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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
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
INSERT, SCREW THREAD, SELF LOCKING PLASTIC LOCKING DEVICE, SOLID FILM LUBRICATED SELF-BROACHING KEYS, UNS S66286AS3502A (Current)5/4/2026
E-25 General Standards for Aerospace and Propulsion Systems
NUT, SELF-LOCKING, 12 POINT, REDUCED HEIGHT, SILVER PLATE, UNS S66286, CLASS 160 KSI/1200 °FAS3485C (Current)2/13/2026
E-25 General Standards for Aerospace and Propulsion Systems
Silicone Rubber Compound Room Temperature Vulcanizing, 15,000 Centipoise Viscosity Durometer 35 - 55AMS3362D (Current)1/17/2012
This specification covers a silicone rubber in the form of a two-component liquid compound.
AMS G9 Aerospace Sealing Committee
Organic Fiber (Para-Aramid), Yarn and Roving, High ModulusAMS3901C (Current)9/1/1998
This specification and its supplementary detail specifications covers organic fibers in the form of continuous, multifilament yarn and roving.
AMS P17 Polymer Matrix Composites Committee
Inflator Assembly and Gage Elements, Pneumatic Pressure, Remote Control, Direct ReadingAS85352A (Current)4/9/2018
This specification covers a direct reading, remote control, pneumatic pressure inflator assembly, for use on aircraft tires and struts having pneumatic pressure requirements up to 600 psi. It includes pressure relief provisions to provide for safe inflation. Also included are dual chuck stem gages for measuring tire pressure.
A-5 Aerospace Landing Gear Systems Committee
Nickel Alloy, Corrosion and Heat-Resistant, Round Bars and Wire 52.5Ni - 19Cr - 3.0Mo - 5.1Cb - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Treated and Work Strengthened Precipitation HardenableAMS5962A (Current)5/12/2022
This specification covers a corrosion and heat resistant work strengthened nickel alloy in the form of bars and wire, 1½ inches (38 mm) and under in nominal diameter (See 8.2).
AMS F Corrosion and Heat Resistant Alloys Committee
Core Material, Plastic Honeycomb, Laminated Glass Fabric Base for Aircraft Structural and Electronic ApplicationsAMSC8073 (Current)8/10/2022
This specification covers the requirements for glass fabric base plastic honeycomb core materials for aircraft structural applications, including aircraft exterior parts, such as radio and radar antenna housings, and other parts.
AMS P17 Polymer Matrix Composites Committee
Rivets, Blind, Corrosion Resistant Alloy 67Ni - 31Cu Procurement Specification ForAS7234A (Current)4/23/2024
This procurement specification covers tubular, blind rivets fabricated from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04405, and of 52 ksi minimum shear strength for self-plugging style rivets.
E-25 General Standards for Aerospace and Propulsion Systems
Rubber Cellular Sheet, Molded and Hand-Built Shapes; Latex FoamAMSR5001A (Current)4/13/2015
This specification covers cored and uncored open cell latex foam rubber sheets, molded and hand- built shapes having good shock-absorbing, vibration-damping, and comfort cushioning characteristics (see 6.1).
AMS P Polymeric Materials Committee
Flux, Brazing, High TemperatureAMS3417C (Current)10/31/2007
This specification covers a high temperature brazing flux in the form of paste or powder.
AMS B Finishes Processes and Fluids Committee
Specification for O-Ring Materials Used with Hydraulic ConnectorsJ515_202205 (Current)5/26/2022
SAE J515 covers the specification for hydraulic O-ring material and properties and sizes applicable to face seal fittings, metric and inch stud ends, and four-bolt flange fittings. The standard includes a size code to allow industry and government agencies to order O-rings with a coded part number.
Hydraulic Tube Fittings Committee
CLAMP ASSEMBLY, SADDLE TYPE, CUSHIONED, HIGH TEMPERATUREAS85449/3A (Current)4/21/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel Tubing, Seamless, 0.95Cr - 0.20Mo (0.33 - 0.38C) (4135), Aircraft-Quality, Normalized and Tempered or Stress RelievedAMS6365M (Current)3/3/2026
This specification covers an aircraft-quality, low-alloy steel in the form of seamless tubing.
