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Connectors and Inlets for the North American Charging System (NACS) for Electric VehiclesJ3400/2_202504 (Current)04/03/2025
This document covers the dimensional definition of the SAE J3400 (NACS) electric vehicle coupler, which includes the connector and inlet.
Hybrid - EV Committee
Technical Standard
Electric Vehicle Charging Adapter Safety and OEM-Qualified Device DesignationJ3400/1_202504 (Current)04/03/2025
This document covers the general physical, electrical, functional, and performance requirements for adapters connected to standards conforming conductive power transfer via handheld conductive coupler capable of transferring either DC or single phase power using two current-carrying contacts. The focus is on defining the process to evaluate the suitability of adapters for NACS couplers. This edition only covers adapters used between SAE J3400 and SAE J1772.
Hybrid - EV Committee
Technical Standard
INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, TYPE I, CLASS 1, COMPOSITION CAS81969/17A (Current)04/02/2025
AE-8C2 Terminating Devices and Tooling Committee
Technical Standard
CRIMPING TOOL AND ACCESSORIES, REMOTE CRIMP HEAD, HYDRAULIC, WIRE SIZE 8 TO 0000 FOR INSULATED AND UN-INSULATED CRIMP BARRELSAS5259/1B (Current)04/02/2025
AE-8C2 Terminating Devices and Tooling Committee
Technical Standard
Procedure for the Calculation of Non-Volatile Particulate Matter Sampling and Measurement System Penetration Functions and System Loss Correction FactorsAIR6504A (Current)04/01/2025
This SAE Aerospace Information Report (AIR) describes a method for assessing size dependent particle losses in a sampling and measurement system of specified geometry utilizing the non-volatile Particulate Matter (nvPM) mass and number concentrations measured at the end of the sampling system.1 The penetration functions of the sampling and measurement system may be determined either by measurement or by analytic computational methods. Loss mechanisms including thermophoretic (which has a very weak size dependence) and size dependent losses are considered in this method2 along with the uncertainties due to both measurement error and the assumptions of the method. The results of this system loss assessment allow development of estimated correction factors for nvPM mass and number concentrations to account for the system losses facilitating estimation of the nvPM mass and number at the engine exhaust nozzle exit plane. As the particle losses are size dependent, the magnitude of correction
E-31P Particulate Matter Committee
Information Report
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, STRAIGHT, SELF-LOCKING, SHIELD BAND TERMINATION (RFI/EMI), SHRINK BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS)AS85049/85D (Current)04/01/2025
AE-8C1 Connectors Committee
Technical Standard
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, 45°, SELF LOCKING, SHIELD, BAND TERMINATION, (RFI/EMI), SHRINK SLEEVE ACCOMMODATION, CATEGORY 3B (FOR AS50151 CRIMP, AS95234, MIL-DTL 26482 SERIES 2, AS81703 SERIES 3 AND MIL-DTL-83723 SERIES III CONNECTORS)AS85049/83D (Current)04/01/2025
AE-8C1 Connectors Committee
Technical Standard
J1939 Digital AnnexJ1939DA_202503 (Current)03/31/2025
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
Supplement
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, STRAIGHT, SELF-LOCKING, SHIELD BAND TERMINATION (RFI/EMI), SHRINK SLEEVE ACCOMMODATION, CATEGORY 3B (FOR AS50151 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3 AND MIL-DTL-83723 SERIES III CONNECTORS)AS85049/82D (Current)03/31/2025
AE-8C1 Connectors Committee
Technical Standard
DATALINK GROUND SYSTEMS STANDARD AND INTERFACE SPECIFICATION (DGSS/IS)ARINC620-9 (Current)12/21/2017
ARINC Specification 620 defines the aircraft interfaces to the ACARS ground system operated by a Datalink Service Provider (DSP). It also defines the interface between the DSP and other ground-based datalink services. The datalink ground system standard definition supports traditional ACARS 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 9 includes methods to optimize the routing of MIAM messages. It adds ACARS Labels and Identifiers in support of Onboard Network System (ONS), Runway State Assessment, Aircraft Tracking for AOC Position Reporting, ATS Wind Services and Fight-deck based Interval Management System (FIMS) applications. It provides Media Advisory Codes for Broadband Systems (i.e., AeroMACS, Inmarsat SwiftBroadband (SBB) Satcom, and Iridium NEXT/Certus Satcom).
