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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, 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, 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, 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
Aerospace Fluid Power - Contamination Sensitivity - Considerations for Establishing Test Procedures for Flight Control ActuatorsARP5941 (Current)10/9/2020
This SAE Aerospace Recommended Practice (ARP) describes the design conditions under which tests should be conducted to demonstrate satisfactory performance of a flight critical servo-actuator under the maximum allowable particulate contamination in the associated airplane hydraulic system. Additionally, this document also describes the recommended tests and the required acceptance criteria.
A-6B1 Hydraulic Servo Actuation Committee
Pass-Thru Extended Feature - Single Wire CANJ2534-2/1_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 single wire CAN (SW CAN) 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 J2534-2/1_0500 interface shall be compliant to the single wire CAN 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/BA_0500 and SAE J2534-2/RE_0500 documents.
Vehicle E E System Diagnostic Standards Committee
Pass-Thru Extended Features - Ethernet NDISJ2534-2/9_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 ethernet NDIS 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 J2534-2/9_0500 interface shall be compliant to the ethernet NDIS feature only when all the required functionality in this 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/BA_0500 and J2534-2/RE_0500 documents.
Vehicle E E System Diagnostic Standards Committee
429P2-17 Digital Information Transfer System (DITS), Part 2, Discrete Word Data StandardsARINC429P2-17 (Current)8/1/2019
This standard defines the air transport industry's standards for the transfer of digital data between avionics system elements. Part 2 provides the formats of data words with discrete bit encoding.
Airlines Electronic Engineering Committee
429P4 Digital Information Transfer System (DITS), Part 4, Archive of ARINC 429 SupplementsARINC429P4 (Current)10/29/2012
This document was prepared in conjunction with Supplement 18 to ARINC Specification 429, Part 1. It is an archive of all ARINC Specification 429 Supplements, currently published in parts. The technical content of each Supplement (unchanged in contents and in form) are reproduced for historical reference.
Airlines Electronic Engineering Committee
561-11 Air Transport Inertial Navigation System (INS)ARINC561-11 (Current)1/1/1975
This standard defines the requirements of an INS, which provides sensor and steering command outputs. The INS includes inertial sensing and provides outputs for aircraft attitude, present position, and steering signals suitable for operating the pilot's instruments. The basic INS provides complete self-contained horizontal navigation capability intended to serve as the sole means of navigation on a worldwide basis.
Airlines Electronic Engineering Committee
659 Backplane Data BusARINC659 (Current)12/1/1993
Defines standards for the transfer of digital data between components within an IMA cabinet. Includes the protocol and timing characteristics for a synchronous backplane data bus capable of transferring data at 60 Mbps using a data path that is two bits wide. The electrical characteristics and behavior expected of the participating modules are defined.
Airlines Electronic Engineering Committee
Steel, Corrosion-Resistant, Welding Wire 5.2Cr – 0.55MoAMS6466G (Current)12/5/2017
This specification covers a corrosion-resistant steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Interline Air Cargo PalletsAS1491B (Current)1/13/2023
This SAE Aerospace Standard specifies the dimensional, design criteria, fabrication, performance, operational, environmental, and testing requirements for interline pallets requiring airworthiness approval for loading onto civil transport aircraft equipped with NAS3610/AS36100 restraint systems and using pallet nets meeting the requirements of AS1492. Type II/2 covers NAS3610/AS36100 code sizes. Type III pallets have been removed from this SAE Aerospace Standard revision.
AGE-2 Air Cargo
686 Roadmap for IPv6 Transition in AviationARINC686 (Current)6/19/2020
ARINC Report 686 represents the consensus of industry to prepare a roadmap migration from IPv4 to IPv6. This document describes airline objectives (air and ground side when possible) towards the development and introduction of IPv6. There are three distinct elements considered: 1) the applications for addressing aspects 2) the communication network(s) over which the applications are running for the IP protocol level itself and associated features, and 3) the physical link(s) the network(s) interface.
