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Marking Materials for Use on High-Temperature AlloysAMS3147 (Current)10/21/2026
This specification defines the requirements for in-process and temporary marking material used on nickel, iron, cobalt, and titanium-based turbine engine components during processing or manufacture. Control is required as marking material may contain deleterious or low melting point elements that could negatively affect performance.
AMS F Corrosion and Heat Resistant Alloys Committee
Titanium Alloy Bars, Wire, and Forgings, 6.0Al - 2.0Sn - 4.0Zr - 6.0Mo, Solution and Precipitation Heat TreatedAMS4981K (Current)10/21/2026
This specification covers a titanium alloy in the form of bars, wire, and forgings up through 4.000 inches (101.60 mm), inclusive, in diameter or least distance between parallel sides and forging stock of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Aluminum Alloy, Sheet and Plate, 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-O) Annealed or, When Specified, “As Fabricated” (2219-F)AMS4031L (Current)10/21/2026
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 2.000 inches (0.51 to 50.80 mm), inclusive, in nominal thickness, supplied in the annealed (-O) condition. When specified, product shall be supplied in the “as fabricated” (-F) temper (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Sheet, 6.0Cu - 0.40Zr (2004-F), As RolledAMS4208E (Current)10/21/2026
This specification covers an aluminum alloy in the form of sheet less than 0.250 inch (6.35 mm) thick (see 8.5).
AMS D Nonferrous Alloys Committee
Titanium Alloy Bars, Hand Forgings and Forging Stock, 6.0Al - 4.0V, AnnealedAMS6931E (Current)10/21/2026
This specification covers a titanium alloy in the form of bars and hand forgings up through 10.000 inches (254.00 mm), inclusive, in diameter or least distance between parallel sides and forging stock of any size. Bar over 6.000 inches (152.40 mm) in nominal thickness has a maximum cross-sectional area of 288 square inches (1858 square cm). Hand forgings with nominal thickness over 6.000 inches (152.40 mm) have a maximum cross-sectional area of 79 square inches (509 square cm) (see 8.7).
AMS G Titanium and Refractory Metals Committee
Inverter Requirements for Class Eight Trucks - Truck and BusJ2697_202610 (Current)10/16/2026
This SAE Recommended Practice is intended to describe the application of single-phase DC to AC inverters, and bidirectional inverter/chargers, which supply power to ac loads in Class heavy duty on-highway trucks (10K GVW). The document identifies appropriate operating performance requirements and adds some insight into inverter selection. This document applies to factory and after-market installed DC-to-AC inverter systems (Including inverter chargers) providing up 3000 W of 120 VAC line-voltage power as a convenience for operator and passenger use. Such inverters are intended to power user loads not essential to vehicle Operation or safety (e.g., HVAC, TV, microwave ovens, battery chargers for mobile phones or laptop computers, audio equipment, etc.). Systems incorporate the inverter itself as well as the input, output, control, and signal wiring associated with the inverter. Requirements are given for the performance, safety, reliability, and environmental compatibility of the system. These are recommended requirements to be used by vehicle manufacturers in the development of their own specifications, which may incorporate more or less stringent requirements. This document scope excludes military vehicles, bus and 28 V systems.
Truck and Bus Electrical Systems Committee
Primary and Auxiliary Seven Conductor Electrical Connector for Truck-Trailer Jumper CableJ560_202610 (Current)10/16/2026
This SAE Standard provides the minimum requirements for primary and auxiliary jumper cable plug and receptacle for the truck-trailer and converter dolly jumper cable systems for 12 VDC nominal applications. It includes the test procedures, design, and performance requirements.
Truck and Bus Electrical Systems Committee
Steel Bars, Wire, Forgings and Forging Stock, Mechanical Tubing, Rings, and Extrusions, Corrosion-Resistant, 11.8Cr - 2.5Ni - 1.8Mo - 0.33V (0.08 - 0.15C) (M152), Annealed, Vacuum Arc or Electroslag RemeltedAMS5719F (Current)10/16/2026
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.
