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This document provides recommendations to vehicle manufacturers, ECU developers, and other device suppliers in securing the SAE J1939 network from cybersecurity risks. This document focuses on security measures related to on-vehicle network architecture and security measures for communication interfaces between devices, ECUs, or networks. The focus is on security related to network communications on the vehicle side of off-vehicle interfaces, such as the SAE J1939-13 connector. The recommendations in this document aim to address cybersecurity risks presented by communication between the vehicle and the rest of the supporting ecosystem via the vehicle networks. The risk focus is on safety and operational risks, although other risks are possible. This document should be used as a reference to current best practices for addressing off-vehicle communication security. This document focuses on recommendations related to the Secure Architecture and Secure Connectivity aspects of vehicle
Truck and Bus Control and Communications Network Committee
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
This SAE Recommended Practice defines the test stand and procedure for evaluating radial impacts of all wheels intended for passenger cars and light trucks. A minimum performance requirement is intentionally not provided. The intent is to establish a uniform method and test stand for imparting damage and evaluating radial impacts. A minimum performance requirement will be a proposed change when users determine what is of most value.
Wheel Standards Committee
This SAE Recommended Practice contains dimensions and their tolerances concerning disc wheel to hub or drum interface areas for truck and bus applications. Disc wheels designed only for single wheel applications (not dual wheels) for light trucks and special or less common applications are not covered in this document.
Truck and Bus Wheel Committee
This SAE lab recommended practice may be applied to corrosion test methods such as salt spray, filiform, Corrosion creep back, etc. This procedure is intended to permit corrosion testing to be assessed between Laboratories for correlation purposes.
Wheel Standards Committee
This test procedure defines a laboratory procedure for generating and evaluating filiform corrosion on painted aluminum wheels and painted aluminum wheel trim. While this test was developed specifically for the testing of painted aluminum wheels and wheel trim, it may be applicable to other components. The application owner will need to assess if this test generates filiform similar to that found in the relevant usage to ensure it will provide accurate data for the application.
Wheel Standards Committee
The supplier shall use the following process to respond to a customer request for corrective and preventive action.
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
This document covers the process to be applied to design characteristics (as defined in AS9102), parts or inspection processes as defined by the purchaser. Design characteristics not included within the scope include electronic, electromechanical or mechanical systems where alternative means of acceptance are approved such as through acceptance test procedures (ATPs). This document does not define processes for identifying or communicating the classification of the parts or design characteristics. This document does not define the procedure to qualify a supplier to undertake these requirements. It is expected that each purchaser will have a procedure to manage the flow-down of these requirements. This document applies to suppliers that demonstrate adequate proficiency in applicable process control methods as determined by the purchaser.
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
This SAE Recommended Practice is intended to serve as a guide for standardization of features, dimensions, and configurations of balance weights for aluminum and steel wheels intended for use on passenger cars, light trucks, and multipurpose vehicles to assure good installation and retention of the balance weight. This document also provides test procedures and minimum performance requirements for testing balance weight retention.
Wheel Standards Committee
This SAE lab test procedure should be used when performing the following specialized weathering tests for wheels; Florida Exposure, QUV, Xenon and Carbon Weatherometer. In addition to these procedures, some additional post-weathering tests may be specified. Please refer to customer specifications for these requirements.
Wheel Standards Committee
This recommended practice contains dimensions and tolerances for outboard mounted brake drums and disc wheel hubs in the interface areas. This recommended practice is intended for outboard mounted brake drums and disc wheel hubs commonly used on class 7 and 8 commercial vehicles. Included are SAE J694 mounting systems II, III, IV, XIV, and X. Special and less common applications are not covered.
Truck and Bus Wheel Committee
To provide a procedure to inspect a refrigerant cylinder used in equipment servicing mobile air-conditioning (A/C) systems. This includes the pressure cylinder used for refrigerant recovery/recycling and charging equipment.
Interior Climate Control Fluids Committee
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. This SAE No. 2 friction test monitors the µ-v curve for a negative slope which can be used to evaluate a wet clutch system (WCS) anti-shudder performance and can be used for any wet driveline mechanism. WCS shudder is considered a clutch failure condition. The cause of shudder is consistent with glazing as the primary failure mode. It has been shown that a substantial loss of the wet friction material surface porosity leads to a glaze forming on the friction material surface. This process typically leading to a negative dµ/dv slope over time as addressed in SAE 2020-01-0560. This procedure includes evaluation friction characteristics of wet clutch stystem (WCS) at various specific pressures, speeds, and temperatures, and an extended durability duty cycle test to
Automatic Transmission and Transaxle Committee
This specification covers a titanium alloy in the form of wire for welding filler metal.
AMS G Titanium and Refractory Metals Committee
This specification covers requirements for the material, design, testing and packaging of straight thread tube fitting boss O-rings. O-rings covered by this specification are acrylonitrile-butadiene rubber.
