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EUROCAE/SAE WG80/AE-7AFC Hydrogen Fuel Cells Aircraft Fuel Cell Safety GuidelinesAIR6464 (Current)7/17/2026
This document defines the technical guidelines for the safe integration of Proton Exchange Membrane (PEM) Fuel Cell Systems (FCS), fuel (considered to be liquid and compressed hydrogen storage types only), fuel storage, fuel distribution and appropriate electrical systems into the aircraft. Editorial Note: Today PEM systems and fuel storage represent the most mature FCS technology and currently forms the basis for this standard. Other types of fuel cell systems and fuels (including reforming technologies and electrolyzers), may be covered by a further update to this document.
AE-7F Hydrogen and Fuel Cells
Exposure Levels of UV Radiation in Nondestructive Inspection ProcessesAIR4964A (Current)7/17/2026
Long wave ultraviolet or UV-A irradiation (between 320 and 400 nm) is used for fluorescent inspections in magnetic particle and liquid penetrant examinations. UV-A irradiation is obtained from either LED, fluorescent, or high intensity discharge lamps that are stationary or portable. Commercially available UV-A lamps possess a large variation in intensity output that may introduce a legitimate concern for possible health hazards. This document reviews the nature of UV-A irradiation emitted by lamps and acceptable UV dosage limits adopted by the American Conference of Governmental Industrial Hygienists (ACGIH®) and European Union and recommendation of proper practices when working with UV-A irradiation.
AMS K Non Destructive Methods and Processes Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CUP WASHER LOCKED, CRES, UNS S66286, 130 KSI MIN, .2500-28 UNJF-3AAS9677C (Current)7/17/2026
E-25 General Standards for Aerospace and Propulsion Systems
Procedure for Thermal Aging Test for Polyol Ester Gas Turbine Engine LubricantsARP6299A (Current)7/17/2026
This method is intended to evaluate the thermal and oxidative stability of synthetic, ester-based aviation lubricants under defined conditions of time and temperature. This method is applicable to lubricants meeting the compositional and performance requirements of AS5780.
E-34 Propulsion Lubricants Committee
J1979-DA, Digital Annex of E/E Diagnostic Test ModesJ1979DA_202607 (Current)7/16/2026
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
Lighting, Aircraft Interior, Installation ofAS18276B (Current)7/16/2026
This specification covers the installation of aircraft interior lighting for military aircraft.
A-20C Interior Lighting
Starter Battery Identification and ClassificationJ2981_202607 (Current)7/15/2026
This document provides recommendations to identify battery group sizes and dimensions for 6 V, 8 V, 12 V, and 24 V lead acid batteries.
Starter Battery Standards Committee
Manganese Alloy, Brazing Filler Metal 66Mn - 16Ni - 16Co - 0.80B 1770 to 1875 °F (966 to 1024 °C) Solidus-Liquidus RangeAMS4780J (Current)7/15/2026
This specification covers a manganese alloy in the form of powder, preforms, and a viscous mixture (paste) of the powder in a suitable binder.
AMS F Corrosion and Heat Resistant Alloys Committee
Hard Anodic Coating of Magnesium Alloys Alkaline Type, High VoltageAMS2467B (Current)7/15/2026
This specification establishes the procedures used to produce a hard anodic coating on magnesium alloys and the properties of the coating.
AMS B Finishes Processes and Fluids Committee
Steel, Corrosion-Resistant, Sheet, Strip, and Plate, 9.0Mn - 20Cr - 6.5Ni - 0.28N (21-6-9LC), Solution Heat TreatedAMS5595J (Current)7/15/2026
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Physical Layer, 250 kbit/s, Twisted Shielded PairJ1939-11_202607 (Current)7/15/2026
This document defines a physical layer having a robust immunity to EMI and physical properties suitable for harsh environments. This document is suitable for CAN interfaces applying CAN HS (high-speed) transceivers as specified in ISO 11898-2. These SAE Recommended Practices are intended for light- and heavy-duty vehicles on- or off-road, as well as appropriate stationary applications which use vehicle derived components (e.g., generator sets). Vehicles of interest include, but are not limited to, on- and off-highway trucks and their trailers, construction equipment, and agricultural equipment and implements.
