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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, 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, 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 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
FITTING ASSEMBLY, STRAIGHT, EXTENDED BULKHEAD SHANK, FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSIAS6106B (Current)5/5/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Balancing Machines – Description and Evaluation Vertical, Single-Plane, Non-Rotating Type for Gas Turbine RotorsARP6217 (Current)8/13/2025
Characteristics of vertical non-rotating balancing machines are described which make such machines suitable for balancing rigid unbladed gas turbine rotors or rotors with fixed, integral blades.
EG-1A Balancing Committee
PIN, STRAIGHT, HEADLESS, AMS5688, LOCKAS9105A (Current)1/9/2015
E-25 General Standards for Aerospace and Propulsion Systems
Commercial Aircraft Hydraulic System SizingARP6277 (Current)1/26/2021
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide guidelines for determining the hydraulic flow demands for all phases of commercial flight including details of sizing of associated hydraulic components such as hydraulic pumps, hydraulic accumulators, hydraulic reservoirs, hydraulic filters, and hydraulic tubing.
A-6A1 Commercial Aircraft Committee
COUPLING, MALE, 12 INCH AIR DUCTAS7365/3A (Current)6/11/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
COOLING DATA FOR TURBINE ENGINES IN HELICOPTERSARP996A (Current)3/27/2025
A tested method of data presentation and use is described herein. The method shown is a useful guide, to be used with care and to be improved with use.
S-12 Powered Lift Propulsion Committee
In-Service Fiber Optic Inspection, Evaluation and Cleaning, Best Practices, Physical Contact TerminiARP6283 (Current)10/7/2024
This document provides recommended best practice methods and processes for the in-service inspection, evaluation and cleaning of all physical contact (PC) fiber optic interconnect components (termini, alignment sleeves and connectors), test equipment and test leads for maintainers qualified to the approved aerospace fiber optic training courses developed in accordance with ARP5602 or ARINC807. This document also provides a decision-making disposition flowchart to determine whether the fiber optic components are acceptable for operation. For definitions of individual component parts refer to ARP5061.
AS-3 Fiber Optics and Applied Photonics 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
INSERT - CRES HELICAL COIL FINE THREAD, STRAIGHT, STUD LOCKING, 3 DIA NOM LENGTHAS3083A (Current)4/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
CLAMP, RECTANGULAR LOOP, CUSHIONED, WITH WEDGE, HIGH TEMPERATURE, STAINLESS STEEL, METRICMA2155/5 (Current)4/27/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYMIDE INSULATED, SMOOTH SURFACE, LIGHT WEIGHT, SILVER-COATED HIGH STRENGTH OR ULTRA HIGH STRENGTH COPPER ALLOY, 200 °C, 600 VOLTS ROHSAS22759/181A (Current)12/18/2019
AE-8D Wire and Cable Committee
CONNECTORS, ELECTRICAL, RECTANGULAR, RECEPTACLE ENVIRONMENT RESISTANT, CRIMP CONTACTS, DOUBLE INSERT, TYPE II, CLASS 1 (−65 °C TO +125 °C), SERIES 1, SHELL DESIGNATOR AAS81659/9B (Current)1/28/2022
AE-8C1 Connectors Committee
Balancing Machines: Tooling Design CriteriaARP4163A (Current)7/9/2025
This document establishes general design criteria, tolerances, and limits of application for tooling, fixtures, and accessories for mounting and driving gas turbine engine rotors on horizontal and vertical balancing machines.
EG-1A Balancing Committee
Marine Stern Drive and Inboard Spark-Ignition Engine On-Board Diagnostics Implementation GuideJ1939/5_201710 (Current)10/13/2017
This document describes the application of the SAE J1939 recommended practices for compliance with on-board diagnostic malfunction detection system requirements for marine sterndrive and inboard spark ignition engines, as mandated by the California Air Resources Board (CARB). These Otto-cycle engines are not derived from automotive diesel-cycle engines.
