Search
Advanced Search
of the following are true
(
)

Results

Items (216,063)
Missile Hydraulic Pumps and Their Power SourcesAIR560D (Current)
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
Test Method for Measuring Wet Color Transfer CharacteristicsJ1326_202604 (Current)4/8/2026
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
Passenger Vehicle Windshield Demisting and Defrosting SystemsJ902_202604 (Current)4/8/2026
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
Measurement Procedures for Short Pulse Width Strobe Anticollision LightsARP5029C (Current)4/8/2026
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
Magnesium Alloy, Investment Castings, 9.0Al - 2.0Zn (AZ92A-T6), Solution and Precipitation Heat TreatedAMS4453H (Current)4/8/2026
This specification covers a magnesium alloy in the form of investment castings (see 8.6).
AMS D Nonferrous Alloys Committee
STUD, LOCKED-IN RING, SERRATED, HIGH STRENGTHAS51992D (Current)4/8/2026
E-25 General Standards for Aerospace and Propulsion Systems
Integration and Certification Considerations for Electrified Propulsion AircraftAIR7128 (Current)4/8/2026
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
Sampling, Conformance Strategies, and Recommended Practices for Closed Loop Processing of Powder for Additive ManufacturingARP7302 (Current)4/8/2026
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
Aluminum Alloy, Sheet, 3.2Cu - 0.52Mg - 0.30Ag - 0.95 Li - 0.12Zr (2198-T8), Solution Heat Treated, Cold Worked, and Artificially AgedAMS4412C (Current)4/8/2026
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
Steel, Sheet, Strip, and Plate, 0.75Si - 0.62Cr - 0.20Mo - 0.10Zr (0.10 - 0.17C) (NAX 9115-AC)AMS6354H (Current)4/8/2026
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
Copper Alloy (Brass), Sheet, Strip, and Plate, 70Cu - 30Zn, Half Hard (H02)AMS4507K (Current)4/8/2026
This specification covers a copper-zinc alloy (brass) in the form of sheet, strip, and plate (see 8.6).
AMS D Nonferrous Alloys Committee
Brake Lining Quality Test ProcedureJ661_202604 (Current)4/6/2026
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
FITTING, PLUG, PIPE, EXTERNAL THREAD, COUNTERSUNK HEX HEADAS4864B (Current)4/6/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Rubber: Ethylene Propylene (EP) Phosphate Ester Resistant Low Temperature Tg -67 °F (-55 °C), 75 to 85 Type M Hardness for Seals in Hydraulic SystemsAMS7361B (Current)12/13/2023
This specification covers an ethylene propylene rubber in the form of molded rings, molded compression seals, molded O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications.
AMS CE Elastomers Committee
Anodic Treatment of Aluminum Alloys Sulfuric Acid Process Thin FilmAMS2490 (Current)2/16/2022
This specification establishes the requirements for undyed thin anodic coatings on aluminum alloys using chemical solutions containing sulfuric acid.
AMS B Finishes Processes and Fluids Committee
Alloy Welding Electrodes, Covered, Corrosion and Heat Resistant 63Ni - 5.0Cr - 24.5Mo - 5.5FeAMS5787B (Current)11/9/2021
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu Solution and Precipitation Heat Treated (H1100)AMS5659/H1100 (Current)9/14/2022
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
Aluminum Alloy, 7075, Plate and Sheet (Improved Exfoliation Resistant)AMSQQA250/24C (Current)5/21/2021
This specification covers the specific requirements for aluminum alloy 7075 plate and sheet for applications requiring improved exfoliation resistance.
AMS D Nonferrous Alloys Committee
Elastomer: Rubber, Silicone (MQ/VMQ/PVMQ) Flame Retardant, Low Smoke Density, Low Smoke Toxicity 50 – 60 Durometer Type A Hardness for Products in Pressurized Aircraft Compartment InteriorsAMS3742 (Current)3/29/2022
This specification covers a self-extinguishing, pigmentable silicone (MQ/VMQ/PVMQ) elastomer that can be used to manufacture product in the form of molded, extruded, and/or calendared, sheets, strips, and shapes.
AMS CE Elastomers Committee
Carbon Fiber and Fiberglass Epoxy/Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 42, Class 4, Grade 48, Style 108AMS6891/4 (Current)3/10/2021
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
Steel, Corrosion Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb (Nb) - 4.0Cu Solution and Precipitation Heat Treated (H1075)AMS5643/H1075 (Current)1/20/2022
This specification covers a corrosion-resistant steel product 8 inches (203 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides, and having a maximum cross-sectional area of 64 in2 (413 cm2) in the solution and precipitation heat treated (H1075) condition
AMS F Corrosion and Heat Resistant Alloys Committee
Elastomer: Nitrile Rubber (NBR) Synthetic Oil Resistant Sheets, 65 to 75 Type A Hardness for Products in Engine Oil SystemsAMS3786 (Current)10/22/2021
This specification covers a nitrile rubber (NBR) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7289 specification.