AMS F Corrosion and Heat Resistant Alloys Committee
Titanium Alloy, Cold-Rolled Sheet and Strip, 5Al - 1Fe, AnnealedAMS4947A (Current)10/16/2026
This specification covers a titanium alloy in the form of cold-rolled sheet and strip up to 0.100 inch (2.540 mm), inclusive, in thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
Steel Bars, Forgings, and Mechanical Tubing and Forging Stock, 1.1Si - 1.45Cr - 1.0Mo - 0.08Al (0.16 - 0.22C), [CBS600], Premium Aircraft-Quality, Double Vacuum MeltedAMS6255H (Current)10/16/2026
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Titanium Alloy, Hot-Rolled Sheet and Strip, 5Al - 1Fe, AnnealedAMS4948A (Current)10/16/2026
This specification covers a titanium alloy in the form of hot-rolled sheet and strip up to 0.165 inch (4.20 mm), inclusive, in thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
Gold-Palladium-Nickel Alloy, Brazing Filler Metal, High-Temperature, 70Au - 8.0Pd - 22Ni, 1845 to 1915 °F (1007 to 1046 °C) Solidus-Liquidus RangeAMS4786L (Current)10/15/2026
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
General Characteristics and Heat Treatments of SteelsJ412_202610 (Current)10/15/2026
The information and data contained in this SAE Information Report are intended as a guide in the selection of steel types and grades for various purposes. Consideration of the individual types of steel is preceded by a discussion of the factors affecting steel properties and characteristics. SAE J4xx steels are generally purchased on the basis of chemical composition requirements (SAE J403, SAE J404, and SAE J405). High-strength, low-alloy (HSLA) steels (SAE J1392 and SAE J1442) are generally purchased on the basis of mechanical properties; different chemical compositions are used to achieve the specified mechanical properties. Because these steels are characterized by their special mechanical properties obtained in the as-rolled condition, they are not intended for any heat treatment by the purchaser either before, during, or after fabrication. In many instances, as in the case of steels listed in SAE J1268 and SAE J1868, hardenability is also a specification requirement. This information report can be used as a reference for determining the general characteristics and applications of commonly used SAE steels. The use of the typical heat treatments listed in Tables 1 through 7 is recommended. These and other heat treatments commonly used on steel are briefly described at the end of this section.
Metals Technical Committee
CONNECTOR ACCESSORIES, ELECTRICAL, ADAPTER, SHRINK BOOT, CATEGORY 5 (FOR AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)AS85049/60E (Current)10/15/2026
AE-8C1 Connectors Committee
Aircraft Asset Life Cycle and Digital Data Standards OverviewAIR7501A (Current)10/15/2026
This SAE Aerospace Information Report (AIR) reviews technical, operational, and maintenance data being exchanged between key stakeholders in aerospace asset life cycle and data standards available for such exchanges. It identifies gaps and non-availability of data standards in certain areas. The scope of the current document is limited to aircraft operations, maintenance, and disposal stages post-build phase, and does not include the detailed interactions during the aircraft build phase. This updated version reflects all aerospace digital data standards published following the release of the initial document.
G-31 Digital Transactions for Aerospace
Automotive Safety Glazing MaterialsJ673_202610 (Current)10/14/2026
This SAE Recommended Practice is a guidance document, which covers current safety glazing materials applicable for use in motor vehicles and motor vehicle equipment. Nominal specifications for thickness, flatness, curvature, size, and fabrication details are included. This guidance document does not precede or replace customer specifications and requirements.
Glazing Materials Standards Committee
CRIMPING TOOLS, TERMINAL, HAND, WIRE TERMINATION, INSPECTION GAGE FOR TYPE I AND II TOOLSAS22520/3E (Current)10/12/2026
AE-8C2 Terminating Devices and Tooling Committee
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, ELECTRONIC, IN-LINE JUNCTIONS, INTEGRAL FUSE, SERIES IAS81714/23C (Current)10/12/2026
AE-8C2 Terminating Devices and Tooling Committee
Steel, Corrosion-Resistant, Seamless and Welded Aircraft Tubing, 19Cr - 9.5Ni (SAE 304), Cold Drawn, 1/2 Hard TemperAMS5868D (Current)10/9/2026
This specification covers a corrosion-resistant steel in the form of two types of aircraft tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK UNS S66286, 130 KSI MIN, .2500-28 UNJF-3AAS91111E (Current)10/9/2026
E-25 General Standards for Aerospace and Propulsion Systems
Assessment of Aircraft Wheel Sealing SystemsARP5146A (Current)10/9/2026
This SAE Aerospace Recommended Practice (ARP) is intended to provide guidance on verifying the integrity of inflation pressure sealing systems of aircraft wheel/tire assemblies.
