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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, 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, 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 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
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
J1979-DA, Digital Annex of E/E Diagnostic Test ModesJ1979DA_202510 (Current)10/20/2025
The SAE J1979 document set includes the communication between the vehicle's On-Board Diagnostic (OBD) systems and test equipment implemented across vehicles within the scope of regulated emissions and propulsion related OBD. The SAE J1979 Digital Annex supplements the J1979 base documents primarily by maintaining a global registry of regulated emissions and propulsion related data identifiers.
Vehicle E E System Diagnostic Standards Committee
Aircraft Ground Deicing Training and Qualification ProgramAS6286E (Current)5/27/2026
This document establishes the minimum training and qualification requirements for ground-based aircraft deicing methods and procedures. All guidelines referred to herein are applicable only in conjunction with the applicable documents. Due to aerodynamic and other concerns, the application of deicing fluids shall be carried out in compliance with engine and aircraft manufacturers’ recommendations. The scope of training should be adjusted according to local demands. There are a wide variety of winter seasons and differences of the involvement between deicing operators, and therefore, the level and length of training should be adjusted accordingly. However, the minimum level of training shall be covered in all cases. As a rule of thumb, the amount of time spent in practical training should equal or exceed the amount of time spent in classroom training.
G-12T Training and Quality Programs Committee
NUT, SELF-LOCKING, PLATE, TWO LUG, FLOATING, REDUCED RIVET SPACING, LOW HEIGHT, UNS S66286, CLASS: 125 KSI/800 °FAS3481K (Current)5/10/2023
E-25 General Standards for Aerospace and Propulsion Systems
High-Voltage DC Electromechanical, Solid State, and Hybrid Switching Devices in Aerospace ApplicationsAIR7058 (Current)5/10/2023
The scope of this SAE Aerospace Information Report (AIR) is first to establish applicable definitions and terms prior to considering the application domain and use cases in HVDC applications. Then it will identify commanded switching technologies to be considered for aerospace applications and provide rationale for their selection.
AE-10 High Voltage Committee
STUD-STEPPED, 1.5 DIA ENGAGEMENT, .375-16 UNJC-3A MOD X .3125-24 UNJF-3A (UNS S66286)AS3490A (Current)1/31/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, TEE HEAD - AMS5662, CHAMFERED, .3750-24 UNJF-3A (STRESS RUPTURE RESISTANT)AS3412C (Current)6/12/2026
E-25 General Standards for Aerospace and Propulsion Systems
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35,000 kPa), 275°F (135°C), Aircraft Hydraulic Systems (Supplement 1)AS5951SUP1 (Current)9/24/2012
This supplement forms a part of the Aerospace Standard AS5951, Hose Assembly, Polytrafluoroethyloene,Para-Aramid Reinforced, 5080 psi (35,000 kPa), 275°F (135°C), Aircraft Hydraulic Systems, and shall be used to identify hose assembly standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Stockist Distributors Quality System Questionnaire Associated with AS9120AS9121B (Current)11/19/2012
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Insulating Components, Molded, Electrical, Heat Shrinkable, General Specification ForAS81765A (Current)2/28/2017
This specification covers requirements for material used in electrical insulating heat shrinkable components. The continuous operating temperature of these materials shall range from -75°C to +200°C (-103°F to +392°F). (See 6.1).
AE-8D Wire and Cable Committee
Mobile Air Conditioning Industry Criteria and GuidelinesJ2219_201108 (Current)8/12/2011
The purpose of this SAE Information Report is to provide information on refrigerant issues of concern to the mobile air-conditioning industry.
Interior Climate Control Steering Committee
Supplier Self Verification Process, Delegation ProgramsAS9015A (Current)8/12/2016
This SAE Aerospace Standard (AS) further defines the requirements for a delegation process identified in Aerospace Quality Management System (AQMS) standards (i.e., AS9100, AS9110, AS9120). This standard establishes minimum requirements for the delegation of product verification to an organization's suppliers; outlining requirements for the initial delegation (qualification/selection), maintenance, and removal/withdrawal of delegations.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Off-Road Tire and Rim Selection and ApplicationJ1315_201911 (Current)11/20/2019
This SAE Standard provides general guidelines for the proper selection and application of off-road tires and rims, as defined in SAE J751 and applied to earthmoving machines described in SAE J1116 and ISO 6165.
MTC8, Tire and Rim
Alloy, Sheet, Strip, and Plate, 15cr 45ni 4w 4mo 3ti 1al Consumable Electrode Vacuum MeltedAMS5509A (Current)1/1/1992
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE as of April, 1991.
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy Alclad 2014, Plate and SheetAMSQQA250/3A (Current)3/6/2014
This specification covers the specific requirements for 2014 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy (2014) core with thin layers of an aluminum alloy (6003) anodic to the core and of approximately equal thickness bonded to both surfaces.
AMS D Nonferrous Alloys Committee
Bolts and Screws, Steel, Corrosion and Heat Resistant Roll ThreadedAMS7476C (Current)1/1/1982
AMS E Carbon and Low Alloy Steels Committee
Interface Standard, Airborne EO/IR Systems, ElectricalAS6129A (Current)11/19/2019
This standard defines a generic set of electrical interfaces between a host aircraft (“platform”) and an electro-optic/infrared (EO/IR) sensor. This includes connectors, cabling, fiber optics, signals, and power.
