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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 THRU BULKHEAD, WALL MOUNTING FLANGE, SERIES I (CLASS E)AS31391A (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, 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, 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
Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For (Supplement 1)AS85421SUP1A (Current)7/7/2026
This supplement forms a part of SAE Aerospace Specification AS85421. It shall be used to identify fitting standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Measurement of Exhaust Sound Levels of Stationary SnowmobilesJ2567_202607 (Current)7/6/2026
This SAE Standard establishes the test procedure, environment, and instrumentation for determining the sound levels of snowmobiles in the stationary test mode. This test method is intended to provide an accurate measurement of exhaust and other engine noise and may be used to evaluate new and in-use snowmobiles to determine compliance with noise control regulations. Sound level measurements obtained with this test method are not intended as an engineering determination of overall machine noise. For this purpose, the use of SAE J192 is recommended.
Snowmobile Technical Committee
Electric Speedometer Specification - On RoadJ1226_201108 (Current)8/5/2011
This SAE Recommended Practice covers electric speedometer systems for general on-road (passenger car, multi-purpose passenger vehicle, truck, and bus) applications.
Odometer and Speedometer Standards
Clamp Loop Cushion Integral LockAS4149A (Current)10/1/2000
No scope available.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Spark Plug Installation SocketsJ548/2_201303 (Current)3/11/2013
This SAE Standard applies to spark plug installation sockets of the long length type which are to be used for installing spark plugs of the most commonly used sizes for the North American market.
Ignition Standards 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
SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN .3750-24 UNF-3AAS116101B (Current)7/29/2014
E-25 General Standards for Aerospace and Propulsion Systems
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
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
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
GENERAL ENVIRONMENTAL REQUIREMENTS FOR DEEP SUBMERSIBLE VEHICLES AND SUBMARINESAIR1063 (Current)4/15/1969
The scope of this HIR is to specify general oceanographic environments. Specific environmental requirements shall be specified in a detail specification. Specific requirements are in the state of constant flux because the ocean environment is constantly changing and the changes occur not only on a seasonal basis but also monthly, weekly, daily, and in some cases even hourly. This HIR is to be used as a guide only.
Fluid Power Utilization
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
Eddy Current Inspection of Circular Holes in Nonferrous Metallic Aircraft Engine HardwareAS4787A (Current)5/2/2025
This SAE Aerospace Standard (AS) establishes minimum requirements for eddy current inspection of circular holes in nonferrous, metallic, low conductivity (less than 5% IACS) aircraft engine hardware with fasteners removed. The inspection is intended to be performed at maintenance and overhaul facilities on engine run hardware.
AMS K Non Destructive Methods and Processes Committee
679 Aircraft Server, Communications, and Interface StandardARINC679 (Current)11/10/2021
ARINC Report 679 defines the functional characteristics of an airborne server that will support Electronic Flight Bags (EFBs) and similar peripherals used in the flight deck, cabin, and maintenance applications. The document defines how EFBs will efficiently, effectively, safely, and securely connect to the airborne server in a way that offer expanded capabilities to aircraft operators. The airborne server has two main functions, first to provide specific services to connected systems, and second to provide centralized security for the EFB and its data. This document is a functional airborne server definition. It does not define the physical characteristics of the server.
Airlines Electronic Engineering Committee
821 Aircraft Network Server System (NSS) Functional DefinitionARINC821 (Current)12/9/2008
This document describes a collection of Aircraft Network Services (ANS) and Network Server System (NSS) functions that are suitable for installation in all types of aircraft. It defines network services intended for both aircraft and cabin installations that will manage and maintain the NSS in a common way. This document describes methods for the aircraft to effectively communicate with ground-based information management systems.
Airlines Electronic Engineering Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS4967 (UNS R56400), 160 KSI, .1900-32 UNJF-3AAS3147C (Current)5/6/2026
E-25 General Standards for Aerospace and Propulsion Systems
Fastener Part Standard - Tapping Screws and Metallic Drive Screws (Inch Dimensioned)J2596_201308 (Current)8/21/2013
This SAE Part Standard covers selected inch dimensioned tapping screws and metallic drive screws manufactured in accordance with American Society for Mechanical Engineers dimensional standards. This SAE standard covers material most often used in ship systems and equipment but its use may be applied wherever fasteners of the covered materials are used. This standard permits the fasteners to be identified and ordered by a Part Identification Number (PIN) as defined in this standard.
