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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
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
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
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
Digital Fiber Optic Link Loss Budget Methodology for Aerospace PlatformsAS5603A (Current)10/7/2024
This document defines the steps and documentation required to perform a digital fiber optic link loss budget. This document does not specify how to design a digital fiber optic link. This document does not specify the parameters and data to use in a digital fiber optic link loss budget.
AS-3 Fiber Optics and Applied Photonics Committee
Braking Performance--Roller/CompactorsJ1136_198704 (Current)9/1/1987
Minimum performance criteria for service braking systems, secondary stopping systems, and parking systems for all self-propelled vibratory and static roller/compactors are provided in this SAE Recommended Practice. The purpose of this document is to define minimum braking system performance for in-service machines and to provide test criteria by which machine braking system performance may be verified.
Construction Agricultural and Off Road Machinery Council
Disc Wheel Hub/Spoke Wheel and Axle Interface Dimensions - Truck and BusJ1842_202306 (Current)6/12/2023
This SAE Recommended Practice is intended for hubs and spoke wheels used on Class 6, 7, and 8 truck/truck-tractor non-powered front axles, powered and non-powered rear axles and trailer axles, for which bearing setting is manually adjusted. Assemblies using spacers to control bearing preload and endplay may differ in geometry and bearing componentry.
Truck and Bus Wheel Committee
Self-Propelled Sweepers - Air Flow Performance - Part 2: Suction/Blower Fan PerformanceJ1792/2_202607 (Current)7/1/2026
This SAE Standard establishes a test method and a definition for disclosing the performance of suction/blower fans when applied to self-propelled sweepers that solely use a pneumatic conveyance means for the collection and transfer of “sweepings” into a collection hopper.
MTC2, Sweeper, Cleaner, and Machinery
Rubber, Ethylene-Propylene, General PurposeAMSR83285A (Current)11/7/2011
This specification covers two grades of ethylene-propylene rubber having excellent resistance to ozone and hot water, but poor resistance to hydrocarbon oils or solvents.
AMS CE Elastomers Committee
Unsalvageable Items Management – Requirements for Aviation, Space, and Defense OrganizationsAS9147 (Current)5/20/2021
This standard is applicable to all items used for manufacturing, maintenance, and repair of aviation, space, and defense products from the raw material to the final product (e.g., aircraft, structural items, constituent assemblies, standard parts, consumables with conformity and/or safety impact). This standard considers items dispositioned as scrap in accordance with 9100-series standards’ supporting nonconformity management, corrective action, or organization decisions (e.g., obsolescence, inventory management, missing traceability documentation). The requirements specified in this standard are complementary (not alternative) to contractual and applicable statutory and regulatory requirements. Should there be a conflict between the requirements of this standard and applicable statutory or regulatory requirements, the applicable statutory or regulatory requirements take precedence. This standard defines requirements and actions to be taken after the disposition decision to control the
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, EXTRUDED TFE, POLYIMIDE COATED, NICKEL-COATED COPPER CONDUCTOR, 600-VOLT, ROHSAS22759/29B (Current)4/5/2019
AE-8D Wire and Cable Committee
Aluminum Alloy, Rolled or Cold-Finished, Bars, Rods, Wire, and Flash-Welded Rings, Annealed, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-O)AMS4115L (Current)6/19/2026
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, wire, and flash-welded rings and of stock for flash-welded rings.
AMS D Nonferrous Alloys Committee
Rolling Element Bearing Axial and Radial Internal ClearanceARP5483/3B (Current)6/10/2026
This test method outlines the standard procedure for measuring the radial and axial internal clearance of rolling element bearings used in airframe controls.
ACBG Rolling Element Bearing Committee
CLAMP, LOOP TYPE, CUSHIONED SUPPORTAS5874 (Current)4/23/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CLAMP, LOOP, CUSHIONED, ELONGATED, METRICAS14272A (Current)12/30/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Environmental Conditions Applicable to Transport Aircraft Electrical EquipmentAIR31 (Current)12/16/2002
AE-7P Protective and Control Devices
CONNECTOR, RECEPTACLE, ELECTRIC THRU BULKHEAD, WALL MOUNTING FLANGE, SERIES I (CLASS E)AS31391A (Current)7/9/2026
AE-8C1 Connectors Committee
Design Objectives For Handling Qualities Of Transport AircraftARP842C (Current)2/1/1994
This recommended practice sets forth the design objectives for handling qualities applicable to transport aircraft operating in the subsonic, transonic and supersonic speed range. These objectives are not necessarily applicable to rotor or VTOL aircraft.
