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CRIMP TOOLS, TYPE 1, TERMINAL, HAND OR POWER ACTUATED, WIRE TERMINATION, PNEUMATIC TOOL FOR WIRE BARREL SIZES 8 THROUGH 0000AS22520/23C (Current)
SCOPE IS UNAVAILABLE.
AE-8C2 Terminating Devices and Tooling Committee
INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, TYPE II, CLASS 1, COMPOSITION CAS81969/19B (Current)
SCOPE IS UNAVAILABLE.
AE-8C2 Terminating Devices and Tooling Committee
Test Document 314TESTMARCH14 (Current)
scope
G-41 Reliability
11012024-new-air110124-new-air (Current)
11012024-new-air
A-6 Aerospace Actuation, Control and Fluid Power Systems
ARP4754B Clarification NoticeAIR070226 (Current)7/2/2026
The purpose of this AIR is to provide additional information on some areas of ARP4754B/ED-79B that may need additional clarification in order to be put into practice. This document should be used in conjunction with ARP4754B/ED-79B. The contents are recommendations and should not be construed to be regulatory requirements. This document may be revised with additional information as ARP4754B/ED-79B is put into practice.
A-20 Aircraft Lighting Steering Committee
Procedure and Instrumentation for Measuring Acoustic Impulses from Deployment of Automotive Inflatable DevicesJ247_201304 (Current)4/3/2013
The purpose of this SAE Recommended Practice is to provide guidelines for selection of transducers, data acquisition systems, and other instrumentation as well as analysis methods to help ensure proper measurement and evaluation of acoustic impulses in automobiles. While this Recommended Practice focuses on automotive inflatable devices, such as, frontal airbag systems, pretensioners, inflatable curtains, side airbags, etc., it can be used for measurement of other impulsive sounds in a vehicle if needed. The objective is to achieve uniformity in instrumentation practice and reporting of test measurements. Use of this recommended practice should provide a basis for meaningful comparisons of test results from different sources. This recommended practice specifies procedures for static measurement of acoustic impulses, but due to the much more complicated nature of crash testing, does not specify procedures for measuring impulses in vehicles during crash tests.
Inflatable Restraints Committee
Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35,000 kPa), 400°F (204°C), Aircraft Hydraulic Systems (Supplement 1)..AS5960SUP1 (Current)9/24/2012
This supplement forms a part of the Aerospace Standard AS5960, Hose Assembly, Polytrafluoroethyloene, Metallic Braid Reinforced, 5080 psi (35,000 kPa), 400°F (204°C), Aircraft Hydraulic Systems, and shall be used to identify hose assembly standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Guidelines for Laboratory Cyclic Corrosion Test Procedures for Painted Automotive PartsJ1563_201604 (Current)4/5/2016
These guidelines are intended for those engineers and scientists who evaluate the corrosion performance of painted automotive parts in laboratory cyclic tests. The guidelines are intended to help ensure that the results of the tests can be used to reach conclusions concerning the variables under study without being confounded by the test procedure itself. The guidelines also serve as a means to assist users of this type of test in obtaining good inter-laboratory agreement of results.
Materials, Processes and Parts Council
Hard Anodic Coating on Aluminum and Aluminum AlloysAMS2469J (Current)12/8/2025
This specification establishes the requirements for a hard anodic coating on aluminum and aluminum alloys.
