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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
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
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
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
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
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
Aluminum Alloy, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn; (2024-T861), Solution Heat Treated and Cold Worked, and Artificially AgedAMS4271A (Current)7/25/2013
This specification covers an aluminum alloy in the form of sheet and plate supplied in the - T861 temper.
AMS D Nonferrous Alloys Committee
FITTING, TEE, BEAM SEAL, 3000/4000 PSI, BULKHEAD ON BRANCH, MALE ENDSAS85421/17D (Current)10/26/2022
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Lightning Protection and Static ElectrificationAIR1406 (Current)12/26/1991
AE-4 Electromagnetic Compatibility (EMC) 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
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
Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation AircraftAS8049E (Current)5/16/2025
This SAE Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal is to achieve comfort, durability, and occupant protection under normal operational loads and to define test and evaluation criteria to demonstrate occupant protection when a seat/occupant/restraint system is subjected to statically applied ultimate loads and to dynamic impact test conditions set forth in Title 14, Code of Federal Regulations (14 CFR) parts 23, 25, 27, or 29 (as applicable to the seat type). Two formats of this standard (MS Excel and Adobe PDF) are available. The standards provided in both formats (MS Excel and Adobe PDF) contain the same text.
Aircraft Seat Committee
TEE ASSEMBLY, FLARED TUBE, RETAINED NUT ON SIDE, FOR SEAL RINGAS4304A (Current)5/2/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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
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
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
727-1 Airborne Microwave Landing SystemARINC727-1 (Current)8/1/1987
This standard sets forth the characteristics of MLS receiver processors intended for installation in all types of commercial transport aircraft. The function of the airborne MLS receiver processor is the reception and processing of the MLS azimuth signals, the elevation signals, and the data transmitted from the MLS ground stations.
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
756-3 GNSS Navigation and Landing Unit (GNLU)ARINC756-3 (Current)2/27/2004
This standard describes the function of the GNLU, capable of providing enroute/terminal navigation, non-precision approach, and precision approach capabilities. The GNLS consists of a GNLU, associated controls and displays, antenna, and interfaces to other aircraft systems.
Airlines Electronic Engineering Committee
701-1 Flight Control Computer System (FCCS)ARINC701-1 (Current)4/1/1983
This standard sets forth the characteristics of a FCCS within an Automatic Flight System. The FCCS is intended to provide autoland capability for commercial aircraft. The document provides design guidance for the development and installation of a FCCS.
Airlines Electronic Engineering Committee
704A Inertial Reference System (IRS)ARINC704A (Current)3/26/1999
This standard defines a 4 MCU IRS, consisting of inertial measuring devices and associated electronics specifically designed for installation in commercial transport type aircraft. It may be used in place of ARINC 704 Inertial Reference Systems. This system additionally provides capability to be interfaced to an ARINC 743A GNSS Sensor, to enhance the accuracy of the inertially derived navigation data.
Airlines Electronic Engineering Committee
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
CIRCUIT BREAKER, RECYCLING, TRIP-FREE, PUSH-PULL, 1/2 THRU 5 AMPERE, TYPE IAS22074A (Current)6/17/2014
AE-7P Protective and Control Devices
Synchro, Control Differential Transmitter, Type 26V-11CDX4CAS20708/9B (Current)6/9/2016
AE-7A Generators and Controls Motors and Magnetic Devices
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
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
820 Cabin Architecture for Wireless Distribution SystemARINC820 (Current)8/13/2019
This document defines a secure Wi-Fi distribution network installed in the aircraft passenger cabin for passenger and crew use. Carry-on Portable Electronic Devices (PEDs) such as smart phones, tablets, and laptops may use this network to access public internet services provided on the aircraft.
Airlines Electronic Engineering Committee
Magnesium Alloy Castings, Die 9.0Al - 0.70Zn (AZ91D, Temper F) As CastAMS4490K (Current)5/30/2017
This specification covers a magnesium alloy in the form of die castings.
AMS D Nonferrous Alloys Committee
Sealing Compound, Electrically Conductive Corrosion InhibitingAMS3377A (Current)3/25/2015
This specification covers a synthetic rubber sealing compound which is electrically conductive when used in a faying surface, contains corrosion inhibitors, and supplied as a two-component system which cures at room temperature, suitable for application by extrusion gun or spatula.
AMS G9 Aerospace Sealing Committee
AS43800-899 BOLT, DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, .3125-24 UNJF-3AAS43800-7 (Current)2/26/2024
Scope is unavailable.
Engine and Airframe Technical Standards Committee (TSC)
Interior Automotive Plastic Part TestingJ1717_201707 (Current)7/13/2017
SAE J1717 is an advisory document suggesting minimum recommended testing, appearance evaluation, and protocol for specifying the recommendations with regard to Singular Unassembled Automotive Interior Trim Parts.
Plastics Committee
GASKET, FUSELAGE LIGHT – COVER SCREWAS8991A (Current)8/9/2018
E-25 General Standards for Aerospace and Propulsion Systems
A Comparison of Government Relay SpecificationsAIR875 (Current)12/16/2002
AE-7P Protective and Control Devices
TS331 Test for Electrical Connectors Climatic TestsTS331-2 (Current)10/1/1987
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS121 Manufacturing Specification for Studs, Bolts and Screws in DTD5639, EN2959 and EN3220 Material 1210 MPa (175,000 lbf/in²) Tensile at Room Temperature (for which Forging is Optional and Qualification is not a RequirementTS121-4 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS97 Recommended Design Guide on Rubber Materials for Aerospace ApplicationsTS97-2 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS172 Performance Specification for Nut, Union, Metric, Threaded, Self- Locking A286 Dry Film LubricatedTS172-4 (Current)12/1/2004
This technical specification document describes tests that certain parts may be required to meet. For example, this tech spec applies to AS63280-289. To view suppliers qualified against this standard, visit https://ts200.sae-itc.org/.
Engine and Airframe Technical Standards Committee (TSC)
TS80 Recommendations for the Control of Flammability Testing of Non-Metallic Materials and Textiles for Aeronautical PurposesTS80-2 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS64 Standard Method for Microscopic Evaluation of Hydraulic Fluid Samples for Particle ContaminationTS64-2 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS78 Recommended Technical Requirements for a General Purpose Grade of Silicone RubberTS78-3 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS70-AR Amendment Record for Technical Specification No .TS70TS70AR-5 (Current)11/1/2012
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
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
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