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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 specification covers metric aircraft quality spacers for use as positioners for tubes, flat washers for use as load spreaders, galling protection of adjacent surfaces and or material compatibility, and key or tab washers for use as locks for bolts, nuts, and screws.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286.
E-25 General Standards for Aerospace and Propulsion Systems
E-25 General Standards for Aerospace and Propulsion Systems
The purpose of this document is to define: - compensation washer application requirements - recommended materials - washer thickness determination - dimensioning
E-25 General Standards for Aerospace and Propulsion Systems
This document covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286.
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers studs made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286.
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, and of 130000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
E-25 General Standards for Aerospace and Propulsion Systems
This SAE Aerospace Standard provides minimum design, installation, and removal requirements for AS3319 through AS3322 studs and is applicable when specified on engineering drawings, or in procurement documents.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers aircraft quality bolts and screws made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of room temperature tensile strengths ranging from 125000 to 185000 psi.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718. The following specification designations and their properties are covered:
E-25 General Standards for Aerospace and Propulsion Systems
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