Standards - SAE Mobilus

SAE standards are internationally recognized as some of the most trusted collections of scientific data to globally optimize the processes, practices, and products that advance technology in our industry and are vital to ensure safety, quality, and reliability. Over 40,000+ current documents available within the aerospace, automotive, and commercial vehicle industries.

Items (50,720)

Forgings, Magnesium Alloy, 5.5Zn - 0.45Zr (ZK60A-T5), Precipitation Heat Treated

AMS4362J (Current)

8/18/2026

This specification covers a magnesium alloy in the form of die forgings 3 inches (76 mm) and under in nominal thickness at time of heat treatment, hand forgings 6 inches (152 mm) and under in nominal thickness, and forging stock of any size (see 8.5).

AMS D Nonferrous Alloys Committee

Steel, Corrosion-Resistant, Sheet, Strip, and Plate, 17Cr (SAE 430), Annealed

AMS5503H (Current)

8/18/2026

This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.

AMS F Corrosion and Heat Resistant Alloys Committee

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, NICKEL ALLOY, UNS N07718, 185 KSI MIN, .3125-24 UNJF-3A

AS3245E (Current)

8/18/2026

E-25 General Standards for Aerospace and Propulsion Systems

FITTING, TEE, STANDARD AND REDUCER, FLARELESS

AS1005J (Current)

8/18/2026

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

WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED CROSSLINKED MODIFIED ETFE, LOW FLUORIDE, NORMAL WEIGHT, 80 MICROINCH SILVER-COATED COPPER 200 °C, 600 VOLT, ROHS

AS22759/50C (Current)

8/18/2026

AE-8D Wire and Cable Committee

WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, CROSSLINKED MODIFIED ETFE, LOW FLUORIDE, LIGHTWEIGHT, 80 MICROINCH SILVER-COATED HIGH-STRENGTH COPPER ALLOY, 200 °C, 600 VOLT, ROHS

AS22759/47C (Current)

8/18/2026

AE-8D Wire and Cable Committee

BOLT, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUM PLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD, UNS K14675, 195 KSI MIN, .2500-28 UNJF-3A

AS9209D (Current)

8/18/2026

E-25 General Standards for Aerospace and Propulsion Systems

BOLT, MACHINE-DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, CORROSION RESISTANT STEEL (UNS S17400), 140 KSI UTS MIN, .2500-28, UNJF-3A

AS3168C (Current)

8/18/2026

E-25 General Standards for Aerospace and Propulsion Systems

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, FULL SHANK, STEEL AMS6322, CADMIUM PLATED, .250-28 UNJF-3A

AS9933C (Current)

8/18/2026

E-25 General Standards for Aerospace and Propulsion Systems

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CORROSION AND HEAT RESISTANT NICKEL ALLOY (UNS N07001), 165 KSI MIN, .3750-24 UNJF-3A

AS9699D (Current)

8/18/2026

E-25 General Standards for Aerospace and Propulsion Systems

Plain Bearing Radial Limit and Ultimate Load Tests

ARP5448/1B (Current)

8/18/2026

This test method outlines the recommended procedure for performing radial limit load and ultimate load tests on low-speed airframe and high-speed helicopter rotor head bearings.

ACBG Plain Bearing Committee

Unshielded High Voltage Primary Cable

J1654_202608 (Current)

8/18/2026

This SAE Standard covers unshielded cable, 22 gauge and larger, intended for use at a nominal system voltage up to 600 V or 1000 V (ACrms or DC). It is intended for use in surface vehicle electrical systems.

Cable Standards Committee

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, STEEL AMS6322, CADMIUM PLATED, .190-32 UNJF-3A

AS9914C (Current)

8/18/2026

E-25 General Standards for Aerospace and Propulsion Systems

Steel, Corrosion- and Heat-Resistant, Forgings and Forging Stock, 12.5Cr (SAE 410), Enhanced Fracture Toughness, Annealed

AMS5867D (Current)

8/17/2026

This specification covers a corrosion- and heat-resistant steel in the form of forgings and forging stock.