A-5A Wheels, Brakes and Skid Controls Committee
Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (ePTFE), Oil and Water ResistantAMS3255D (Current)10/9/2026
This specification establishes the requirements for an expanded polytetrafluoroethylene (ePTFE) in the form of sealing tape, gaskets, or sheets requiring no mixing or curing.
AMS G9 Aerospace Sealing Committee
Flux, Aluminum Dip Brazing, 1030 °F (554 °C) or Lower LiquidusAMS3415F (Current)10/9/2026
This specification covers the requirements for an aluminum brazing flux in granular form.
AMS B Finishes Processes and Fluids Committee
Extrusions, Nickel-Aluminum Bronze, Martensitic, 78.5Cu - 10.5Al - 5.1Ni - 4.8Fe, Quenched and Tempered (TQ50)AMS4590E (Current)10/9/2026
This specification covers one type of nickel-aluminum bronze in the form of extruded bars, rods, and tubes up to 4.00 inches (101.6 mm) in nominal diameter, distance between parallel sides, or wall thickness (see 8.5).
AMS D Nonferrous Alloys Committee
Wire, Phosphor Bronze, 94Cu - 5.0Sn - 0.19P, Cold Drawn, Spring Temper (H08)AMS4720K (Current)10/9/2026
This specification covers one type of bronze in the form of round wire 0.500 inch (12.70 mm) and under in nominal diameter (see 8.5).
AMS D Nonferrous Alloys Committee
Steel, Corrosion-Resistant, Sheet, Strip, and Plate, 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu (15-5 PH®), Consumable Electrode Remelted, Premium Aircraft Quality, Solution Heat Treated and Precipitation-Hardened (H1075)AMS5862/H1075 (Current)10/9/2026
This specification covers a corrosion-resistant steel product in the solution and precipitation heat treated (H1075) condition, 4 inches (102 mm) and under in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Automatic Transmission Intake Filter Test ProcedureJ2312_202610 (Current)10/9/2026
This test procedure is intended to apply to hydraulic pump suction filters and strainers used in automotive automatic transmissions that include hydraulic power pumps. The various paragraphs of Section 5 include a variety of tests and alternative tests that are not applicable to all filters and applications, so the engineer must specify which tests are to be performed for a particular application. These test procedures are intended to evaluate filter functional performance characteristics only; durability is not evaluated under this standard. Filter design requirements must be specified by the engineer on the filter assembly drawing, an applicable engineering specification, or summarized on an application data sheet similar to that found in this recommended practice. See Figure 6. Pressure circuit filters, both barrier and system contamination control types, are not covered under this standard. They are similar in design and construction to filters used in many hydraulic and lubricating applications. Testing for pressure filters is covered by the ISO and SAE standards listed in Section 2.
Automatic Transmission and Transaxle Committee
Processes for Application-Specific Qualification of Electrical, Electronic, and Electromechanical Parts and Sub-Assemblies for Use in Aerospace, Defense, and High Performance SystemsARP6379A (Current)10/9/2026
This document describes a process for use by ADHP integrators of EEE parts and subassemblies (items) that may have been targeted by part manufacturers for other applications. This methodology allows for existing data, such as manufacturer qualification test results, in-service use, and system qualification test data, to meet the application requirement and to identify gaps in data that require additional testing or analysis. This document describes a process to define and accomplish application-specific qualifications that provide confidence to both the ADHP integrators and the integrators’ customers that the item will perform its function(s) reliably in the ADHP application. It does not describe specific tests to be conducted, sample sizes to be used, or results to be obtained.