AMS B Finishes Processes and Fluids Committee
Arinc Automation Document - Standard Information Report - PageCount 151 - 209 KJH006 (Current)12/19/2024
Arinc Automation Document - Standard Information Report - PageCount 151 - 209
Aviation Maintenance Committee
TUBE BENDING RADIUSAS130A (Current)1/2/2013
This standard establishes basic design criteria including preferred bend radii, straight lengths between bends, flattening and surface conditions in the bend area. Also included is a table of preferred tubing sizes and wall thicknesses and a formula for determining a minimum bend radius for a given tube diameter.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
J1939 Digital AnnexJ1939DA_201402 (Current)12/8/2025
The J1939 Digital Annex The J1939 Digital Annex, introduced in August 2013, offers key J1939 technical data in an Electronic Spreadsheet that can be easily searched, sorted, and adapted to other formats. J1939DA contains all of the SPNs (parameters), PGNs (messages), and other J1939 data previously published in the SAE J1939 top level document. J1939DA also contains all of the SLOTs, Manufacturer ID Codes, NAME Functions, and Preferred Addresses previously published in the SAE J1939 top level and the J1939-71 document. J1939DA contains the complete technical details for all of the SPNs and PGNs previously published in the SAE J1939-71 document. For all other SPNs and PGNs which are published in a document other than SAE J1939-71, J1939DA lists only basic details along with a reference to the document that contains the complete technical details. J1939DA replaces, and expands upon, the 1939 Companion Spreadsheet (CS1939), which was last published through November 2012. The data fields
Truck Bus Control and Communications Network Committee
Arinc Automation Document - Standard Specificiation - PageCount Greater than 475KJH008 (Current)12/19/2024
Arinc Automation Document - Standard Specificiation - PageCount Greater than 475
Airlines Electronic Engineering Committee
Appendix C Electronic Display Symbology for Engine DisplaysARP4102/7_APXC (Current)7/10/2007
S-7 Flight Deck Handling Qualities Stds for Trans Aircraft
Dedicated Short Range Communications (DSRC) Performance Requirements for V2V Safety AwarenessJ2945/2_202606 (Current)6/25/2026
This SAE Document specifies DSRC interface requirements for V2V Safety Awareness applications, including detailed Systems Engineering documentation (needs and requirements mapped to appropriate message exchanges). These applications include: Emergency Vehicle Alert, Roadside Alert, and Safety Awareness Alerts for Objects and Adverse Road Conditions. This document extends the V2V Communications capabilities defined in J2945/1 to support these applications, and the National ITS Architecture. The purpose of this SAE Document is to enable interoperability for V2V Safety Awareness communications.
V2X Vehicular Applications Technical Committee
Test Method for Measuring Wet Color Transfer CharacteristicsJ1326_202606 (Current)6/25/2026
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
Terminology and Measurement Methodology for Determining Vehicle Overlap in Offset-Frontal CrashesJ3227_202606 (Current)6/25/2026
This SAE Information Report establishes procedures and terminology for measuring, calculating, and referencing the percent vehicle overlap for a case vehicle in real-world or staged end plane collisions where the end plane of the case vehicle is engaged at one of the two bumper corners but not both. This SAE Information Report may be applied to rear or front plane impacts.
Data Collection and Archiving Standards Committee
Airborne Icing TankersARP5904A (Current)6/26/2026
This SAE Aerospace Recommended Practice (ARP) document establishes criteria and recommended practices for the use of airborne icing tankers to aid in design and certification of aircraft ice protection systems and components. Several icing tankers are described, along with their capabilities and suggested use. Sample data for these tanker spray systems are included, shown with 14 CFR Parts 25 and 29, Appendix C icing envelopes for continuous maximum and intermittent maximum icing conditions. (Note: In the remainder of this document, the phrase “Appendix C icing envelopes” will be used for brevity.) This ARP is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances.
AC-9C Aircraft Icing Technology Committee
Method of Measuring and Reporting the Pressure Differential Flow Characteristics of a Hydraulic Fluid Power ValveJ1117_202606 (Current)6/26/2026
Applies to hydraulic fluid power valves as applied to Off-Road Self-Propelled Work Machines defined in SAE J1116.
CTTC C1, Hydraulic Systems
Digital Standards TEST w/Standards/SupplementSAE-SUP-TEST12 (Current)3/27/2026
Chose Standards and Supplement instead of Media/Software.