Ship Systems - Fasteners Committee
653P0-4 Avionics Application Software Standard Interface, Part 0, Overview of ARINC 653ARINC653P0-4 (Current)12/1/2025
This document provides an overview of the entire set of documents collectively referred to as ARINC 653. As this set of documents evolves, Supplements to Parts 1 through 5 have been made more consistent with Part 0 in conjunction with the technical changes made in the evolution of ARINC 653. A summary of the ARINC 653 documents follows: Part 0 – Overview of ARINC 653 Part 1 – Required Services Part 2 – Extended Services Part 3A – Conformity Test Specification for ARINC 653 Required Services Part 3B – Conformity Test Specification for ARINC 653 Extended Services Part 4 – Subset Services Part 5 – Core Software Recommended Capabilities The term “this document” refers to Part 0 only, while the term “ARINC 653” or “the Specification” refers to the whole set of ARINC 653 documents, currently, Parts 0 to 5. The primary objective of ARINC 653 is to define a general-purpose APplication/EXecutive (APEX) interface, i.e., an API (Application Program Interface) between the Core Software (CSW) of an
Airlines Electronic Engineering Committee
Nut, Self-Locking, Double Hexagon, Reduced Envelope, AMS7251AS3070A (Current)9/24/2020
Scope is unavailable.
E-25 General Standards for Aerospace and Propulsion Systems
National Aerospace and Defense Contractors Accreditation Program Requirements for Fittings and Other Machined ComponentsAS7112/2A (Current)6/19/2017
This document has been declared "CANCELLED" as of June 2017 and has been superseded by PRI AC7112/2. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7112/2. Cancelled specifications are available from SAE.
Nadcap Management Council
648 Cabin Passenger Seat Production TestingARINC648 (Current)12/18/2019
This report defines the requirements and recommended practices for production testing of aircraft passenger seats and seat groups. Production testing is performed at the seat manufacturers' facilities prior to the shipment of the seats to the airframe manufacturers, Maintenance, Repair, and Overhaul (MRO), or airlines/operators for installation in the aircraft. Using this guidance, rework is minimized and schedules remain minimally affected.
Airlines Electronic Engineering Committee
CONNECTORS, ELECTRICAL, RECTANGULAR, RECEPTACLE, CRIMP CONTACTS, (DUAL INSERT, TYPE II, CLASS 1, (-65 °C TO +125 °C), SERIES 2, SHELL DESIGNATOR A)AS81659/35B (Current)1/20/2022
AE-8C1 Connectors Committee
Thermal Sensitive Inflation Pressure Release Devices for Tubeless Aircraft WheelsAS707C (Current)2/15/2019
The focus of this SAE Aerospace Standard (AS) is the integration of thermally actuated pressure release devices, hereafter referred to as fuse plugs, with the wheel and brake assembly. It does not address the manufacturing, quality or acceptance test requirements pertaining to the production of these fuse plugs. It establishes minimum design, installation, qualification, and operational requirements for fuse plugs which are used only in tubeless tire type aircraft braked wheels. Fuse plugs are designed to completely release the contained inflation pressure from a tubeless tire and wheel assembly when brake generated heat causes the tire or wheel to exceed a safe temperature level. The objective is to prevent tire or wheel rupture due to brake generated heat that could cause an unsafe condition for personnel or the aircraft. (Reference: U.S. Department of Transportation FAA Advisory Circular No. 23-17C; Title 14, Code of Federal Regulations (14 CFR) Part 25.735 (j); U.S. Department of
A-5A Wheels, Brakes and Skid Controls Committee
Synchro, Control Differential Transmitter, Type 18CDX6DAS20708/36B (Current)10/16/2016
AE-7A Generators and Controls Motors and Magnetic Devices
Steel, Corrosion-Resistant, Bars, Wire, and Forgings 12Cr - 11Ni - 1.7Ti - 1Mo Vacuum Induction Plus Vacuum Consumable Electrode Remelted Solution Heat Treated, Precipitation HardenableAMS5936D (Current)3/26/2019
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
Synchro, Torque Receiver Transmitter, Type 18TRX4AAS20708/32B (Current)10/13/2016
AE-7A Generators and Controls Motors and Magnetic Devices
Airborne Chemicals in Aircraft CabinsAIR4766/2A (Current)6/22/2021
This SAE Aerospace Information Report (AIR) provides information on aircraft cabin air quality, including: Origins of chemical airborne contaminants during routine operating and failure conditions. Exposure control measures, including design, maintenance, and worker training/education. This AIR does not deal with airflow requirements.