Airlines Electronic Engineering Committee
Supplemental Propulsion System Performance Station DesignationAIR6508 (Current)10/26/2023
This SAE Aerospace Information Report (AIR) supplements the AS755 performance station designation system for complex or unconventional propulsion cycles and their derivatives. The station numbering conventions presented herein are for use in all communications concerning propulsion system performance such as computer programs, data reduction, design activities, and published documents. They are intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier. The contents of this document will follow AS755 and AS6502 where applicable. The list of symbols presented herein will be used for identification of input and output parameters. These symbols are not required to be used as internal parameter names within the engine subprogram.
S-15 Gas Turbine Perf Simulation Nomenclature and Interfaces
450-1 Flight Simulator Design and Performance Data RequirementsARINC450-1 (Current)9/10/2019
This document provides Flight Simulation Training Device (FSTD) operators, FSTD manufacturers, airplane manufacturers or other sources of approved data and vendors of airplane equipment, with a standard describing the scope and content of data required to build, test, and qualify FSTDs of adequate fidelity to meet flight crew training requirements.
Flight Simulator Engineering and Maintenance Committee
Reliability Physics Analysis of Electrical, Electronic, and Electromechanical Equipment, Modules and ComponentsJ3168_202112 (Current)12/30/2021
This recommended practice has been developed for use in any EEE system used in the AADHP industries. RPA is especially important to AADHP systems, which are often safety critical applications that must operate for long times in rugged environments. These EEE systems often use EEE components that were originally designed and produced for more benign consumer applications. Although the focus of this recommended practice is on AADHP applications, the process described herein is not limited to AADHP and may be used for EEE systems and components in any industry.
Automotive Electronic Systems Reliability Standards
Steel, Bars, Forgings, and Tubing 1.45Cr (0.93 - 1.05C) (SAE 52100) For Bearing ApplicationsAMS6440T (Current)4/5/2021
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Reticulated Polyurethane Foam Explosion Suppression Material for Fuel Systems and Dry BaysAIR4170C (Current)12/20/2021
This document describes the initial development, evolution, and use of reticulated polyurethane foam as an explosion suppression material in fuel tanks and dry bays. It provides historical data, design practice guidelines, references, laboratory test data, and service data gained from past experience. The products discussed in this document may be referred to as "Safety Foam," "Reticulated Polyurethane Foam," "Baffle and Inerting Material," or "Electrostatic Suppression Material." These generic terms for the products discussed in this document are not meant to imply any safety warranty. Each individual design application should be thoroughly proof tested prior to production installation.
AE-5D Fuel Tank Flammability Reduction Systems Committee
HOSE ASSEMBLY, RUBBER, FLARELESS, FIELD ATTACHABLE FITTING, STRAIGHT TO 45°AS1864A (Current)9/17/2024
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, SEMI-RIGID, LOW PRESSURE, FLARELESS, POTABLE WATER, 45° TO 45°AS1486A (Current)1/16/2024
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Rotorcraft Engine Foreign Object Debris and DamageAIR4096A (Current)9/28/2023
The purpose of this SAE Aerospace Information Report (AIR) is to disseminate qualitative information regarding foreign object debris (FOD) damage to the gas path of rotorcraft gas turbine engines and to discuss methods of FOD prevention. Although turbine-powered fixed-wing aircraft are also subject to FOD, the unique ability of the rotorcraft to hover above, takeoff from, and land on unprepared surfaces creates a special need for a separate treatment of this subject.
S-12 Powered Lift Propulsion Committee
623-3 Character-Oriented Air Traffic Service (ATS) ApplicationsARINC623-3 (Current)4/1/2005
This standard defines the application text formats for character-oriented ATS messages that can be transmitted over the ACARS data link. Several ACARS data links are available, including but not limited to VHF, HF and satellite. The messages defined herein are not specific to any data link. This standard is limited in scope to character-oriented applications.
Airlines Electronic Engineering Committee
445 Guidance for Configuration and Control of Loadable Software Parts in Flight Simulation Training DevicesARINC445 (Current)1/1/2014
This report defines the types of software used in FSTDs, outlines the configuration control that is required to maintain the devices, and provides guidance on software updates and changes.
