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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
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
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
Cloth, Nylon, MetallizedAMS3848B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Cord, Coreless, Para-Aramid Intermediate Modulus 250 Lb (1110 N), 1800 Ft Per Lb (1210 M/Kg)AMS3814/13A (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
Cord, Coreless, Para-Aramid Intermediate Modulus 4000 Lb (17,790 N), 75 Ft Per Lb (50 M/Kg)AMS3814/16A (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
Cord, Coreless, Para-Aramid Intermediate Modulus 300 Lb (1335 N), 1500 Ft Per Lb (1005 M/Kg)AMS3814/15A (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
Cord, Coreless, Para-Aramid Intermediate Modulus 2750 Lb (12,230 N), 100 Ft Per Lb (65 M/Kg)AMS3814/14A (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
Cloth, Twill Nylon, Warp, Rayon FillingAMS3789B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Identification Welding Wire, Tab Marking MethodAMS2816W (Current)7/21/2025
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.
AMS B Finishes Processes and Fluids Committee
Bars and Rods, Rolled, Drawn, or Cold Finished, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr, AnnealedAMS4187C (Current)5/17/2006
This specification covers an aluminum alloy in the form of bars, rods, and wire.
AMS D Nonferrous Alloys Committee
Compound, Alkaline Rust Remover Aircraft Turbine Engine ComponentsAMS1379A (Current)6/23/2025
This specification covers an alkaline rust remover compound in the form of a liquid concentrate or a water-soluble powder for dilution with water.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Test Method for Condition in Container of Liquid Organic Coating ComponentsAS7378 (Current)8/25/2020
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
Identification and Assessment of Damage to Composite Aircraft Structures Training DocumentAIR6825 (Current)8/3/2020
Individuals who complete the applicable modules aligned with this training document will be able to define the type of damage, define the extent of damage, determine if further inspection is required, evaluate the damage against published allowable damage limits, and provide accurate documentation of the damage. The intended outcome of the training is increased safety such that no aircraft is released with unknown damage and that the aircraft meets continued airworthiness requirements. The goal is to change the culture from damage discovery to damage reporting while also reducing or eliminating flight delays due to incorrect or insufficient information. Teaching levels have been assigned to the curriculum to define the knowledge, skills, and abilities graduates will need. Minimum hours of instruction have been provided to ensure adequate coverage of all subject matter including lecture and practical exercise. These minimums may be exceeded and may include an increase in the total
AMS CACRC Commercial Aircraft Composite Repair Committee
Minimization of High Temperature Oxidation, Aluminum Alloy Heat TreatmentARP7500 (Current)7/3/2024
This recommended practice provides recommendations for minimizing high temperature oxidation (HTO) during the heat treatment of aluminum alloy products and parts. HTO leads to deterioration of properties.
AMS D Nonferrous Alloys Committee
Static Seal Test Fixture and ProcedureAS7982 (Current)11/13/2025
This SAE Aerospace Standard (AS) provides dimensions and procedures for a standardized test fixture used to evaluate the static performance of O-rings and other seal types in glands per AS4716 and AS5857.
AMS CE Elastomers Committee
Metallic WhiskersAIR4129A (Current)1/9/2025
This AIR presents an abbreviated review of the metallurgical phenomena known as whiskers. It is not all encompassing; rather, it is intended to introduce the design engineer to the technical issues of metallic whiskers, their formation, and the potentially dangerous problems they can cause.
AMS B Finishes Processes and Fluids Committee
Manufacturing Sequence for Fabrication of High-Strength Steel Parts 300M or 4340 Modified Low-Alloy Steels 270,000 psi (1860 MPa) Tensile Strength and HigherARP1631A (Current)6/24/2024
This document establishes the requirements for the sequencing of processes relating to parts fabricated from 300M or 4340 modified steel heat treated to, or to be heat treated to, 270,000 psi (1860 MPa) minimum ultimate tensile strength (UTS) and higher.
AMS E Carbon and Low Alloy Steels Committee
Physical-Chemical Characterization Techniques, Epoxy Adhesive and Prepreg Resin SystemsARP1610A (Current)6/5/2022
This recommended practice describes the physical and chemical characterization techniques for identification of epoxy adhesive and prepreg resin systems in order to verify the chemical formulation, resin B-staging (See 8.1), cure reaction rates, adhesive moisture content, and resin component mix ratios, as necessary to achieve manufacturing and quality producibility and engineering performance.
AMS P17 Polymer Matrix Composites Committee
Polyimide Printed Circuit Boards Fabrication ofARP1612A (Current)6/5/2022
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
Colors Used in Government ProcurementAMSSTD595A_A2 (Current)9/1/2021
AMS G8 Aerospace Organic Coatings Committee
Colors Used in Government ProcurementAMSSTD595A_A3 (Current)5/9/2022
AMS G8 Aerospace Organic Coatings Committee
Titanium Alloy, Round Bars 5Al - 1Fe AnnealedAMS4895 (Current)8/1/2023
This specification covers a titanium alloy in the form of round bars up to 10 inches (254 mm), inclusive, in diameter.
AMS G Titanium and Refractory Metals Committee
Medium Temperature, Out-of-Autoclave, Oven-Vacuum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite MaterialsAMS6562 (Current)8/1/2023
The purpose of this specification is to allow procurement of defined carbon fiber and fiberglass epoxy prepreg materials corresponding to their statistically derived material properties published in CMH-17 (formerly MIL-HDBK-17). As a result, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program shall notify the Qualifying Agency per 4.2.1.
