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Vehicle, Magnetic Particle Inspection Petroleum BaseAMS2641D (Current)09/12/2025
This specification covers two types of refined hydrocarbon compounds in the form of liquids. This specification only covers newly manufactured materials.
AMS K Non Destructive Methods and Processes Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Investment Castings, 53.3Ni - 16.5Cr - 17Mo - 4.5W - 5.8Fe - 0.40V (CW-12MW), As-CastAMS5388L (Current)09/12/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Hardware Protected Security Environment - GlobalPlatform Technologies Information ReportJ3101-5_202509 (Current)09/12/2025
The scope of the analysis is on the GlobalPlatform Secure Element (SE) and Trusted Execution Environment (TEE) standard specifications correspondence to SAE J3101 recommended practices. This analysis includes focuses on the platform specifications but not the scope of any future security application/applets. Both of these GlobalPlatform specifications have associated protection profiles to validate compliance, although GlobalPlatform does not currently have any specific SAE J3101 protection profiles. GlobalPlatform has communicated that it is assessing whether or not to develop application-level protection profiles to more explicitly cover the remaining requirements of SAE J3101 in order to allow for standardized testing and certification of complete solutions.
Vehicle Electrical System Security Committee
Aluminum Alloy, Castings, 5.0Si - 1.2Cu - 0.50Mg (C355.0-T6), Solution and Precipitation Heat TreatedAMS4215K (Current)09/12/2025
This specification covers an aluminum alloy in the form of sand, permanent mold, composite mold, and investment castings (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Castings, Permanent Mold, 5.0Si - 1.2Cu - 0.50Mg (355.0-T6), Solution and Precipitation Heat TreatedAMS4281H (Current)09/12/2025
This specification covers an aluminum alloy in the form of permanent mold castings (see 8.6).
AMS D Nonferrous Alloys Committee
AIRCRAFT FIRE PROTECTION FOR RECIPROCATING AND GAS TURBINE ENGINE INSTALLATIONSAIR1076 (Current)09/11/2025
This document is reissued for application to helicopters.
S-12 Powered Lift Propulsion Committee
Cleaner, Aircraft Glass WindowAMS1534C (Current)04/07/2021
This specification covers two types of aircraft glass window cleaners in the form of a ready-to-use liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
CIRCUIT BREAKER, AIRCRAFT, TRIP-FREE PUSH PULL, TYPE I, DUAL SAFETY, −55 THRU +121 °CAS58091/1A (Current)05/31/2019
AE-7P Protective and Control Devices
Reflex Reflectors for Use on Vehicles 2032 mm or More in Overall WidthJ2041_201310 (Current)10/21/2013
This SAE Standard provides test procedures, requirements, and guidelines for reflex reflectors used on vehicles 2032 mm or more in overall width. Reflex reflectors conforming to these requirements may also be used on vehicles less than 2032 mm in overall width.
Heavy Duty Lighting Standards Committee
Steel Castings, Sand, Corrosion and Heat Resistant 24.5Cr - 20.5Ni Solution Heat TreatedAMS5365E (Current)10/21/2013
This specification covers a corrosion and heat resistant steel in the form of sand castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Ground Electrical Power Unit, Transportable 115/200 Volt AC (Nominal) 400 Hertz, 3-Phase 4-Wire (Grounded Neutral) Y-Connected SystemARP1148B (Current)10/22/2013
This Recommended Practice outlines the electrical performance characteristics for a continuous duty, diesel or gasoline engine driven brushless alternator unit for supplying 400-Hertz electrical power to commercial transport aircraft. It is intended to assist the airlines in standardizing recommendations for various sizes and configurations of equipment and it is a guide for the preparation of detailed specifications. The unit is primarily intended to supply power to the aircraft during passenger loading and unloading, and during servicing operations. The combination of the equipment specified herein and the interconnecting cables(s) between the 400-Hertz alternator and the aircraft shall provide power characteristics at the aircraft receptacle which meet MIL-STD-704 requirements for Category "B" equipment. Other limits which are necessary to meet specific conditions must be specified by the purchaser.
