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Measurement of Exhaust Sound Levels of Stationary SnowmobilesJ2567_202607 (Current)7/6/2026
This SAE Standard establishes the test procedure, environment, and instrumentation for determining the sound levels of snowmobiles in the stationary test mode. This test method is intended to provide an accurate measurement of exhaust and other engine noise and may be used to evaluate new and in-use snowmobiles to determine compliance with noise control regulations. Sound level measurements obtained with this test method are not intended as an engineering determination of overall machine noise. For this purpose, the use of SAE J192 is recommended.
Snowmobile Technical Committee
Engine Electrostatic Gas Path MonitoringAIR4986A (Current)10/28/2009
Turbine engine malfunctions account for a substantial portion of the maintenance actions required to keep both fixed and rotary wing aircraft operational. Undetected incipient component failures can result in secondary engine damage and expensive unscheduled maintenance actions. Recent developments of electrostatic methods now provide the potential for the detection of foreign object ingestion and early detection of distress in gas path components. This SAE Aerospace Information Report (AIR) seeks to outline the history of the electrostatic technique and provides examples of state-of-the-art systems for both inlet and exhaust gas debris monitoring systems along with examples of most recent testing.
E-32 Aerospace Propulsion Systems Health Management
Tamper Resistance for Adjustable Parameters on Diesel Fuel Injection PumpsJ2317_202103 (Current)3/17/2021
This SAE Recommended Practice defines a guideline for the fuel injection pump designer to select appropriate fastener designs which are considered to be tamper-resistant. It applies to fuel injection pumps used on diesel engines.
Diesel Fuel Injection Equipment Standards Committee
SCREW, MACHINE - HEXAGON HEAD, PD SHANK, CRES AMS5731 (UNS S66286), .164-36 UNJF-3AAS3098A (Current)4/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
Steel, Corrosion and Heat Resistant 13.5Cr - 26Ni - 1.75Mo - 3Ti Consumable Electrode Vacuum MeltedAMS5741D (Current)10/1/1982
AMS F Corrosion and Heat Resistant Alloys Committee
SLEEVING, FOR IDENTIFICATION MARKING HEAT SHRINKABLE, POLYVINYLIDENE FLUORIDE, FLEXIBLEAS85848/2A (Current)7/7/2017
AE-8D Wire and Cable Committee
NUT, PLAIN, HEXAGON, CHECK, UNS S66286 130 KSI MINAS9361B (Current)1/26/2026
E-25 General Standards for Aerospace and Propulsion Systems
Recommended Design and Test Requirements for Hydraulic Thermal Expansion Relief ValvesARP4835A (Current)8/26/2021
This Aerospace Recommended Practice (ARP) provides recommendations for the design and test requirements for a hydraulic thermal relief valve. The thermal relief valve is intended for use in a civil or military aircraft hydraulic system with a rated system pressure up to 5000 psi (34500 kPa).
A-6C5 Components Committee
Roving, Type "S-2" Glass Epoxy Resin ImpregnatedAMS3832D (Current)12/16/2016
This specification covers continuous, multiple-strand, roving of Type "S-2" glass impregnated with a heat-curable epoxy resin matrix and processed to a "B" stage condition.
AMS P17 Polymer Matrix Composites Committee
BEARING, BALL, AIRFRAME, ANTIFRICTION, EXTERNAL SELF-ALIGNING, EXTRA LIGHT DUTY CORROSION-RESISTANT NITROGEN STEEL (CREN)AS27648/1A (Current)6/15/2026
ACBG Rolling Element Bearing Committee
Hydraulic Filter Elements - Method for Evaluating Dynamic Efficiency with Cyclic FlowARP4205A (Current)6/15/2026
This SAE Aerospace Recommended Practice (ARP) describes a method for evaluating the performance of filter elements designed for aerospace hydraulic systems. The performance is measured and reported in terms of filtration ratios and stabilized contamination levels while testing with cyclic flow.
A-6C1 Fluids and Contamination Control Committee
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, DRILLED, CLOSE TOL SHANK, AMS5643 (UNS S17400), 140 KSI, .3750-24 UNJF-3AAS3177C (Current)6/15/2026
SCOPE IS UNAVAILABLE.
E-25 General Standards for Aerospace and Propulsion Systems
USCAR FRONTAL AIRBAG PERFORMANCE SPECIFICATIONUSCAR52 (Current)4/9/2025
This specification establishes the DV/PV performance and validation requirements for frontal airbag modules, namely driver, passenger, and knee airbags. In cases where airbag designs fall outside the scope of this standard, the Responsible Vehicle Engineering Organization (RVEO) is the final arbiter of all performance requirements within this specification. Additional system level requirements may be introduced by the RVEO but are outside the scope of this specification.