Plain Bearing Selection for Landing Gear ApplicationsAIR1594E (Current)11/11/2025
This document is intended to give advisory information for the selection of plain bearings and bearing materials most suitable for aircraft landing gear applications. Information included herein was derived from bearing tests and service experience/reports. Airframe/landing gear manufacturers, commercial airlines, the U.S. Air Force and Naval Air Systems Command provided input for the document. Information is given on bearing installation methods and fits that have given satisfactory performance and service life. Base metal corrosion is a major cause of problems in bearing installations for landing gears. Therefore, methods of corrosion prevention are discussed. Effort is directed toward minimizing maintenance and maximizing life expectancy of landing gear bearings. Lubricated and self-lubricating bearings are also discussed. There are wide ranges of bearing load and motion requirements for applications in aircraft landing gears. For this reason, it is the responsibility of the
A-5B Gears, Struts and Couplings Committee NEW Name Goes Her
Ship Systems and Equipment - Hydraulic Systems - Noise ControlJ1782_201305 (Current)5/31/2013
Hydraulic systems are used on marine vehicles for steering, vehicle control, and utility services. System components that generate and transmit noise are of concern. This SAE Information Report (a) addresses noise requirements which may apply to the hydraulic systems of ships and submersibles, and (b) identifies noise sources and techniques which may be used to reduce system noise. Noise of power sources (e.g., electric motors) and end items (e.g., steering linkages) is beyond the scope of this document.
Ship Fluid Systems Committee
Lubricants, Industrial Oils, and Related Products - Type X (Greases) - SpecificationMS1011_201808 (Current)8/29/2018
The greases have been classified according to the operating conditions under which they are used, because the versatile nature of greases makes it impractical to classify them according to end use. It will therefore be necessary to consult the supplier to be certain that the grease can be used in; for example, rolling bearings or pumped supply systems, and also concerning the compatibility of products (see Remarks in Table 1).
Fuel and Lubricants TC2 Industrial Lubricants
Crack Initiation and Growth Considerations for Landing Gear Steel With Emphasis on Aermet 100AIR5052C (Current)11/10/2025
Steel alloys, such as AF1410 (AMS 6527, UNS K92571) and AerMet 100 (AMS 6532), have been developed which have improved Fracture Toughness characteristics compared to the current landing gear steel alloy, 300M (AMS 6419 and AMS 6257, MIL-S-8844, UNS K44220). The 300M steel is the most widely used material in current landing gear designs. It has been successfully used in thousands of applications. The use of the 300M material necessitates a safe life design criterion where components are retired after on-fourth to one-sixth the laboratory test life. This criterion was established in part due to the relative low fracture toughness of low-alloy steel in the 260 to 300 ksi strength range. The high fracture tough alloys give comparable strength levels with an increase in fracture toughness and better resistance to stress corrosion cracking. These alloys may make possible the consideration of new procedures for operation, maintenance, and inspection. For the present, these materials in the
A-5B Gears, Struts and Couplings Committee NEW Name Goes Her
GV WIP TestJA99990_202606 (Current)6/22/2026
GV WIP Test Scope
A-6 Aerospace Actuation, Control and Fluid Power Systems
Interior DoorsARP499D (Current)6/25/2026
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide recommendations which will lead to the standardization of interior door design and operation in all transport aircraft. Interior doors are broadly classified into two main categories which include egress path doors and non-egress path doors. The scope of this ARP does not include crew rest doors, secondary barriers to the flight deck, or doors incorporated in furniture surrounding passenger seats as defined in AS6960.
S-9B Cabin Interiors and Furnishings Committee
Potential Failure Mode and Effects Analysis (FMEA) Including Design FMEA, Supplemental FMEA-MSR, and Process FMEAJ1739_202606 (Current)6/25/2026
This FMEA standard describes potential failure mode and effects analysis in design (DFMEA), supplemental FMEA-MSR, and potential failure mode and effects analysis in manufacturing and assembly processes (PFMEA). It assists users in the identification and mitigation of risk by providing appropriate terms, requirements, rating charts, and worksheets. As a standard, this document contains requirements—”must”—and recommendations—”should”—to guide the user through the FMEA process. The FMEA process and documentation must comply with this standard as well as any corporate policy concerning this standard. Documented rationale and agreement with the customer are necessary for deviations in order to justify new work or changed methods during customer or third-party audit reviews.