AMS CE Elastomers Committee
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 2 - Qualification Program for Fiber, Carbon Fiber Tape Prepreg, and Film AdhesiveAMS6885/2 (Current)2/23/2021
AMS6885/2 gives specific information about the qualification program for unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The prepreg system shall include an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
AMS CACRC Commercial Aircraft Composite Repair Committee
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 0 - IntroductionAMS6885 (Current)2/23/2021
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
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 1 - General RequirementsAMS6885/1 (Current)2/23/2021
AMS6885/1 gives information about the technical requirements and qualification procedure for unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The repair system includes an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
AMS CACRC Commercial Aircraft Composite Repair Committee
Vehicle, Magnetic Particle Inspection Petroleum BaseAMS2641D (Current)9/12/2025
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
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 4 - Purchasing Specification for Film AdhesiveAMS6885/4 (Current)2/22/2021
This Purchasing Specification, AMS6885/4, specifies the batch release and delivery requirements for film adhesive used for repair. This specification is applicable only when the film adhesive is used as part of the repair system defined in AMS6885 and AMS6885/1. This specification also defines the procedure and requirements for storage life extension of materials purchased against this specification. It is only applicable for materials qualified against AMS6885 (refer to PRI-QPL-AMS6885), and shall be carried out within the responsibility of the purchaser and under control of its Quality organisation.
AMS CACRC Commercial Aircraft Composite Repair Committee
Tungsten Carbide-Cobalt PowderAMS7879G (Current)9/18/2025
This specification covers tungsten carbide-cobalt in the form of powder.
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy, Sheet and Plate, Alclad 4.3zn 3.3mg 0.6cu 0.20mn 0.17crAMS4199A (Current)4/1/1991
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet 4.4mg-0.70mn-0.15cr (5083-H323)AMS4057E (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS D Nonferrous Alloys Committee
Cloth, Nylon Twill 5.4 Ounces per Square Yard (183 g/m₂), Smooth Finish, Heavily Calendered, Water Repellent TreatedAMS3788/6B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Cloth, Nylon Twill 5.4 Ounces per Square Yard (183 g/m₂), Smooth Finish, Heavily CalenderedAMS3788/5B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Cloth, Nylon Twill 5.5 Ounces per Square Yard (186 g/m₂), Smooth Finish, Water Repellent TreatedAMS3788/4B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Aluminum Alloy, Sheet 4.4mg-0.70mn-0.15cr (5083-373)AMS4058E (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS D Nonferrous Alloys Committee
Bronze, Aluminum Silicon, Rods, Bars, and Forgings 90cu 7.0al 1.8si Drawn and Stress Relieved (Hr50)AMS4264A (Current)8/1/1995
This specification has been Superseded by AMS 4633.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet and Plate, Alclad, 5.6zn 2.5mg 1.6cu 0.26crAMS4196A (Current)1/1/1992
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of September, 1991.
AMS D Nonferrous Alloys Committee
Steel Castings, Sand, Corrosion and Heat Resistant 24.5Cr - 20.5Ni Solution Heat TreatedAMS5365E (Current)10/21/2013
This specification covers a corrosion and heat resistant steel in the form of sand castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Bolts and Screws-Steel Corrosion and Heat Resistant, Upset Headed, Heat Treated, Roll Threaded Solution and Precipitation Treated (Ams 5731)AMS7477D (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Conformal Coatings for Panels, Printed Circuit and Panels, Electronic CircuitAMS59_047 (Current)1/28/2021
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
Interior Decorative Clear Coating for Metal SurfacesAMS7200 (Current)2/10/2020
This specification establishes requirements for an interior decorative clear coating for wear protection of metal substrates.
AMS G8 Aerospace Organic Coatings Committee
Steel, Investment Castings 0.50Cr - 0.55Ni - 0.20Mo (0.25 - 0.35C) (SAE 8630 Mod) Normalized and TemperedAMS5334J (Current)1/19/2024
This specification covers a low-alloy steel in the form of investment castings.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Foil for Sandwich ConstructionAMSA81596A (Current)3/27/2025
This specification covers the requirements of uncoated aluminum alloy foil for core materials required for structural sandwich construction.
AMS D Nonferrous Alloys Committee
Steel, Maraging, Investment Castings 18.5Ni - 9.0Co - 5.0Mo - 0.70Ti - 0.12Al Vacuum Melted Homogenized, Overaged, and Solution Heat TreatedAMS5337E (Current)6/5/2022
This specification covers an alloy steel in the form of investment castings.
AMS E Carbon and Low Alloy Steels Committee
Cleaner, Carpet Shampoo TypeAMS1630D (Current)11/22/2024
This specification covers a shampoo type carpet cleaner in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Compound, Carbon Removing Orthodichlorobenzene for Engine PartsAMS1546B (Current)8/1/2001
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 1994. It is recommended, therefore, that this specification not be specified for new designs.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Sheet and Plate - 4.4mg 0.70mn 0.15crAMS4059F (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS D Nonferrous Alloys Committee
Cord, Aromatic Polyamide, NonmeltingAMS3853B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Alloy Welding, Electrodes, Covered, Corrosion and Heat Resistant 72ni 15cr 9fe 2.8(Cb + Ta)AMS5684E (Current)8/1/1996
This specification covers a corrosion and heat resistant nickel alloy in the form of covered welding electrodes. Primarily for shielded metal arc welding of corrosion and heat resistant steels and alloys. Alloy: Inconel WE 132 UNS Number: W86132
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy, Castings, Sand, 4cu 2ni 1.5mg 0.2cr, Solution Treated and OveragedAMS4220E (Current)11/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of November 1995.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate 1.0mg 0.60si 0.28cu 0.25crAMS4053B (Current)3/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of March 1995. By this action, subject specification number and title will be deleted from the active specification index of Aerospace Material Specifications.
AMS D Nonferrous Alloys Committee
Items per page:
1 – 50 of 216063