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Use Cases for Wireless Charging Communication for Plug-in Electric VehiclesJ2836/6_202606 (Current)6/24/2026
This SAE Information Report SAE J2836/6 establishes use cases for communication between plug-in electric vehicles and the EVSE for wireless energy transfer as specified in SAE J2954. It addresses the requirements for communications between the on-board charging system and the wireless EV supply equipment (WEVSE) in support of detection of the WEVSE, the charging process, and monitoring of the charging process. Since the communication to the charging infrastructure and the power grid for smart charging will also be communicated by the WEVSE to the EV over the wireless interface, these requirements are also covered. However, the processes and procedures are expected to be identical to those specified for V2G communications specified in SAE J2836/1. Where relevant, the specification notes interactions that may be required between the vehicle and vehicle operator, but does not formally specify them. Similarly, communications between the on-board charging sub-system and the on-board vehicle
Hybrid - EV Committee
Powder, Chromium Carbide Plus Nickel-Chromium Alloy 75Cr3C2 + 25 (80Ni - 20Cr Alloy)AMS7875F (Current)6/24/2026
This specification covers a blend of chromium carbide and a nickel-chromium alloy in the form of powder.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Bars, Wire, and Forgings 12Cr - 9Ni - 2Mo – 0.7Al – 0.3Ti Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Precipitation HardenableAMS5928 (Current)6/24/2026
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
633-6 AOC Air-Ground Data and Message Exchange FormatARINC633-6 (Current)6/24/2026
ARINC Specification 633 defines the format and the exchange of Aeronautical Operational Control (AOC) messages. Supplement 6 adds new ARINC 633 AOC data structures as well as revises existing data structures, including: Flight Plans, Special Loads (i.e., Weight and Balance and Cargo Planning Load Sheets), NOTAM, ETOPS, Terrain Avoidance, FuelHeader, Minimum Equipment Lists (MEL), Crew List, etc. The standardization of AOC messages facilitates the development of applications shared by numerous airlines on different aircraft types. Benefits include improved dispatchability and reduce operator cost. ARINC 633 is a complete definition of AOC message sets used in commercial aviation with XML schema definition.
Airlines Electronic Engineering Committee
Standards for Battery Secondary UseJ2997_202606 (Current)6/24/2026
This document provides recommendations involving BEV battery data retention and battery design that enhance the potential for BEV battery reuse and serviceability and that can improve recyclability. These recommendations have been developed by a group of professionals skilled in the secondary-use of batteries and in the research, development, and manufacture of BEV batteries and battery systems.
Secondary Battery Use Committee
BAND, MALE COUPLING, 12 INCH AIR DUCTAS7365/7A (Current)6/23/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BAND, FEMALE COUPLING, 6 INCH AIR DUCTAS7365/8A (Current)6/23/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
COUPLING, MALE, 6 INCH AIR DUCTAS7365/5A (Current)6/23/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BAND, MALE COUPLING, 6 INCH AIR DUCTAS7365/9A (Current)6/23/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
COUPLING, FEMALE, 6 INCH AIR DUCTAS7365/4A (Current)6/23/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Automotive Air-Conditioning Service Ports Task Force Field Survey ResultsJ3267_202606 (Current)6/23/2026
The automotive air-conditioning service ports task force conducted a field survey with MACS (Mobile Air Climate Systems Association) in June 2021. The scope of this survey was to determine the types of failures reported primarily at member service shops related to automotive air-conditioning service ports.
Interior Climate Control MAC Supplier Committee
Dimensional and Performance Testing Specifications for Secondary Pouch Cells for Group 1 Small Uncrewed Aerial Vehicle(s) (sUAV)JA1016_202606 (Current)6/23/2026
This document establishes standardized dimensional cell geometry, performance-test procedures, and reporting requirements for secondary (i.e., rechargeable) pouch cells used in Group 1 sUAV. It defines reference geometries, test conditions, and uniform data formats to allow direct comparison of pouch-cell performance across manufacturers and to improve interoperability within the sUAV ecosystem.