AMS P17 Polymer Matrix Composites Committee
Aluminum Alloy Sheet and Plate, Alclad 5.6zn 2.5mg 1.6cu 0.26crAMS4197A (Current)7/1/1991
AMS D Nonferrous Alloys Committee
Cord, Coreless, Para-Aramid Intermediate Modulus 5000 Lb (22,240 N), 58 Ft Per Lb (40 M/Kg)AMS3814/11A (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
Coating, Abrasion Resistant for Polycarbonate PartsAMS3510B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Rings, Flash Welded Ferritic and Martensitic Corrosion-Resistant SteelsAMS7493L (Current)9/23/2025
This specification covers flash welded rings made of ferritic and martensitic corrosion-resistant steels.
AMS F Corrosion and Heat Resistant Alloys Committee
Terms Used in Aerospace Metals SpecificationsAS7766 (Current)9/15/2021
This SAE Aerospace Standard (AS) defines and clarifies terms used in aerospace materials and process specifications, standards, and recommended practices.
AMS B Finishes Processes and Fluids Committee
Qualification of Aerospace Personnel Performing Special ProcessesAS7767 (Current)7/23/2021
AMS B Finishes Processes and Fluids Committee
Required O-ring Sizes for Quality Conformance TestingAS6837 (Current)6/10/2021
The purpose of this document is to specify the O-ring sizes that are suitable for quality conformance testing (limited to hardness, tensile tests, compression set, specific gravity, and volume swell per ASTM D1414) required by AMS-7xxx series of specifications. In addition, suppliers and/or users, at their own discretion and/or according to their procurement documents, may choose to invoke this specification for procurement or other purposes for O-ring sizes that are not covered by AS568. If additional tests are specified as quality conformance tests in any AMS-7xxx specification, then that specification shall also specify the required test size for that additional test. This document does not address O-ring size for qualification testing required by AMS-7xxx series of specifications since that is already specified in the AMS-7xxx specification. This document only covers O-ring sizes required by test type. These O-ring sizes include, but are not limited to, AS568-xxx O-ring sizes
AMS CE Elastomers Committee
Hardness Testing of Elastomeric O-RingsAIR4738B (Current)11/13/2025
This SAE Aerospace Information Report (AIR) provides a general description of methods for hardness testing of O-rings including factors which affect precision and comparison of results with those obtained in standard tests.
AMS CE Elastomers Committee
Quality Inspection Procedure, Composites Tracer Fluoroscopy and RadiographyARP1611A (Current)6/5/2022
This document describes an inspection procedure for detecting, by use of a radiographic opaque tracer and fluoroscopy or radiography methods, flaws which have been produced as the result of cutting, machining, or drilling operations in composite or laminate structures.
AMS P17 Polymer Matrix Composites Committee
Medium Temperature, Out-of-Autoclave, Oven-Vacuum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite Materials, Type 35, Class 4, Grade 293, Style 7781AMS6562/1 (Current)7/24/2023
This detail specification, along with AMS6562, establishes the requirements for continuous E-glass fabric impregnated with a medium temperature, out-of-autoclave, oven-vacuum-bag cure modified B-staged epoxy resin. The prepreg is produced using a one side coated (one side tacky) hot-melt process.
AMS P17 Polymer Matrix Composites Committee
Rubber: Fluorosilicone (FVMQ), Engine Oil / Fuel-Resistant, For Seals in Engine Oil Systems/Fuel SystemsAMSR25988B (Current)6/27/2023
This material has resistance to diester-based engine oil (MIL-PRF-7808) and fuel, but usage is not limited to such applications. This material is not suitable for use in synthetic phosphate ester based hydraulic fluids (AS1241) or helicopter transmission lubricating oils (DOD-PRF-85734, MIL-PRF-32538). For gas turbine engine lubricating oils (AS5780, MIL-PRF-23699), resistance varies by class and should be evaluated individually (see Note regarding high performance oils). This material has a typical service temperature range of -70 to +392 °F (-56.7 to +200 °C) for Class 1 and Class 2 and -70 to +437 °F (-56.7 to +225 °C) for Class 3. The service temperature range of the material is a general temperature range, but the presence of particular fluids and specific design requirements may modify this range. Each application should be considered separately. It is the responsibility of the user to determine that this specification is appropriate for the environments (temperature range
AMS CE Elastomers Committee
Dynamic Seal Test FixtureAS6944 (Current)7/14/2023
This SAE Aerospace Standard (AS) provides dimensions for a standardized test fixture that can be used to evaluate the dynamic performance requirements defined in some elastomer material standards of O-rings in rod glands per AS4716.
AMS CE Elastomers Committee
Residual Stress Measurement and Classification, Metallic Structural Alloy Products and Finished PartsAS7045 (Current)5/22/2023
The purpose of this standard is to provide uniform methods for defining, quantifying, and classifying the residual stress in metallic structural alloy products and finished parts. These stresses may exist within a single element, or they may be the result of a joining process. Such quantification and classification may be required when residual stresses within mill stock or preforms can impact further in-process distortion during machining or other processes, and when residual stresses within finished components can impact final mechanical properties and performance (especially strength, durability, and fracture performance).
AMS B Finishes Processes and Fluids Committee
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