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Items (212,300)

05/22/2023

This specification covers hand and air operated, solvent and oil spray guns.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Cleaner, Alkaline Hot-Tank Type

AMS1537B (Current)

08/23/2018

This specification covers an alkaline cleaner in the form of a liquid for use above 65 °C (154 °F).

AMS J Aircraft Maintenance Chemicals and Materials Committee

Deoxidizer, Acidic, for Magnesium Alloys

AMS1538B (Current)

07/09/2012

This specification covers an acidic deoxidizer in the form of a liquid.

AMS J Aircraft Maintenance Chemicals and Materials Committee

High-Preload Deflection and Compressibility Test Procedures for Friction Materials

J2468_201811 (Current)

11/12/2018

This standard specifies a method for testing and measuring the deflection of friction materials assemblies and compressibility of friction materials. This standard applies to disc brake pad assemblies and its coupons or segments, brake shoe lining and its coupons or segments, and brake blocks segments used in road vehicles. This SAE test method is consistent in intent with the ISO 6310 and the JIS 4413.

Brake Linings Standards Committee

Polishing Compound, Aircraft Metal

AMS1650D (Current)05/06/2021

This specification covers a polishing compound for aircraft metals in the form of a liquid or paste.

AMS J Aircraft Maintenance Chemicals and Materials Committee

SAE No. 2 Friction Test Machine 3600 rpm Stepped Power Test

J2487_201905 (Current)

05/23/2019

This SAE Recommended Practice is intended as the definition of a standard test, but may be subject to frequent change to keep pace with experience and technical advances. This should be kept in mind when considering its use. The SAE No. 2 Friction Test Machine is used to evaluate the friction characteristics of automatic transmission plate clutches with automotive transmission fluids. It can also be used to conduct durability tests on wet friction systems. The specific purpose of this document is to define a 3600 rpm Stepped Power Test for the evaluation of wet friction system performance variation as a function of power level. This procedure uses an initial engagement speed of 3600 rpm and is intended as a standard procedure for common use by both suppliers and end users. The only variables selected by the supplier or user of the friction system are: a Friction Material b Fluid c Reaction Plates These three variables must be clearly identified when reporting the results of using this

Automatic Transmission and Transaxle Committee

Cleaner, Carpet Shampoo Type

AMS1630D (Current)

11/22/2024

This specification covers a shampoo type carpet cleaner in the form of a liquid.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Cleaner, Anodic, Electrolytic, Alkaline For Steel, Tank Type

AMS1547A (Current)

08/23/2018

This specification covers an electrolytic alkaline cleaner in the form of a water soluble powder.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Cleaner for Exterior Aircraft Surfaces Thickened or Gel-Type, Water-Base

AMS1523B (Current)

06/03/2019

This specification covers a thickened, water-base, type cleaner in the form of a gel.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Scale Conditioner, Alkaline Aircraft Turbine Engine Components

AMS1380B (Current)

07/29/2020

This specification covers a strongly alkaline scale conditioner in the form of a liquid or a water-soluble powder.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Compound, Cleaning, Foaming, for Aircraft Surfaces

AMS79_017 (Current)

12/15/2017

This SAE Standard specifies requirements for a foaming liquid cleaning compound which, when diluted with water 1:9 v/v, is suitable for cleaning the soiled exterior of Service aircraft. The cleaning compound may be applied by spraying, either as foam or liquid, by brushing or by swabbing. The surfaces to be cleaned may be unpainted metal or surfaces painted with glossy or matt schemes, including strippable acrylic paint complying with DTD 5599. This Standard includes tests to limit specific forms of corrosion that affect aircraft structural materials.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials

ARP1795A (Current)10/01/1990

This document establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress-corrosion cracking of titanium alloy parts. The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on tendency of pre-stressed titanium alloys to crack when subsequently heated to elevated temperatures.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Cleaner for Aircraft Exterior Surfaces Wipe-On, Wipe-Off, Containing Suspended Abrasive Solids

AMS1531D (Current)04/29/2020

This specification covers a water-soluble cleaner containing suspended abrasive solids in the form of a ready-to-use liquid.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Remover, Anti-Galling Compound Aircraft Turbine Engine Components Room Temperature Application

AMS1387B (Current)

11/26/2018

This specification covers an anti-galling compound remover in the form of a water-soluble powder, a concentrated liquid for dilution with water, or a ready-to-use liquid.

AMS J Aircraft Maintenance Chemicals and Materials Committee

J1939 Digital Annex

J1939DA_202506 (Current)06/18/2025

This document is intended to supplement the J1939 documents by offering the J1939 information in a form that can be sorted and searched for easier use.