S-7 Flight Deck Handling Qualities Stds for Trans Aircraft
O-Ring Molded from AMS7276 Material, MetricMA3352A (Current)9/3/2019
A-6C2 Seals Committee
Shipping Containers - Aircraft Engines and ComponentsAS338 (Current)5/1/1995
E-25 General Standards for Aerospace and Propulsion Systems
Qualification Test Requirements & Procedures for Aerospace Industry Standard PartsTS202-13 (Current)8/24/2017
No Scope available.
Engine and Airframe Technical Standards Committee (TSC)
Aerospace Series Quality Management System Assessment for Maintenance Organizations (Based on ISO 9001:2000)AS9111A (Current)11/19/2012
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Application Guide for Aerospace Hydraulic MotorsARP4940A (Current)11/9/2021
This SAE Aerospace Recommended Practice (ARP) is an application guide for fixed and variable displacement hydraulic motors. It provides details of the characteristics of fixed and variable displacement hydraulic motors, architectures, circuit designs, controls, and typical applications. The applications include airborne and defense vehicles with emphasis on high performance applications.
A-6C4 Power Sources Committee
Polytetrafluoroethylene Film General Purpose GradeAMS3662D (Current)5/13/2015
This specification covers one grade of polytetrafluoroethylene resin in the form of film.
AMS P Polymeric Materials Committee
Alternative Automotive FuelsJ1297_201710 (Current)10/4/2017
This SAE Information Report provides information on certain fuels that are being used or have been suggested as alternatives to motor gasoline (SAE J312) or automotive diesel fuel (SAE J313) for use in spark-ignition or compression-ignition engines. Some of these fuels are derived from petroleum while others are from non petroleum sources.
Fuels and Lubricants TC 7 Fuels Committee
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 5 - Material Specification for Unidirectional Carbon Fiber Tape Epoxy Prepreg for Repair and Film Adhesive for Repair, 120 to 145 °C (250 to 290 °F) CuringAMS6885/5 (Current)5/7/2026
AMS6885/5 is the Material Specification (MS) which defines the requirements of a unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. It also defines the requirements of an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
AMS CACRC Commercial Aircraft Composite Repair Committee
CONNECTORS, ELECTRICAL, CIRCULAR, MINIATURE, COMPOSITE, HIGH DENSITY, QUICK COUPLING, ENVIRONMENT RESISTANT, REMOVABLE CRIMP CONTACTS, RECEPTACLE, FLANGED (SERIES B)AS29600/20B (Current)1/27/2026
AE-8C1 Connectors Committee
Monitoring Aircraft Noise and Operations in the Vicinity of Airports: System ValidationARP4721/2 (Current)7/12/2012
This SAE Aerospace Recommended Practice (ARP) provides engineering methods that can be applied to monitoring aircraft noise and operations in the vicinity of airports using either attended or unattended monitoring systems, as well as methods for validation of measurement results from permanent systems. Part 1 provides guidance on the components, installation and administration of permanent systems and guidance on analysis of data collected from temporary monitoring of aircraft noise. Part 2, this part, describes both system screening tests and detailed test methods for validating the data reported by permanently installed systems. This document is intended as a guide toward standard practice and is subject to change with experience and technical advances. Potential users include: airport proprietors, airport neighbors, federal, state and local government agencies, equipment vendors and other public bodies and officials. Potential applications include: Part 1 - development of a basis
A-21 Aircraft Noise Measurement Aviation Emission Modeling
AGS912 BOW, D-SHAPED (FOR CHAIN SHACKLE)AGS912-8 (Current)9/3/2024
Scope is unavailable.