AGE-3 Aircraft Ground Support Equipment Committee
SLEEVE, TUBE END, ACORN TO WELD, SHORT FLARELESSAS4695C (Current)10/20/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
INFLATOR ASSEMBLY GAGE ELEMENTSAS85352/3A (Current)10/20/2013
A-5 Aerospace Landing Gear Systems Committee
FITTING, TEE, INTEGRAL WELD RING, 3000 PSIAS1583E (Current)10/20/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
In-Service Brake Performance Test Procedure Passenger-Car and Light-Duty TruckJ201_201307 (Current)07/24/2013
This SAE Recommended Practice establishes a uniform procedure for testing the brake systems (service and parking) of all passenger cars, light-duty trucks, and multipurpose passenger vehicles up to and including 4500 kg (10 000 lb) GVWR. The purpose of the test code is to evaluate brake system performance of vehicles in service for compliance with regulations. The test code is expected to be utilized as a basis for a brake evaluation conducted by State or Federal officials engaged in highway safety programs. The primary consideration is that this test requires a minimum of instrumentation, time, driver skill, and cost to conduct.
Road Test Procedures 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)07/25/2013
This specification covers an aluminum alloy in the form of sheet and plate supplied in the - T861 temper.
AMS D Nonferrous Alloys Committee
Application of Pure-Tone Atmospheric Absorption Losses to One-Third Octave-Band DataARP5534 (Current)01/05/2021
This document presents a practical method for calculating atmospheric absorption for wide-band sounds analyzed with one-third octave-band filters, called the SAE Method. The SAE Method utilizes pure-tone attenuation algorithms originally published in ISO 9613-1 and ANSI S1.26-1995 to calculate path-length attenuation at mid-band frequencies. The equations introduced in this standard transform the pure-tone, mid-band attenuation to one-third octave-band attenuation. The purpose of this guidance document is to extend the useful attenuation range of the Approximate Method outlined in ANSI S1.26-1995, and to replace ARP866A. Calculation of sound attenuation caused by mechanisms other than atmospheric absorption such as divergence, refraction, scattering due to turbulence, ground reflections, or non-linear propagation effects, is outside the scope of this document.
A-21 Aircraft Noise Measurement Aviation Emission Modeling
CONNECTOR, PLUG, ATTACHABLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, SINGLE-JACKETED CABLE ASSEMBLIES, 115/200 VOLT, 400 HERTZAS7974/3A (Current)08/12/2013
AE-8C1 Connectors Committee
Sound Measurement - Off-Road Work Machines - Operator - Singular TypeJ919_201307 (Current)07/24/2013
This SAE Standard sets forth the instrumentation and procedure to be used in measuring sound pressure levels at the operator position for self-propelled off-road work machines as defined in SAE J1116. This document does not address the operation of safety devices such as backup alarms, horns, or accessories. This SAE document is applicable to machines that have operator stations where the operator can either stand or sit and will be either transported by, or walk with the machine during its operation. The sound levels obtained using this procedure are repeatable and representative of the higher range of sound levels generated by machines under actual field operating conditions. Due to variability of field operating conditions, this data is not intended to be used for operator noise exposure evaluations.
OPTC3, Lighting and Sound Committee
J1939 Digital AnnexJ1939DA_4Q2012 (Current)08/07/2013
The J1939 Digital Annex The J1939 Digital Annex, introduced in August 2013, offers key J1939 technical data in an Electronic Spreadsheet that can be easily searched, sorted, and adapted to other formats. J1939DA contains all of the SPNs (parameters), PGNs (messages), and other J1939 data previously published in the SAE J1939 top level document. J1939DA also contains all of the SLOTs, Manufacturer ID Codes, NAME Functions, and Preferred Addresses previously published in the SAE J1939 top level and the J1939-71 document. J1939DA contains the complete technical details for all of the SPNs and PGNs previously published in the SAE J1939-71 document. For all other SPNs and PGNs which are published in a document other than SAE J1939-71, J1939DA lists only basic details along with a reference to the document that contains the complete technical details. J1939DA replaces, and expands upon, the 1939 Companion Spreadsheet (CS1939), which was last published through November 2012. The data fields
Truck and Bus Control and Communications Network Committee
Coating Material, Silicone Resin 400 °F (205 °C)AMS3135G (Current)07/22/2013
This specification covers an unpigmented silicone-resin-base coating material.