Truck and Bus Control and Communications Network Committee

Effect of Cleaning Agents on Aircraft Engine Materials Stock Loss Test Method

ARP1755B (Current)

08/23/2018

This SAE Aerospace Recommended Practice (ARP) covers the determination of the amount of stock loss caused by use of chemical cleaning agents on aircraft turbine engine materials.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Hardware Protected Security Environment - Application Programming Interface Analysis - Information Report

J3101-1_202407 (Current)

07/03/2024

To gain an understanding of the software Application Programming Interface (API) landscape for SAE J3101 [SAEJ3101] devices, the SAE Vehicle Electrical Hardware Security Task Force conducted an analysis of various automotive-relevant crypto APIs. The purpose of this analysis was to identify how well the existing APIs cover the SAE J3101 requirements and to highlight the areas of coverage within these APIs. By examining these APIs, the Task Force aimed to gain insights into the current state of API support for SAE J3101 devices and identify any gaps in coverage that need to be addressed.

Vehicle Electrical System Security Committee

Low Speed Thorax Impact Test Procedure for the HIII 50th Male Dummy

J2779_202206 (Current)

06/29/2022

Dummy Testing and Equipment Committee

AS27465-499 UNION, TUBE, DOUBLE-ENDED, UNIFIED THREADS, CORROSION RESISTANT STEEL, UNPLATED

AS27465-6 (Current)10/10/2022

No scope available.

Engine and Airframe Technical Standards Committee (TSC)

Hardware Protected Security for Ground Vehicles

J3101_202002 (Current)

02/10/2020

Access mechanisms to system data and/or control is a primary use case of the hardware protected security environment (hardware protected security environment) during different uses and stages of the system. The hardware protected security environment acts as a gatekeeper for these use cases and not necessarily as the executor of the function. This section is a generalization of such use cases in an attempt to extract common requirements for the hardware protected security environment that enable it to be a gatekeeper. Examples are: Creating a new key fob Re-flashing ECU firmware Reading/exporting PII out of the ECU Using a subscription-based feature Performing some service on an ECU Transferring ownership of the vehicle Some of these examples are discussed later in this section and some have detailed sections of their own. This list is by no means comprehensive. Other use cases that require hardware protected security environment-based access control may be used by each manufacturer

Vehicle Electrical System Security Committee

Hardware Protected Security Environment Management of Confidential Data

J3101-3_202407 (Current)

07/26/2024

This document provides an information report to the readers for the management of confidential data associated with hardware protected security environment (HPSE). The scope of the present document is common principles of confidential data, methodologies, conformance of SAE J3101 with regulations and standards, and use cases.

Vehicle Electrical System Security Committee

Road Vehicles - Cybersecurity Engineering

ISO/SAE21434 (Current)08/31/2021

This document specifies engineering requirements for cybersecurity risk management regarding concept, product development, production, operation, maintenance and decommissioning of electrical and electronic (E/E) systems in road vehicles, including their components and interfaces. A framework is defined that includes requirements for cybersecurity processes and a common language for communicating and managing cybersecurity risk. This document is applicable to series production road vehicle E/E systems, including their components and interfaces, whose development or modification began after the publication of this document. This document does not prescribe specific technology or solutions related to cybersecurity.

Vehicle Cybersecurity Systems Engineering Committee

Guidelines for Automotive Environment Cybersecurity Key Management and Credential Distribution

J3201_202409 (Current)

09/17/2024

This document specifically pertains to cybersecurity for road vehicles. This document encompasses the entire vehicle lifecycle of key management. It has been developed by SAE Committee TEVEES18F, Vehicle Security Credentials Interoperability (VSCI), a subcommittee of SAE Committee TEVEES18A, Vehicle Cybersecurity Systems Engineering Committee. This committee is authorized under the scope and authority fo the SAE Electronic Design Automation Steering Committee (also known as the Electronic Systems Group) that is directly under the scope and authority fo the SAE Motor Vehicle Council. The SAE Motor Vehicle Council’s stated scope of influence and authority, as defined by the SAE includes, passenger car and light truck in conjunction with ISO/SAE 21434.