AS-1C Avionic Subsystems Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CORROSION- AND HEAT-RESISTANT STEEL, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3AAS9556F (Current)2/27/2024
E-25 General Standards for Aerospace and Propulsion Systems
Requirements for Development, Implementation and Control of Aerospace Auditor TrainingAIR5493B (Current)7/29/2009
This document has been declared “CANCELLED” as of July 2009 and has been superseded by AS9104/3. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by AS9104/3.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Silicone Resin, Elastomeric, Transparent Room Temperature CureAMS3370B (Current)1/17/2012
This specification covers a silicone resin in the form of a two-component liquid.
AMS G9 Aerospace Sealing Committee
Verification of Discrete and Packaged Photonic Device Technology ReadinessARP6318 (Current)10/8/2024
This document is intended for discrete and integrated digital, wavelength division multiplexing (WDM), and analog/radio frequency (RF) photonic components developed for eventual transition to aerospace platforms. The document provides the reasons for verification of photonic device life test and packaging durability. The document focuses on pre-qualification activity at the optical component level to achieve TRL 6. The recommended tests in this document are intended to excite typical failure mechanisms encountered with photonic devices in an aerospace operating environment, and to build confidence that a technology is qualifiable during a program’s engineering and manufacturing development phase. This recommended practice is targeting components to support electrical-to-optical, optical-to-electrical, or optical-to-optical functionality. Passive optical waveguide, fiber optic cable, and connector components that are integral to a photonic package are included. Component and photonic
AS-3 Fiber Optics and Applied Photonics Committee
Rolling Element Bearing Test Method for Dimensional StabilityARP5483/6A (Current)8/23/2018
This test method outlines the recommended procedure for performing dimensional stability tests on rolling element bearings used in airframe applications. Bearings covered by this document shall be antifriction ball bearings and spherical roller bearings with through-hardened outer rings.
ACBG Rolling Element Bearing Committee
Lubricants, Industrial Oils, and Related Products Type P Pneumatic Tool Oils - SpecificationMS1009_201808 (Current)8/8/2018
See Table 1.
Fuel and Lubricants TC2 Industrial Lubricants
TEE, FLARED TUBE WITH PIPE THREAD ON RUN, FOR SEAL RINGAS4312 (Current)4/20/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
WASHER, FLAT, BEAM SEAL FITTINGAS5018 (Current)4/21/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Network LayerJ1939/31_202306 (Current)6/6/2023
SAE J1939-31 network layer describes the requirements and services for network interconnection ECUs (NIECU) that enable electronic control units (ECUs) on an SAE J1939 network segment to intercommunicate with other ECUs on different network segments of the vehicle or system network. This document defines various types of NIECUs. The information in this document applies only to ECUs that are intended to provide networking services. It is not necessary for an ECU to provide any of these services in order to be compliant with the SAE J1939 protocol.
Truck and Bus Control and Communications Network Committee
451 Guidance on the Application of Extended Reality (XR) And Supporting Technologies to Flight Training and SimulationARINC451 (Current)1/14/2026
This document offers a comprehensive and detailed guide on the application of Extended Reality (XR) technologies – including Augmented Reality (AR), Mixed Reality (MR), and Virtual Reality (VR) – in aviation training. It covers a wide range of topics from foundational technology and instructional design to regulatory and safety considerations, aiming to assist training organizations, regulators, and manufacturers in effectively integrating XR into pilot training for both civil and military aviation contexts.
Flight Simulator Engineering and Maintenance Committee
Conventional Towing System 0 up to 9072 kg (20000 Pounds) Trailer GVWJ3352_202512 (Current)12/9/2025
This document establishes a minimum performance criteria for conventional towing systems for the towing interface between a tow vehicle and trailer up to 9072 kg (20000 pounds) Gross Trailer Weight Rating. This does not include weight distributing hitches. This creates the minimum performance criteria for the hitch, trailer attachment structure, coupling, and tow vehicle attachment structure. This standard may be used as a regulatory guide in the selection of products covered. This document is intended to be used voluntarily by the industry producing these products.
Trailer Committee
801-3 Fiber Optic ConnectorsARINC801-3 (Current)6/6/2013
ARINC Specification 801 is intended to provide standardization of a fiber optic interconnect assembly, which is composed of a connector, fiber optic cable, and fiber optic termini for the air transport industry. The goal is to avoid the proliferation of different designs of connectors to serve the same functions on different aircraft models. This specification defines generic fiber optic connectors needed for commercial aircraft. The connector family is based around a standard terminus (fiber optic contact) design and associated cavity, which is used in all of the connector styles and arrangements. The standard terminus comes in variants for different cable types. All termini will fit the same cavities in the connectors and are intended to be interchangeable.
Airlines Electronic Engineering Committee
Spark Plug Heat Rating ClassificationsJ2162_201303 (Current)3/11/2013
This SAE Standard details a uniform method for classifying heat ratings of unshielded spark plugs.