AMS CE Elastomers Committee
This SAE Information Report establishes a minimum level of uniform recipes for contaminants which may be used when durability testing pneumatic components to obtain additional information on how a device may perform under more true-to-life operating conditions. This type of contamination testing, however, is not meant to replace the type of performance testing described in SAE J1409 and SAE J1410. Durability testing in the presence of contamination will yield results more reflective of actual in-service field conditions and provide an additional evaluation of pneumatic devices. While the contaminant supply rate and other test criteria of the device being tested must be set by the device manufacturer or user, the items covered in this document will be:
Truck and Bus Brake Supply and Control Components Committee
This specification covers a high-expansion steel in the form of bars 1.063 inch (27 mm) and under in nominal diameter or distance between parallel sides.
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Aerospace Information Report (AIR) presents data on hydraulic fluids which are of interest to detail designers of hydraulic systems and components for aerospace flight vehicles. The data pertains to fluids conforming to the following specifications: MIL-PRF-5606 MIL-H-8446 MIL-PRF-27601 (canceled) MIL-PRF-27601 has been canceled without replacement and the data presented herein is for information purposes only. MIL-PRF-83282 MIL-H-53119 MIL-PRF-87257 AS1241 Type IV, Classes 1 and 2, and Type V
A-6C1 Fluids and Contamination Control Committee
This specification covers disinfectants or chemicals for use in disinfecting aircraft after carrying livestock.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a cleaner in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification defines limits of variation for determining acceptability of the composition of wrought low-alloy and carbon steel parts and material acquired from a producer.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a chloroprene rubber (CR) that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes such as window channels, bumper pads, chafing strips, etc. For molded rings, compression seals, molded O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the equivalent AMS7XXX specification.
AMS CE Elastomers Committee
This specification covers grease for use within an aircraft. It also defines the quality control requirements to assure batch conformance and materials traceability, and the procedures to manage and communicate changes in the grease formulation and brand. This specification invokes the Performance Review Institute (PRI) product qualification process. Requests for submittal information may be made to the PRI at the address in 2.2, referencing this specification. Products qualified to this specification are listed on a Qualified Products List (QPL) managed by the PRI. Additional tests and evaluations may be required by individual equipment builders before a grease is approved for use in their equipment. Approval and/or certification for use of a specific grease in aero and aero-derived marine and industrial applications is the responsibility of the individual equipment builder and/or governmental authorities and is not implied by compliance with or qualification to this specification.
AMS M Aerospace Greases Committee
This recommended practice provides the dimensional data for the diameters of surfaces that interface with the following tee head bolt series: AS3232 thru AS3235, MS9397 thru MS9402 and MS9432 thru MS9437, or other parts with compatible dimensions.
E-25 General Standards for Aerospace and Propulsion Systems
This SAE Recommended Practice describes a test method for measuring the forces and moments generated at a spindle when a tire rolls over a rectangular obstacle, cleat, at very low speed. The cleat used in a particular test condition is configured with its crest either perpendicular, 90 degrees, to the path of the tire or optionally with its crest inclined at an angle to the path of the tire. The carriage to which the spindle is attached is rigidly constrained in position during each test condition so as to provide a good approximation to fixed loaded radius operation. The method discussed in this document provides cleat envelopment force and moment and tire angular position histories as functions of distance traveled. These histories are essentially free from variations due to tire non-uniformities. The method applies to any size tire so long as the equipment is properly scaled to conduct the measurements for the intended test tire. The data are suitable for use in determining
Vehicle Dynamics Standards Committee
This specification establishes the engineering requirements for producing anodic coatings on magnesium and magnesium alloys, from an alkaline electrolyte, and the properties of those coatings.
AMS B Finishes Processes and Fluids Committee
This specification covers an aluminum-beryllium alloy in the form of bars, rods, tubing, and shapes consolidated from powder by extrusion.
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion-resistant steel in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers one grade (Grade 1) of commercially-pure titanium in the form of sheet, strip, and plate up through a thickness of 1.000 inch (25.40 mm), inclusive.
AMS G Titanium and Refractory Metals Committee
This specification covers established inch/pound manufacturing tolerances applicable to copper and copper alloy wire ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted.
AMS D Nonferrous Alloys Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) 0.040 to 4.500 inches (1.02 to 114.30 mm), inclusive, in thickness produced with maximum cross sectional area of 56.1 square inches (36199 mm2) and a maximum circumscribing circle diameter (circle size) of 24.4 inches (620 mm) (see 2.4.1 and 8.6).
AMS D Nonferrous Alloys Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Spring clips (inner and outer) and associated PTFE single split cushion designed to support metric metal tubes (or inch tubes, using the inch series cushion).
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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