Battery Cell Size Standardization Committee
Metallic Connections for Fluid Power and General Use - Part 1: 37-Degree Flared FittingsJ514-1_202606 (Current)6/22/2026
This part of SAE J514 covers general and dimensional specifications for 37 degree flared tube fittings. Also included are 37 degree flared fittings with NPTF pipe threads in Appendix B. These fittings are intended for general application in hydraulic systems on industrial equipment and commercial products. These fittings are capable of providing leak-proof, full flow connections in hydraulic systems operating at working pressures as specified in Table 6. Since many factors influence the pressure at which a hydraulic system will or will not perform satisfactorily, the values shown in Table 6 should not be construed as a guaranteed minimum. For any application, it is recommended that sufficient testing be conducted and reviewed by both the user and fitting manufacturer to assure that performance levels will be safe and satisfactory.
Hydraulic Tube Fittings Committee
Reduced Effort Brakes and Reduced Effort Vacuum Powered Brake Backup SystemsJ2671_202606 (Current)6/22/2026
This Information Report relates to a special class of automotive adaptive equipment which consists of modifications to the power brake booster systems provided as original equipment of motor vehicles. These modifications are generically called "Reduced Effort Power Brakes" (REPB) The purpose of the modification is to lower the amount of driver effort required to apply the brakes. Retention of reliability, ease of use and maintainability for disabled drivers, passengers, and the general public is of primary concern. Reduced Effort Power Brake modifications should be qualified by the tests referenced in the Recommended Test Procedure. The tests set forth in that procedure should be applied, and failure of a Reduced Effort Power Brake modification to meet those tests should disqualify the modification from the claim of meeting the specifications of this Information Report. Because this is an Information Report, the numerical values for performance measurements presented in this report and
Adaptive Devices Standards Committee
High-Strength Carbon and Alloy Die Drawn SteelsJ935_202606 (Current)6/22/2026
This SAE Recommended Practice is intended to provide basic information on properties and characteristics of high-strength carbon and alloy steels which have been subjected to special die drawing. This includes both cold drawing with heavier-than-normal drafts and die drawing at elevated temperatures.
Metals Technical Committee
827-2 Electronic Distribution of Software by Crate (EDS Crate)ARINC827-2 (Current)12/3/2025
This standard describes the format for electronic distribution of aircraft software parts and other contents between aerospace business partners using a digital container referred to as an EDS crate. This EDS standard is intended to promote consistent, secure distribution of EDS content to any appropriate destination.
Airlines Electronic Engineering 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
660C CNS/ATM Avionics Architectures Supporting NextGen/SESAR ConceptsARINC660C (Current)8/2/2024
The origin of this ARINC 660C is traced to a number of industry activities but focuses primarily on the evolving airspace operations to be implemented by NextGen and SESAR that appear feasible in the next decade. From these inputs, the AEEC defined impacts on avionics architectures that would apply to in-production and in-service airplanes, recognizing that the impacts on the architectures would vary as a function of the existing avionics baseline. The equipage impacts described in ARINC Report 660C are intended to provide the airlines with the necessary information to evaluate modernization proposals and to support the overall goal of fleet commonality while meeting operational requirements.
