Search
Advanced Search
of the following are true
(
)

Results

Items (222,093)
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
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
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
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
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
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
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
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
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
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
CVJ Efficiency Test Recommended PracticeJ3249_202607 (Current)7/14/2026
This recommended practice describes the procedure to measure and report the operating efficiency for all types of constant velocity joints (including fixed and plunging/end motion type joints) used in cars, SUVs, and trucks. This includes halfshaft as well as propshaft applications. This does not apply to non-CV joints. Rotational inertia is not considered within the scope of this recommended practice. This recommended practice provides a common method to quantify and report the operating efficiency characteristics of a CVJ. This practice does not apply to parasitic losses (spin loss, churning loss, or zero torque loss) as experienced on deactivated AWD/4WD systems. The losses in this condition are significantly less and require higher accuracy than what is required in this recommended practice.
Drivetrain Standards Committee
Guidelines for Aerodynamic Assessment of Medium and Heavy Commercial Ground Vehicles Using Computational Fluid DynamicsJ2966_202607 (Current)7/14/2026
This document outlines general requirements for the use of CFD methods for aerodynamic simulation of medium and heavy commercial ground vehicles weighing more than 10000 pounds. The document provides guidance for aerodynamic simulation with CFD methods to support current vehicle characterization, vehicle development, vehicle concept development, and vehicle component development. The guidelines presented in the document are related to Navier-Stokes and Lattice-Boltzmann based solvers. This document is only valid for the classes of CFD methods and applications mentioned. Other classes of methods and applications may or may not be appropriate to simulate the aerodynamics of medium and heavy commercial ground vehicle weighing more than 10000 pounds.
Truck and Bus Aerodynamics and Fuel Economy Committee
Worldwide On-Board Diagnostic Requirements OverviewJ3248_202607 (Current)7/14/2026
This document focuses on the latest in-force regulations. However, in addition to latest information, the report may include historical information. As regulations are superseded, the previous entry will remain to help understand the change in requirements over time. The initial focus of the document includes light-, medium-, and heavy-duty on-road vehicles with all propulsion systems. The document will include information from the United States and Canada, with later publications expanding to other regions. Forecasts for future regulations will not be included in the spreadsheet but be kept in a separate document. The document may be expanded to other types of applications/vehicles as information becomes available.
Vehicle E E System Diagnostic Standards Committee
RESS Cell Package Integrity Requirements and TestsJ3337_202607 (Current)7/14/2026
This recommended practice (RP) presents a methodology to evaluate RESS Cells Closure Integrity (Leak Tightness) requirement. This RP applies to two types of RESS Cells, each containing liquid electrolyte: Lithium ion (Li-ion) Cells and Sodium ion (Na-ion) Cells. The Equivalent Channel Method is used as a suggested cell closure integrity requirement for a given RESS Cell design during its production and product validation phases. The Closure Integrity requirements intended to assure no electrolyte leakage and no excessive moisture ingress during the usage of these cells as part of the RESS (Battery Pack), which is crucial to assure the safety and performance of these RESS. This RP specifies non-destructive Integrity (leak) testing processes of the Cell Closure. It describes approved leak testing technologies, testing procedures, tooling requirements, and leak test systems validation/verification requirements. This document may be applied to RESS Cell Closure Integrity testing during
Battery Standards Testing Committee
Storage Batteries for Start-Stop OperationsJ3012_202607 (Current)7/14/2026
This SAE Standard applies to 12-volt lead-acid storage batteries that are designed specifically for start-stop operations in on-road passenger vehicles or light trucks. Included are definitions of terms, general testing recommendations, key performance characteristics, and life testing. Properties not unique to start-stop batteries should be tested according to SAE J537 or other applicable testing protocols.
Start-Stop Battery Committee
Reverse Automatic Emergency Braking (AEB) Testing SummaryJ3339_202607 (Current)7/14/2026
This SAE Information Report provides a broad summary of existing Reverse Automatic Emergency Braking test protocols to help assess whether additional test protocols are needed. Eventually, the task force may develop additional protocols to support testing of Reverse Automatic Emergency Braking systems.