USCAR
Delegated Product Release VerificationAS9117 (Current)3/29/2016
This standard specifies requirements for DPRV to establish common product/service requirements for use at all levels of the supply chain. This standard shall apply when an organization elects to delegate product release verification by contractual flow down to their supplier (reference 9100 and 9110 standards); to perform product acceptance on their behalf. The delegating organization shall use this standard as the baseline for establishing a DPRV process, although they may include additional contract requirements to meet their specific needs.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, 1400 CPM (15 FPM) OSCILLATION, -65 TO +160 °F (-54 TO +71 °C)AS83819/1 (Current)8/23/2018
ACBG Plain Bearing Committee
Nickel Alloy, Corrosion and Heat Resistant, Covered Welding Electrodes 48ni 22cr 1.5co 9.0mo 0.60w 18.5feAMS5799D (Current)4/1/1996
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of April 1996 and has been superseded by AWS A5.11 ENiCrMo-2.
AMS F Corrosion and Heat Resistant Alloys Committee
Engine Rotation and Cylinder NumberingJ824_202206 (Current)6/29/2022
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry.
Engine Power Test Code Committee
Night Vision Goggle (NVG) FiltersARP4169B (Current)8/18/2025
This SAE Aerospace Recommended Practice (ARP) discusses the desired characteristics of night vision goggle (NVG) filters that can be used with incandescent, electroluminescent (EL) and light emitting diode (LED) light sources to achieve NVG compatible lighting of aerospace crew stations. This document also discusses the parameters that need to be considered when selecting a night vision goggle/daylight viewing (NVG/DV) filter for proper contrast enhancement to achieve readability in daylight. The recommendations set forth in this document are to aid in the design of NVG compatible lighting that will meet the requirements of MIL-L-85762A and MIL-STD-3009.
A-20A Crew Station Lighting
Automatic Test Equipment, Relays Fully Rated 25 Amperes or GreaterARP4767B (Current)2/24/2013
This SAE Aerospace Recommended Practice (ARP) is intended to be used as a guide for defining the methods to be used in performing electrical acceptance tests with automatic test equipment and to ensure repeatability and compatibility of results between manufacturers and between manufacturers and users.
AE-7P Protective and Control Devices
Radome, Foam Sandwich Hot-Melt, Addition-Type PolyimideAMS3913B (Current)8/10/2022
This specification covers the material and process requirements for fabricating sandwich radomes having hot-melt, addition-reaction polyimide-resin-impregnated quartz cloth shells and polyimide-resin syntactic foam cores.
AMS P17 Polymer Matrix Composites Committee
COUPLING, SHEET METAL, 40° V-BAND, STANDARD LATCHAS1960/1B (Current)11/6/2024
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
TS24 MANUFACTURING SPECIFICATION FOR BOLTSTS24-9 (Current)9/3/2024
This specification covers the requirements for forged bolts in DTD5638, EN 2952, EN 3219 or AMS5662 material with rolled underhead radii. The bolts will develop a minimum tensile strength of 1275 MPa (185,000 lbf/in2) at room temperature and 1000 MPa (145,000 lbf/in2) at 650°C.
Engine and Airframe Technical Standards Committee (TSC)
Insulating Components, Molded, Electrical, Heat Shrinkable, Boot, Strain Relief and Sealing, StraightAS5258/1A (Current)2/8/2011
The complete requirements for acquiring the molded components described herein shall consist of this document and the latest issue of AS 5258.
AE-8C1 Connectors Committee
FITTING, ELBOW, 90°, EXTERNAL SWAGE TO FLARELESS, HYDRAULICAS6473 (Current)10/27/2016
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
PI-BusAS4710A (Current)5/3/2012
This document is a result of the desire for interoperability of modules on a Pi-Bus. This standard is a stand alone document that used the Very High Speed Integrated Circuit (VHSIC) Phase 2, Interoperability Standard Pi-Bus Specification 2.2, as a starting point.
AS-1A Avionic Networks Committee
INFLATOR ASSEMBLY KITAS85352/1A (Current)10/10/2013
A-5 Aerospace Landing Gear Systems Committee
Synchro, Control Transmitter, Type 23CX6DAS20708/52B (Current)3/21/2017
AE-7A Generators and Controls Motors and Magnetic Devices
BOSS-FLUID CONNECTION, INTERNAL STRAIGHT THREAD, SHALLOW TAPAS1171B (Current)5/16/2022
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Butadiene Acrylonitrile (NBR) Rubber Dry Heat Resistant 35 - 45AMS3201M (Current)8/23/2018
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Rivets, Solid, Alloy-Corrosion Resistant, 67ni 31cuAMS7233D (Current)1/1/1991
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Bars and Forgings, Corrosion and Moderate Heat-Resistant 15Cr - 7.1Ni - 2.5Mo - 1.1AlAMS5657D (Current)4/5/2017
AMS F Corrosion and Heat Resistant Alloys Committee
Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 4.0V AnnealedAMS6931D (Current)12/7/2017
This specification covers a titanium alloy in the form of bars and forgings up through 10.000 inches (254.00. mm), inclusive, in diameter or least distance between parallel sides with a maximum cross-sectional area of 79.0 in2 (506.45 cm2) and forging stock of any size (see 8.7).
