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Steel Bars, Forgings, and Mechanical Tubing and Forging Stock, Nitriding, 1.4Cr - 1.2Mo - 0.3V (0.29 - 0.36C) (32CrMoNiV5), Electroslag Remelted or Consumable Electrode Vacuum Remelted, Premium Aircraft-Quality for Bearing ApplicationsAMS6497C (Current)8/3/2026
This specification covers a nitriding grade of premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. AMS6496 and AMS6498 cover UNS K23280 with other quality levels.
AMS E Carbon and Low Alloy Steels Committee
Manganese Bronze, Sand and Centrifugal Castings, 65Cu - 24Zn - 6.2Al - 3.8Mn - 3.0Fe, High Strength, As CastAMS4862G (Current)8/3/2026
This specification covers a manganese bronze alloy in the form of sand and centrifugal castings (see 8.5).
AMS D Nonferrous Alloys Committee
Gold-Palladium-Nickel Alloy, Brazing Filler Metal, High-Temperature, 30Au - 34Pd - 36Ni, 2075 to 2130 °F (1135 to 1166 °C) Solidus-Liquidus RangeAMS4785L (Current)8/3/2026
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
Iron-Nickel Alloy, Strip, 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al (Ni-Span-C® 902), Solution Heat Treated, Cold Rolled, 50% ReductionAMS5225H (Current)8/3/2026
This specification covers an iron-nickel alloy in the form of strip 0.020 to 0.250 inch (0.51 to 6.35 mm), inclusive, in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire, 70Ni - 2.5Mn - 15.5Cr - 3.0Ti - 7.0Fe (Inconel® FM92)AMS5675K (Current)8/3/2026
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Welding Wire, 16.4Cr - 4.8Ni - 0.22Cb (Nb) - 3.6Cu, (17-4 PH), Consumable Electrode or Vacuum Induction MeltedAMS5803J (Current)8/3/2026
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Bars, Wire, Forgings, Extrusions, Rings, and Forging Stock 5.0Mn - 22Cr - 12.5Ni - 2.2Mo - 0.20Cb - 0.30N - 0.20V (SAE XM-19), Solution Heat TreatedAMS5764G (Current)8/3/2026
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, extrusions, flash-welded rings, and stock for forging, extruding, or flash-welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire, 52.5Ni - 19Cr - 3.0Mo - 5.1Cb(Nb) - 0.90Ti - 0.50Al - 18Fe (Inconel® 718), Consumable Electrode or Vacuum Induction MeltedAMS5832K (Current)8/3/2026
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Welding Wire, 12.5Cr (SAE 410)AMS5776J (Current)8/3/2026
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire, 72Ni - 15.5Cr - 1.0Cb(Nb) - 2.4Ti - 0.70Al - 7.0Fe (Inconel® FM69)AMS5778L (Current)8/3/2026
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire, 72Ni - 3.0Mn - 20Cr - 2.5Cb(Nb) (Inconel® FM82)AMS5836F (Current)8/3/2026
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
A Methodology for Assessing Inlet Swirl DistortionAIR5686 (Current)7/31/2026
This Aerospace Information Report (AIR) addresses the subject of aircraft inlet-swirl distortion. A structured methodology for characterizing steady-state swirl distortion in terms of swirl descriptors and for correlating the swirl descriptors with loss in stability pressure ratio is presented. The methodology is to be considered in conjunction with other SAE inlet distortion methodologies. In particular, the combined effects of swirl and total-pressure distortion on stability margin are considered. However, dynamic swirl, i.e., time-variant swirl, is not considered. The implementation of the swirl assessment methodology is shown through both computational and experimental examples. Different types of swirl distortion encountered in various engine installations and operations are described, and case studies which highlight the impact of swirl on engine stability are provided. Supplemental material is included in the appendices. This AIR is issued to bring together information and ideas required to address the inlet-swirl problem for which common industry practice has yet to be established. This document should foster the tests and analyses necessary to mature the ideas proposed by the committee to a recommended practice. These tests and analyses must include information that justifies three main features of the proposed swirl methodology: (1) swirl descriptors for correlating inlet swirl and stability pressure ratio loss, (2) computational techniques for analyzing compression systems (inlets, fans, compressors), and (3) test protocols (instrumentation and test techniques). The committee anticipates serving the industry by using such information to establish the consensus necessary for issuance of an SAE recommended practice.
S-16 Turbine Engine Inlet Flow Distortion Committee
FITTING, ADAPTER, REDUCER/EXPANDER, FLARED TO BOSSAS934D (Current)7/30/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
J1939 Digital AnnexJ1939DA_202607 (Current)7/30/2026
This document is intended to supplement the J1939 documents by offering the J1939 information in a form that can be sorted and searched for easier use.
