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Voltage Regulation and LimitsJ3226_202607 (Current)7/10/2026
This document defines the test procedures and performance limits of steady state and transient voltage characteristics for 12 V, 24 V, or 48 V electrical power generating systems used in commercial ground vehicles.
Truck and Bus Electrical Systems Committee
CONNECTOR, RECEPTACLE, ELECTRIC, DUMMY STOWAGE, WALL MOUNTING FLANGE, PUSH-PULL COUPLING (SERIES 1 AND 2 CONNECTORS)AS31351B (Current)7/9/2026
AE-8C1 Connectors Committee
CONNECTOR, RECEPTACLE, ELECTRIC, SOLDER TYPE, WALL MTG. FLANGE, PUSH-PULL COUPLING, SERIES 1 (CLASS E, P, AND J)AS31301B (Current)7/9/2026
AE-8C1 Connectors Committee
CONNECTOR, RECEPTACLE, ELECTRIC, SOLDER TYPE, JAM NUT MOUNTING, PUSH-PULL, COUPLING, SERIES 1 (CLASS E, P, J AND H)AS31341B (Current)7/9/2026
AE-8C1 Connectors Committee
CONNECTOR, RECEPTACLE, ELECTRIC, BOX MOUNTING FLANGE, PUSH-PULL COUPLING, SERIES 1 (CLASS E AND H)AS31321B (Current)7/9/2026
AE-8C1 Connectors Committee
CONNECTOR, RECEPTACLE, ELECTRIC THRU BULKHEAD, WALL MOUNTING FLANGE, SERIES I (CLASS E)AS31391A (Current)7/9/2026
AE-8C1 Connectors Committee
CONNECTOR, PLUG, ELECTRIC, SOLDER TYPE LANYARD, PUSH-PULL COUPLING, SERIES 1 (CLASS E, P, AND J)AS31381B (Current)7/8/2026
AE-8C1 Connectors Committee
Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock, 0.50Cr - 0.12Mo (0.89 - 1.01C)AMS6476G (Current)7/8/2026
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging or tubing stock.
AMS E Carbon and Low Alloy Steels Committee
National Aerospace and Defense Contractors Accreditation Program (Nadcap) Quality Program RequirementsAS7106A (Current)6/12/2017
This document has been declared "CANCELLED" as of June 2017. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index. Cancelled specifications are available from SAE.
Nadcap Management Council
Propeller Control Installation ClearanceARP244B (Current)2/5/2013
E-25 General Standards for Aerospace and Propulsion Systems
Electromagnetic Testing by Eddy Current MethodsJ425_201801 (Current)1/9/2018
The purpose of this SAE Information Report is to provide general information relative to the nature and use of eddy current techniques for nondestructive testing. The document is not intended to provide detailed technical information but to serve as an introduction to the principles and capabilities of eddy current testing, and as a guide to more extensive references listed in Section 2.
Metals Technical Committee
Thrust Washers – Design and ApplicationJ924_201106 (Current)6/13/2011
This SAE Standard presents the basic size and tolerance information for the design and manufacture of thrust washers. In most cases, the standard employs nominal figures in both metric and inch-pound units and, therefore, does not necessarily provide exact equivalents.
SAE IC Powertrain Steering Committee
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METAL BRAID, MEDIUM PRESSURE, FLARELESS, STRAIGHT TO 90°AS649C (Current)6/20/2011
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
National Aerospace and Defense Contractors Accreditation Program Requirements for Elastomer SealsAS7115A (Current)6/19/2017
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7115. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7115. Cancelled specifications are available from SAE.