Truck and Bus Control and Communications Network Committee
Automatic Transmissions - Schematic DiagramsJ647_202512 (Current)12/1/2025
The following schematic diagrams reflect various methods of illustrating automotive transmission arrangements. These have been developed to facilitate a clear understanding of the functional interrelations of the gearing, clutches, hydrodynamic drive unit, and other transmission components. Two variations of transmission diagrams are used: in neutral (clutches not applied) and in gear. For illustrative purposes, some typical transmissions are shown.
Automatic Transmission and Transaxle Committee
AS9000 Audit Summary and Supplier Profile InstructionsAS9000-APPNDX1A (Current)12/19/2003
To assure customer satisfaction, aerospace industry manufacturers must produce world class quality products at the lowest possible cost. AS9000 standardizes, to the greatest extent possible, the quality system requirements of the aerospace industry. Standardization of compliance requirements results in cost savings due to the elimination or reduction of unique requirements developed for each different customer. AS9000 Appendix 1, AS9000 Audit Summary and Supplier Profile Instructions, facilitates the standardization of this process.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
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
VIRGIN BERYLLIUM BARS, RODS, AND SHAPESAMS7900 (Current)10/1/1991
AMS G Titanium and Refractory Metals Committee
Low Speed Thorax Impact Test Procedure for the HIII 50th Male DummyJ2779_202206 (Current)6/29/2022
Dummy Testing and Equipment Committee
Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) Vacuum Consumable Electrode RemeltedAMS6414N (Current)3/1/2023
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Titanium Alloy, Forgings 10V - 2Fe - 3Al Consumable Electrode Melted, Single-Step Solution Heat Treated and Aged 180 ksi (1241 MPa) Tensile StrengthAMS4983G (Current)5/28/2019
This specification covers a titanium alloy in the form of forgings 1.00 inch (25.4 mm) and under in nominal cross-sectional thickness and of forging stock of any size.
AMS G Titanium and Refractory Metals Committee
Electron Beam-Powder Bed Fusion (EB-PBF) Produced Preforms and Parts Titanium Alloy, 6Al - 4V Hot Isostatically PressedAMS7011 (Current)11/22/2022
This specification covers a titanium alloy in the form of preforms and parts produced by electron beam-powder bed fusion (EB-PBF) that are subjected to post-deposition hot isostatic press (HIP). Preforms may require subsequent machining or surface finishing to meet requirements for their intended final part application.
AMS AM Additive Manufacturing Metals
Treatment of Sheet Metal Parts Corrosion-Resistant SteelAMS2550F (Current)9/20/2017
This specification covers the engineering requirements for a treatment to provide enhanced corrosion resistance to sheet metal parts, such as brackets, spacers, and washers, fabricated from martensitic Corrosion-resistant steels, usually AMS 5504 or AMS 5508 and having hardness not higher than 40 HRC, or ferritic corrosion-resistant steels, usually AMS 5506. The treatment is not recommended for use on parts subject to impact in service.
AMS B Finishes Processes and Fluids Committee
Magnesium Alloy Castings, Sand 6.0Zn - 0.80Zr (ZK61A-T5) Precipitation Heat TreatedAMS4444E (Current)5/19/2017
This specification covers a magnesium alloy in the form of sand castings.
AMS D Nonferrous Alloys Committee
Uniform Measurement Units for Leakage RatesARP1405 (Current)1/1/1992
AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee
Metal Clad Fibers for Electrical Shielding and Harness OverbraidAIR5464A (Current)12/5/2023
Over the past two and one-half decades several metal clad fibers and fabrics have been developed to provide aerospace vehicle designers with a conductive, lighter weight alternative to coated copper, coated stainless steel and steel wire used for cable and wire shielding and harness overbraids on electrical cables. Several of these candidates have been unable to provide the strength or thermal stability necessary for the aerospace environment. However, several polymer-based products have shown remarkable resistance to the rigorous environment of aerospace vehicles. Concurrent with these fiber developments, there have been changes in the structures of aerospace vehicles involving greater use of nonmetallic outer surfaces. This has resulted in a need for increased shielding of electrical cables which adds substantial weight to the vehicle. Thus, a lighter weight shielding material has become more critical to meet the performance requirements of the vehicle. This report covers the
AE-8D Wire and Cable Committee
Methods and Processes for Evaluation of Aerodynamic Effects of SAE-Qualified Aircraft Deicing/Anti-Icing FluidsARP6852E (Current)4/1/2024
This ARP describes methods that are known to have been used by aircraft manufacturers to evaluate aircraft aerodynamic performance and handling effects following application of aircraft ground deicing/anti-icing fluids (“fluids”), as well as methods under development. Guidance and insight based upon those experiences are provided, including: Similarity analyses. Icing wind tunnel tests. Flight tests. CFD and other numerical analyses. This ARP also describes: The history of evaluation of the aerodynamic effects of fluids. The effects of fluids on aircraft aerodynamics. The testing for aerodynamic acceptability of fluids for SAE and regulatory qualification performed in accordance with AS5900. Additionally, Appendices A to E present individual aircraft manufacturers’ histories and methodologies, which substantially contributed to the improvement of knowledge and processes for the evaluation of fluid aerodynamic effects, and Appendix F considers the modeling of fluid removal from
G-12ADF Aircraft Deicing Fluids
Mechanical Splice for Aerospace Fiber Optic CablesAS5405 (Current)10/7/2024
This document defines performance standards which mechanical fiber optic cable splices must meet to be accepted for use in aerospace platforms and environments.