AMS G8 Aerospace Organic Coatings Committee
DecalcomaniasAMS7290H (Current)07/22/2013
This specification covers a face-up type of water-applied, solvent-applied, or adhesive-applied decalcomanias.
AMS G8 Aerospace Organic Coatings Committee
Aluminum Coating Material, Corrosion and Heat Resistant Thermosetting, Inorganic BinderAMS3126D (Current)07/22/2013
This specification covers a corrosion and heat resistant aluminum coating material supplied as a liquid of suitable consistency for coating parts after being thoroughly mixed.
AMS G8 Aerospace Organic Coatings Committee
Enamel, Phenolic Black BakingAMS3122G (Current)07/22/2013
This specification covers a semigloss black baking enamel based on a phenolic resin.
AMS G8 Aerospace Organic Coatings Committee
Tubing, Steel, Corrosion-Resistant (S30400), Aerospace Vehicle Hydraulic System 1/8 Hard ConditionAMST6845B (Current)07/31/2013
This specification presents requirements for thin-walled (inside diameter greater than four times the wall thickness and outside diameter 1/4 inch and larger) corrosion-resistant steel tubing in approximately the 1/8 hard condition, of special quality, suitable for use in high-pressure hydraulic systems.
AMS F Corrosion and Heat Resistant Alloys Committee
Rubber, Fluorocarbon Elastomer (FKM) 70 to 80 Hardness, Low Temperature Sealing Tg -22 °F (-30 °C) For Elastomeric Shapes or Parts in Gas Turbine Engine Oil, Fuel and Hydraulic SystemsAMS3384 (Current)08/05/2013
This specification covers a high temperature, compression set and fluid resistant fluorocarbon (FKM) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes for aeronautical and aerospace applications.
AMS CE Elastomers Committee
CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT, SINGLE-JACKETED 115/200 VOLT, 400 HERTZAS7974/4A (Current)08/10/2013
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
Wave Soldering ProcedureARP1332D (Current)08/12/2013
The purpose of this recommended practice is to provide recommendations concerning the procedure for wave soldering.
AMS B Finishes Processes and Fluids Committee
Rubber: Butadiene-Acrylonitrile (NBR) Synthetic Lubricant Resistant 65 – 75 Hardness For Seals in Synthetic Lubricant SystemsAMS7272G (Current)04/12/2013
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
ADAPTER, ASSEMBLY - PORT CONNECTION RING LOCKED TO 60° FLARELESS TUBE END, METRICMA2119B (Current)04/09/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Service Brake System Performance Requirements - Passenger Car-Trailer CombinationsJ135_201304 (Current)04/09/2013
This SAE Recommended Practice presents service brake performance requirements for brake systems of all combinations of new passenger cars and new trailers (braked or unbraked) intended for roadway use (excluding special-purpose vehicles such as ambulances, hearses, etc.). Acceptable performance requirements are based on data obtained from SAE J134.
Road Test Procedures Standards Committee
Safe Carriage of Impaired and Disabled PassengersAIR1815A (Current)04/04/2013
This AIR defines the major groups of impairments and disabilities among passengers who use aircraft as a transportation mode, and the types of safety problems which might be associated with each impairment. These impairments, and their safety-related problems, should be considered when referring to ARP's related to the design of cabin furnishings and equipment.