APMC Avionics Process Management
PIN, FEMALE COUPLINGAS7365/1A (Current)10/9/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Recommended Practices for Shipping, Transport, and Handling of Automotive-Type Battery System - Lithium IonJ2950_202610 (Current)10/9/2026
This SAE Recommended Practice (RP) aids in the identification, handling, and shipping of lithium batteries to and from specified locations. It is the specific intent of this RP to identify, utilize, and reference existing U.S. and international hazardous materials (dangerous goods) transportation regulations, which are the only methodologies to be used to establish transportability. It is also the intent of this RP to provide recommendations to be used by service and shipping personnel for the purpose of determining a possibly damaged/defective battery’s transportability. In support of the service and shipping personnel, these recommendations seek to use standard tools of the trade and avoid laboratory-type equipment.
Battery Transportation and Storage Committee
Design and Handling Guide Radio Frequency Absorptive Type Wire and Cables (Filter Line, AS85485)AIR4465C (Current)10/9/2026
This document presents design and application information which will allow optimized utilization of filter line wire and cable purchased to AS85485. Filter line wire is defined and design information is presented. The electrical and mechanical performance characteristics of the wire, along with recommended harnessing methods and techniques, are also presented.
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
BEARING, BALL, AIRFRAME, ANTIFRICTION, SELF-ALIGNING, DOUBLE ROW, HEAVY DUTYAS27643E (Current)10/9/2026
ACBG Rolling Element Bearing Committee
Considerations for Hydrogen Fuel Cells in Airborne ApplicationsAIR7765A (Current)10/5/2026
The scope of this joint EUROCAE/SAE report is to compile the considerations relating to airborne application of hydrogen fuel cells. This document provides a comprehensive analysis of the use of hydrogen as a fuel by describing its existing applications and the experience gained by exploiting fuel cells in sectors other than aviation. The use of hydrogen fuel cells in aircraft can help in meeting aviation environmental targets (including noise pollution) and can be vital to achieving efficient electrically propelled air vehicles. The experience gained with mature fuel cells in terrestrial applications and the handling of other gases in aviation, as presented herein, will help in alleviating safety concerns and in demystifying the usage of hydrogen in aviation.
AE-7F Hydrogen and Fuel Cells
FITTING END, INTEGRAL WELD, LIP, DESIGN STANDARDAS1579E (Current)10/2/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
High-Carbon Cast-Steel GritJ1993_202610 (Current)10/2/2026
This SAE Recommended Practice describes the chemical composition, and physical characteristic requirements for high-carbon cast-steel grit, to be used for blast cleaning and etching operations.
Surface Enhancement Committee
BEARING, BALL, AIRFRAME ANTIFRICTION, PULLEYAS21443D (Current)10/2/2026
ACBG Rolling Element Bearing Committee
ADAPTER, ASSEMBLY - PORT CONNECTION RING LOCKED TO 60° FLARELESS TUBE END, METRICMA2119C (Current)10/2/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Requirements for Retrofitting Refrigerants in Mobile Thermal Management SystemsJ3332_202610 (Current)10/1/2026
This technical report provides minimum requirements for subordinate technical reports that define the specifics for retrofitting refrigerants in various mobile thermal management applications.
ICTMS Service Committee
Disc Wheel and Hub or Drum Interface Dimensions - Truck and BusJ694_202609 (Current)9/28/2026
This SAE Recommended Practice contains dimensions and their tolerances concerning disc wheel to hub or drum interface areas for truck and bus applications. Disc wheels designed only for single wheel applications (not dual wheels) for light trucks and special or less common applications are not covered in this document.
Truck and Bus Wheel Committee
Battery Management System: Surface Vehicle Battery Diagnostic Technical Information ReportJ3356_202609 (Current)9/28/2026
The purpose of this document is to expressly describe the required diagnostics (DIAG) related to the on-road traction battery management systems (BMS). This document will attempt to clearly educate and explain four key areas of BMS DIAG: (1) fault identification, (2) fault classification, (3) system reaction, and (4) diagnostic data and reporting.