AS-3 Fiber Optics and Applied Photonics Committee
Human Engineering Considerations for Design and Implementation of Perspective Flight Guidance DisplaysARP5589 (Current)1/5/2005
The document focuses on perspective flight displays with or without guidance and is intended for flight deck display applications. Further, this document does not directly address the presence or absence of background information, e.g., synthetic and/or enhanced imagery. Such issues are addressed in a separate E/SVS document. Since this document provides recommendations, the guidance is provided in the form of “should” statements as opposed to the “shall” statements that appear in standards and regulations. When “shall” statements are used, the regulation or standard is referenced (where applicable).
G-10P Perspective Flight Guidance Committee
Insulation Blanket, Thermal-AcousticalAMSI7171A (Current)9/23/2011
This specification covers the requirements of composite blankets suitable for acoustical and thermal insulation of the walls of aircraft compartments within the temperature range of -65°F to +175°F (-54°C to +80°C).
AMS CE Elastomers Committee
BOLT, MACHINE, DOUBLE HEX, EXTENDED WASHER HEAD, CLOSE TOL. SHANK, UNS N07718, 185 KSI MIN, .1900-32 UNJF-3A (STRESS RUPTURE RESISTANT)AS3417C (Current)8/19/2022
E-25 General Standards for Aerospace and Propulsion Systems
Splices, Fiber Optics, For Aerospace Inter-Connection SystemsMA5405B (Current)3/18/2018
This specification covers design and performance requirements of fiber optic splices for optical distribution systems in aerospace vehicles and provides a means of procurement of such devices.
AS-3 Fiber Optics and Applied Photonics Committee
Molybdenum Disulfide, Technical, Lubrication GradeAMSM7866B (Current)9/22/2017
This specification covers the requirements for procurement of one grade of powdered molybendum disulfide to be used in lubricants and greases for surfaces where boundary conditions exist.
AMS B Finishes Processes and Fluids Committee
Polyamide Type 6-6, Plastic Moldings and ExtrusionsAMS3617F (Current)6/13/2019
This specification covers one type of Polyamide Type 6-6 (nylon) thermoplastic resin in the form of moldings and extrusions.
AMS P Polymeric Materials Committee
Steel Sheet, Strip, and Plate 0.48 - 0.55C (SAE 1050)AMS5085K (Current)4/13/2022
This specification covers a carbon steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)AMSS6758B (Current)11/30/2017
This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
Pass-Thru Extended Feature - IPv4J2534-2/16_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 4 (IPv4) 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 J2534-2/16_0500 interface shall be compliant to the Internet Protocol version 4 (IPv4) 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 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
ABS Exciter Ring Location StandardizationJ1730_202310 (Current)10/2/2023
This SAE Recommended Practice establishes the antilock brake system (ABS) sensor interface and envelope dimensions for standardizing the location of the ABS rings mounted on or integral to the inboard end of spoke wheels, hubs, rotors, and hub-rotor assemblies on the following axle designations as defined in SAE J1842. a FF b FL c FC d FH e L f R g U h W j N k P
Truck and Bus Wheel Committee
Aircraft Tire Selection and QualificationARP6822 (Current)12/3/2025
This document provides basic information that should be considered when an aircraft tire is needed for a new application. These guidelines are harmonized with existing regulatory and SAE documents and with the Care and Service Manuals of the tire manufacturers. In general, they should be pertinent to both civil and military aircraft.