S-9B Cabin Interiors and Furnishings Committee
Test Procedure for the Measurement of Gaseous Exhaust Emissions from Small Utility EnginesJ1088_201303 (Current)03/28/2013
This SAE Recommended Practice specifies a uniform procedure for the evaluation of gaseous exhaust emissions from small utility engines typically less than 20 kW. Details of engine test setup and exhaust gas analysis techniques are specified with the intent of providing a uniform and reproducible method of measurement. The intent has been to allow as much flexibility as possible in the physical construction of the experimental apparatus. Therefore, only those portions of the apparatus whose operation is critical to the accurate measurement of emissions levels are prescribed in detail. An engine test procedure including a test sequence is outlined such that it would cover the various applications in which small engines are used. The intent is to provide an understanding of the levels of exhaust emissions and does not imply that in given application, an engine would operate in all the modes outlined in the test procedure. This document is intended as a guide toward standard practice and
Small Engine and Powered Equipment Committee
Columbium (Niobium) Alloy Bars, Rods, and Extrusions 10Hf - 1.0Ti, Recrystallization AnnealedAMS7857C (Current)01/11/2017
This specification covers a columbium (niobium) alloy in the form of bars, rods, and extrusions.
AMS G Titanium and Refractory Metals Committee
Passenger Hypoxia Protection Utilizing Oxygen Enriched Gas MixturesAIR6036 (Current)09/13/2024
Currently, existing civil aviation standards address the design and certification of oxygen dispensing devices that utilize oxygen sources supplying at least 99.5% oxygen. This Aerospace Information Report discusses issues relating to the use in the passenger cabin of oxygen enriched breathing gas mixtures having an oxygen content of less than 99.5% and describes one method of showing that passenger oxygen dispensing devices provide suitable hypoxia protection when used with such mixtures.
A-10 Aircraft Oxygen Equipment Committee
Gas Turbine Jet Exhaust Noise PredictionARP876F (Current)01/05/2021
ARP876 is intended to provide specific recommended procedures for the prediction of gas turbine jet exhaust system noise sources. Procedures are issued as separate sections, to allow for future updating as additional methods, consistent with state-of-the-art, become available.
A-21 Aircraft Noise Measurement Aviation Emission Modeling
Disposable Hydraulic Filter Element - 115 L/min Flow, 1.0 MPa Collapse Pressure, Filtration Ratio = 75 at 6 and 10 μmJ2321/1_201305 (Current)05/31/2013
This specification sheet establishes requirements for low collapse pressure elements of a specific configuration with various efficiency ratings designed and tested in accordance with SAE J2321 and the requirements of this specification sheet.
Ship Fluid Systems Committee
Disposable Hydraulic Filter Element - 190 L/min Flow, 21 MPa Collapse Pressure, Filtration Ratio = 75 at 7 μmJ2321/2_201305 (Current)05/31/2013
This specification sheet establishes requirements for a high collapse pressure configuration filter element of a specific configuration with a minimum filtration ratio of 75 for particles larger than 7 µm when designed and tested in accordance with SAE J2321 and this specification sheet.
Ship Fluid Systems Committee
CABLE, 3-PHASE POWER, ELECTRIC, PORTABLE, MULTICONDUCTOR, 90°C, 600V, OZONE RESISTANT, SPLIT NEUTRALAS5756/5A (Current)06/05/2013
AE-8D Wire and Cable Committee
CLAMP, LOOP, NYLON, METRICAS14243A (Current)05/28/2013
AE-8C2 Terminating Devices and Tooling Committee
Electronmagnetic Compatibility Measurement Procedure for Vehicle Components - Part 21: Immunity to Electromagnetic Fields, 30 MHz to 18 GHz, Absorber-Lined ChamberJ1113/21_201305 (Current)05/28/2013
This part of SAE J1113 specifies test methods and procedures for testing electromagnetic immunity (of vehicle radiation sources) of electronic components for passenger cars and commercial vehicles. To perform this test method, the electronic module along with the wiring harness (prototype or standard test harness) and peripheral devices will be subjected to the electromagnetic disturbance generated inside an absorber-lined chamber. The electromagnetic disturbances considered in this part of SAE J1113 are limited to continuous narrowband electromagnetic fields. Immunity measurements of complete vehicles are generally only performed at the vehicle manufacturer. The reasons, for example, are high costs of a large absorber-lined chamber, preserving the secrecy of prototypes, or the large number of different vehicle models. Therefore, for research, development and quality control, a laboratory measuring method shall be applied by the manufacturers. Part 1 of SAE J1113 specifies the general
Electromagnetic Compatibility (EMC) Standards
Ship Systems and Equipment - Hydraulic Systems - Filter Selection ParametersJ2333_201305 (Current)05/31/2013
This SAE Recommended Practice identifies and examines the various parameters which must be considered in selecting hydraulic system filters, their locations within the system and the dirt capacity of the filter elements.