AC-9 Aircraft Environmental Systems Committee
CONNECTORS, ELECTRICAL, RECTANGULAR, RECEPTACLE, CRIMP CONTACTS, DUAL INSERT, TYPE III, CLASS 1 (−65 °C TO +125 °C), SERIES 2, SHELL DESIGNATOR AAS81659/62B (Current)2/2/2022
AE-8C1 Connectors Committee
Health and Usage Monitoring System Data Interchange SpecificationAS5395A (Current)9/18/2025
This document establishes the Rotorcraft Industry Technology Association (RITA) Health and Usage Monitoring System Data Interchange Specification. The RITA HUMS Data Interchange Specification will provide information exchange within a rotorcraft HUMS and between a rotorcraft HUMS and external entities.
HM-1R Rotorcraft Integrated Vehicle Health Management
FITTING ASSEMBLY, ELBOW, 45°, AXIALLY SWAGED, HYDRAULIC, 5080 PSIAS5971D (Current)6/10/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CONNECTORS, ELECTRICAL, RECTANGULAR, RECEPTACLE, CRIMP CONTACTS, TRIPLE INSERT, TYPE III, CLASS 1 (−65 °C TO +125 °C), SERIES 2, SHELL DESIGNATOR AAS81659/63B (Current)1/28/2022
AE-8C1 Connectors Committee
STUD - STRAIGHT, KEY LOCKED, CRES UNS S66286 .1900-32 UNJF X .1900-32 UNJFAS3090A (Current)4/4/2024
E-25 General Standards for Aerospace and Propulsion Systems
FITTING, LUBRICATION, HYDRAULIC, SURFACE CHECK, .250-28 TAPER THREADS, NICKEL-COPPER ALLOY, TYPE IVAS15004D (Current)8/21/2017
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, PLUG, SHORT FLARELESSAS4662C (Current)8/16/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
606-1 Guidance for Electrostatic Sensitive Device Utilization and ProtectionARINC606-1 (Current)7/1/1993
The primary goal of this standard is to describe the nature of Electrostatic Discharge (ESD) and its effects on digital avionics equipment. It provides information concerning methods to protect against ESD damage which could originate in many different ways.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, COMPOSITE, HIGH DENSITY, QUICK COUPLING, ENVIRONMENTAL RESISTANT, REMOVABLE CRIMP CONTACTS, BACKSHELL 90°, SELF LOCKING (SERIES A AND B)AS29600/3A (Current)9/23/2014
AE-8C1 Connectors Committee
Alloy Sheet, Strip, and Plate, Corrosion and Heat Resistant 58Ni - 15.5Cr - 16Mo - 3.8W - 5.5Fe Solution Heat TreatedAMS5530H (Current)4/20/2017
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Titanium and Titanium-Alloy Castings, InvestmentAMST81915B (Current)12/6/2016
This specification prescribes the requirements for Titanium and Titanium-alloy castings produced by the investment casting process.
AMS G Titanium and Refractory Metals Committee
Nut, Self-Locking, Double Hexagon, Reduced Envelope, AMS7251AS3069A (Current)9/17/2020
SCOPE IS UNAVAILABLE.
E-25 General Standards for Aerospace and Propulsion Systems
Fiber Optics Mechanization of a Digital Time Division Command/Response Multiplex Data BusAS1773A (Current)3/14/2018
This document defines requirements for digital, command/ response time division multiplexing (data bus) techniques for fiber optic implementation. The concept of operation and information flow on the multiplex data bus and the functional formats to be employed are also defined.
AS-3 Fiber Optics and Applied Photonics Committee
Aluminum Alloy, Extrusions 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T61511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Precipitation Heat TreatedAMS4307C (Current)4/24/2017
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.
AMS D Nonferrous Alloys Committee
Aluminum Alloy Plate, Alclad - 5.6zn - 2.5mg - 1.6cu - 0.26cr (Alclad 7075-T651)AMS4039C (Current)1/1/1968
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4049, ALUMINUM ALLOY SHEET AND PLATE (Alclad 7075; -T6 Sheet, -T651 Plate). The requirements of the latest issue of AMS 4049 shall be fulfilled whenever reference is made to this specification.
AMS D Nonferrous Alloys Committee
Riding Range Test Procedure for On-Highway Electric MotorcyclesJ2982_202210 (Current)10/13/2022
This SAE Recommended Practice incorporates dynamometer test procedures that produce riding range estimates for electric motorcycles during stop-and-go urban riding on surface streets and commuting trips in urban areas that include operation on freeways. This is typically done using a “coastdown” approach by disengaging the engine and assuming all losses are aerodynamic. However, with inherent losses in an electric motor, and no way to fully disengage the motor, another approach is to use a “on-road, constant speed” (Appendix B) method for fully electric vehicles to develop dynamometer coefficients.
Motorcycle Technical Steering Committee
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