Truck and Bus Control and Communications Network Committee
Hose, Polytetrafluoroethylene TFE Fluorocarbon Resin Wire Braid ReinforcedAMS3380E (Current)4/30/2019
This specification covers a polytetrafluoroethylene resin in the form of extruded and sintered flexible tube reinforced with wire braid.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Procedure for the Calculation of Aircraft EmissionsAIR5715 (Current)7/27/2009
This AIR describes procedures for calculating emissions resulting from the main engines of commercial jet and turboprop aircraft through all modes of operation for all segments of a flight. Piston engine aircraft emissions are not included in this AIR. Some information about piston engine aircraft emissions can be found in FOCA 2007. The principal purpose of the procedures is to assist model developers in calculating aircraft emissions in a consistent and accurate manner that can be used to address various environmental assessments including those related to policy decisions and regulatory requirements. The pollutants considered in this document are: Nitrogen Oxides (NOx) Carbon Monoxide (CO) Total unburned Hydrocarbons (THC) Carbon Dioxide (CO2) Water (H2O) Sulfur Oxides (SOx) Volatile Organic Compounds (VOC) Methane (CH4) Non-Methane Hydrocarbons (NMHC) Non-Methane Volatile Organic Compounds (NMVOC) Nitrous Oxide (N2O) Particulate Matter (PM2.5 and PM10) As indicated above, hazardous
A-21 Aircraft Noise Measurement Aviation Emission Modeling
JAUS Unmanned Ground Vehicle Service SetAS6091 (Current)4/24/2025
This document defines a set of standard application layer interfaces called JAUS Unmanned Ground Vehicle Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned systems to communicate and coordinate their activities. The Unmanned Ground Vehicle Services represent the platform-specific capabilities commonly found in UGVs, and augment the Mobilty Service Set [AS6009] which is platform-agnostic. At present ten (10) services are defined in this document. These services are categorized as:
AS-4JAUS Joint Architecture for Unmanned Systems Committee
Aluminum Alloy, Sheet 2.4Li - 1.3Cu - 0.95Mg - 0.10Zr (8090-T6) Solution and Precipitation Heat Treated (Unrecrystallized)AMS4259B (Current)5/28/2015
This specification covers an aluminum alloy in the form of sheet.
AMS D Nonferrous Alloys Committee
Filaments, Boron Tungsten Substrate, ContinuousAMS3865C (Current)10/4/2022
This specification covers continuous filaments consisting of boron deposited on a tungsten substrate by the hydrogen reduction of boron trichloride.
AMS P17 Polymer Matrix Composites 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
Coating, Tungsten Carbide-Cobalt Coating, Detonation ProcessAMS2435H (Current)9/20/2017
This specification covers the engineering requirements for applying tungsten carbide/cobalt coatings to metal parts by the detonation process and the properties of such coatings.
AMS B Finishes Processes and Fluids Committee
350 °F Autoclave Cure, Low Flow Toughened Epoxy PrepregsAMS3961 (Current)12/2/2015
The intent of this specification is for the procurement of the material listed on the QPL and, therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program shall refer to the Quality Assurance section of this base specification, AMS3961. All material qualification and equivalency data has been archived and is available for review upon request. Contact the CMH-17 Secretariat (www.cmh17.org) for additional information.
AMS P17 Polymer Matrix Composites Committee
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
O-Ring Machined from AMS3668 MaterialAS9955B (Current)6/8/2020
This standard establishes the dimensional and visual quality requirements, lot requirements, and packaging and labeling requirements for O-rings machined from AMS3668 material. It shall be used for procurement purposes.
A-6C2 Seals Committee
Corrosion-Resistant Steel Parts: Sampling, Inspection and Testing for Surface PassivationAMSSTD753B (Current)4/4/2017
This standard describes general and detailed methods of sampling and testing for surface passivity of corrosion-resistant steel parts. These tests may also be useful to determine if there is a need for passivation.
AMS F Corrosion and Heat Resistant Alloys Committee
Pass-Thru Extended Feature - UART Echo ByteJ2534-2/3_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 UART Echo Byte 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 J2534-2/3_0500 interface shall be compliant to the UART Echo Byte 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 the SAE J2534-2/BA_0500 and SAE J2534-2/RE_0500 documents.
Vehicle E E System Diagnostic Standards Committee
Installation of Fuel Cell Systems in Large Civil AircraftAS6858 (Current)4/21/2023
This is a joint SAE/EUROCAE development. This document will be released as both an SAE Aerospace Specification (AS) and a EUROCAE Minimum Aviation System Performance Standard (MASPS). This document defines the technical requirements for the safe integration of gaseous hydrogen fueled Proton Exchange Membrane (PEM) Fuel Cell Systems (FCS) within the aircraft. Most of the technical concepts and approaches covered by this document represent current industry "best practice". Others require specific approval from the procuring activity before use. This requirement for approval is not intended to prohibit their use; but rather to ensure that the prime contractor has fully investigated their capability to perform reliably and to be sufficiently durable under the required conditions and that the prime contractor can present substantiating evidence for approval before the design is committed to.