Battery Management Systems Committee
Principles and Process for Developing Icons for Electronic DisplaysJ3113_202609 (Current)9/28/2026
SAE J3113 provides principles and a process for developing icons for use in electronic displays related to off-road work machines as stated defined in SAE J1116. Following the process ensures that icons are derived from ISO-registered graphical symbols or ISO-compliant non-registered graphical symbols.
HFTC2, Machine Displays and Symbols
Battery Management System: Surface Vehicle Battery SOH Technical Information ReportJ3356/2_202609 (Current)9/28/2026
The purpose of this document is to expressly describe the method of calculating state of health (SOH) related to the on-road traction battery management systems (BMS). This document will attempt to clearly educate and explain four key areas of BMS SOH: (1) basic SOH definition, (2) SOH calculation methods, (3) influence items for SOH, and (4) SOH reporting.
Battery Management Systems Committee
Battery Management System: Surface Vehicle Battery SOC Technical Information ReportJ3356/1_202609 (Current)9/28/2026
The purpose of this document is to expressly describe the method of calculating state of charge (SOC) related to the on-road traction battery management systems (BMS). This document will attempt to clearly educate and explain four key areas of BMS SOC: (1) basic SOC definition, (2) SOC calculation methods, (3) influence items for SOC, and (4) SOC warnings.
Battery Management Systems Committee
Sealing Compound, Polythioether Rubber Fast Curing, Light Weight (Specific Gravity 0.78, Max) for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C)AMS3102B (Current)9/28/2026
This specification covers a fuel-resistant polythioether sealing compound with low specific gravity, supplied as a two-component system which cures at room temperature.
AMS G9 Aerospace Sealing Committee
Steel, Corrosion-Resistant, Bars, Wire, and Forgings, and Forging Stock, 17Cr - 0.52Mo (0.95 - 1.20C) (440C), for Bearing ApplicationsAMS5923B (Current)9/25/2026
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Screw Threads - UNJ Profile, Inch, Controlled Radius Root with Increased Minor DiameterAS8879E (Current)9/25/2026
This SAE Aerospace Standard (AS) specifies the characteristics of screw threads - UNJ profile, inch, series, including a mandatory controlled radius as specified in Table 1 at the root of the external thread. The minor diameter of both external and internal threads provides a basic thread height of .5625H to accommodate the external thread maximum root radius. The following detailed design requirements are included: Screw threads - UNJ basic profile and design profiles. Standard series of diameter-pitch combinations for nominal thread diameters from 0.060 to 6.000 inches. Standard thread classes and form tolerances. Formulae for thread dimensions and tolerances. Method of designating UNJ threads. Tables for selected diameter-pitch combinations for close tolerance mechanical thread applications. Tables for screw thread - UNJ profile thread limit dimensions.
E-25 General Standards for Aerospace and Propulsion Systems
Aluminum Alloy, Sheet and Plate, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr, 7075: (-T76 Sheet, -T7651 Plate), Solution and Precipitation Heat TreatedAMS4315C (Current)9/25/2026
This specification covers an aluminum alloy in the form of sheet and plate up to 2.000 inches (50.80 mm), inclusive, in thickness. (see 8.5)
AMS D Nonferrous Alloys Committee
Cable Assemblies and Attachable Plugs, External Electrical Power, Aircraft, General Specification ForAS7974B (Current)9/25/2026
This specification contains requirements for, and applies to, commercial and military aircraft external/ground electrical power cable assemblies, using either overmolded or attachable plug connectors used to connect external/ground electrical power to aircraft and to attachable plugs used as replacements for plugs damaged in service.
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
Steel, Corrosion-Resistant, Plate, 13Cr - 8.0Ni - 2.2Mo - 1.1Al (PH 13-8 Mo), Premium Aircraft-Quality, Vacuum Induction Plus Consumable Electrode Melted, Solution Heat Treated, Precipitation HardenableAMS5864E (Current)9/25/2026
This specification covers a corrosion-resistant steel in the form of plate up to 3.00 inches (76.2 mm), inclusive, in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, BLACK OXIDE, STEEL, UNS G87400, 125 KSI MIN .2500-28 UNF-3AAS91701C (Current)9/25/2026
E-25 General Standards for Aerospace and Propulsion Systems
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