AMS E Carbon and Low Alloy Steels Committee
SLEEVE, FLARED TUBE FITTINGAS4327 (Current)4/20/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
WIRE, ELECTRIC, CROSSLINKED POLYALKENE INSULATED, TIN-COATED COPPER, NORMAL WEIGHT, 600 VOLT, 150 °CAS81044/6A (Current)7/29/2022
AE-8D Wire and Cable Committee
FITTING, PLUG, TUBE END, FLARELESSAS5231C (Current)11/12/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340)AMS6415V (Current)11/22/2022
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy, Bars, Rods, and Wire 4.4cu 1.5mg 0.60mn Rolled, Drawn, Or Cold FinishedAMS4112D (Current)1/1/1996
This specification has been declared 'CANCELLED' by the Aerospace Materials Division, SAE, as of January 1996. Alloy: 2024-T6 UNS Number: A92024
AMS D Nonferrous Alloys Committee
Sealing Compound, Silicone Rubber, Two-Part, Electrically Conductive and Corrosion Resistant (Nonchromated) for Use from -67 to 500 °F (-55 to 260 °C)AMS3262A (Current)9/23/2011
This specification covers a silicone, electrically conductive and corrosion-inhibiting sealing compound.
AMS G9 Aerospace Sealing Committee
Rubber, Synthetic General Purpose, Fluid Resistant 55 - 65AMS3220H (Current)6/11/2019
This specification covers a synthetic rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Electroless Nickel Plating Low PhosphorusAMS2405E (Current)10/16/2013
This specification covers the engineering requirements for electroless deposition of low-phosphorus nickel on various materials and the properties of the deposit.
AMS B Finishes Processes and Fluids Committee
Control of Aviation Critical Safety ItemsAS9017 (Current)3/17/2017
This document is intended to prescribe consistent requirements for CSI management for organizations and suppliers who perform work for prime contractors receiving direct contracts from U.S. government agencies (i.e., first-tier or prime suppliers).
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Statistical Product Acceptance Requirements Using Continuous Sampling, Skip-Lot Sampling, or Methods for Special CasesARP9013/4A (Current)6/2/2018
The purpose of ARP9013/4 is to ensure conformance for each product characteristic being verified under these methods. ARP9013/4 provides the requirements for continuous sampling, skip-lot sampling, and for statistical methods for product acceptance that do not derive from industry standard tables.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Safety Labels of Off-Road Work MachinesJ115_202401 (Current)1/16/2024
SAE J115 specifies the relevant ISO standards for application to safety labels for use on off-road work machines as defined in SAE J1116.
HFTC2, Machine Displays and Symbols
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
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
Hydraulic Pump Airborne Noise Bench TestJ2747_201909 (Current)9/13/2019
Communicate the process of accurately measuring sound power levels of positive displacement hydraulic pumps commonly used in ground vehicle steering systems. This recommended practice defines the pump mounting (pulley, belt tension, isolation), operating conditions (fluid, speed, temperature, pressure), room acoustics, instrumentation, noise measurement technique and data acquisition setup to be used. Included are recommendations for test sample size, and format for data presentation/reporting.
Vehicle Performance Steering Committee
Recommended Practice for Pass-Thru Vehicle ProgrammingJ2534_201907 (Current)7/29/2019
This SAE Recommended Practice provides the framework to allow reprogramming software applications from all vehicle manufacturers the flexibility to work with multiple vehicle data link interface tools from multiple tool suppliers. This system enables each vehicle manufacturer to control the programming sequence for electronic control units (ECU’s) in their vehicles, but allows a single set of programming hardware and vehicle interface to be used to program modules for all vehicle manufacturers. This document does not limit the hardware possibilities for the connection between the PC used for the software application and the tool (e.g., RS-232, RS-485, USB, Ethernet…). Tool suppliers are free to choose the hardware interface appropriate for their tool. The goal of this document is to ensure that reprogramming software from any vehicle manufacturer is compatible with hardware supplied by any tool manufacturer. The U.S. Environmental Protection Agency (EPA) and the California Air
Vehicle E E System Diagnostic Standards Committee
Hot Stamp Wire Marking Concerns for Aerospace Vehicle ApplicationsAIR5575A (Current)1/24/2017
This SAE Aerospace Information Report (AIR) discusses the often overlooked relationship between hot stamp marking and the environmental conditions that contribute aircraft wiring problems and discusses current beliefs of military service experts, regulatory agencies and industry standard writing bodies about the potential hazards imposed by the hot stamping process.