AMS F Corrosion and Heat Resistant Alloys Committee

CLAMP, LOOP TYPE, CUSHIONED SUPPORT

AS21919E (Current)

8/17/2026

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

BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), .4375-20, UNJF-3A

AS3171C (Current)

8/17/2026

E-25 General Standards for Aerospace and Propulsion Systems

BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), 140 KSI, .5000-20, UNJF-3A

AS3172C (Current)

8/17/2026

E-25 General Standards for Aerospace and Propulsion Systems

Chemical Process Test Specimen Material

AS2390B (Current)

8/17/2026

This standard establishes definitions, guidelines, and requirements governing materials (e.g., alloy and heat-treat condition) allowed for use in chemical process test specimens when requirements call for a generic class of alloy.

AMS B Finishes Processes and Fluids Committee

BOLT, MACHINE - DOUBLE HEX, EXTENDED WASHER HD, PD SHANK, CUP WASHER LOCKED, CADMIUM PLATED, STEEL, UNS G87400, 125 KSI MIN, .2500-28 UNJF-3A

AS9681C (Current)

8/17/2026

E-25 General Standards for Aerospace and Propulsion Systems

WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED CROSSLINKED MODIFIED ETFE, LOW FLUORIDE, LIGHTWEIGHT, 80 MICROINCH SILVER-COATED COPPER, 200 °C, 600 VOLT, ROHS

AS22759/48C (Current)

8/17/2026

AE-8D Wire and Cable Committee

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, UNS S66286, 130 KSI, .3125-24 UNJF-3A

AS9112D (Current)

8/17/2026

E-25 General Standards for Aerospace and Propulsion Systems

User’s Guide to AMS Specifications

AIR4779E (Current)

8/17/2026

The scope of this SAE Aerospace Information Report (AIR) is to explain the functions of the various sections of the specifications, why some of the terms in AMS specifications are used, and how the specification system works. Starting with Section 4 of this document, the topics are presented in the order they usually appear in AMS specifications.

Aerospace Materials Systems Group

BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, CORROSION-RESISTANT STEEL (UNS S17400), 140KSI UTS MIN, .3125-24, UNJF-3A

AS3169C (Current)

8/17/2026

E-25 General Standards for Aerospace and Propulsion Systems

BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), . 3750-24, UNJF-3A

AS3170C (Current)

8/17/2026

E-25 General Standards for Aerospace and Propulsion Systems

BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, CORROSION-RESISTANT STEEL (UNS S17400), 140 KSI UTS MIN, .1900-32, UNJF-3A

AS3167C (Current)

8/15/2026

E-25 General Standards for Aerospace and Propulsion Systems

Safety Assessment of Transport Airplanes in Commercial Service

ARP5150B (Current)

8/15/2026

This document describes guidelines, methods, and tools used to perform the ongoing safety assessment process for transport airplanes in commercial service (hereafter termed “airplane”). The process described herein is intended to support an overall management of safety. It is associated with showing compliance to regulations and also establishing and meeting internal company safety standards. The methods identify a systematic means, but not the only means, to assess ongoing safety. While economic decision-making is an integral part of the safety management process, this document addresses only the ongoing safety assessment process. To put it succinctly, this document addresses the “Is it safe?” part of safety management; it does not address the “How much does it cost?” part of safety management. This document also does not address any specific organizational structures for accomplishing the safety assessment process. While the nature of the organizational structure is significant to the quality of a safety program, this document focuses on the functions to be accomplished and does not attempt to define what the structure should be. The intent is to leave the greatest amount of flexibility to the organizations that use this document.