Engine and Airframe Technical Standards Committee (TSC)
Production, Handling, and Dispensing of SAE J1703 Motor Vehicle Brake Fluids and SAE J1704 Borate Ester-Based Brake FluidsJ1706_202306 (Current)6/27/2023
This SAE Recommended Practice is intended to provide basic recommended practices for aid in the development and use of safe and efficient practices for all operations involving the production, handling, and dispensing of SAE J1703 motor vehicle brake fluids and SAE J1704 borate ester-based brake fluids.
Brake Fluids Standards Committee
815 Embedded Interchange Format for Obstacle DatabasesARINC815 (Current)12/21/2018
This document defines an open encoding format for obstacle databases. This format, when designed and implemented, will enable a quick, economic, and efficient use of Obstacle Databases (ObsDBs). However, since industry does not require applications to be standardized, data interpretation is not addressed in this document.
Airlines Electronic Engineering Committee
Considerations for Hydrogen Fuel Cells in Airborne ApplicationsAIR7765 (Current)11/18/2019
The scope of this joint EUROCAE/SAE report is to compile the considerations relating to airborne application of hydrogen fuel cells. This document provides a comprehensive analysis of the use of hydrogen as a fuel by describing its existing applications and the experience gained by exploiting fuel cells in sectors other than aviation. The use of hydrogen fuel cells in aircraft can help in meeting aviation environmental targets (including noise pollution) and can be vital to achieving efficient electrically propelled air vehicles. The experience gained with mature fuel cells in terrestrial applications and the handling of other gases in aviation, as presented herein, will help in alleviating safety concerns and in demystifying the usage of hydrogen in aviation.
AE-7F Hydrogen and Fuel Cells
INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE POLYETHYLENE TEREPHTHALATE, NON-CROSSLINKEDAS23053/7 (Current)1/12/2022
AE-8D Wire and Cable Committee
628P2-9 Cabin Equipment Interfaces, Part 2, Cabin Management and Entertainment Systems - Seat InterfacesARINC628P2-9 (Current)7/10/2017
This document defines standard electrical and mechanical interfaces of the In-Flight Entertainment system (IFES) equipment associated with the seat (including the headphones, passenger control unit, seat video display, personal video player, telephone hand set, and seat electronics box). Supplement 9 updates applicable interfaces for USB 3.1 outlets in passenger seats.
Airlines Electronic Engineering Committee
422-1 Guidance for Modification Status Indicators and Avionics Service BulletinsARINC422-1 (Current)7/6/2016
This standard provides guidance to the maintenance community for identifying the modification status of avionics components and for preparing avionics service bulletins. This standard coordinates various methods used by airframe manufacturers and operators, for marking or identifying avionics that has been modified.
Avionics Maintenance Committee
664P3-2 Aircraft Data Network, Part 3 - Internet-Based Protocols and ServicesARINC664P3-2 (Current)2/1/2009
This specification defines Network and Transport layer provisions for data networks that are installed on commercial aircraft. The definitions are based on Internet Engineering Task Force (IETF) Internet protocol and service standards that have been published as Request for Comments (RFC). In some cases the protocols and services are tailored for use on board aircraft. The specification identifies two types of networks: First, Compliant Aircraft Data Network, which operates fully within the applicable Internet specifications. Second, Profiled Aircraft Data Network, in which one or more industry standard protocols have been extended to address the unique environment of aircraft installations. Within the specification, the functionality of Internet protocols and services are defined with the intent that interoperability of components connected to onboard data networks can be achieved without undue restrictions on the component designer.
Airlines Electronic Engineering Committee
FITTING, PLUG, BEAM SEAL, HYDRAULIC, 5000 PSIAS8440 (Current)8/14/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Adhesive Compound, Epoxy Resin High Temperature ApplicationAMS3692C (Current)1/20/2022
This specification covers a two-component adhesive compound, an epoxy resin base and a hardener, in the form of a paste.
AMS P17 Polymer Matrix Composites Committee
Infrasound Phenomenon in Engine Test CellsAIR5303A (Current)10/1/2024
This SAE Aerospace Information Report (AIR) has been written for individuals associated with the ground-level testing of large turbofan and turbojet engines, particularly those who are interested in infrasound phenomena.