Nadcap Management Council
Stepwise Coastdown Methodology for Measuring Tire Rolling ResistanceJ2452_201707 (Current)7/26/2017
This SAE Recommended Practice is applicable to pneumatic Passenger Car “P” Type, Light Truck Metric, and Light Truck High Flotation tires, or similar tires approved by bodies other than Tire & Rim Association. The methodology is applicable within normal operating ranges of vertical load and inflation pressure, and for velocities between 115 km/h and 15 km/h (71 mph and 9 mph) during a relatively short duration event such as a coastdown. This procedure is applicable only to operation in the free-rolling mode at zero slip and camber angle for ambient temperatures between 20 °C and 28 °C (68 °F and 82 °F) and for surfaces with diameters of 1.2 m (48 in) diameter or greater. Details regarding the equipment, tires, and test methods used specifically for validation of this document are included in Appendix A. Two basic measurement methods covered by this document are as follows:
Highway Tire Committee
ARINC 851 Aircraft Ground System Software Distribution and ReceptionARINC851 (Current)12/2/2025
This document provides comprehensive guidance on the secure distribution of Aircraft Relevant Software (ARS) from software providers such as Original Equipment Manufacturers (OEMs) or Design Approval Holders (DAHs) to end users including airline operators and Maintenance, Repair, and Overhaul (MRO) organizations. It aims to standardize software delivery processes to reduce complexity and improve security across the aviation industry ecosystem.
Airlines Electronic Engineering Committee
620-10 Datalink Ground System Standard and Interface Specification (DGSS/IS)ARINC620-10 (Current)7/31/2020
ARINC Specification 620 defines the interfaces between the Datalink Service Provider (DSP) and the aircraft, other ground-based datalink services, and users. The datalink ground system standard definition supports traditional ACARS and AOA protocols, as well as Media Independent Aircraft Messaging (MIAM) as defined by ARINC Specification 841. MIAM messages can be much larger than ACARS messages (5 MB versus 3.3 kB per message). Supplement 10 improves Controller-Pilot Data Link Communications (CPDLC) by defining a "Deliver By (DB)" period that allows the DSP, that originated the message, to intercept and discard the message if it is not delivered by the specified time. Supplement 10 also adds a Media Advisory code for ACARS over IP (AoIP) indicating that an ACARS non Safety Services messages is being transferred over IP links. New Reason Codes are assigned for un-transmittable or undeliverable messages. ACARS Character set clarifications are also provided in Supplement 10.
Airlines Electronic Engineering Committee
601 Control/Display InterfacesARINC601 (Current)2/1/1981
This Specification provides standards for the effective control of the environment for avionic equipment, including basic design standards for avionics equipment and its installation to assure suitable thermal interfaces, design criteria, and cooling appraisal.
Airlines Electronic Engineering Committee
Pass-Thru Extended Feature - UDPJ2534-2/17_0500_202201 (Current)1/17/2022
This SAE Recommended Practice is part of the SAE J2534-2/X_0500 set of documents that extends the SAE J2534-1_0500 API (version 05.00) specification, and defines how to implement user datagram protocol (UDP) within the SAE J2534 API framework. This document details only the changes from SAE J2534-1_0500 and items not specifically detailed in this document are assumed to have not changed. An SAE J2534-2/17_0500 interface shall be compliant to the UDP feature only when all the required functionality in this SAE Recommended Practice is implemented. Any functionality not required for compliance will be specifically marked as “optional” in this document. This document must be used in conjunction with the SAE J2534-2/13_0500 (ethernet), SAE J2534-2/16_0500 (IPv4), SAE J2534-2/15_0500 (IPv6), SAE J2534-2/BA_0500, and SAE J2534-2/RE_0500 documents.
Vehicle E E System Diagnostic Standards Committee
Bearings, Plain, Rod End, Self-Aligning, Self-Lubricating, General Specification For (-65 to +325 °F)AS81935C (Current)6/20/2011
This specification covers plain rod end bearings, corrosion resistant steel (CRES) or alloy steel, which are self-aligning and self-lubricating by incorporating polytetrafluoroethylene (PTFE) in a liner between the ball and race for use in the temperature range -65 to +325 °F (-54 to +163 °C).