Airlines Electronic Engineering Committee
Technical Standard
665-5 Loadable Software StandardsARINC665-5 (Current)08/13/2019
This document defines the aircraft industry's standards for Loadable Software Parts (LSPs) and Media Set Parts (MSPs). It describes the common principles and rules to be applied to any part of a data load system to ensure compatibility and inter-operability of software parts. It includes part numbering, content, labeling, and formatting of an LSP, and a Media Set containing LSPs. Supplement 5 refers to a companion document, ARINC Report 645: Common Terminology and Functions for Software Distribution and Loading.
Airlines Electronic Engineering Committee
Information Report
429P1-19 Digital Information Transfer System (DITS), Part 1, Functional Description, Electrical Interfaces, Label Assignments and Word FormatsARINC429P1-19 (Current)01/22/2019
ARINC 429 is the most widely used data transfer method used in aviation. This document provides the standard formats for data parameters and status words transferred between avionic systems. It specifies the physical data bus, electrical characteristics, and data formats. Supplement is 19 is a routine update that defines new ARINC 429 data words, new labels, new equipment IDs, and new System Address Labels (SAL).
Airlines Electronic Engineering Committee
Specification
Engine Rotation and Cylinder NumberingJ824_202206 (Current)06/29/2022
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry.
Engine Power Test Code Committee
Technical Standard
840A Electronic Flight Bag (EFB) Application Control Interface (ACI) for Tablet DevicesARINC840A (Current)08/23/2019
This document specifies how application to application navigation is managed on tablet EFB devices. Topics include: inter-application navigation for users, blending of multiple applications into a single workflow, single data entry with data shared across applications.
Airlines Electronic Engineering Committee
Specification
664P2-3 Aircraft Data Network, Part 2, Ethernet Physical and Data Link Layer SpecificationARINC664P2-3 (Current)10/24/2018
This specification provides Ethernet physical parameters and data link layer specifications for use in a commercial aircraft environment. This specification provides general and specific guidelines for the use of IEEE 802.3 compliant Ethernet, 2000 edition. Physical layer and Medium Access Control (MAC) sub-layers are expected to comply with the Open System Interconnection (OSI) Reference Model to enable maximal utilization of off-the-shelf components, both hardware and software, for aviation use. The Ethernet Physical layer specification defines the electrical and optical parameters for the 10BASE-T, 100BASE-TX, and 100BASE-FX Ethernet implementations. This specification references ARINC Specification 600: Air Transport Avionics Equipment Interfaces for definition of copper-based implementations of the Ethernet Physical layer.
Airlines Electronic Engineering Committee
Specification
714-6 Mark 3 Airborne SELCAL SystemARINC714-6 (Current)08/15/1990
Ground-to-air selective calling system characteristics are defined by this standard. The system allows selective calling of individual aircraft over radio communications circuits linking the ground station to the aircraft. Elements comprising overall system are ground selecting calling unit (coder), ground-to-air transmitter (HF or VHF), airborne receiver (HF or VHF), airborne selective calling unit (decoder), and code selection panel.
Airlines Electronic Engineering Committee
Characteristic
718-4 Mark 3 Air Traffic Control Transponder (ATCRBS/MODE S)ARINC718-4 (Current)12/15/1989
This document defines the Air Traffic Control Transponder (ATCRBS/Mode S) with that supports emerging Automatic Dependent Surveillance - Broadcast (ADS-B) requirements. Supplement 4 adds ADS-B Out capabilities and enables the Mode S Transponder to comply with Mode S Transponder MOPS (RTCA DO-181E and EUROCAE ED-73E) as entered into ICAO Annex 10 Volume IV and ICAO Doc. 9871.
Airlines Electronic Engineering Committee
Characteristic
709A-1 Precision Airborne Distance Measuring Equipment (DME/P)ARINC709A-1 (Current)08/17/1994
This standard provides general and specific design guidance for the development of a DME/P, which provides slant range distance from an aircraft to a selected DME ground facility. For landing purposes, the DME/P complements the angle MLS/ILS with precise range data.
Airlines Electronic Engineering Committee
Characteristic
760-1 GNSS Navigation Unit (GNU)ARINC760-1 (Current)03/20/2000
Characteristics desired of a GNU are defined in this standard. The GNU provides enroute/terminal navigation, and non-precision approach capabilities. The GNU is intended to support CNS/ATM functions available in the near term, as well as provide growth for the long-term.