Flight Simulator Engineering and Maintenance Committee
803-5 Fiber Optic System Design GuidelinesARINC803-5 (Current)7/5/2023
The purpose of ARINC Report 803 is to provide design and implementation guidelines together with a selection guide, providing a fiber optic system design engineer with documentation to assess the design requirements for an aerospace fiber optic installation.
Airlines Electronic Engineering Committee
INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE, SILICONE RUBBER, FLEXIBLEAS23053/10B (Current)2/14/2023
AE-8D Wire and Cable Committee
Electric Motors for Driveline Actuation Standard Terminology, Test Parameters, and Equipment RequirementsJ3104_202308 (Current)8/31/2023
This document will apply to the most common applications of electric motors, used for activating all-wheel drive (AWD) and four-wheel drive (4WD) disconnect systems as used in passenger (car and light truck) vehicles. The standard will provide consistent definition, terminology, tests, and reporting methods.
Drivetrain Standards Committee
Descriptions of Systems Integration Test Rigs (Iron Birds) for Aerospace ApplicationsAIR5992 (Current)4/26/2023
This Aerospace Information Report (AIR) provides information on systems integration rigs, commonly referred to as “Iron Birds” for aerospace applications. a It includes background historical information including descriptions of Iron Birds produced to date, important component elements and selection rationale, hydraulic system design and operational modes and illustrates the design approaches to be considered. b It provides illustrations of the various systems that should be considered for Iron Bird testing in the development phase and utilization during the production program. c It includes recommendations for simulation, component development tests, system integration and lessons learned.
A-6A3 Flight Control and Vehicle Management Systems Cmt
NUT, PLAIN - HEXAGON, STEEL UNS G87400, CADMIUM PLATED, 125 KSI MINAS121501C (Current)2/16/2022
E-25 General Standards for Aerospace and Propulsion Systems
Directional Drilling Planning and Mapping NomenclatureJ2583_202512 (Current)12/10/2025
This SAE Standard applies to planning and mapping various types of information associated with directional boring/drilling machines. This type of planning and mapping information is typically used with horizontal directional drilling (HDD) machines as defined by ISO 21467:2023.
MTC9, Trenching and Horizontal Earthboring Machines
Fittings, Beaded to Pipe Threaded, Fluid ConnectionAS4843/2A (Current)6/6/2016
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both beaded hose connections and pipe threaded connections for use in all types of fluid systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN .3750-16 UNC-3AAS116051B (Current)7/29/2014
E-25 General Standards for Aerospace and Propulsion Systems
Structural Modification for Personally Licensed Vehicles to Meet the Transportation Needs of Persons with DisabilitiesJ1725_202506 (Current)6/30/2025
This SAE Information Report applies to structural integrity, performance, drivability, and serviceability of personally licensed vehicles not exceeding 10000 pounds GVWR such as sedans, crossovers, SUVs, MPVs, light trucks, and van-type vehicles that are powered by gas and alternative fuel such as electric, plug-in hybrid, or hybrid technologies. It provides engineering direction to vehicle modifiers in a manner that does not limit innovation, and it specifies procedures for preparing vehicles to enhance safety during vehicle modifications. It further provides guidance and recommendations for the minimum acceptable design requirements and performance criteria on general and specific structural modifications, thereby allowing consumers and third-party payers the ability to obtain and purchase equipment that meets or exceeds the performance and safety of the OEM production vehicle.
Adaptive Devices Standards Committee
Vacuum Excavation and Sewer Cleaning Equipment Classification and NomenclatureJ3106_201911 (Current)11/19/2019
This document lists common terminology for vacuum excavation and sewer cleaning equipment, including component names and specific work completed by these machines. This document also illustrates some common types of equipment.
MTC9, Trenching and Horizontal Earthboring Machines
612 BITE GlossaryARINC612 (Current)12/1/1986
The purpose of this standard is to provide a source of definitions of terms and acronyms commonly used in the air transport maintenance community for test and evaluation with an emphasis on terms applicable to BITE.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
Control of Forgings Requiring First Article ApprovalAMS2375F (Current)9/23/2022
This specification covers procedures for obtaining first-article (preproduction) approval of forgings and the controls to be exercised in producing subsequent production forgings.