ACBG Plain Bearing Committee
Three-Point Hitch (Type A) Backhoe Personnel ProtectionJ1518_201908 (Current)8/28/2019
This SAE Recommended Practice applies to three-point hitch (Type A) backhoes as defined in SAE J326 when mounted on either an agricultural tractor as defined in ANSI/ASAE S390 or other off-road self-propelled work machine as defined in SAE J1116. This criterion is intended for the manufacturer of the backhoe, whether or not the backhoe is manufactured or marketed by the same company that manufactures or markets the propelling machine.
OPTC1, Personnel Protection (General)
Artificial Intelligence in Aeronautical Systems: TaxonomyAIR6987 (Current)12/12/2024
The objective of this document is to provide a classification of AI techniques that may be used in AI-based systems for aeronautical products. Aeronautical products include products in Airborne and Air Traffic Management (ATM) and Air Navigation Systems (ANS) domains for crewed and uncrewed aircraft. This document is: Intended to provide an understanding of the AI space, which will improve over time Not intended to provide guidance, objectives, or safety considerations A scenario builder for AI technologies, in particular supervised learning The publication of a taxonomy document for the aviation domain is an opportunity to support other AI standardization initiatives that will also publish taxonomy documents. Disclaimer: This document provides content to support other products of the SAE G-34/EUROCAE WG-114 Committee.
G-34 Artificial Intelligence in Aviation
Ergonomic Guidelines for Small Lot Delivery OperationsUSCAR42 (Current)3/10/2015
This document describes the design, assessment methods and physical requirements associated with material handling systems. This would include, but not limited to manual dollies, small lot systems and kitting. All possible designs and applications could not be anticipated in creating these guidelines. Where there are questions of adherence to this document, such as use of an “off-the shelf” design, always consult the responsible Ergonomics Department.
USCAR
Hand Held Aircraft Tire Inflation Pressure GaugesARP5542A (Current)5/19/2022
This SAE Aerospace Recommended Practice (ARP) covers the design, construction, performance and testing requirements for hand held aircraft tire inflation pressure gauges with valve stem attachment chuck to be used with all aircraft types. The ground-based gauges in this specification are those which are designed to read the tire inflation pressure from a position adjacent to the tire.
A-5C Aircraft Tires Committee
Curing Agent, Solid Aromatic Amine, 4, 4-Diaminodiphenyl SulfoneAMS3099B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization ofAS1831A (Current)4/3/2023
This SAE Aerospace Standard (AS) establishes the characteristics and utilization of 270 V DC electric power at the utilization equipment interface and the constraints of the utilization equipment based on practical experience. These characteristics shall be applicable for both airborne and ground support power systems. This document also defines the related distribution and installation considerations. Utilization equipment designed for a specific application may not deviate from these requirements without the approval of the procuring activity.
AE-7C Systems
629 Part 1-5 - Multi-Transmitter Data Bus, Part 1-Technical DescriptionARINC629P1-5 (Current)3/1/1999
Defines the aviation industry standards for transfer of digital data between avionics system elements using multiple access, bi-directional protocol. Developed to provide an efficient data distribution system resulting in a reduction in the amount of airplane wiring and equipment interfaces.
Airlines Electronic Engineering Committee
836A Cabin Standard EnclosuresARINC836A (Current)11/20/2018
The purpose of this specification is to define standard cabin equipment enclosures and provisions for equipment attachment on monuments. This standard is intended to enable simpler installation and maintenance of cabin equipment, resulting in time and cost reduction.
Airlines Electronic Engineering Committee
641-1 Logical Software Part Packaging for TransportARINC641-1 (Current)11/16/2020
The purpose of this standard is to provide a method for packaging aircraft software parts for distribution using contemporary media or by electronic distribution. This project intends to standardize and provide guidance for the storage of floppy based software, currently packaged in media set parts. This standard format can be then stored or distributed on a single physical media member (CD-ROM), or by electronic crate. The obsolescence of floppy disks drive an urgent need for this guidance.