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
Steel Sheet, Strip, and Plate, Corrosion and Heat Resistant 25cr 20ni 2.0si (314) Solution Heat TreatedAMS5522E (Current)1/1/1991
AMS F Corrosion and Heat Resistant Alloys 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
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
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
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
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
Titles, SAE Subcommittee G-3A Aerospace Coupling Documents, Selection ofARP1987/4A (Current)5/4/2022
The scope of this SAE Aerospace Recommended Practice (ARP) is to establish the procedure for creating titles of aerospace coupling documents generated by SAE Subcommittee G-3A.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, CLOSE TOLERANCE SHANK, COBALT-NICKEL ALLOY, UNS R30159, 260 KSI MINAS3659A (Current)5/4/2026
E-25 General Standards for Aerospace and Propulsion Systems
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, MIL-DTL-83723 SERIES I AND III, AND MIL-DTL-83733 CONNECTORS)AS39029/4D (Current)7/23/2024
AE-8C1 Connectors Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, COBALT-NICKEL ALLOY, UNS R30159, 260 KSI MINAS3658B (Current)5/4/2026
E-25 General Standards for Aerospace and Propulsion Systems
NUT, SELF-LOCKING, DOUBLE HEXAGON, SILVER PLATED, COUNTERBORED 180 KSI, 1400 °F, UNS N07001AS3553B (Current)5/5/2026
E-25 General Standards for Aerospace and Propulsion Systems
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
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
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
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000 psi, 275°F, Heavy Duty, Aircraft Hydraulic Systems (Supplement 1)AS4623SUP1 (Current)9/24/2012
This supplement forms a part of the Aerospace Standard AS4623, Hose Assembly, Polytrafluoroethyloene, Para-Aramid Reinforced, 3000 psi, 275°F, Heavy Duty, Aircraft Hydraulic Systems, and shall be used to identify hose assembly standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Adhesive/Sealant, Fluorosilicone Aromatic Fuel Resistant, One-Part Room Temperature VulcanizingAMS3375C (Current)1/17/2012
This specification covers a one-part fluorosilicone (FVMQ) adhesive/sealant, supplied in cartridges, suitable for extrusion and curing to an elastomeric material upon exposure to air. It also covers a compatible primer.
AMS G9 Aerospace Sealing Committee
Titanium Alloy, Investment Castings 6Al - 4V 130 UTS, 120 YS, 6% EL Hot Isostatically Pressed Anneal Optional or When SpecifiedAMS4985E (Current)11/21/2018
This specification covers a titanium alloy in the form of investment castings.
AMS G Titanium and Refractory Metals Committee
CONNECTOR, RECEPTACLE, ELECTRIC, CRIMP TYPE, WALL MOUNTING FLANGE, PUSH-PULL, COUPLING, SERIES 2 (CLASS E AND J)AS31401A (Current)5/18/2021
AE-8C1 Connectors Committee
JAUS Manipulator Service SetAS6057A (Current)4/24/2025
This document defines a set of standard application layer interfaces called JAUS Manipulator Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned systems to communicate and coordinate their activities. The Manipulator Services represent platform-independent capabilities commonly found across domains and types of unmanned systems. At present, twenty-five (25) services are defined in this document. These services are categorized as: Low Level Manipulator Control Services – The one service in this category allows for low-level command of the manipulator joint actuation efforts. This is an open-loop command that could be used in a simple tele-operation scenario. The service in this category is listed as follows: Primitive Manipulator Service Manipulator Sensor Services – These services, when queried, return instantaneous sensor data. Three services are defined that return respectively joint positions, joint velocities, and joint
AS-4JAUS Joint Architecture for Unmanned Systems Committee
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