S-18C Ongoing Safety Assessment Committee

Vehicle OBD II Compliance Test Cases

J1699/3_202608 (Current)

8/15/2026

The main purpose of this SAE Recommended Practice is to verify that vehicles are capable of communicating a minimum subset of information in accordance with the diagnostic test services specified in SAE J1979, or the equivalent document ISO 15031-5. Any software meeting these specifications will utilize the vehicle interface that is defined in SAE J2534. SAE J1699-3 tests shall be run using an SAE J2534-1 (API Version 04.04) Interface. However, the use of an SAE J2534-2 (API Version 04.04) Interface shall be permitted if the following conditions are met: The number of 29-bit ISO 15765 OBD ECUs exceeds the capability of the SAE J2534-1 Interface. The SAE J2534-2 Interface meets or exceeds all of the SAE J2534-1 requirements and also supports the SAE J2534-2 feature “Mixed Format Frames on a CAN Network.”

Vehicle E E System Diagnostic Standards Committee

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CORROSION AND HEAT RESISTANT STEEL, UNS S66286, UTS 130 KSI MIN, .3750-24 UNJF-3A

AS9559F (Current)

8/15/2026

E-25 General Standards for Aerospace and Propulsion Systems

Standard Test Method for Aerodynamic Acceptance of AMS1424 and AMS1428 Aircraft Deicing/Anti-Icing Fluids

AS5900F (Current)

8/14/2026

This SAE Aerospace Standard (AS) establishes the aerodynamic flowoff requirements and test procedures for AMS1424 Type I and AMS1428 Type II, III, and IV fluids used to deice and/or anti-ice aircraft. The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/anti-icing fluids as they flow off of aircraft lifting and control surfaces during the takeoff ground acceleration and climb. Aerodynamic acceptance of an aircraft ground deicing/anti-icing fluid is based upon the fluid’s boundary layer displacement thickness (BLDT) on a flat plate, measured after experiencing the free stream velocity time history of a representative aircraft takeoff. Acceptability of the fluid is determined by comparing BLDT measurements of the candidate fluid with a datum established from the values of a reference fluid BLDT and the BLDT over the dry (clean) test plate. Testing is carried out in the temperature range at which the fluid, undiluted and diluted, is to be used in aircraft service. NOTE: No additional aerodynamic testing is required for non-glycol fluids at this time. For more information about non-glycol fluids, please refer to AMS1424 and AMS1428.

G-12ADF Aircraft Deicing Fluids

CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR MIL-DTL-28840 CONNECTORS)

AS39029/84C (Current)

8/14/2026

AE-8C1 Connectors Committee

SCREW, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUM PLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD, UNS K14675, 195 KSI MIN, .1640-36 UNJF-3A

AS9207D (Current)

8/14/2026

E-25 General Standards for Aerospace and Propulsion Systems

STRIP, MOUNTING, NUT INSULATING, FOR AS27212 TERMINAL BOARD

AS33731B (Current)

8/14/2026

AE-8C2 Terminating Devices and Tooling Committee

Steel Corrosion-Resistant Investment Castings, Vacuum Melted, Vacuum Cast, 13Cr - 8.0Ni - 2.2Mo - 1.1Al (PH 13-8 Mo), Homogenized, Solution, and Precipitation Heat Treated (Condition H1000)

AMS5412C (Current)

8/14/2026

This specification covers a corrosion-resistant steel in the form of investment castings.

AMS F Corrosion and Heat Resistant Alloys Committee

Rings, Flash-Welded, Aluminum and Aluminum Alloys

AMS7488H (Current)

8/14/2026

This specification covers flash-welded rings made of aluminum and aluminum alloys (see 8.5).

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si - 0.90Cu - 0.60Mn - 0.90Mg Solution Heat Treated and Naturally Aged

AMS4405D (Current)

8/14/2026

This specification covers an aluminum alloy procured in the form of sheet 0.078 to 0.197 inch (2.00 to 5.00 mm), inclusive, in nominal thickness, Alclad on both sides (see 8.5).