Airlines Electronic Engineering Committee
842-3 Guidance for Usage of Digital CertificatesARINC842-3 (Current)7/1/2022
The purpose of this document is to provide operational guidance for key life-cycle management, which refers to the phases through which digital certificates and associated cryptographic keys progress, from creation through usage to retirement. Additionally, this document provides implementation guidance for online certificate provisioning of aircraft systems. The scope includes both the onboard part (aircraft system) as well as the ground part (PKI provider and Ground Infrastructure). Consideration of both onboard and ground provides the benefit of security considerations being included in the process flow and chain of custody. Specifically, the management to and from the aircraft is defined within a workflow. The guidance is based on open international standards that are adapted to the aviation environment, recognizing that a typical commercial airplane has a long lifespan, its operational environment is highly complex and regulated, and multiple stakeholders operate ground-based
Airlines Electronic Engineering Committee
791P3-1 Mark I Aviation Ku-Band and Ka-Band Satellite Communication System, Part 3, Information Transfer and InternetworkingARINC791P3-1 (Current)2/6/2025
This document (ARINC Characteristic 791, Part 3) provides the internetworking networking interface definition of the Mark I (ARINC 791) and Mark II (ARINC 792) Ku-Band and Ka-Band Satellite Communication (satcom) system intended for passenger entertainment on commercial transport aircraft. Any signal crossing into or out of the communication system is documented to ease aircraft integration. ARINC Characteristic 791 Part 1 of this document provides an overview of Ku-band and Ka-band satcom systems. System provisions, including Line Replaceable Unit (LRU) form factors, attachments, cooling, and inter-system wiring, are defined. Signals between the Modem/Modem Manager (Modman) and the Antenna Subsystem are described to permit interchangeability between any Modman and any Antenna Subsystem. ARINC Characteristic 791 Part 2 of this document provides the non-networking interface definition of the satcom system. Any signal crossing into or out of the communication system is documented to ease
Airlines Electronic Engineering Committee
688 Intersystem Network IntegrationARINC688 (Current)6/24/2021
The purpose of this document is to provide guidelines for integrating previously standalone cabin systems such as cabin management systems, In-Flight Entertainment (IFE) systems, In-Flight Connectivity (IFC) systems, galley systems, surveillance systems, etc. Resource sharing between systems can reduce airline costs and/or increase functionality. But, as systems expose their internal resources to external systems, the risk of an intrusion that could degrade function and/or negatively expose the supplier's or airline's brand increases. This document provides a recommended IP networking design framework between aircraft systems to reduce the operational security threats while still supporting the necessary intersystem routing.
Airlines Electronic Engineering Committee
678 Guidance for Distributed Radio ArchitecturesARINC678 (Current)7/15/2021
The purpose of this document is to evaluate Communication, Navigation, and Surveillance (CNS) Distributed Radio architectures and the feasibility of distributing the RF and systems processing sections to ensure the following: Reduce cost of equipment Reduce Size, Weight, and Power (SWaP) Ease of aircraft integration Growth capability built into the design Maintain or improve system availability, reliability, and maintainability It provides a framework to determine whether it is feasible to develop ARINC Standards that support CNS distributed radio architectures.
Airlines Electronic Engineering Committee
644 Portable Maintenance Access Terminal (PMAT)ARINC644 (Current)5/1/1993
This standard contains the electrical interface definition, and a functional description of a PMAT. The intent of this standard is to provide general and specific design guidance for the development of a PMAT primarily for airline use.
Airlines Electronic Engineering Committee
660 CNS/ATM Avionics, Functional Allocation and Recommended ArchitecturesARINC660 (Current)12/1/1995
Defines a set of standard aircraft avionics architectures that support a cost-effective evolution to the fully operational CNS/ATM environment. These architectures are intended to meet near-term requirements (e.g., FANS-1, SCAT-1, etc.) and provide growth for supporting the full CNS/ATM function set. This standard represents broad airline consensus for developing avionics equipment providing CNS/ATM operating capabilities.
Airlines Electronic Engineering Committee
658 Internet Protocol Suite (IPS) for Aeronautical Safety Services - Roadmap DocumentARINC658 (Current)12/18/2017
ARINC 658 was prepared to recognize the expanding role of data communication technology and the evolutionary path forward starting from ACARS protocols, to ATN/OSI protocols, and eventually ATN/IPS protocols using highly secure networks. The ATN/IPS network will be implemented onboard an aircraft and in the ground infrastructure to support safety services, including Air Traffic Services (ATS) and Aeronautical Operational Control (AOC). As such it provides a so-called "roadmap" for the development of the aviation standards for ATN/IPS services. ATN/IPS standards will evolve in coming years and be coordinated with other international standards organizations such as ICAO, EUROCAE and RTCA.
