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Items (216,063)

Missile Hydraulic Pumps and Their Power Sources

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 Characteristics

J1326_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 Systems

J902_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 Lights

ARP5029C (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 Treated

AMS4453H (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 STRENGTH

AS51992D (Current)

4/8/2026

E-25 General Standards for Aerospace and Propulsion Systems

Integration and Certification Considerations for Electrified Propulsion Aircraft

AIR7128 (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 Manufacturing

ARP7302 (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 Aged

AMS4412C (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

FITTING, PLUG, PIPE, EXTERNAL THREAD, COUNTERSUNK HEX HEAD

AS4864B (Current)

4/6/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Brake Lining Quality Test Procedure

J661_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

Sheet and Plate - 4.4mg 0.70mn 0.15cr

AMS4059F (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 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

Aluminum Alloy, Castings, Sand, 4cu 2ni 1.5mg 0.2cr, Solution Treated and Overaged

AMS4220E (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, 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

Cloth, Nylon Twill 5.5 Ounces per Square Yard (186 g/m₂), Smooth Finish, Water Repellent Treated

AMS3788/4B (Current)10/1/1995

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.

AMS P Polymeric Materials Committee

Cloth, Nylon, Metallized

AMS3848B (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

Aluminum Alloy, Plate 1.0mg 0.60si 0.28cu 0.25cr

AMS4053B (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

Tungsten Carbide-Cobalt Powder

AMS7879G (Current)

9/18/2025

This specification covers tungsten carbide-cobalt in the form of powder.

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

Aluminum Alloy, Sheet and Plate, Alclad, 5.6zn 2.5mg 1.6cu 0.26cr

AMS4196A (Current)1/1/1992

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of September, 1991.

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Sheet and Plate, Alclad 4.3zn 3.3mg 0.6cu 0.20mn 0.17cr

AMS4199A (Current)4/1/1991

AMS D Nonferrous Alloys Committee

Cleaner, Carpet Shampoo Type

AMS1630D (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

Steel, Maraging, Investment Castings 18.5Ni - 9.0Co - 5.0Mo - 0.70Ti - 0.12Al Vacuum Melted Homogenized, Overaged, and Solution Heat Treated

AMS5337E (Current)

6/5/2022

This specification covers an alloy steel in the form of investment castings.

AMS E Carbon and Low Alloy Steels Committee

Aluminum Foil for Sandwich Construction

AMSA81596A (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

Putty, General Purpose, Non-Hardening, Corrosion-Inhibiting

AMS1321 (Current)

9/8/2022

This specification covers a general purpose, non-curing, corrosion-inhibiting putty compounds with non-hexavalent chromium corrosion inhibitors.

AMS G9 Aerospace Sealing Committee

Peening Media, Ceramic Shot, Yttria-Zirconia (AYZ)

AMS2431/10 (Current)

9/11/2024

This specification, in conjunction with the general requirements for peening media covered in AMS2431, establishes the requirements for the procurement of yttria-zirconia ceramic shot.

AMS B Finishes Processes and Fluids Committee

Steel, Extra High Toughness, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 13Cr - 8.0Ni - 2.2Mo - 1.1Al Vacuum Induction Plus Consumable Electrode Melted, Solution Heat Treated, Precipitation Hardened (H1025)

AMS5934/H1025 (Current)

8/27/2024

This specification covers a corrosion-resistant steel product in the solution and precipitation heat-treated (H1025) 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

Laser Beam Machining

AMS2548 (Current)

10/1/2024

This specification covers the engineering requirements for laser beam machining, such as cutting and drilling.

AMS B Finishes Processes and Fluids Committee

AMS5934/H1100 (Current)

8/27/2024

This specification covers a corrosion-resistant steel product in the solution and precipitation heat-treated (H1100) condition, 12 inches (305 mm) and under in nominal diameter, thickness, or, for hexagons, least distance between parallel sides. The aged product may be supplied directly by a producer or by another entity performing the functions of a producer as defined in AS6279. The latter can be accomplished by precipitation heat treatment of solution treated material previously certified to AMS5934. The entity assuming responsibility for the aging operation is designated the producer of AMS5934/H1100.