Vehicle Electrical System Security Committee

Compound, Cleaning Gel for Aircraft Surfaces

AMS79_015 (Current)

12/15/2017

This SAE Standard specifies requirements for a gelled compound for cleaning the soiled exterior of service aircraft. The cleaning gel may be applied by pressure pump as a thixotropic liquid, by brushing or by swabbing. The surfaces to be cleaned may be unpainted metal or surfaces painted with glossy or matt schemes, including strippable acrylic paint complying with DTD 5599. This Standard includes tests to limit specific forms of corrosion that affect aircraft structural materials.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Deodorant, Aircraft Toilet

AMS1476D (Current)

05/03/2025

This specification covers a biodegradable deodorant in the form of a liquid concentrate, solid, or gel.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Cleaner for Aircraft Components Cold Tank Type, Solvent-Base

AMS1536C (Current)09/05/2018

This specification covers a tank-type cleaner in the form of a liquid.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Desorption of Brake Friction Materials

J3281_202305 (Current)

05/10/2023

This SAE Recommended Practice specifies a method to reduce and stabilize the moisture of products containing brake friction material (disc brake pads, drum brake shoes, friction blocks) so the parts are conditioned and maintained in a stable low moisture state.

Brake Linings Standards Committee

Hydrogen Embrittlement Effect on Metals By Aircraft Maintenance Chemicals, Mechanical Test Methods

ARP1525 (Current)07/01/1977

The Test Procedure of ARP 1525 is Embodied in ASTM F519, Hydrogen Embrittlement Testing of Aerospace Materials. The requirements of the latest issue of ASTM F519 shall be fulfilled whenever reference is made to ARP1525.)

AMS J Aircraft Maintenance Chemicals and Materials Committee

Disinfectant (Insecticide), Aircraft

AMS1450B (Current)

11/22/2024

This specification covers insecticides for use in disinsection of aircraft as required on international passenger flights.

AMS J Aircraft Maintenance Chemicals and Materials Committee

SAE Megawatt Charging System for Electric Vehicles

J3271_202503 (Current)

03/05/2025

This SAE Technical Information Report (TIR) is based on the initial assumption that a system level standard covering all aspects of EV charging components and use cases would grow to be too large for one comprehensive document. Hence, the SAE J3271 work group was launched with five subtopics that could be subsections of one standard or a separate document for each topic. In this document, all five subtopics are compiled into one document. The recommended practice level documents will follow this structure, with added detail and streamlined content. The five subtopics that are now subsection numbers in this document include: SAE J3271/1 (see 5.1) Electromechanical Coupler Specifications SAE J3271/2 (see 5.2) Communication and Controls SAE J3271/3 (see 5.3) Cables/Cable Handling, Cooling, and Automated Connection Systems SAE J3271/4 (see 5.4) Use Cases Including Grid Interconnection, Black Start, and Bidirectional Power Transfer SAE J3271/5 (see 5.5) Interoperability Testing Requirements

Hybrid - EV Committee

Compound, Corrosion Preventive Soft Film, Thixotropic, Cold Application

AMS3077A (Current)

04/24/2018

This specification covers a ready-mixed thixotropic compound in the form of a stable film-forming compound suitable for application by brushing or spraying.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Cleaning Compound, Terpene Circuit Board Cleaner

AMS1539A (Current)

04/24/2018

This specification covers a terpene base solvent cleaner in the form of a liquid, which forms a transient emulsion with water.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Desmutter, Aluminum Powdered

AMS1625C (Current)04/29/2020

This specification covers powdered materials, solutions of which are used to remove smut from aluminum surfaces treated with etch-type oxidation and corrosion removers.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Remover, Acid Activated, For Amine-Cured Epoxy Coating Systems

AMSR81903A (Current)05/06/2021

This specification covers the requirements for removers used on amine-cured epoxy coating systems (see 6.1).

AMS J Aircraft Maintenance Chemicals and Materials Committee

Oxide Remover Compound, Acidic Aircraft Turbine Engine Components

AMS1382B (Current)

07/29/2020

This specification covers an acidic oxide remover compound in the form of a ready-to-use liquid, liquid concentrate, or water-soluble powder for dilution with water or for dilution with mineral acid as defined by the compound manufacturer.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Cleaning/Scale Removing Compound Aircraft Vacuum Toilet Systems

AMS1454A (Current)

07/06/2023

This specification covers a cleaning/scale removing compound in the form of a liquid concentrate or gel.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Remover, Epoxy Paint Acid-Type, Thickened

AMS1376B (Current)

08/23/2018

This specification covers a paint remover in the form of a liquid.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Compound, Rust Inhibiting Aircraft Engine Components

AMS3060B (Current)

04/29/2020

This specification covers a rust-inhibiting compound in the form of a liquid concentrate or a water soluble powder.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Corrosion of Low-Embrittling Cadmium Plate By Aircraft Maintenance Chemicals

ARP1511B (Current)10/01/1991

AMS J Aircraft Maintenance Chemicals and Materials Committee

Measurement of Copper and Other Elements in Brake Friction Materials

J2975_202007 (Current)

07/23/2020

This procedure describes a method for generating, preparing and analyzing samples of new and unused brake friction materials for their chemical constituents.