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
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
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
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
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
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
577-1 Audible Warning SystemARINC577-1 (Current)3/1/1975
This standard provides basic requirements for audible warning generators, whose function is to provide 25 different channels with sound and/or voice warnings, activated by discrete input signals and generated as a function of an unsafe condition of important systems of the aircraft. The outputs are available for audible display to the cockpit crew.
Airlines Electronic Engineering Committee
707-7 Radio AltimeterARINC707-7 (Current)4/6/2009
This standard provides the desired characteristics of a RALT intended for installation in all types of commercial transport aircraft. Its primary function is to determine the aircraft's height above terrain for visual display to the pilot (essentially ground level to 2500 feet), and for use by the AFCS during automatically controlled approaches and landings.
Airlines Electronic Engineering Committee
741P2-11 Aviation Satellite Communication System, Part 2, System Design and Equipment Functional DescriptionARINC741P2-11 (Current)6/27/2012
This document describes the desired operational capability of the equipment as configured with the first generation Satellite Data Unit (SDU) to provide data and voice communications, as well as additional standards necessary to ensure interchangeability. Supplement 11 adds commentary on the commonality of physical interfaces between ARINC 741 systems defined for SwiftBroadband safety services and ARINC 741 systems defined only for the Inmarsat Classic Aero safety services. It adds the SwiftBroadband safety services to the SDU functional definition.
Airlines Electronic Engineering Committee
ARINC Characteristic 759: Aircraft Interface Device (AID)ARINC759 (Current)7/15/2014
This document sets forth the characteristics of an Aircraft Interface Device (AID) intended for installation in commercial aircraft. The intent of the document is to provide general and specific design guidance for the development of an AID for use in retrofit applications associated with aircraft typically developed between the mid-1970s through the 1990s, that primarily utilize ARINC 700 series avionics, and that interface with the aircraft via ARINC 429 and ARINC 717 unidirectional buses and Hi/Lo discrete signals. This document describes the desired operational capability of the AID and the standards necessary to ensure interchangeability.
Airlines Electronic Engineering Committee
573-7 Aircraft Integrated Data System Mark 2 (AIDS Mark 2)ARINC573-7 (Current)12/1/1974
This standard provides design guidance for the development and installation of an expandable Flight Data Acquisition and Recording System. The functions defined include flight data acquisition through suitable electrical interfaces, conversion of analog input signals into a standard serial data output and the capability for expansion to permit increased data handling capacity.
Airlines Electronic Engineering Committee
702-6 Flight Management Computer System (FMCS)ARINC702-6 (Current)6/1/1994
This standard defines a FMCS for installation in commercial transport aircraft. The FMCS provides performance data, performance computations, fuel management functions, and navigation and guidance to a desired flight plan.
Airlines Electronic Engineering Committee
538C Handheld Microphone and Boom MicrophoneARINC538C (Current)1/1/2014
This document describes the aircraft industry recommendations for a handheld microphone and boom microphone for use with airborne radio installations. This document, ARINC Characteristic 538C, is in addition to and does not supersede the older ARINC Characteristic 538B: Hand-Held Microphone, dated February 16, 1983.
Airlines Electronic Engineering Committee
766 Aeronautical Mobile Airport Communication System (AeroMACS) Transceiver and Aircraft Installation StandardsARINC766 (Current)7/7/2017
This document defines the Installation Characteristics of an airborne radio transceiver capable of broadband wireless communication with an Airport Surface Network. The Aeronautical Mobile Airport Communications System (AeroMACS) Radio Unit (ARU) will operate in the aeronautical protected frequency of 5091 MHz to 5150 MHz, utilizing the IEEE 802.16e WiMAX protocol. It is intended to offload some of the congested narrowband VHF airport traffic used for ATS and AOC communications. ARU and Antenna Form, Fit, Function and Interfaces are described.
Airlines Electronic Engineering Committee
729-1 Analog and Discrete Data Converter System (ADDCS)ARINC729-1 (Current)9/10/1981
This standard sets forth the characteristics of an ADDCS designed for installation in commercial transport aircraft. The ADDCS is intended to process, convert and multiplex analog and discrete signals in order to provide them in digital format described in ARINC 429.
