sand, permanent mold, and composite mold castings with nominal wall thickness up to 1.0 inch (25 mm) or nominal weight up to 50 pounds (23 kg) (see 8.2 and 8.8).
AMS D Nonferrous Alloys Committee
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