A-5C Aircraft Tires Committee
RING, RETAINING SPIRAL, INTERNAL, HEAVY DUTY, CRES (UNS S30200)AS3215B (Current)5/10/2023
E-25 General Standards for Aerospace and Propulsion Systems
Iron, Electrical, Bar and Strip Cold Finished, AnnealedAMS7713C (Current)1/13/2016
This specification covers electrical iron in the form of bar and strip.
AMS E Carbon and Low Alloy Steels Committee
Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Lightweight, Hydraulic and PneumaticAS1339K (Current)5/2/2025
This SAE Aerospace Standard (AS) defines the requirements for a lightweight polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, 400 °F, high pressure, 3000 psi, aircraft hydraulic systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Silicone (PVMQ) Rubber Extreme-Low-Temperature Resistant 75 - 85AMS3338G (Current)5/27/2014
This specification covers a silicone (PVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
On-Board Diagnostics Implementation GuideJ1939/03_202105 (Current)5/19/2021
SAE J1939-03 provides requirements and guidelines for the implementation of on-board diagnostics (OBD) on heavy-duty vehicles (HDV) using the SAE J1939 family of standards. The guidelines identify where the necessary information to meet OBD regulations may be found among the SAE J1939 document set. Key requirements are identified here to ensure the interoperability of OBD scan tools across individual OBD-compliant vehicles. Market-defined regulations permit the use of SAE J1939 to meet OBD requirements. Implementers are cautioned to obtain and review the specific regulations for the markets where their products are sold. This document is focused on guidelines and requirements to satisfy the State of California Air Resources Board (CARB), the authors of 13 CCR 1971.1, United States Environmental Protection Agency, Euro IV and V requirements from European Commission directives, and UN/ECE WP 29 GRPE WWH OBD Global Technical Regulation (GTR).
Truck and Bus Control and Communications Network 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
TS220 Amendment Record for Technical Specification TS220TS220AR-2 (Current)4/30/2017
No Scope available.
Engine and Airframe Technical Standards Committee (TSC)
FITTING ASSEMBLY, CROSS, REDUCER, BEAM SEAL, 3000/4000 PSI, FOUR FEMALE ENDSAS85421/9B (Current)11/20/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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
Delegated Product Release VerificationAS9117A (Current)6/12/2026
This standard specifies requirements for DPRV to establish common product/service requirements for use at all levels of the supply chain. This standard shall apply when an organization elects to delegate product release verification by contractual flow down to their supplier (reference 9100 and 9110 standards) to perform product acceptance on their behalf. The delegating organization shall use this standard as the baseline for establishing a DPRV process, although they may include additional contract requirements to meet their specific needs.
SAE Committee
FIBER OPTIC ACTIVE DEVICE SPECIFICATIONARINC804-1 (Current)11/15/2007
This document provides information on active devices used for avionics fiber optic applications. The main body of the document begins with the scope and rationale. It continues with a technology introduction to optoelectronic active devices and then a selection guide that would enable a system design engineer to use the documents in the Fiber Optics series to select or specify suitable optoelectronic active devices for avionics applications. The main document also includes environmental guidelines for active devices to be used in avionics applications. These are included as guidance for commercial aircraft use and are included with the caveat that the requirements of any particular aircraft platform or customer would supersede these generic guidelines.
Airlines Electronic Engineering Committee
Motor Vehicle Brake FluidJ1703_202510 (Current)10/15/2025
This SAE Standard covers motor vehicle brake fluids of the nonpetroleum type, based upon glycols, glycol ethers, and appropriate inhibitors, for use in the braking system of any motor vehicle, such as a passenger car, truck, bus, or trailer. These fluids are not intended for use under arctic conditions. These fluids are designed for use in braking systems fitted with rubber cups and seals made from styrene-butadiene rubber (SBR) or a terpolymer of ethylene, propylene, and a diene (EPDM).
Brake Fluids Standards Committee
National Aerospace and Defense Contractors Accreditation Program Quality Assurance Program Requirements - ProcurementAS7106/3A (Current)6/12/2017
This document has been declared "CANCELLED" as of June 2017. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index. Cancelled specifications are available from SAE.
Nadcap Management Council
INSERT - CRES HELICAL COIL FINE THREAD, LOCKING (LOW FRICTION SYSTEMS) 2 DIA NOM LENGTHAS3095A (Current)4/4/2024
E-25 General Standards for Aerospace and Propulsion Systems
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