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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
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
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
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
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
825-4 General Standardization of CAN (Controller Area Network) Bus Protocol for Airborne UseARINC825-4 (Current)9/25/2018
This document defines a Controller Area Network (CAN) interface for current and future commercial aircraft applications. The latest version, Supplement 4, expands the document to include CAN Flexible Data rate also known as CAN FD. CAN FD has the potential to provide 4 Mbps of data transfer. Supplement 4 also introduces four new appendices on the topics of: ARINC 825 Compliance, Configuration of Bit Timing, Management Information Base (MIB) Counters, and CAN Bus Security Considerations.
Airlines Electronic Engineering Committee
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)
A Guide to Aircraft Power Train MonitoringAIR4174B (Current)5/28/2026
The purpose of this SAE Aerospace Information Report (AIR) is to provide management, designers, and operators with information to assist them to decide what type of power train monitoring they desire. This document is to provide assistance in optimizing system complexity, performance, and cost effectiveness. This document covers all power train elements from the point at which energy in a turbine or electric engine is converted via a gear train to mechanical energy for propulsion purposes. The document covers aircraft engine driven transmission and gearbox components, their interfaces, drivetrain shafting, drive shaft hanger bearings, and associated rotating accessories, propellers, and rotor systems as shown in Figure 1. For guidance on monitoring additional engine components not addressed herein (e.g., main shaft bearings and compressor/turbine rotors), refer to ARP1839. This document addresses rotary and fixed wing applications for rotor, turboprop, turbofan, prop fan, and lift fan
E-32 Aerospace Propulsion Systems Health Management
WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYMIDE INSULATED, NORMAL WEIGHT, NICKEL COATED, EXTRA HIGH STRENGTH COPPER ALLOY, 260 °C, 600 VOLT, ROHSAS22759/96B (Current)3/15/2022
AE-8D Wire and Cable Committee
Seat Belt Hardware Webbing Abrasion Test ProcedureJ339_201306 (Current)6/11/2013
This SAE Recommended Practice describes a test procedure for evaluating the abrasion resistance characteristics of webbing when used in hardware of seat belt assemblies such as those described in SAE J140.
Motor Vehicle Council
Determination of Costs and Benefits from Implementing an Integrated Vehicle Health Management SystemARP6275A (Current)2/11/2021
This Aerospace Recommended Practice (ARP) provides insights on how to perform a cost versus benefit (C/B) analysis (CBA) to determine the return on investment that would result from implementing an integrated health management (HM) system on an air vehicle. The word “integrated” refers to the combination or “roll up” of sub-systems health management tools to create a platform-centric system. This document describes the complexity of features that can be considered in the analysis and the different tools and approaches for conducting a CBA, and it differentiates between military and commercial applications. This document is intended to help those who might not have a deep technical understanding or familiarity with HM systems but want to either quantify or understand the economic benefits (i.e., the value proposition) that an HM system could provide. Prognostics is a capability within some HM systems that provides an estimation of remaining useful life (RUL) or time to failure and so
HM-1 Integrated Vehicle Health Management Committee
Electrical Propulsion Rotating Equipment - Off-Road DumperJ1317_201302 (Current)2/21/2013
This recommended practice applies to the rotating equipment in the electrical propulsion systems on electrically propelled dumpers. It also applies to the rotating equipment installed on trailers connected to electrically propelled dumpers. The recommended practice does not apply to rotating equipment such as windshield wiper motors, battery charging generators, etc. that may be used on dumpers.
CTTC C2, Electrical Components and Systems
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)
TS112 Manual of Recommended Lofting ProceduresTS112-3 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS146 Technical Specification for the Performance of Insert - Metric, Thinwall, Screw Locking EN2404 (Inconel 718) Silver CoatedTS146-2 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
802-3 Fiber Optic CablesARINC802-3 (Current)8/27/2018
This specification covers the performance requirements, dimensions, quality assurance criteria, test procedures, and cable codification for fiber optic cables suitable for use on commercial aircraft.
Airlines Electronic Engineering Committee
800P1 Cabin Connectors and Cables, Part 1, Description and OverviewARINC800P1 (Current)11/19/2012
This document is the first of a multi-part specification that will provide a catalog of cabin connector and cables that may be used in ARINC Standard cabin systems, including In-Flight Entertainment. Part 1 describes connector and cable requirements and evaluation criteria for the interface components used in the integration of cabin systems. Future releases will define connectors, contacts, and termination methods in Part 2. Cables will be specified in Part 3.
Airlines Electronic Engineering Committee
INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE POLYETHYLENE TEREPHTHALATE, NON-CROSSLINKEDAS23053/7 (Current)1/12/2022
AE-8D Wire and Cable Committee
Test Cell Thrust MeasurementAIR4951A (Current)10/20/2023
Thrust measurement systems come in many sizes and shapes, with varying degrees of complexity, accuracy and cost . For the purposes of this information report, the discussions of thrust measurement will be limited to axial thrust in single-axis test systems.
EG-1E Gas Turbine Test Facilities and Equipment
FITTING, PLUG, BEAM SEAL, HYDRAULIC, 5000 PSIAS8440 (Current)8/14/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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
Load Support Characteristics of Aircraft GreasesAIR44 (Current)5/1/1995
The objective of this work was to develop a relatively simple bench test or performance test, or a combination of tests, which would be valid for evaluating greases in respect to load support characteristics, when the greases were used in journal bearings or in actuator-type mechanisms.