Ignition Standards Committee
628P9-5 Cabin Equipment Interfaces (CEI), Part 9, Cabin Interface Network (CIN)ARINC628P9-5 (Current)12/28/2017
ARINC 628, Part 9 defines general architectural philosophy and aircraft infrastructure for the proper use and interface of various cabin information network related equipment. It specifies a generic on-board infrastructure with commercial server technology, high-speed data communication and exchange via wired and wireless LAN for a wide range of applications. Supplement 5 significantly modifies the standard to remove references to obsolete cabin information network definition. It adds references to current cabin network definitions, ARINC 664: Aircraft Data Network and ARINC 808: Third Generation Network (3GCN).
Airlines Electronic Engineering Committee
845 Fiber Optic Expanded Beam TerminiARINC845 (Current)12/19/2016
This document defines a fiber optic Expanded Beam (EB) termini for the air transport industry. The goal is to avoid the proliferation of different designs of termini to serve the same functions on different aircraft models. This specification defines generic fiber optic EB termini needed for all types of aircraft.
Airlines Electronic Engineering Committee
628P0-4 Cabin Equipment Interfaces, Part 0, Cabin Management and Entertainment System - OverviewARINC628P0-4 (Current)8/28/2018
The purpose of this document is to provide an introduction and overview of the ARINC 628 series of Specifications. ARINC 628 defines equipment and installation standards for cabin equipment, which is generally defined as communication and entertainment equipment designed for passenger use. Part 0 provides the concepts and overview of ARINC 628 and descriptions of each individual part. Appendix B is written in briefing chart format to facilitate the understanding of high-level objectives. Supplement 4 represents a summary of recent changes to Parts 1 through 9 of ARINC Specification 628.
Airlines Electronic Engineering Committee
720-1 Digital Frequency/Function Selection for Airborne Electronic EquipmentARINC720-1 (Current)7/1/1980
This standard sets forth the air transport industry's recommended standards for a digital frequency selection system. This standard addresses two opposite ends of the DFS integration possibilities: a totally centralized and a federated system. This is necessary to assure that the radio interface specifications are adequate to cover a range of DFS integration.
Airlines Electronic Engineering Committee
Mechanical and Material Requirements for Steel NutsJ995_201707 (Current)7/20/2017
This SAE Standard covers the mechanical and material requirements for three grades of steel nuts suitable for use in automotive and related engineering applications, in sizes 1/4 to 1-1/2 inches, inclusive, and with dimensions conforming with the requirements of the latest issue of SAE J482 or ASME B18.2.2, except for machine screw nuts which are not covered in this standard. This document does not include limits for surface discontinuities. Where usage requires such control, limits may be specified separately. For sizes 1/4 through 1 inch, this may be done by the statement: “Surface discontinuities shall not exceed the limits specified in ASTM F812/F812M.”
Fasteners Committee
COUPLING BODY, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDINGAS5835 (Current)1/9/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Turbocharger Gas Stand Test CodeJ1826_202204 (Current)4/25/2022
The test procedures outlined in this SAE Standard are applicable to turbocharging systems having either fixed- or variable-geometry.
Engine Power Test Code Committee
TS21 MANUFACTURING SPECIFICATION FOR FASTENERSTS21-12 (Current)3/2/2022
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Statistical Product Acceptance Requirements Using Attribute or Variable Lot Acceptance Sampling PlansARP9013/2A (Current)6/2/2018
The purpose of ARP9013/2 is to ensure conformance for each product characteristic being verified in each lot in the series. ARP9013/2 document specifies a product acceptance system using either attribute or variable lot acceptance methods documented in ANSI/ASQC Z1.4, ANSI/ASQC Z1.9, and "Zero Acceptance Number Sampling Plans " by Nicholas L. Squeglia.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
CLAMP, LOOP TYPE, CUSHIONED SUPPORTAS5874 (Current)4/23/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Determination of Cost Benefits from Implementing a Blockchain SolutionARP6984 (Current)8/19/2021
This SAE Aerospace Recommended Practice (ARP) provides insights on how to perform a Cost Benefit Analysis (CBA) to determine the Return on Investment (ROI) that would result from implementing a blockchain solution to a new or an existing business process. The word “blockchain” refers to a method of documenting when data transactions occur using a distributed ledger with desired immutable qualities. The scope of the current document is on enterprise blockchain which gives the benefit of standardized cryptography, legal enforceability and regulatory compliance. The document analyzes the complexity involved with this technology, lists some of the different approaches that can be used for conducting a CBA, and differentiates its analysis depending on whether the application uses a public or a private distributed network. This document is intended for people who do not have a deep technical understanding or familiarity with blockchain solutions to qualify and quantify its economic benefits
G-31 Digital Transactions for Aerospace
Adhesive, Film Form Metallic Structural Sandwich ConstructionAMSA25463 (Current)10/4/2022
This specification covers the requirements for adhesives in film form for bonding metal facings to metal cores and to metal components of sandwich panels which are intended for use in primary and secondary structural airframe parts that may be exposed to temperatures up to 500°F (260°C).
AMS P17 Polymer Matrix Composites Committee
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