AMS D Nonferrous Alloys Committee

TERMINAL BOARD ASSEMBLY, MOLDED-IN-STUD, ELECTRIC

AS27212F (Current)

8/14/2026

AE-8C2 Terminating Devices and Tooling Committee

Perspectives on Integrating Structural Health Monitoring Systems into Fixed-Wing Military Aircraft

AIR6245A (Current)

8/11/2026

This SAE Aerospace Information Report (AIR) is prepared for stakeholders seeking information about the evolution, integration, and approval of SHM technologies for military aircraft systems. The report provides this information in the form of (a) two military organizations’ perspectives on requirements, and (b) general SHM challenges and industry perspectives. The report only provides information to generate awarness of prespectives for military aircraft and, hence, assists those who are involved in developing SHM systems understanding the broad range of regulations, requirements, and standards published by military organizations that are available in the public domain from the military organizations.

Aerospace Industry Steering Committee on Structural Health

Steel, Corrosion-Resistant, Wire, 17Cr - 7.1NI - 1.1Al (17-7 PH®), Cold Drawn, Precipitation-Hardenable

AMS5678H (Current)

8/10/2026

This specification covers a corrosion-resistant steel in the form of wire 0.007 to 0.625 inch (0.18 to 15.88 mm), inclusive, in nominal diameter, cold drawn to Condition C, and capable of being precipitation heat treated to Condition CH900.

AMS F Corrosion and Heat Resistant Alloys Committee

Gaining Approval for Seats with Integrated Electronics in Accordance with AC 21-49 Section 7.b

ARP6448C (Current)

8/10/2026

This SAE Aerospace Recommended Practice (ARP) provides a framework for establishing methods and stakeholder responsibilities to ensure that seats with integrated electronic components (e.g., actuation system, reading light, inflatable restraint, in-flight entertainment equipment, etc.) meet the seat technical standard order (TSO) minimum performance standards (MPS). These agreements will allow seat suppliers to build and ship TSO-approved seats with integrated electronic components. The document presents the roles and accountabilities of the electronics manufacturer (EM), the seat supplier, and the TC/ATC/STC applicant/holder in the context of AC 21-49, Section 7.b (“Type Certification Using TSO-Approved Seat with Electronic Components Defined in TSO Design”). This document applies to all FAA seat TSOs C39( ), C127( ), etc. The document defines the roles and responsibilities of each party involved in the procurement of electronics, their integration on a TSO-approved seat, and the seat’s installation on an aircraft. Requirements for design and quality control and the methods for communicating design and change data between EMs and seat suppliers are defined such that standardization is possible across the industry to ensure continued airworthiness of TSO-approved seats with integrated electronic components. This document primarily focuses on correspondence between the seat supplier and the EM. Appendix A: Presents key characteristics of electronic components and guidance on how changes are classified per the requirements of Table 1 of AC 21-49. Appendix B: Provides an outline of a typical data approval process and the change management process between EMs and seat suppliers. Appendix C: While the responsibility rests solely with the seat supplier to ensure all TSO attributes identified in Table 1 of AC 21-49 are acceptable, Appendix C has been included to outline the process for delegating EMs authorization to assess the impact of changes on their equipment with respect to seat TSO attributes. This authorization will allow the classification of the change and the appropriate administration of the change by the EM via seat supplier delegation. Appendix D: Given the mix of business arrangements that can exist in the seat, in-flight, and aircraft procurement life cycle (buyer-furnished equipment, supplier-furnished equipment, customer-furnished equipment), there is discussion on the potential need for separate agreements between the EMs and seat suppliers to ensure binding flow down of design and quality control requirements. As such, a working together agreement (WTA) template is provided as Appendix D.

Aircraft Seat Committee

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 0 - Introduction

AMS3970B (Current)

8/10/2026

This document (Technical Specification) gives information about qualification rules and the relation between the different specification parts involved, such as the Technical Specification (TS), Material Specification (MS), and Purchasing Specification (PS). The link to the material qualification and qualified products is presented.

AMS CACRC Commercial Aircraft Composite Repair Committee