E-25 General Standards for Aerospace and Propulsion Systems
TS321 Test for Electrical Connectors Insert RetentionTS321-1 (Current)8/1/1985
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS114 Guide to Packaging SpecificationsTS114-2 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Steel, Bars, Wire, and Forgings 10.5Mo - 6W - 3.75Cr - 2V (1.25 - 1.40C) Powder Metallurgy Product Hot Isostatically PressedAMS6558A (Current)5/16/2023
This specification covers a premium aircraft-quality, high-alloy steel gas-atomized and HIP-consolidated in the form of bars, wire, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Contamination Studies of Aircraft GreasesAIR42 (Current)5/1/1995
Certain techniques involved in determining the dirt or abrasive content of aircraft greases are considered inadequate. It is desirable to develop a method of analysis which will definitely identify the quantity, size, and degree of abrasiveness of foreign substances in lubricating greases.
E-25 General Standards for Aerospace and Propulsion Systems
Dynamic Durability Testing of Seat Cushions for Off-Road Work MachinesJ1454_202302 (Current)2/14/2023
This SAE Standard describes a laboratory test procedure for comparatively evaluating the durability and fatigue life qualities of a complete seat cushion by submitting the seating surface of the cushion to repetitive compressive and rotational loading with a simulated human buttocks.
HFTC4, Operator Seating and Ride
Spark PlugsJ548_198708 (Current)8/1/1987
Ignition Standards Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, BLACK OXIDE, STEEL, UNS G87400, 125 KSI MIN .3750-24 UNF-3AAS91721B (Current)6/16/2015
E-25 General Standards for Aerospace and Propulsion Systems
Health, Safety and First AidAS6286/5A (Current)11/12/2019
This document shall be used in conjunction with: AS6286 - Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground AS6286/1 - Processes including Methods AS6286/2 - Equipment AS6286/3 - Fluids AS6286/4 - Weather AS6286/6 - Aircraft Deicing/Anti-icing Diagrams, No-Spray-Zones
G-12T Training and Quality Programs 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
Qualification Test Requirements & Procedures for Aerospace Industry Standard PartsTS202-13 (Current)8/24/2017
No Scope available.
Engine and Airframe Technical Standards Committee (TSC)
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
AS6021 Aerospace Fiber Optic Cable Assembly Drawing SpecificationAS6021A (Current)12/29/2020
This SAE Aerospace Standard (AS) defines the items that shall be considered when creating a fiber optic cable assembly specification and source control drawing intended for installation on aerospace platforms.
AS-3 Fiber Optics and Applied Photonics Committee
COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDINGAS7515C (Current)8/21/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
ELBOW, TUBE - 90°, BULKHEAD, FLARELESS TUBE UNIVERSAL TO FLARED TUBEAS24651B (Current)1/17/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Aerospace Pressurization System DesignAIR1168/7A (Current)7/25/2011
The pressurization system design considerations presented in this AIR deal with human physiological requirements, characteristics of pressurization air sources, methods of controlling cabin pressure, cabin leakage control, leakage calculation methods, and methods of emergency cabin pressure release.
AC-9 Aircraft Environmental Systems Committee
Safety Considerations - Smoking in Lavatories of Transport AircraftARP4740A (Current)2/24/2016
This ARP addresses the issue of passengers smoking in aircraft lavatories and the need to improve warnings about the danger of fire caused by smoking.
S-9B Cabin Interiors and Furnishings Committee
Aircraft Surface Coating Interaction with Aircraft Deicing/Anti-Icing FluidsAIR6232 (Current)6/10/2026
This SAE Aerospace Information Report (AIR) provides descriptions of test methods for determining if an aircraft surface coating of any thickness has adverse effects on aircraft deicing/anti-icing fluids with respect to fluid holdover time performance and aerodynamic performance. Although not the primary mandate of the G-12 Aircraft Ground Deicing Committee, this document also provides descriptions of suggested test methods for evaluating aircraft surface coatings with respect to durability, hardness, weathering, aerodynamic drag, ice adhesion, ice accumulation, contact angle, and thermal conductivity. These additional tests can provide informational data for characterizing the coatings and may be useful to operators when evaluating the coatings.
G-12ADF Aircraft Deicing Fluids
Vacuum Excavation and Sewer Cleaning Equipment - Safety RequirementsJ3107_202109 (Current)9/21/2021
This SAE Standard provides safety requirements for vacuum excavation and sewer cleaning equipment. This document is not intended to cover equipment addressed by other on-road federal, state, and local regulations. Truck-mounted or trailer-mounted vehicles are required to meet local or regional on-road requirements, as applicable.
MTC9, Trenching and Horizontal Earthboring Machines
INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE, POLYOLEFIN, HEAVY-WALL, COATED, FLEXIBLE, OUTER WALL CROSSLINKEDAS23053/15 (Current)1/11/2022
AE-8D Wire and Cable Committee
ELBOW, 90°, BEAM SEAL, MALE 4000 psi, HYDRAULICAS4542 (Current)1/7/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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
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