Airlines Electronic Engineering Committee
Characteristic
745-2 Automatic Dependent Surveillance (ADS)ARINC745-2 (Current)06/30/1993
This standard defines ADS system functions. It describes the ADS to ground-based application end-to-end operation. Includes a brief overview of the entire ADS system in order to aid the reader in understanding the ADS environment.
Airlines Electronic Engineering Committee
Characteristic
746-6 Cabin Communications Systems (CCS)ARINC746-6 (Current)11/19/2010
This document provides general and specific design guidance for the development, installation, and desired operational capability of Cabin Communications Systems, including satellite communications, air-to-ground communications, and gatelink. Supplement 6 incorporates guidance for protection of personal information using methods consistent with the Payment Card Industry (PCI) Data Security Standard (DSS). The CCS characteristic provides encryption approaches for payment card information and suggestions for key management.
Airlines Electronic Engineering Committee
Characteristic
717-15 Flight Data Acquisition and Recording SystemARINC717-15 (Current)06/06/2011
This document provides design guidance for the development and installation of a Digital Expandable Flight Data Acquisition and Recording System (DEFDARS) primarily intended for airline use. As such, this guidance will include specific requirements necessary to accommodate mandatory flight data recording and other flight data acquisition needs plus the requirements to ensure customer controlled interchangeability of equipment in a standard aircraft installation. The system capability was expanded to accommodate a data bus speed of 1024 words per second.
Airlines Electronic Engineering Committee
Characteristic
716-11 Airborne VHF Communications TransceiverARINC716-11 (Current)06/10/2003
This standard sets forth characteristics of a VHF Communications Transceiver for installation in all types of commercial transport aircraft. The VHF transceiver can support 8.33 kHz AM or 25 kHz AM voice or ACARS (2400 bps) data communications.
Airlines Electronic Engineering Committee
Characteristic
719-5 Airborne HF/SSB SystemARINC719-5 (Current)07/06/1984
This standard sets forth characteristics of a new-generation HF/SSB System intended for installation in all types of commercial transport aircraft. Covers requirements for airborne transmitter-receiver equipment capable of transmitting and receiving HF radio intelligence.
Airlines Electronic Engineering Committee
Characteristic
722 Projection Video System (PVS)ARINC722 (Current)11/05/1980
This standard sets forth design guidance and airplane interfaces for the development and installation of a PVS in commercial transport aircraft. Basic function of the PVS is to display projected television images to each passenger.
Airlines Electronic Engineering Committee
Characteristic
735-2 Traffic Alert and Collision Avoidance System (TCAS)ARINC735-2 (Current)01/15/1993
This standard defines as TCAS system capable of calculating the range, altitude and bearing of other aircraft equipped with Mode S transponders. The system monitors the trajectory of these aircraft for the purpose of determining if any of them constitute a potential collision hazard.
Airlines Electronic Engineering Committee
Characteristic
735A-1 Mark 2 Traffic Alert and Collision Avoidance System (TCAS)ARINC735A-1 (Current)01/15/2003
This update to the TCAS system standard introduces changes necessary to be compliant with RTCA Document DO-185A that includes TCAS software version 7.0.
Airlines Electronic Engineering Committee
Characteristic
738A-1 Air Data and Inertial Reference System (ADIRS)ARINC738A-1 (Current)07/31/2001
This standard sets forth characteristics for a 4 MCU integrated digital ADIRS intended for installation in subsonic commercial transport aircraft. It is envisioned that the ADIRS will incorporate the capabilities of both an air data system and an inertial reference system.
Airlines Electronic Engineering Committee
Characteristic
732-1 Mark 2 Airborne Passenger Audio Entertainment Tape ReproducerARINC732-1 (Current)03/20/1996
This standard defines an airborne tape reproducer for passenger entertainment. The function of this equipment is to play pre-recorded tapes to the passengers through the airplane passenger entertainment system. Some channels may be used for boarding music through the public address system.