Automotive Quality and Process Improvement Committee
Combination Tail and Floodlamp for Agricultural EquipmentJ976_202606 (Current)6/16/2026
test
Agricultural Tractor Standards Committee (ATSC)
Provisions of Medical Oxygen for Aircraft OccupantsCODE234 (Current)6/26/2026
This document provides information on provisions for passengers with disabilities on board commercial aircraft. In this context the term "provision of medical oxygen" shall be understood as application of oxygen on board an aircraft not linked to (post) decompression in the sense of Airworthiness Requirements FAR/CS 25 and Operational Regulations of FAR 121/135. Information about available equipment and physiological treatment in clinical practice will be provided in this document. It covers the use of oxygen concentrators according to guidance of FAR Advisory Circular AC120-95.
A-20C Interior Lighting - Test
Road Vehicles - Cybersecurity EngineeringISO/SAE21434 (Current)8/31/2021
This document specifies engineering requirements for cybersecurity risk management regarding concept, product development, production, operation, maintenance and decommissioning of electrical and electronic (E/E) systems in road vehicles, including their components and interfaces. A framework is defined that includes requirements for cybersecurity processes and a common language for communicating and managing cybersecurity risk. This document is applicable to series production road vehicle E/E systems, including their components and interfaces, whose development or modification began after the publication of this document. This document does not prescribe specific technology or solutions related to cybersecurity.
Vehicle Cybersecurity Systems Engineering Committee
Technical Publications for Agricultural EquipmentJ1035_202606 (Current)6/16/2026
test
Agricultural Tractor Standards Committee (ATSC)
Fuel Cell Vehicle TerminologyARP5265D (Current)6/18/2026
This SAE Information Report contains definitions for hydrogen fuel cell powered vehicle terminology. It is intended that this document be a resource for those writing other hydrogen fuel cell vehicle documents, specifically, Standards or Recommended Practices.
A-5C Aircraft Tires Committee
Steel Bars, Forgings, and Tubing 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) AMS6312L (Current)11/25/2025
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Fuel Cell Vehicle TerminologyUSCAR47-1 (Current)6/18/2026
This SAE Information Report contains definitions for hydrogen fuel cell powered vehicle terminology. It is intended that this document be a resource for those writing other hydrogen fuel cell vehicle documents, specifically, Standards or Recommended Practices.
USCAR
System Validation & Verification Plan Template - ARP4754A - AFuzionARP4754A_PL_009 (Current)To be published on 08/13/2201
BULKHEAD BRACKET FOR USE WITH MS3367 PLASTIC TIEDOWN STRAPSAS33401B (Current)5/14/2026
SCOPE IS UNAVAILABLE.
AE-8C2 Terminating Devices and Tooling Committee
Quality Management Systems - Requirements for Aviation, Space, and Defense OrganizationsAS9100D (Current)12/8/2025
This standard includes ISO 9001:20152 quality management system requirements and specifies additional aviation, space, and defense industry requirements, definitions, and notes. It is emphasized that the requirements specified in this standard are complementary (not alternative) to customer and applicable statutory and regulatory requirements. If there is a conflict between the requirements of this standard and customer or applicable statutory or regulatory requirements, the latter shall take precedence. This International Standard specifies requirements for a quality management system when an organization: a needs to demonstrate its ability to consistently provide products and services that meet customer and applicable statutory and regulatory requirements, and b aims to enhance customer satisfaction through the effective application of the system, including processes for improvement of the system and the assurance of conformity to customer and applicable statutory and regulatory
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Using a System Reliability Model to Optimize Maintenance Costs A Best Practices GuideJA6097_201905 (Current)5/7/2019
SAE JA6097 (“Using a System Reliability Model to Optimize Maintenance”) shows how to determine which maintenance to perform on a system when that system requires corrective maintenance to achieve the lowest long-term operating cost. While this document may focus on applications to Jet Engines and Aircraft, this methodology could be applied to nearly any type of system. However, it would be most effective for systems that are tightly integrated, where a failure in any part of the system causes the entire system to go off-line, and the process of accessing a failed component can require additional maintenance on other unrelated components.