Airlines Electronic Engineering Committee
763A Mark 2 Network Server System (NSS) Form and Fit DefinitionARINC763A (Current)12/9/2008
This document defines both wired and wireless NSS components that enable the creation of airborne networks that are scalable, interchangeable, upgradeable, and remotely manageable with minimum cost. Aircraft equipment configurations and aircraft wiring recommendations are also described to allow aircraft network growth through the simple addition or replacement of NSS components. Hardware characteristics of standardized components are described without specifying equipment capacity or the operational functions of those components.
Airlines Electronic Engineering Committee
725-2 Electronic Flight Instruments (EFI)ARINC725-2 (Current)11/5/1984
This standard sets forth the features of a color EFI system for installation in commercial transport aircraft. The EFI provides display functions that include Attitude Director Indicator (ADI), Horizontal Situation Indicator (HSI), Air Data, Map display, Weather display, Radio Altitude data, Flight Control Mode annunciation, Flight Path information, and Flight Warning display.
Airlines Electronic Engineering Committee
712-7 Airborne ADF SystemARINC712-7 (Current)7/15/1992
This standard sets forth characteristics of an ADF system for installation in commercial transport aircraft. Function is to receive and process signals from non-directional range and other transmitters in the frequency band 190 kHz to 1750 kHz, to provide serial digital outputs of bearing, and to provide aural identification of the selected station.
Airlines Electronic Engineering Committee
743B-1 GNSS Landing System Sensor Unit (GLSSU)ARINC743B-1 (Current)6/22/2018
This document sets forth the characteristics of the GNSS Landing System Sensor Unit (GLSSU) intended for installation in commercial aircraft. The intent of this document is to provide general and specific design guidance for the development of GLSSU for airline use. It describes the desired operational capability of the GLSSU and the standards necessary to ensure interchangeability.
Airlines Electronic Engineering Committee
747-3 Flight Data RecorderARINC747-3 (Current)6/7/2011
This document provides design guidance for the development and installation of Flight Data Recorders (FDR) which may utilize solid state memory and which may employ some means of data compression. The Flight Data Recorder will be utilized with a Flight Data Acquisition Unit (FDAU) (ARINC Characteristic 573) or a Digital Flight Data Acquisition Unit (DFDAU) (ARINC Characteristic 717) to accommodate mandatory flight data recording and other flight data acquisition needs. The document provides guidance and information to ensure customer controlled interchangeability of equipment in a standard aircraft installation and in data retrieval. The system capability was expanded to accommodate a data bus speed of 1024 words per second.
Airlines Electronic Engineering Committee
Aluminum Alloy, Tubing, Hydraulic (6062 T6)AMS4093A (Current)1/1/1966
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4083, ALUMINUM ALLOY TUBING, HYDRAULIC, SEAMLESS, DRAWN (6061-T6). The requirements of the latest issue of AMS 4083 shall be fulfilled whenever reference is made to this specification.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, ExtrusionsAMS4155B (Current)1/1/1966
SUPERSEDING SPECIFICATION: The requirements of this specifications are embodied in the latest issue of AMS 4150, ALUMINUM ALLOY EXTRUSIONS (6061-T6). The requirements of the latest issue of AMS 4150 shall be fulfilled whenever reference is made to this specification.
AMS D Nonferrous Alloys Committee
Alloy Bars and Forgings, Corrosion and Heat Resistant 43co 20cr 20ni 4.0mo 4.0w 4.0cb Solution and Precipitation Heat TreatedAMS5765C (Current)4/1/1991
AMS F Corrosion and Heat Resistant Alloys Committee
Bolts and Screws, Work-Strengthened Alloy, Corrosion and Heat Resistant, Forged Head, Roll Threaded After AgingAMS7475B (Current)1/1/1991
AMS F Corrosion and Heat Resistant Alloys Committee
Labels, Aluminum Foil Etched and EnameledAMS7294A (Current)1/1/1987
This specification has been 'Cancelled' by the Aerospace Materials Division, SAE, as of September 1996.
AMS D Nonferrous Alloys Committee
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