Truck and Bus Control and Communications Network Committee
Valve; Air Relief, Low PressureAS8712A (Current)7/30/2026
This specification covers the requirements for one type of low-pressure relief valve for use in pressurized shipping containers.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Digital Annex of Diagnostic Trouble Code Definitions and Failure Type Byte DefinitionsJ2012DA_202607 (Current)7/29/2026
The J2012 Digital Annex of Diagnostic Trouble Code Definitions Spreadsheet provides DTC information in an excel format for use in your organization's work processes. The column headings include the same information as contained in the J2012 standard. Information in the excel spreadsheet will be updated several times annually and the spreadsheet includes a column heading denoting which DTCs have been updated in the current version.
Vehicle E E System Diagnostic Standards Committee
Across Hex Corner Dimension for Fluid Fittings and NutsARP1942B (Current)7/29/2026
This SAE Aerospace Recommended Practice (ARP) defines the minimum across hexagon corner dimensions for fluid tube fittings and nuts. The ARP covers commonly specified inch and millimeter hexagon sizes.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
TP1.6 Vehicle Diagnostic ProtocolJ3054_202607 (Current)7/29/2026
This SAE Information Report defines the diagnostic communication protocol TP1.6. This document should be used in conjunction with SAE J2534-2 in order to fully implement the communication protocol in an SAE J2534 interface. Some Volkswagen of America and Audi of America vehicles are equipped with ECU(s), in which a TP1.6 proprietary diagnostic communication protocol is implemented. The purpose of this document is to specify the requirements necessary to implement the communication protocol in an SAE J2534 interface. This SAE Information Report describes how a tester can be connected to a vehicle to perform diagnostics using the TP1.6 protocol. Details regarding ECU to ECU communication have been left out.
Vehicle E E System Diagnostic Standards Committee
FLANGE PROFILES, V-COUPLING, DESIGN STANDARDAS24563C (Current)7/28/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Hose, Air Duct, Flexible, AircraftAS8796A (Current)7/28/2026
This specification covers lightweight, circular cross-sectional flexible airduct hose, fabricated from laminated fabric reinforced plastics, or laminated fabric reinforced synthetic rubbers, to be used in aircraft air-conditioning and anti-icing systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Landing Gear Structural Health MonitoringAIR6168A (Current)7/27/2026
This SAE Aerospace Information Report (AIR) discusses past and present approaches for monitoring the landing gear structure and shock absorber (servicing), opportunities for corrosion detection, methods for transient overload detection, techniques for measuring the forces seen by the landing gear structure, and methods for determining the fatigue state of the landing gear structure. Landing gear tire condition and tire pressure monitoring are detailed in ARP6225, AIR4830, and ARP6137, respectively. Aircraft Brake Temperature Monitoring Systems (BTMS) are detailed in AS1145.
A-5 Aerospace Landing Gear Systems Committee
Plain Bearing No-Load Rotational Breakaway Torque MeasurementARP5448/5C (Current)7/24/2026
This test method provides a procedure for measuring no-load rotational breakaway torque of self-lubricating spherical bearings.
ACBG Plain Bearing Committee
BEARING, BALL, ANTI-FRICTION, AIRFRAMEAS20218C (Current)7/24/2026
ACBG Rolling Element Bearing Committee
115/200 Volt, 400 Hz Aircraft External Electrical Power Connector Contact Maintenance ProceduresAIR4365C (Current)7/23/2026
This SAE Aerospace Information Report (AIR) describes procedures for use in the field to determine if 115/200 Volt, 400 Hz aircraft external electrical power connectors are excessively worn, which may result in the inability of the external power plug to be retained, intermittent electrical performance, and arcing.
AGE-3 Aircraft Ground Support Equipment Committee
Vehicle OBD II Compliance Test Cases for SAE J1979-2/J1979-3J1699/5_202607 (Current)7/23/2026
The primary objective of this recommended practice is to confirm that vehicles can communicate a minimum set of information in accordance with diagnostic test services specified in SAE J1979-2, or the equivalent ISO 14229-1:2013 (Ed. 2) and SAE J1979-3 documents. A successful result using the SAE J1699-5 Automotive Alliance for Innovation (AAI) software for OBD-II testing indicates that the main aspects of UDS communication have been examined, but it does not provide assurance of complete compliance with all aspects of SAE J1979-2 or SAE J1979-3. SAE J1699-5 tests run with a SAE J2534 device hardware and API that is not fully compliant will result in a test failure. This specification takes precedence over all conflicts in the documents cited in this section.