AE-7F Hydrogen and Fuel Cells
Air Cargo Unit Load Devices – Center of Gravity Control MethodsARP36103A (Current)11/21/2012
This SAE Aerospace Recommended Practice (ARP) provides the industry agreed methods to keep the center of gravity (C.G.) location of loaded air cargo Unit Load Devices (ULDs) within the maximum horizontal and vertical limits allowed by their airworthiness approval.
AGE-2 Air Cargo
PLUG, PIPE, EXTERNAL THREADAS4863A (Current)1/28/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel Castings, Vacuum Melted, Vacuum Cast, Investment, Corrosion-Resistant 13Cr - 8.0Ni - 2.2Mo - 1.1Al 195 ksi (1344 MPa) Tensile Strength (Condition H1000) Homogenized, Solution, and Precipitation Heat TreatedAMS5412B (Current)5/10/2019
This specification covers a corrosion-resistant steel in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Aircraft Fuel Pump Mechanical and Electrical Safety DesignARP6385 (Current)10/18/2022
The requirements presented in this document address the key considerations for mechanical and electrical safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank.
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Physical Layer, 250 Kbps, Twisted Shielded PairJ1939/11_201612 (Current)12/6/2016
This document defines a physical layer having a robust immunity to EMI and physical properties suitable for harsh environments. CAN controllers are available which support the CAN Flexible Data Rate Frame Format. These controllers, when used on SAE J1939-11 networks, must be restricted to use only the Classical Frame Format compliant to ISO 11898-1:2015. 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
FITTING END, EXTERNAL TAPER PIPE THREAD, DESIGN STANDARDAS5201A (Current)3/13/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Plain Spherical Bearing Conformity ExaminationARP5448/6A (Current)4/24/2024
This method outlines a standard procedure for performing conformity tests of bearings utilizing liners of bonded polytetrafluoroethylene (PTFE). The data from these tests shall be used to determine if the product meets the conformity requirements of the applicable specification.
ACBG Plain Bearing 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
SHIELD FOR USE WITH AS90362 EXTERNAL POWER RECEPTACLESAS17845A (Current)3/2/2020
AE-8C1 Connectors Committee
Steel, Low Carbon Bars, and Wire 0.08 - 0.20AMS5061H (Current)8/14/2017
This specification covers a low-carbon steel in the form of bars and wire 0.750 inch (19.05 mm) and under in nominal diameter or distance between parallel sides.
AMS E Carbon and Low Alloy Steels Committee
CONNECTOR, RECEPTACLE, JAM NUT MOUNT, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING, CRIMP TYPE CONTACTS; AND ACCESSORIES (CLASS A, F, AND E - SERIES 2)AS81511/3A (Current)1/6/2020
AE-8C1 Connectors Committee
FASTENER, ELECTRONIC EQUIPMENT, POSITIVE SELF-LOCKING, FORCE LIMITINGAS85731/2A (Current)12/20/2015
SCOPE IS UNAVAILABLE.
AE-8C2 Terminating Devices and Tooling Committee
Rubber: Butadiene-Acrylonitrile (NBR) Synthetic Lubricant Resistant 65 – 75 Hardness For Seals in Synthetic Lubricant SystemsAMS7272G (Current)4/12/2013
This specification covers a butadiene-acrylonitrile (NBR) rubber in the form of molded rings, compression seals, o-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications.
AMS CE Elastomers Committee
CONNECTOR, RECEPTACLE, ELECTRIC, CRIMP TYPE, JAM NUT MOUNTING, PUSH-PULL, COUPLING, SERIES 2 (CLASS E AND J)AS31441A (Current)5/18/2021
AE-8C1 Connectors Committee
Fluid for Automotive Electrified DrivetrainsJ3200_202210 (Current)10/13/2022
This SAE Information Report details the important new performance properties and suggested test methods for lubricants used in e-Mobility drivetrain components. The lubricants under discussion are those used in electrified drivetrains, mainly electric-transmissions and axles (e-transmissions and e-axles). The scope is limited to those geared systems in which an electric motor (e-motor) is immersed in the powertrain lubricant or comes in contact with the powertrain lubricant. Though the report focuses on new lubricant attributes, some information on conventional lubricant attributes is included. The information presented here will be helpful in understanding the similarities and differences between conventional (i.e., internal combustion engine (ICE)) and e-Mobility powertrain systems.
Fuels and Lubricants TC 3 Driveline and Chassis Lubrication
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