HM-1 Integrated Vehicle Health Management Committee
Elbow Assembly 45°, Flared Tube to Retained Nut, for Seal Ring** FK Test-2026-04-12 **AS4316B (Current)5/8/2026
SCOPE IS UNAVAILABLE.1
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Automation Title for Group Code D22PC-Auto-1780276282909 (Current)6/1/2026
Automation Abstract for Group Code D22
Airlines Electronic Engineering Committee
AESQ Quality Management System Requirements for Aero Engine Design and Production OrganizationsAS13100A (Current)4/14/2025
This standard establishes supplemental requirements for 9100 and 9145 and applies to any organization receiving it as part of a Purchase Order or other contractual document from a customer. AS13100 also provides details of the Reference Materials (RM13xxx) developed by the SAE G-22 AESQ committee and listed in Section 2 - Applicable Documents, that can also be used by organizations in conjunction with this standard.
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
SPECIFICATION FOR AN AUTOMATED INTERCHANGE OF STANDARDS DATAAS4159 (Current)4/12/1988
The requirements contained herein are intended for those standards that are promulgated by national standards organizations and used in the aerospace industry. These technical data include narrative text, tables and various graphic data which comprise the standards. Both interface control and interface definitions are covered in this specification. The internal architectures of the computer facilities of either the providers or the users are not constrained by this interchange specification. Rather, neutral formats and transmitting media are defined in order to enable more cost-effective ways to distribute information for computer users than by sending printed documents. This method for digital delivery of aerospace standards is intended to allow the users to display and maintain standards on current computer systems in addition to producing hard copy comparable to existing printed standards.
Aerospace Council
Aerospace Standard Test Methods for Aerospace Sealants Methods for Preparing Aerospace Sealant Test SpecimensAS5127D (Current)6/26/2024
This standard describes the accepted methods used for preparing aerospace sealant test specimens for qualification and quality conformance or acceptance testing. AS5127/1 and AS5127/2 are to be used in conjunction with this document and the applicable AMS specifications.
AMS G9 Aerospace Sealing Committee
Tube Fittings, Aerospace Fluid Systems, Separable, for 24 Degree Cone, General Specification, Metric (ISO 7169)1MA2005D (Current)5/8/2026
This document specifies performance and quality requirements for the qualification and manufacture of 24 degree cone fittings to ensure reliable performance in aircraft hydraulic systems.This document specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines.This document covers fittings of temperature types and pressure classes specified in MA2001.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Determination of Trace Elements in High Temperature AlloysARP1313E (Current)5/8/2026
This SAE Aerospace Recommended Practice (ARP) describes procedures for the determination of trace elements listed in AMS2280 for Nickel, Cobalt, and Iron-based high temperature alloys.
AMS F Corrosion Heat Resistant Alloys Committee
Lubricants, Industrial Oils, and Related Products Type P Pneumatic Tool Oils - SpecificationMS1009_201808 (Current)8/8/2018
See Table 1.
Fuel and Lubricants TC2 Industrial Lubricants
Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Heavyweight, Hydraulic and Pneumatic (Supplement 1)AS604SUP1 (Current)1/9/2013
This supplement forms a part of the Aerospace Standard AS604, Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Heavyweight, Hydraulic and Pneumatic, and shall be used to identify hose assembly standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Electron-Beam Welding For Fatigue Critical ApplicationsAMS2680D (Current)9/30/2025
This specification defines the procedures and requirements for joining metals and alloys using the electron beam welding process.
AMS B Finishes Processes and Fluids Committee
Cast Aluminum Alloy Composite 4.6Cu - 3.4Ti - 1.4B - 0.75Ag - 0.27Mg (205.0/TiB2/3p-T7P) Sand Cast, Solution, and Precipitation Heat TreatedAMS4482B (Current)11/25/2025
This specification covers a dilute aluminum/TiB2 metal matrix composite in the form of sand castings.
AMS D Nonferrous Alloys Committee
Cover Assembly, Electrical, for MS27212 Terminal Board AssemblyAS18029G (Current)10/31/2025
Scope is unavailable.
AE-8C2 Terminating Devices and Tooling Committee
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