Vehicle E E System Diagnostic Standards Committee
Remote Steering Control SystemsJ2588_202607 (Current)7/23/2026
This SAE Information Report establishes a uniform procedure for assuring the manufactured quality, installed utility, and performance of automotive remote steering controls other than those provided by the vehicle manufacturer (OEM). These products are intended to provide driving capability to persons with physical disabilities. The adaptive modifications seek to compensate for lost or reduced function in the extremities of the driver with a disability. Remote steering controls are designed to provide a steering input device alternative to the OEM steering wheel that either reduces the required input force, changes the required range of motion or changes the location of the steering control, or any combination of the above. These controls supplement by power, other than by the driver’s own muscular efforts, the force output of the driver with a disability. Because this is an Information Report, the numerical values for performance measurements presented in this report and in the accompanying Test Procedure, while based upon the best knowledge available at the time, have not been validated by a testing of the Test Procedure.
Adaptive Devices Standards Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Plate, 54Ni - 22Cr - 12.5Co - 9.0Mo - 1.2Al (Alloy 617), Consumable Electrode or Vacuum Induction Melted, AnnealedAMS5888E (Current)7/23/2026
This specification covers a corrosion- and heat-resistant nickel alloy in the form of plate nominally 2.00 inches (50.8 mm) and under in thickness, inclusive.
AMS F Corrosion and Heat Resistant Alloys Committee
NOx Tracking Parameter AccuracyJ3349_202607 (Current)7/23/2026
This SAE Information Report provides SAE’s recommendations for meeting the requirements for Real Emissions Assessment Logging (REAL) oxides of nitrogen (NOx) accuracy demonstration and for the implementation of REAL NOx binning requirements as defined in onboard diagnostics (OBD) regulations 13 CCR 1971.1 and 13 CCR 1968.2.
Vehicle E E System Diagnostic Standards Committee
Cobalt Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings, 40Co - 22Cr - 22Ni - 14.5W - 0.07La (HS188), Solution Heat TreatedAMS5772G (Current)7/22/2026
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of bars, forgings, flash-welded rings, and stock for forging or flash-welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Gold Wire and Ribbon, 99.97Au, AnnealedAMS7731E (Current)7/22/2026
This specification covers pure gold in the form of wire 0.005 to 0.040 inch (0.012 to 1.000 mm), inclusive, in nominal diameter and ribbon 0.002 to 0.051 inch (0.05 to 1.28 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
Heat Treatment, Precipitation-Hardening Corrosion-Resistant, Maraging, and Secondary Hardening Steel PartsAMS2759/3K (Current)7/21/2026
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of precipitation-hardening corrosion-resistant, maraging, and secondary hardening steel parts. Parts are defined in AMS2759. Parts made from steels other than those specified in this specification may be heat treated in accordance with the applicable requirements herein using processing temperatures, times, and other parameters recommended by the material producer unless otherwise specified by the cognizant engineering organization. General ordering instructions are specified in AMS2759.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate, 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B (Waspaloy), Consumable Electrode or Vacuum Induction Melted, AnnealedAMS5544M (Current)7/21/2026
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Sheet, Strip, and Plate, 15Cr - 6.5Ni - 0.75Mo - 0.60Cb - 1.5Cu (Custom 450®), Solution Heat Treated, Precipitation HardenableAMS5863G (Current)7/21/2026
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Filler Pipes and Openings of Motor Vehicle Fuel TanksJ1140_202607 (Current)7/21/2026
This SAE Recommended Practice was developed primarily for gasoline-powered passenger car and truck applications to interface vapor recovery systems, but it may be used in diesel, marine, industrial, and similar applications where a nozzle is required for filling. The zones cover nozzle spout access and handle clearance to a refilling port. In addition, this recommended practice includes a design window for nozzle manufacturers to develop with.
Fuel Systems Standards Committee
Definition and Introduction of Digital Mesh/Digital Fabric FrameworkAIR8614 (Current)7/21/2026
The proposed Digital Mesh/Fabric concept builds upon the Digital Thread Framework (refer to AIR7161) by representing the interconnection of multiple digital threads across multiple data stores, logical organizing segments, and product life-cycle stages. Unlike a single digital thread, which follows a linear or sequential flow of data utilization through a product life cycle, the Digital Mesh/Fabric forms a complex mesh of n-dimensional interconnected digital threads, allowing for greater value creation, flexibility in data utilization, scalability, and integration.
G-31 Digital Transactions for Aerospace
Adapter, Closed-Circuit Fuel Servicing - StandardizationAS6848 (Current)7/21/2026
The Adapter Receiver specified herein has no classification. No distinction is made between commercial or military use.
