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This document defines the test procedures and performance limits of steady state and transient voltage characteristics for 12 V, 24 V, or 48 V electrical power generating systems used in commercial ground vehicles.
Truck and Bus Electrical Systems Committee
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging or tubing stock.
AMS E Carbon and Low Alloy Steels Committee
This supplement forms a part of SAE Aerospace Specification AS85421. It shall be used to identify fitting standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers a ready-to mix, two component, self-curing, inorganic zinc rich primer for use on steel surfaces.
AMS G8 Aerospace Organic Coatings Committee
This specification is designed to present detailed procedure to be followed in splicing cable terminals. The types of cable to which this specification applies are listed in Section 2 and table I.
Aerospace Council
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers a titanium alloy in the form of pre-alloyed powder.
AMS AM Additive Manufacturing Metals
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers aluminum foil tape with a pressure sensitive adhesive.
AMS P Polymeric Materials Committee
Procedures included within this specification supplement are, when used in conjunction with SAE/USCAR 2, intended to cover performance testing at all phases of development, production, and field analysis of electrical terminals, connectors, and components that constitute the electrical connection systems in high voltage (60~600V) road vehicle applications. These procedures are applicable to terminals used for In-Line, Header, and Device Connector systems with and without Shorting Bars. This supplement applies to both sealed and unsealed connection systems.
USCAR
This SAE Recommended Practice establishes a single bolt pattern for the No. 1 clutch housing (see Figure 1) and the No. 2 clutch housing (see Figure 2). These four bolt patterns are designated to give commonality of mounting brackets in existing frame rails. The 420 mm (16.5 in) span, pad face to pad face, allows the ease of installation in existing frame rail widths. This is also the minimum spacing which will accommodate commonly used clutches.
Truck and Bus Powertrain Committee
SAE J1979-2 describes the communication between the vehicle’s OBD systems and test equipment required by OBD regulations. OBD regulations require passenger cars and light-, medium-, and heavy-duty trucks to support a minimum set of diagnostic information to external (off-board) “generic” test equipment.
Vehicle E E System Diagnostic Standards Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This SAE Aerospace Recommended Practice (ARP) includes the minimum human factors requirements and recommendations for the flight deck display of data linked Aeronautical Information (AI), specifically Notices to Airmen (NOTAMs). The goal of human factors is to make it easy for users to do things right and hard to do them wrong. The guidance in this ARP supports this goal by defining minimum requirements and recommendations that focus on the text and potential graphics for NOTAMs as well as the human’s interaction with these on the flight deck. In this ARP “flight deck” includes both single pilot flight decks as well as multi-pilot flight decks. The FAA defines NOTAMs1 as any information concerning the establishment, condition, or change in any component of, or hazard to, the National Airspace System. ICAO Annex 15 defines a NOTAM as “a notice distributed by means of telecommunication containing information concerning the establishment, condition, or change in any aeronautical facility
G-10A Aeronautical Information System Committee
This SAE Aerospace Standard (AS) defines the items that shall be considered when creating a fiber optic cable assembly specification and source control drawing intended for installation on aerospace platforms.
AS-3 Fiber Optics and Applied Photonics Committee
This specification covers a carbon steel in the form of sheet and strip.
AMS E Carbon and Low Alloy Steels Committee
The requirements of 9100 apply with the following clarification for software. This standard supplements the 9100 standard requirements for deliverable software and contains quality management system requirements for organizations that design, develop, and/or produce deliverable software and services for the aviation, space, and defense industry. This includes, as required, support software that is used in the development and maintenance of deliverable software and services. The deliverable software may be stand-alone, embedded, mobile application, or loadable into a target computer. This deliverable software may also be part of services (e.g., cloud environment, web hosted solutions or platforms). Where the use of Hardware Description Language (HDL) or high order language is utilized as the design source of electronic hardware [e.g., Application Specific Integrated Circuit (ASIC), Programmable Logic Device (PLD)]; the organization and customer, and/or supplier shall agree on the extent
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This specification covers silicone (VMQ) rubber sheet reinforced with glass cloth.
AMS P Polymeric Materials Committee
This specification covers the requirements for filled, resinous thermosetting compound and sheet pre-preg to fabricate shims for use during assembly of aircraft and marine components and parts.
AMS P Polymeric Materials Committee
This specification covers a heat-resistant gamma titanium aluminide alloy in the form of pre-alloyed powder.
AMS AM Additive Manufacturing Metals
SAE Aerospace Information Report AIR1871 provides valuable insight into lessons learned in the development, implementation, and operation of various health monitoring systems for propulsion engines and drive train systems. This document provides an overview of the lessons learned for ground-based systems, oil debris monitoring systems, lubrication systems, and Health and Usage Monitoring Systems (HUMS) for military and commercial programs. For each case study, this document presents a brief technical description, the design requirements, accomplishments, lessons learned, and future recommendations. The lessons learned presented in this document represent a fragment of the knowledge gained through experience when developing and implementing a propulsion health management system. Previous versions of this document contain additional lessons learned during the 1980’s and 1990’s that may be of additional value to the reader. This document will be maintained as technology progresses so that
E-32 Aerospace Propulsion Systems Health Management
This specification covers an aluminum alloy in the form of sheet clad on both sides with a different aluminum alloy.
AMS D Nonferrous Alloys Committee
The following are suggested policies, procedures, and practices required to maintain mobile and fixed ground support equipment at airport passenger and cargo terminals. The principal purpose for ground support equipment maintenance is to provide the owner/user with safe, serviceable equipment, in good appearance, at minimal cost, and with minimum downtime. Maintenance programs initiated on ground support equipment must also conform to regulations controlling airport operations. This document has been divided into three sections corresponding to the three stages of equipment life; acquisition, maintenance, and disposal.
AGE-3 Aircraft Ground Support Equipment Committee
The materials defined by this U.S. CAR / S.A.E Recommended Practice are low VOC water based coatings for automotive tooling and general maintenance.
USCAR
This document describes a physical layer utilizing Unshielded Twisted Pair (UTP) cable with extended stub lengths for flexibility in ECU placement and network topology. Also, connectors are not specified. CAN controllers used on SAE J1939-15 networks must be restricted to use only Classical Frames as defined in ISO 11898- 1. A network which may have legacy controllers cannot tolerate FD Frames. 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
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
E-25 General Standards for Aerospace and Propulsion Systems
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