Brake Linings Standards Committee

Remover, Organic Coating, Hot Tank Type

AMSR81835 (Current)

01/25/2008

This specification covers the requirements for one grade of remover of various organic coatings from aircraft parts.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Cleaning Compounds, For Parts Washers and Spray Cabinets

AMSC29602A (Current)

07/09/2012

This specification establishes the requirements for cleaning compounds, used in parts washers and spray cabinets for cleaning aircraft components.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Cleaner, Fuel Drop Tank Water Soluble

AMS1541D (Current)

05/22/2023

This specification covers a water-soluble, oil-dispersing cleaner in the form of a liquid.

AMS J Aircraft Maintenance Chemicals and Materials Committee

CLEANING EFFICIENCY OF TURBINE ENGINE GAS PATH CLEANERS Laboratory Test Method

ARP1862A (Current)

08/23/2018

This SAE Aerospace Recommended Practice (ARP) covers a laboratory procedure for determining the cleaning efficiency of aircraft turbine engine gas path cleaners. Results are indicative of cleaning compound performance in the compressor sections of installed aircraft turbine engines, when used in a starter crank/soak/rinse application.

AMS J Aircraft Maintenance Chemicals and Materials Committee

Desmutter, Aluminum Liquid

AMS1626C (Current)04/29/2020

This specification covers materials in the form of a liquid used to remove smut from aluminum surfaces treated with etch-type oxidation and corrosion removers.

AMS J Aircraft Maintenance Chemicals and Materials Committee

SAE No. 2 Friction Test Machine Durability Test

J2489_201203 (Current)

03/19/2012

This SAE Recommended Practice is intended as the definition of a standard test, but may be subject to frequent change to keep pace with experience and technical advances. This should be kept in mind when considering its use. The SAE No 2 Friction Test Machine is used to evaluate the friction characteristics of automatic transmission plate clutches with automotive transmission fluids. It can also be used to conduct durability tests on wet friction systems. The specific purpose of this document is to define a Durability Test based on a specific power level selected from either the 3600 r/min Stepped Power Test or from the 6000 r/min Stepped Power Test, for the evaluation of wet friction system performance variation as a function of number of cycles. This standard procedure is intended for common use by both suppliers and end users to allow objective comparisons of wet friction material system performance. The only variables selected by the supplier or user of the friction system are: a

Automatic Transmission and Transaxle Committee

SAE No. 2 Friction Test Machine 6000 rpm Stepped Power Test

J2488_201907 (Current)

07/24/2019

This SAE Recommended Practice is intended as the definition of a standard test, but may be subject to frequent change to keep pace with experience and technical advances. This should be kept in mind when considering its use. The SAE No. 2 Friction Test Machine is used to evaluate the friction characteristics of automatic transmission plate clutches with automotive transmission fluids. It can also be used to conduct durability tests on wet friction systems. The specific purpose of this document is to define a 6000 rpm stepped power test for the evaluation of wet friction system performance variation as a function of power level. This procedure uses an initial engagement speed of 6000 rpm and is intended as a standard procedure for common use by both suppliers and end users. The only variables selected by the supplier or user of the friction system are: a Friction material b Fluid c Reaction plates These three variables must be clearly identified when reporting the results of using this

Automatic Transmission and Transaxle Committee

SAE No. 2 Friction Test Machine μPVT Test

J2490_201905 (Current)

05/31/2019

This SAE Recommended Practice is intended as the definition of a standard test, which may be subject to frequent change to keep pace with experience and technical advances. This should be kept in mind when considering its use. The SAE No. 2 Friction Test Machine is used to evaluate the friction characteristics of automatic transmission plate clutches with automotive transmission fluids. It can also be used to conduct durability tests on wet friction systems. The specific purpose of this document is to define a μPVT Test for the evaluation of the variation of wet friction system performance as a function of speed, temperature, and pressure. This procedure is intended as a standard for both suppliers and end users. The only variables selected by the supplier or user of the friction system are: a Friction material b Fluid c Reaction plates These three variables must be clearly identified when reporting the results of this test. If any of the test parameters or system hardware as described

Automatic Transmission and Transaxle Committee

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