AE-5C Aviation Ground Fueling Systems Committee
BEARINGS, PLAIN, SELF-LUBRICATING SELF-ALIGNING, HIGH SPEED OSCILLATION -65 TO +160 °FAS81819/1B (Current)7/21/2026
ACBG Plain Bearing Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Seamless Tubing, 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe (HASTELLOY® X), Solution Heat TreatedAMS5587H (Current)7/21/2026
This specification covers a corrosion- and heat-resistant nickel alloy in the form of seamless tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, DRILLED, CLOSE TOL SHANK, AMS5643 (UNS S17400), 140 KSI, .1900-32 UNJF-3AAS3174C (Current)7/21/2026
E-25 General Standards for Aerospace and Propulsion Systems
CRIMPING TOOLS, TYPE 1, HAND OR POWER ACTUATED, WIRE TERMINATION, PNEUMATIC TOOL FOR AS22520/1 POSITIONERS, CONTACT WIRE BARREL SIZES 12 THRU 20AS22520/29A (Current)7/21/2026
AE-8C2 Terminating Devices and Tooling Committee
Steel, Corrosion-Resistant, Investment Castings, 13Cr (Alloy 60416), Free Machining; Hardened and TemperedAMS5349G (Current)7/21/2026
This specification covers a corrosion-resistant steel in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Copper-Beryllium Alloy (Copper Alloy Numbers C17500 and C17510), StripAS81021C (Current)7/20/2026
This specification covers the requirements for the acquisition of two alloys of copper-beryllium alloy strip, having higher electrical conductivity than copper-beryllium alloy strip normally used (see 6.1). All sizes of strip are covered by this specification.
AMS D Nonferrous Alloys Committee
Plain Bearing Wear MeasurementARP5448/7A (Current)7/20/2026
This standard details two methods of inspecting PTFE lined spherical or journal bearing wear outside the test apparatus. The methods described herein are applicable only to bearings which were unidirectionally loaded and the area of sliding wear is known and held constant throughout the dynamic test. The two methods described are: a Destructive Inspection - Cut and measure (not applicable to molded liners) b Nondestructive Inspection - Radial play (gauge) measurement
ACBG Plain Bearing Committee
Steel, Corrosion- and Heat-Resistant, Bars, Forgings, and Forging Stock, 16.5Cr - 4.5Ni - 2.9Mo - 0.10N (AM 350®), Consumable Electrode Remelted, Equalized and Over-TemperedAMS5745H (Current)7/20/2026
This specification covers a corrosion- and heat-resistant steel in the form of bars, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Thermal Effectiveness of Sleeve/Tubing/Tape InsulationJ2302_202607 (Current)7/20/2026
This procedure measures the resistance to radiant heat flow of insulating materials in sleeve, tubing, or tape (collectively referred to as “sleeve”) form. The sleeve’s effectiveness (SE) is determined by measuring the difference in surface temperature of a flat black, single-diameter ceramic cylinder with and without the standard diameter sleeve at the specified temperature, position, and distance from the radiant heat source.
Harness Covering Standards Committee
Manufacturers’ Identification of Aerospace Electrical and Electronic Wiring Devices and AccessoriesAIR1351L (Current)7/20/2026
This SAE Aerospace Information Report (AIR) covers the general requirements for, and the listing of, manufacturers’ identification markings, names, symbols or trademarks, and CAGE codes that appear on electrical and electronic wiring devices and accessories as required by individual product specifications. Supplier markings from previous submitted listings are maintained for component traceability.
AE-8C2 Terminating Devices and Tooling Committee
Coating, Thermal Spray, High Velocity Oxygen/Fuel ProcessAMS2447E (Current)7/20/2026
This specification covers the requirements for thermal spray coatings applied using the high velocity oxygen fuel (HVOF) combustion process. This specification is not intended to be used for duplex coatings, i.e., the application of the coating over a previously applied coating.
AMS B Finishes Processes and Fluids Committee
Rotary Flap Peening of Metal PartsAMS2590D (Current)7/20/2026
This specification covers procedures and requirements for peening of metal parts with portable, bonded-shot, rotary flap assemblies in accordance with AS2592. The principles of rotary flap peening are similar to conventional shot peening, except conversion of arc height values using the magnetic test Almen strip holder is required for intensity determination.
AMS B Finishes Processes and Fluids Committee
FITTING, ADAPTER, BULKHEAD, EXTERNAL THREAD, BEAM SEAL TO INTEGRAL WELD RINGAS4229D (Current)7/20/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Endurance Time Test Procedures for SAE Type II/III/IV Aircraft Deicing/Anti-icing FluidsARP5485C (Current)7/20/2026
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide the sample selection and endurance time test procedures for SAE Type II, III, and IV aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G-12 Holdover Time Committee. The related standard ARP5718 provides the process by which endurance time data is converted to holdover times for publication by regulators and subsequent use by aircraft operators.
G-12HOT Holdover Time Committee
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