Airlines Electronic Engineering Committee
600-20 Air Transport Avionics Equipment InterfacesARINC600-20 (Current)7/11/2017
ARINC 600 is a mechanical packaging standard that is used with the ARINC 700-series of digital avionics equipment. It provides mechanical, electrical, and environmental interfaces between LRUs and the racks or cabinets in which they are installed, as well as connector shell definitions, and connector insert layouts and mounting dimensions. Supplement 20 clarifies connector insert arrangements with new diagrams and corrects typographical errors in descriptive text for connector mated pairs.
Airlines Electronic Engineering Committee
Safety Alert Symbol for Agricultural, Construction, and Industrial EquipmentJ284_202606 (Current)6/29/2026
This SAE Recommended Practice covers the safety alert symbol intended for use on construction and industrial equipment as defined in SAE J1116 and on agricultural tractors and machinery as defined in ASABE S390.
HFTC2, Machine Displays and Symbols
844P1 Guidance for Target Hardware Design, Part 1, Airborne High Speed Data Loader (ARINC Report 615-3)ARINC844P1 (Current)7/29/2016
ARINC Specification 844, prepared in two parts, defines the requirements of a Target Data Loader (TDL) from the target hardware "point of view." Both parts are based on two data loading standards: Part 1 clarifies ARINC Report 615-3: Airborne Computer High Speed Data Loader Part 2 clarifies ARINC Report 615-4: Airborne Computer High Speed Data Loader ARINC Report 615 was originally written from the data loader "point of view." It is important that a target designer have a general understanding of the operation of a data loader in its modern implementation. Equally important is the need for data loader manufacturers to understand the standardized implementation requirements and supported subset of ARINC 615 features that are defined in ARINC 844, Parts 1 and 2. Therefore, ARINC Specification 844 is expected to provide value to both data loader and target implementers. The referenced standardized implementation requirements and supported subset of features defined in ARINC 844, Parts 1
Airlines Electronic Engineering Committee
843-1 Aircraft Software Common Configuration ReportingARINC843-1 (Current)8/13/2019
This standard defines a common configuration report format that can be retrieved from an aircraft for use by ground tools and maintenance personnel. Reports will be generated in Extensible Markup Language (XML) format and structured as defined by this document. Several optional elements and attributes are defined to allow flexibility for a given report. This standard provides aircraft manufacturers, regulatory agencies, and airlines a format standard for aircraft configuration reporting, and facilitates automated comparison of configuration data reports (e.g., authorized versus as flying, etc.).
Airlines Electronic Engineering Committee
629 Part 2-2 Multi-Transmitter Data Bus, Part 2-Application GuideARINC629P2-2 (Current)2/1/1999
Defines the aviation industry standards for transfer of digital data between avionics system elements using multiple access, bi-directional protocol. Developed to provide an efficient data distribution system resulting in a reduction in the amount of airplane wiring and equipment interfaces.
Airlines Electronic Engineering Committee
408A Air Transport Indicator Cases and MountingARINC408A (Current)12/15/1976
This standard defines mechanical dimensions and thermal standards for aircraft indicators and displays. Thermal interface data is included for indicators and their operating environment. These indicators may be stand alone or part of larger integrated display system.
Airlines Electronic Engineering Committee
439B Simulated Air Traffic Control Environments in Flight Simulation Training DevicesARINC439B (Current)8/31/2020
This document provides guidance on provision of SATCE systems in Flight Simulation Training Devices (FSTDs) for the benefit of flight crew training. This work builds upon that originally undertaken by International Air Transport Association (IATA) Flight Simulator Working Group in 2002, and further developed in the International Civil Aviation Organization (ICAO) Doc. 9625 Vol 1, Part 2, Editions 3 and 4. This document is intended to be a practical starting point that can serve as the basis for future developments of SATCE.
Flight Simulator Engineering and Maintenance Committee
National Aerospace and Defense Contractors Accreditation Program Requirements for Fluid System ComponentsAS7112A (Current)6/8/2017
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7112. Cancelled specifications are available from SAE.