AMS G Titanium and Refractory Metals Committee
Missile and Rocket Applications: Hose Assemblies, Flexible Metal, High Pressure and High TemperatureARP907A (Current)10/2/2023
This recommended practice covers the requirements and qualification tests for two types of flexible all-metal hose assemblies intended for hydraulic use on missile and rocket applications at rated pressures of 4000 psi. Type I -65° to +650 °F service temperature range Type II -65° to +1000 °F service temperature range
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Type 2 15% Graphite Filled Virgin Polytetrafluoroethylene (PTFE) Moldings or ExtrusionsAMS3678/2B (Current)2/29/2016
This specification covers a polytetrafluoroethylene (PTFE) resin filled with 15% graphite in the form of extruded or molded rods or tubes which are sintered after molding or, in the case of extrusions, sintered during the extrusion process.
AMS P Polymeric Materials Committee
Elastomer: Silicone Rubber, (VMQ) General Purpose 75 – 85 Durometer Type ‘A’ HardnessAMS3305K (Current)4/5/2019
This specification covers a silicone (MQ/VMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, O-ring cord, and molded in place gaskets for aeronautical and aerospace applications without complete consideration of the end use prior to the selection of this material.
AMS CE Elastomers Committee
Ion NitridingAMS2759/8B (Current)6/11/2018
This specification establishes the requirements and procedures for producing a hard, wear resistant ion nitrided surface on steel parts.
AMS B Finishes Processes and Fluids Committee
WASHER, FLAT, COUNTERSUNK UNS S66286AS3565A (Current)11/11/2020
E-25 General Standards for Aerospace and Propulsion Systems
HOSE ASSEMBLY, RUBBER, FLARELESS, FIELD ATTACHABLE FITTING, STRAIGHT TO 90°AS1865A (Current)9/17/2024
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Truck Driver Shin-Knee Position for Clutch and AcceleratorJ1521_202412 (Current)12/6/2024
This SAE Recommended Practice describes two-dimensional, 95th percentile truck driver, side view, seated shin-knee contours for both the accelerator operating leg and the clutch operating leg for horizontally adjustable seats (see Figure 1). There is one contour for the clutch shin-knee and one contour for the accelerator shin-knee. There are three locating equations for each curve to accommodate male-to-female ratios of 50:50, 75:25, and 90:10 to 95:5.
Truck and Bus Human Factors Committee
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METAL BRAID, MEDIUM PRESSURE, FLARED, 45° TO 45°AS643A (Current)6/21/2011
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Heat Treatment of Steel Raw MaterialsAMS2761 (Current)7/8/2020
This specification establishes general requirements for the heat treatment of steel raw material (see 8.2.1) by producers or for producers.
AMS E Carbon and Low Alloy Steels Committee
Connections for Fluid Power and General Use - Hydraulic Couplings - Diagnostic Port Sizes and LocationsJ1298_201704 (Current)4/14/2017
SAE J1298 covers the recommended diagnostic port sizes for use in measuring hydraulic fluid temperature, pressure, flow, and for obtaining fluid samples. See SAE J1502 for the detailed coupling specifications.
Hydraulic Tube Fittings 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
Direct Ship - Recommended Practices for Aerospace CompaniesARP9004A (Current)3/6/2006
Limited to the Aerospace industry where an approved manufacturer requests a supplier to ship an article against the approved manufacturer's quality system directly to a customer. The direct ship process is not required or applicable to standard parts or military parts. In this process the approved manufacturer is responsible for assurance that the article conforms to Type Design information.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Aluminum Alloy 5456, Plate and Sheet, for Sea Water ApplicationsAMSQQA250/20A (Current)8/3/2006
This specification covers the specific requirements for aluminum alloy 5456 plate and sheet for applications requiring a weldable moderate strength alloy having comparatively good corrosion resistance.
AMS D Nonferrous Alloys Committee
Core Material, Plastic Honeycomb, Nylon Paper Base for Aircraft Structural ApplicationsAMSC81986 (Current)8/10/2022
This specification covers the requirements for nonperforated nylon paper base plastic honeycomb core material for aircraft structural applications, including exterior parts such as radio and radar antenna housings.
AMS P17 Polymer Matrix Composites Committee
GASKET, METAL C-RING, FACE SEAL, INTERNAL PRESSURE, UNS N07750, SILVER PLATED, METRICMA2536A (Current)9/19/2018
E-25 General Standards for Aerospace and Propulsion Systems
Steel, Corrosion-Resistant (18-8) Bars, Wire and Forging Stock (Aircraft Quality)AMSS7720B (Current)7/31/2013
This specification covers the requirements for compositions of corrosion-resistant (18-8) steel bars, rods, wire and forging stock.
AMS F Corrosion and Heat Resistant Alloys 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)
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)
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