Airlines Electronic Engineering Committee
Characteristic
743A-6 GNSS SensorARINC743A-6 (Current)06/22/2009
This document sets forth the characteristics of the integrated Global Positioning System (GPS)/Global Orbiting Navigation Satellite System (GLONASS) sensor unit (GNSSU) portion of a GNSS system intended for installation in commercial aircraft. The intent of this document is to provide general and specific design guidance for the development of GNSS sensors for airline use. It describes the desired operational capability of the GNSS system and the standards necessary to ensure interchangeability.
Airlines Electronic Engineering Committee
Characteristic
709-8 Airborne Distance Measuring Equipment (DME)ARINC709-8 (Current)10/31/1988
This standard sets forth characteristics of a DME intended for installation in commercial transport aircraft. It provides slant range distance from an aircraft to a selected DME ground facility, which is presented to the flight crew on an indicator located in the instrument panel. Other applications include utilization of frequency scanning modes by navigation computers.
Airlines Electronic Engineering Committee
Characteristic
704-7 Inertial Reference System (IRS)ARINC704-7 (Current)03/19/1999
IRS characteristics are defined in this standard. It defines the desired performance of inertial measuring devices and associated electronics specifically designed for installation in commercial transport aircraft. This system provides the basic outputs for aircraft angular rate and acceleration, and computed outputs of altitude, true heading, velocity and present position in a 10 MCU form factor.
Airlines Electronic Engineering Committee
Characteristic
705-5 Attitude and Heading Reference System (AHRS)ARINC705-5 (Current)04/30/1985
This standard describes the basic requirements for an AHRS specifically designed for installation in commercial transport aircraft. The AHRS is an attitude and heading sensor that provides outputs in digital form for guidance and display. The AHRS replaces the traditional vertical and directional gyros.
Airlines Electronic Engineering Committee
Characteristic
INDUSTRY GUIDE FOR COMPONENT TEST DEVELOPMENT AND MANAGEMENTARINC625-3 (Current)11/07/2012
This standard provides guidance to those who develop avionics test programs and the source documentation on which they are based. This includes guidelines for all steps and phases within the TPS life cycle.
Avionics Maintenance Committee
Technical Standard
602B Test Equipment GuidanceARINC602B (Current)06/01/2012
This standard provides considerations for the procurement and design requirements of TE to be used for maintenance and troubleshooting of air transport components in both the shop and/or flight line environment. Although the term TE is used, this standard can be applied to other types of support equipment utilized in the aviation industry, such as shop data loaders, portable maintenance aids, etc.
Avionics Maintenance Committee
Information Report
666 - Electronic Distribution of SoftwareARINC666 (Current)05/01/2002
This document describes a secure internet facility for sending all types of aviation software using the world wide web (www). Software suppliers may use this document as a starting point for the construction of a secure web server utility. It provides sufficient flexibility and is compatible with numerous software distribution models. The file management structure is consistent with other ARINC standards for loadable software, and references ARINC 665 and ARINC 667 in particular.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
Information Report
671 Guidance for the Transition to Lead-Free Soldering, Maintenance, and RepairARINC671 (Current)03/01/2006
This document provides guidance for the use of international standards for the maintenance of lead-free electronic equipment. The purpose is to assist manufacturers, maintenance facilities, and operators to define lead-free soldering requirements and to minimize the set of lead-free solders, processes, and practices to gain consistency across the industry.
Avionics Maintenance Committee
Information Report
668-1 Guidance For Tool and Test Equipment (TTE) EquivalencyARINC668-1 (Current)06/18/2013
ARINC 668 provides guidelines for the process used to establish the equivalency of TTE and related procedures other than that recommended by the OEM. Primarily, ARINC 668 is concerned with equipment specified or recommended for the purpose of performing specific tasks concerning the airworthiness of an article (e.g., avionics, hydraulics, pneumatics, mechanical devices, etc.).
Avionics Maintenance Committee
Information Report
609 Design Guidance for Aircraft Electrical Power SystemsARINC609 (Current)01/01/1987
This standard describes electrical power system design and performance standards brought about by extensive use of digital avionics. This Report provides guide lines for designers of aircraft power system components and of power utilization components, both avionics and power converters such as motors and heaters.