AMS E Carbon and Low Alloy Steels Committee
Pass-Thru Extended Features - CAN with Flexible Data RateJ2534-2/11_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 CAN with flexible data rate (CAN FD) 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 J2534-2/11_0500 interface shall be compliant to the CAN with flexible data rate (CAN FD) 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/BA_0500 and SAE J2534-2/RE_0500 documents.
Vehicle E E System Diagnostic Standards Committee
Pass-Thru Extended Feature - IPv6J2534-2/15_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 the internet protocol version 6 (IPv6) 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 J2534-2/15_0500 interface shall be compliant to the internet protocol version 6 (IPv6) 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/BA_0500, and SAE J2534-2/RE_0500 documents.
Vehicle E E System Diagnostic Standards Committee
RING, LOCK, SERRATEDAS51990C (Current)2/10/2020
E-25 General Standards for Aerospace and Propulsion Systems
FITTING, TEE, INTEGRAL WELD RING, 3000 PSIAS1583E (Current)10/20/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
COUPLING, TUBEAS4349A (Current)5/2/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
619-5 ACARS Protocols for Avionic End SystemsARINC619-5 (Current)8/9/2017
The purpose of this document is to delineate, in an organized fashion, the protocols used by Aircraft Communication Addressing and Reporting System (ACARS) Management Units (MU) defined in ARINC Characteristic 724B and Communications Management Unit (CMU) defined in ARINC Characteristic 758, in their interactions with other onboard avionics equipment.
Airlines Electronic Engineering Committee
Steel, Bars, Wire, and Forgings 9.75V - 5.25Cr - 1.3Mo (2.40 - 2.55C) Powder Metallurgy Product Hot Isostatically PressedAMS6559A (Current)5/16/2023
This specification covers a premium aircraft-quality, high-alloy tool steel gas-atomized and HIP-consolidated in the form of bars, wire, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Analytical Methods for Aircraft Seat Design and EvaluationARP5765B (Current)3/30/2021
This SAE Aerospace Recommended Practice (ARP) defines a means of assessing the credibility of computer models of aircraft seating systems used to simulate dynamic impact conditions set forth in Title 14, Code of Federal Regulations (14 CFR) Parts 23.562, 25.562, 27.562, and 29.562. The ARP is applicable to lumped mass and detailed finite element seat models. This includes specifications and performance criteria for aviation specific virtual anthropomorphic test devices (v-ATDs). This document provides a recommended methodology to evaluate the degree of correlation between a seat model and dynamic impact tests. This ARP also provides best practices for testing and modeling designed to support the implementation of analytical models of aircraft seat systems. Supporting information within this document includes procedures for the quantitative comparison of test and simulation results, as well as test summaries for data generated to support the development of v-ATDs and a sample v-ATD
Aircraft Seat Committee
615A-4 - Software Data Loader Using Ethernet InterfaceARINC615A-4 (Current)7/24/2023
This document provides general and specific design guidance for the development of software data loading equipment for all types of aircraft. The primary purpose of data load is to upload loadable software parts to airborne computers. A secondary function of data load is downloading data from airborne computers. Software data load functionality generally falls into the following categories: Portable Data Loader (PDL) for loading equipment on the ground or carried onto aircraft to perform onboard loading. Airborne Data Loader (ADL) for installation on aircraft to perform onboard loading. Data Load Function (DLF) is software that performs the data loading. This document defines data loaders designed to load avionics equipment over a high-speed interface using an Ethernet network protocol. This document defines media interfaces and protocol requirements specific to all data load functions, whether portable or airborne. This document also describes the desired capabilities of data loading
Airlines Electronic Engineering Committee, Avionics Maintenance Committee, Flight Simulator Engineering and Maintenance Committee
Thermophysical Properties of the Natural Environment, Gases, Liquids, and SolidsAIR1168/9A (Current)7/25/2011
This AIR is arranged in the following four sections: 2A - Properties of the Natural Environment 2B - Properties of Gases 2C - Properties of Liquids 2D - Properties of Solids A summary of each section is given below.
AC-9 Aircraft Environmental Systems Committee
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