Nadcap Management Council
CONNECTOR ACCESSORIES, ELECTRICAL, RFI/EMI, STRAIN RELIEF, STRAIGHT, SELF-LOCKING, CATEGORY 3C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS)AS85049/151 (Current)8/4/2022
AE-8C1 Connectors Committee
Human Interface Criteria for Collision Avoidance Systems in Transport AircraftARP4153A (Current)11/3/2020
This document sets forth design and operational recommendations concerning the human factors issues and criteria for airborne collision and avoidance systems. The visual and aural characteristics are covered for the display of traffic information as well as the escape maneuver display on conventional and electronic flight decks. System utilization philosophy and flight deck integration considerations are also presented.
G-10EAB Executive Advisory Group
Titles, SAE Subcommittee G-3E Aerospace Tubing Installation Documents, Selection OfARP1987/3A (Current)6/17/2025
The scope of this SAE Aerospace Recommended Practice (ARP) is to establish the procedure for creating titles of aerospace tubing and clamp installation documents generated by SAE Subcommittee G-3E.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BEARING, ROLLER, NEEDLE-DOUBLE ROW, HEAVY DUTY, SELF-ALIGNING, TYPE IV, ANTIFRACTION, INCHAS24464C (Current)3/8/2023
ACBG Rolling Element Bearing Committee
ARC FAULT CIRCUIT BREAKER - AIRCRAFT, TRIP FREE, 25 TO 35 AMP, TYPE 1AS5692/4 (Current)3/27/2023
AE-7P Protective and Control Devices
814 -1 Extensible Markup Language (XML) Encoding and Compression StandardARINC814-1 (Current)1/18/2019
ARINC 814 defines an XML encoding and compression standard for aviation. It is based on the Open Geospatial Consortium (OGC) Binary XML document. Binary XML encoding is extended in a way that is both flexible and robust. Compression is added on top of the binary encoding. ARINC 814 is expected to be used with Aeronautical Databases, in particular, ARINC Specification 813: Embedded Interchange Format for Terrain Databases, ARINC Specification 815: Embedded Interchange Format for Obstacle Databases, and ARINC Specification 816: Embedded Interchange Format for Airport Mapping Database.
Airlines Electronic Engineering Committee
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE CRES BRAID REINFORCED, 400 °F, 5080 PSI FLARELESS, STRAIGHT TO STRAIGHTAS5961C (Current)11/17/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, CRES UNS S66286, .1900-32 UNJF-3AAS3114B (Current)3/8/2021
E-25 General Standards for Aerospace and Propulsion Systems
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, SHIELDED, SIZE 16 (FOR MIL-DTL-38999 SERIES I, II, III, IV CONNECTORS AND 50 OHM CABLE)AS39029/76D (Current)1/22/2024
AE-8C1 Connectors Committee
CONNECTOR ACCESSORIES, ELECTRICAL, RFI/EMI, STRAIN RELIEF, 90 DEGREE, SELF-LOCKING, CATEGORY 3C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS)AS85049/153 (Current)8/4/2022
AE-8C1 Connectors Committee
WDM LAN StandardAS5659 (Current)11/16/2023
This standard, consisting of five documents, applies to designers, suppliers, and users of optical network services, systems, and components within mobile military and commercial aerospace platforms. The standard applies to any optical network which uses Wavelength Division Multiplexing in any optical media.
AS-3 Fiber Optics and Applied Photonics Committee
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE CRES BRAID REINFORCED, 400 °F, 5080 PSI FLARELESS, 45° ELBOW TO 45° ELBOWAS5964C (Current)11/17/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
EquipmentAS6286/2A (Current)11/8/2019
This document covers the standards of de-icing/anti-icing equipment. In conjunction with the main document and other related slash sheets it will provide guidelines for the proper procedures to deice and anti-ice aircraft on the ground information to support this training program is provided to make the material a better tool for the preparation and execution of the training & qualification. It is intended to provide a common basis for de-icing/anti-icing training and qualification for de- icing providers and airlines. This material was compiled using various international documents with support from SAE documents and individually contributed editorial comments. Its purpose is to serve as a "Globalized Deicing Training Manual".
G-12T Training and Quality Programs Committee
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