Active Safety and Driver Support Systems Standards Committee
GASKET - 37° FLARED TUBE FITTING, NICKEL, AMS5553AS3282C (Current)10/20/2014
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Rivets, Steel, Corrosion and Heat Resistant 15Cr 25.5Ni 1.2Mo 2.1Ti 0.006B 0.30V 1650°F (900°C) Solution Heat Treated and Partially Precipitation Heat TreatedAMS7235D (Current)10/1/1990
AMS F Corrosion and Heat Resistant Alloys Committee
Inserts, Thread Form, Corrosion Resistant Steel 18cr 9.2niAMS7245E (Current)10/1/1990
AMS F Corrosion and Heat Resistant Alloys Committee
Performance Test for Windshield Defrosting Systems for Off-Road, Self-Propelled Work MachinesJ1535_202108 (Current)8/2/2021
This SAE Standard establishes uniform test procedures for the defrosting systems of off-road, self-propelled work machines used in construction, general purpose industrial, agricultural, and forestry machinery as referenced in table one of this document. It includes tests that can be conducted with uniform test equipment in commercially available laboratory facilities, as well as in an appropriate outdoor environment.
HFTC6, Operator Accommodation
Guidelines for Repair Process Evaluation of Aluminum Bonded StructureAIR6291A (Current)5/24/2024
This SAE Aerospace Information Report (AIR) is intended to be used as a process verification guide for evaluating implementation of key factors in repair of metal bond parts or assemblies in a repair shop environment. This guide is to be used in conjunction with a regulatory approved and substantiated repair and is intended to promote consistency and reliability.
AMS CACRC Commercial Aircraft Composite Repair Committee
686 Roadmap for IPv6 Transition in AviationARINC686 (Current)6/19/2020
ARINC Report 686 represents the consensus of industry to prepare a roadmap migration from IPv4 to IPv6. This document describes airline objectives (air and ground side when possible) towards the development and introduction of IPv6. There are three distinct elements considered: 1) the applications for addressing aspects 2) the communication network(s) over which the applications are running for the IP protocol level itself and associated features, and 3) the physical link(s) the network(s) interface.
Airlines Electronic Engineering 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
Inflator Assembly and Gage Elements, Pneumatic Pressure, Remote Control, Direct ReadingAS85352A (Current)4/9/2018
This specification covers a direct reading, remote control, pneumatic pressure inflator assembly, for use on aircraft tires and struts having pneumatic pressure requirements up to 600 psi. It includes pressure relief provisions to provide for safe inflation. Also included are dual chuck stem gages for measuring tire pressure.
A-5 Aerospace Landing Gear Systems Committee
Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35000 kPa), 400 °F (204 °C), Aircraft Hydraulic SystemsAS5960C (Current)4/11/2019
This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35000 kPa) aircraft hydraulic systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Silicone Rubber Compound Room Temperature Vulcanizing, 15,000 Centipoise Viscosity Durometer 35 - 55AMS3362D (Current)1/17/2012
This specification covers a silicone rubber in the form of a two-component liquid compound.
AMS G9 Aerospace Sealing Committee
CLAMP ASSEMBLY, SADDLE TYPE, CUSHIONED, HIGH TEMPERATUREAS85449/3A (Current)4/21/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Nickel Alloy, Corrosion and Heat-Resistant, Round Bars and Wire 52.5Ni - 19Cr - 3.0Mo - 5.1Cb - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Treated and Work Strengthened Precipitation HardenableAMS5962A (Current)5/12/2022
This specification covers a corrosion and heat resistant work strengthened nickel alloy in the form of bars and wire, 1½ inches (38 mm) and under in nominal diameter (See 8.2).
AMS F Corrosion and Heat Resistant Alloys Committee
WIRE, ELECTRIC, CROSSLINKED POLYALKENE INSULATED, TIN-COATED COPPER, NORMAL WEIGHT, 600 VOLT, 150 °CAS81044/6A (Current)7/29/2022
AE-8D Wire and Cable Committee
RING, RETAINING SPIRAL, INTERNAL, HEAVY DUTY, CRES (UNS S30200)AS3215B (Current)5/10/2023
E-25 General Standards for Aerospace and Propulsion Systems
WASHER, KEY - 180 DEG, LOCKING, CRES, UNS S32100AS9276B (Current)1/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
Displacement of Pneumatic Service Brake ActuatorsJ1155_198801 (Current)3/1/1988
This recommended practice specifies a test procedure for determining the volume of pneumatic service brake actuators at any stroke.
MTC4, Forestry and Logging Equipment
Sheet, Polyether Urethane (EU) Elastomer Foam Shock AbsorbingAMS3568B (Current)8/25/2011
This specification and its supplementary detail specifications cover a chemically or mechanically expanded polyether urethane (EU) elastomeric foam material in the form of ready-to-use sheet.