EG-1E Gas Turbine Test Facilities and Equipment
850 System Level Guidance for Data Loading LRU Target SystemsARINC850 (Current)1/12/2024
This document provides LRU Target System manufacturers, airframe manufacturers, and others with principles, concepts, and guidance for the design of data loading targets and complex data loading target systems. The mechanisms described in this paper apply to federated LRUs and complex platforms, such as airborne servers and data loading of IMA systems. The document guides data loading system design for Target Systems: How to avoid common pitfalls during the system/software design architectural design phase Specific considerations to actively decide on in early conceptual design phases Increase of useability and robustness for the end-user and maintainer of data loading targets This document focuses on reaching common design objectives for Target System data loading systems and circumventing repeatedly occurring issues rooted in system design. Commonly desired design objectives include: Architectural choices – Simplify the upload process of LRU Target Systems of the same type Reducing
Airlines Electronic Engineering Committee
Fiber Optic Wavelength Division Multiplexed (WDM) Singlemode Interconnect and Component Standards Mapping for Aerospace Platform Applications – Device Level SpecificationAIR5667 (Current)10/8/2024
The purpose of this document is to serve as a resource to aerospace designers who are planning to utilize Wavelength Division Multiplexed (WDM) interconnects and components. Many WDM commercial systems exist and they incorporate a number of existing, commercially supported, standards that define the critical parameters to guide the development of these systems. These standards ensure interoperability between the elements within these systems. The commercial industry is motivated to utilize these standards to minimize the amount of tailored development. However, since some of the aerospace parameters are not satisfied by the commercial devices, this document will also try to extend the commercial parameters to those that are necessary for aerospace systems. The document provides cross-references to existing or emerging optical component and subsystem standards. These parameter definitions, test methods, and procedures typically apply to telecommunications application and in some cases
AS-3 Fiber Optics and Applied Photonics Committee
Metal Injection Molded Nickel Based Alloy 718 Parts Hot Isostatically Pressed, Solutioned and AgedAMS5917 (Current)6/19/2026
This specification covers a corrosion and heat-resistant nickel alloy in the form of metal injection molded (MIM) parts.
AMS F Corrosion and Heat Resistant Alloys Committee
Cloth, Glass Finished for Resin LaminatesAMS3824C (Current)10/4/2022
This specification covers “E” glass in the form of woven cloth.
AMS P17 Polymer Matrix Composites Committee
Aluminum Alloy 7178, Bar, Rod, Shapes, Tube, and Wire, ExtrudedAMSQQA200/13C (Current)1/4/2018
This specification covers the specific requirements for aluminum alloy 7178 bar, rod, shapes, tube, and wire produced by extrusion.
AMS D Nonferrous Alloys Committee
607-3 Design Guidance for Avionics EquipmentARINC607-3 (Current)8/1/1998
This standard provides general guidelines for the design of avionics equipment. It represents the desires of the airline industry resulting from extensive airline experience. Manufacturers are urged to use this standard when initially starting the design of new equipment. Airplane Personality Module (APM) specifications are included.
Airlines Electronic Engineering Committee
Rivets, Alloy, Corrosion and Heat Resistant 52Co-20Cr-10Ni-15W Solution Heat Treated Procurement Specification ForAS7236A (Current)4/1/2024
This procurement specification covers aircraft-quality solid rivets made from a corrosion- and heat-resistant cobalt alloy of the type identified under the Unified Numbering System as UNS R30605.
E-25 General Standards for Aerospace and Propulsion Systems
INSULATING COMPONENTS, MOLDED, ELECTRICAL, HEAT SHRINKABLE FLUOROELASTOMER, FLEXIBLE, CROSSLINKEDAS81765/4A (Current)4/18/2017
AE-8D Wire and Cable Committee
437-1 Guidelines For Training FacilitiesARINC437-1 (Current)11/7/2012
The purpose of ARINC Report 437 is to provide guidance when planning a new training facility, extending an existing training facility, or adding new equipment to an existing facility.
Flight Simulator Engineering and Maintenance Committee
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