AMS F Corrosion and Heat Resistant Alloys Committee

Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 13Cr - 8.0Ni - 2.2Mo - 1.1Al Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Precipitation Hardened (H1150)

AMS5629/H1150 (Current)

3/23/2023

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 in the solution and precipitation heat treated (H1150) condition.

AMS F Corrosion and Heat Resistant Alloys Committee

AMS5629/H1050 (Current)

3/23/2023

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 in the solution and precipitation heat treated (H1050) condition.

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 (H1075)

AMS5659/H1075 (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 (H1075) condition.

AMS F Corrosion and Heat Resistant Alloys Committee

Colors Used in Government Procurement

AMSSTD595A_A2 (Current)

9/1/2021

AMS G8 Aerospace Organic Coatings Committee

Colors Used in Government Procurement

AMSSTD595A_A3 (Current)

5/9/2022

AMS G8 Aerospace Organic Coatings Committee

Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings and Stock for Forging, Rings and Heading, 65Ni - 15.8Cr - 15.2Mo - 0.30Al - 0.05La (HASTELLOY® S), Consumable Electrode Remelted, Solution Heat Treated

AMS5711G (Current)

12/10/2025

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

Standardized Composite Training Program

AIR6671 (Current)

6/17/2025

This AIR provides means of developing a composite training program, as stipulated by FAA AC 20-107B, FAA AC 65-33A, EASA AMC 20-29, and other similar regulatory guidance. Its approach is a comprehensive, sequential training curriculum build-up, customized to the specific needs of the organization (see Figure 2). It contains recommendations for the skill-building, training, and qualification of persons involved in the design, fabrication, maintenance, and repair of aircraft composite structures or other aviation composite components. It further addresses the qualification of administrative personnel and instructors. Flight operations are usually not in the scope of an SAE CACRC Standard; however, the recommendations of this report may be used also for this target audience. This report addresses persons responsible for the definition of training, qualification and authorization, or the supervision of aviation personnel. Its content intends to facilitate the development of a formal

AMS CACRC Commercial Aircraft Composite Repair Committee

Silicone (PVMQ) Rubber Extreme-Low-Temperature Resistant 65 - 75

AMS3337G (Current)

11/10/2025

This specification covers a silicone (PVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.

AMS CE Elastomers Committee

Nickel Alloy, Corrosion- and Heat-Resistant, Sheet and Strip, 52.5Ni - 19Cr - 3.0Mo - 5.0Cb (Nb) - 0.90Ti - 0.50Al - 18Fe (Inconel® 718SPF), Vacuum Induction and Consumable Electrode Remelted, Solution Heat Treated, Precipitation Hardenable

AMS5950E (Current)

10/15/2025

This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet and strip 0.080 inch (2.03 mm) and under in nominal thickness.

AMS F Corrosion and Heat Resistant Alloys Committee

Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb - 4.0Cu Consumable Electrode Remelted Solution Heat Treated, Precipitation Hardened (H900)

AMS5622/H900A (Current)

9/17/2025

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 in the solution and precipitation heat-treated (H900) condition.

AMS F Corrosion and Heat Resistant Alloys Committee

Cobalt Alloy, Corrosion- and Heat-Resistant, Investment Castings 62Co - 27Cr - 2.8Ni - 5.5Mo (Stellite® 21) As-Cast

AMS5385J (Current)

7/18/2025

This specification covers a corrosion- and heat-resistant cobalt alloy in the form of investment castings.

AMS F Corrosion and Heat Resistant Alloys Committee

Aluminum Alloy, Extrusion 2.7Cu - 1.8Li - 0.7Zn - 0.3Mn - 0.3Mg - 0.08Zr (2099-T81) Solution Heat Treated, Stress Relieved by Stretching 1 to 3% and Aged

AMS4459C (Current)

7/22/2025

This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) from 0.375 to 1.300 inches (9.53 to 33.02 mm) in diameter or thickness, produced with cross-sectional area of 22.5 square inches (145 cm2), maximum, and a circumscribing circle diameter (circle size) of 17.4 inches (44.2 cm), maximum (see 2.4 and 8.8).

AMS D Nonferrous Alloys Committee