AMS P Polymeric Materials Committee
COUPLING, MALE, 12 INCH AIR DUCTAS7365/3A (Current)6/11/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Test Method for Catalytic Carbon Brake Disk OxidationAIR5567A (Current)4/14/2025
The scope of the test method is to provide stakeholders including fluid manufacturers, airport operators, brake manufacturers, aircraft constructors, aircraft operators and airworthiness authorities with a relative assessment of the effect of deicing chemicals on carbon oxidation. This simple test is only designed to assess the relative effects of runway deicing chemicals by measuring mass change of contaminated and bare carbon samples tested under the same conditions. It is not possible to set a general acceptance threshold oxidation limit based on this test method because carbon brake stack oxidation is a function of heat sink design and the operating environment.
A-5A Wheels, Brakes and Skid Controls Committee
SCREW – FLAT FILLISTER HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN. .3125-24 UNF-3AAS115501B (Current)5/22/2014
E-25 General Standards for Aerospace and Propulsion Systems
Fittings, Beaded, Fluid ConnectionAS4843A (Current)6/6/2016
This SAE Aerospace Standard (AS) establishes the requirements for beaded fluid connection fittings (see Section 6) for use in all types of fluid systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
INSERT, SCREW THREAD, SELF LOCKING PLASTIC LOCKING DEVICE, SOLID FILM LUBRICATED SELF-BROACHING KEYS, UNS S66286AS3502A (Current)5/4/2026
E-25 General Standards for Aerospace and Propulsion Systems
CABLE, POWER, ELECTRICAL, 600 VOLTS, PORTABLE, MULTICONDUCTORAS5756/3B (Current)6/22/2021
AE-8D Wire and Cable Committee
Basic Aircraft Oxygen Systems DesignAIR825/14 (Current)8/11/2021
This slash document collects general reference material related to gaseous oxygen system flow requirements and sizing calculations. This document will assist oxygen system equipment designers and operators to establish systems and equipment requirements. The document consists of charts, tables, system schematics, system requirements, and sample calculations for system sizing.
A-10 Aircraft Oxygen Equipment Committee
National Aerospace and Defense Contractors Accreditation Program (NADCAP) Survey Checklists for the NDT Suppliers Accreditation ProgramAS7100/1B (Current)8/13/2008
This document has been declared "CANCELLED" as of August 2008 and has been superseded by PRI AC7114. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7114. Cancelled specifications are available from SAE.
Nadcap Management Council
Steel Corrosion and Heat Resistant, Bars 20cr 9ni 1.4mo 1.4w(B+Ta) 0.22tiAMS5721C (Current)4/1/1991
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of April, 1991.
AMS F Corrosion and Heat Resistant Alloys Committee
Rubber, Synthetic General Purpose, Fluid Resistant 55 - 65AMS3220H (Current)6/11/2019
This specification covers a synthetic rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Functional, Performance, and Safety Guidelines for Tire Pressure Monitoring Systems (TPMS) for AircraftARP6137A (Current)6/1/2026
This SAE Aerospace Recommended Practice (ARP) establishes the overall component and system function guidelines and minimum performance levels for a TPMS. These guidelines include, but are not limited to: Design recommendations for system components, which: Monitor tire inflation Are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment Recommended performance and safety guidelines for a TPMS.
A-5 Aerospace Landing Gear Systems Committee
Individual Inflatable Life PreserverAS1354 (Current)11/21/2024
This SAE Aerospace Standard (AS) provides the minimum design and performance requirements for individual, inflatable life preservers, divided into six categories: “Adult,” “Adult-Child,” “Child,” “Infant-Small Child,” “Adult-Child-Infant-Small Child,” and “Demonstration.”
S-9A Safety Equipment and Survival Systems Committee
Steel Sheet, Strip, and Plate, Corrosion and Heat Resistant 25cr 20ni 2.0si (314) Solution Heat TreatedAMS5522E (Current)1/1/1991
AMS F Corrosion and Heat Resistant Alloys Committee
SLEEVE, FLARED TUBE FITTINGAS4327 (Current)4/20/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BOLT, MACHINE - SPLINE DRIVE, EXTENDED WASHER HEAD, PD SHANK, LONG THREAD, UNS N07001, METRICMA3513A (Current)10/31/2019
E-25 General Standards for Aerospace and Propulsion Systems
Detection of Surface Imperfections In Ferrous Rods, Bars, Tubes, and WiresJ349_201712 (Current)12/20/2017
This SAE Information Report provides a summary of several methods that are available for detecting, and in some instances detecting and measuring, surface imperfections in rods, bars, tubes, and wires. References relating to detailed technical information and to specific applications are enumerated in 2.2.
Metals Technical Committee
Items per page:
1 – 50 of 222093