Airlines Electronic Engineering Committee
Information Report
614 Standard Firmware Loader for Avionics ShopsARINC614 (Current)09/01/1989
This standard describes the characteristics of a standard firmware loader for avionic shops. It is capable of copying digital information into memory devices installed in circuit card assemblies, Line Replaceable Modules (LRMs) and On-Board Replaceable Modules (OBRMs). It contains the recommendations of the air transport community concerning the design and development of firmware loader equipment.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
Information Report
634 HF Data Link System Design Guidance MaterialARINC634 (Current)08/01/1996
This Report provides the reader with material to enhance the understanding of high frequency data link. This standard provides a snapshot of guidance material used in the development of ARINC 753, HF Data Link System, and ARINC 635, HF Data Link Protocols.
Airlines Electronic Engineering Committee
Information Report
613 Guidance for Using the Ada Programming Language in Avionics SystemsARINC613 (Current)01/01/1988
In 1986 the airlines selected Ada as the high-order development language for avionics. ARINC 613 describes the Ada domain most suited for avionics software development. The standard provides valuable guidance to Ada compiler developers and Ada programmers.
Airlines Electronic Engineering Committee
Information Report
608A Design Guidance for Avionics Test Equipment, Part 1 - System DefinitionARINC608A (Current)01/01/1993
This standard is a top-level guidance standard intended for the design of Automatic Test Equipment (ATE). It includes the definition of hardware and software needed for analog and digital signal testing using a Test Unit Adapter common interface. This standard describes the overall ATE system concept as well as the definition of the specific elements of those systems.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
Information Report
607-3 Design Guidance for Avionics EquipmentARINC607-3 (Current)08/01/1998
This standard provides general guidelines for the design of avionics equipment. It represents the desires of the airline industry resulting from extensive airline experience. Manufacturers are urged to use this standard when initially starting the design of new equipment. Airplane Personality Module (APM) specifications are included.
Airlines Electronic Engineering Committee
Information Report
606A Guidance for Electrostatic Sensitive Utilization and ProtectionARINC606A (Current)11/01/2004
This document provides guidance for using industry standards for developing an ESD control program tailored to meet specific user requirements. In addition, it provides uniform guidance for maintenance facilities based on industry ESD standards, and therefore should be accepted throughout the air transport industry. This document is not a stand-alone document - it is intended to be used with the referenced international industry standards.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
Information Report
611-1 Guidance for the Design and Installation of Fuel Quantity SystemsARINC611-1 (Current)01/01/1999
This standard defines accuracy and reliability targets for fuel quantity measuring systems installed on commercial aircraft. It describes fuel quantity system components and design techniques that will contribute to safe and reliable operation. System design goals and installation practices are described. A report of a worldwide fuel survey is included.
Airlines Electronic Engineering Committee
Information Report
610B Guidance for Use of Avionics Equipment and Software in SimulatorsARINC610B (Current)12/01/2001
Guidance for the Use of Avionics and Software in Simulators is intended to simplify the additional functions required of avionics equipment used in simulators. Recommended simulator functions, data base harmonization, use of snapshot functions, and a new training scenario are included. The guidelines contained in the draft are expected to reduce the cost to design and install avionics equipment in simulators.
Airlines Electronic Engineering Committee, Flight Simulator Engineering and Maintenance Committee
Information Report
654 Environmental Design Guidelines for Integrated Modular AvionicsARINC654 (Current)12/01/1994
This standard is concerned with electromagnetic compatibility, shielding, thermal management, vibration and shock of IMA systems. Emphasis is placed both on the design of IMA components and their electrical, optical and electro-mechanical interfaces.
Airlines Electronic Engineering Committee
Information Report
651-1 Design Guidance for Integrated Modular AvionicsARINC651-1 (Current)11/01/1997
This standard is a systems design guide for IMA. It provides guidance for the design and implementation of avionics equipment for new airplanes and retrofit installations. It is conceptual in nature and covers broad subjects of operational objectives, fault tolerance, hardware components, software design and certification issues.
Airlines Electronic Engineering Committee
Information Report
765 Ethernet Switch UnitARINC765 (Current)12/29/2003
ARINC Characteristic 765 defines an Ethernet Switch Unit (ESU), which fits in the general architectural philosophy and aircraft infrastructure for the proper use and interface of various information network related equipment. This document specifies an ESU intended for various aircraft information network related equipment. It provides a wired network connection among the connected devices based on interfaces defined by ARINC Specification 664 and IEEE 802.3 CSMA/CD (Ethernet).
Airlines Electronic Engineering Committee
Characteristic
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