Ship Fluid Systems Committee
Life RaftsARP1356B (Current)05/21/2013
This Aerospace Recommended Practice (ARP) establishes criteria for the design and performance of aircraft life raft devices which will ensure their rapid and effective use as a flotation device in a water landing. This document is not intended to specify particular design methods, mechanisms, or equipment to be used to accomplish the objectives established herein.
S-9A Safety Equipment and Survival Systems Committee
Ship Systems and Equipment - Hydraulic Systems - Noise ControlJ1782_201305 (Current)05/31/2013
Hydraulic systems are used on marine vehicles for steering, vehicle control, and utility services. System components that generate and transmit noise are of concern. This SAE Information Report (a) addresses noise requirements which may apply to the hydraulic systems of ships and submersibles, and (b) identifies noise sources and techniques which may be used to reduce system noise. Noise of power sources (e.g., electric motors) and end items (e.g., steering linkages) is beyond the scope of this document.
Ship Fluid Systems Committee
Bearings, Plain, Self-Aligning, Self-Lubricating, 300 cpm Oscillation (13 fpm), -65 to +160 °F (-54 to +71 °C), Liners Less Than 0.015 inchesAS82819 (Current)08/23/2018
This standard covers the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 °F (-54 to +71 °C) at high cyclic speeds 300 cpm (13 fpm) for liners with a thickness less than 0.015 inch. The scope of this standard is to provide a liner system qualification procedure for helicopter sliding bearings defined and controlled by source control drawings. Once a liner system is qualified, the source-controlled bearings are further tested under application conditions. Under Department of Defense (DoD) Policies and Procedures, any qualification requirements and associated Qualified Products List (QPLs) are mandatory for DoD contracts. Any materials relating to QPLs have not been adopted by SAE and are not part of this SAE technical document.
ACBG Plain Bearing Committee
BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, 300 CPM (13 FPM) OSCILLATION, -65 TO +160 °F, LINERS LESS THAN .015 INCH THICKAS82819/1 (Current)08/23/2018
ACBG Plain Bearing Committee
Glossary of Terms With Specific Reference to Electrical Wire and CableARP1931B (Current)05/09/2013
This glossary provides accepted definitions for terms commonly used by manufacturers and users of electric wire and cable, and their components, intended for use on aerospace vehicles.
AE-8D Wire and Cable Committee
Bearings, Plain, Self-Aligning, Self-Lubricating, 1400 cpm (15 fpm), Oscillation, -65 to +160 °F (-54 to +71 °C)AS83819 (Current)08/23/2018
This standard covers the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 °F (-54 to +71 °C) at high cyclic speeds 1400 cpm (15 fpm). The scope of this standard is to provide a liner system qualification procedure for helicopter sliding bearings defined and controlled by source control drawings. Once a liner system is qualified, the source-controlled bearings are further tested under application conditions. Under Department of Defense (DoD) Policies and Procedures, any qualification requirements and associated Qualified Products List (QPLs) are mandatory for DoD contracts. Any materials relating to QPLs have not been adopted by SAE and are not part of this SAE technical document.
ACBG Plain Bearing Committee
PROPELLER SHAFT ENDS, DUAL ROTATION (PROPELLER SUPPLIED BEARING)AS91D (Current)03/12/2013
E-25 General Standards for Aerospace and Propulsion Systems
FLANGE – TWO-BOLT EXHAUSTAS222B (Current)03/12/2013
E-25 General Standards for Aerospace and Propulsion Systems
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