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CURRENT
2017-11-20
Standard
J587_201711
This SAE Standard provides test procedures, requirements, and guidelines for vehicular license plate illumination devices.
2017-11-16
Article
Hardide has recently completed raising funds for the construction of two additional reactors at the company’s U.S. facility. This comes shortly after Hardide gained Nadcap accreditation for its Hardide-A coating as a replacement for toxic hard-chrome plating.
2017-11-15
WIP Standard
J1698/1
This Recommended Practice provides common data output formats and definitions for a variety of data elements that may be useful for analyzing vehicle crash and crash-like events that meet specified trigger criteria. The document is intended to govern data element definitions, to provide a minimum data element set,and to specify EDR record format as applicable for light-duty motor vehicle Original Equipment applications.
2017-11-10
WIP Standard
SAE5145A
This SAE Aerospace Information Report (AIR) lists whole body anthropometric surveys and provides current sources for the survey raw data and summary statistics. The purpose of this directory is to provide a single source for accessing anthropometric survey data for human modelers, human factors specialists, and other interested in anthropometric data. It is not meant to provide detailed data on each survey, but to provide readers with enough information to allow them to make a decision about which surveys are of possible application to their work. The reader can then obtain further information and actual data from the listed points of contact.
CURRENT
2017-11-09
Standard
ARP594F
The requirements presented in this document address the key considerations for thermal safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank.
CURRENT
2017-11-09
Standard
ARP991C
This document recommends design objectives for navigation, position, and anticollisionlight systems for visual detection and collision avoidance between airplanes in flight and on the ground. Customers for new airplanes or lighting components, and designers or manufacturers may take advantage of this document in specifying the initial requirements that, in most cases, significantly exceed the applicable minimum intensities as shown in the Federal Aviation Regulations as well provide better stability, longer life and lower operating costs.
CURRENT
2017-11-08
Standard
J2854_201711
The CRABI dummy was developed to evaluate small child restraint systems in automotive crash environments, in all directions of impact, with or without air bag interaction Basic anthropometry for this test device was taken from the University of Michigan Transportation Research Institute Report 85-23. Weight distribution and scaling methods for the infant were approved by the Society of Automotive (SAE) Infant Dummy Task Group. The dummy weighs 17.2 pounds and has a 26.4 inches standing or 17.3 inches sitting height. The Hybrid Ill-like neck and lumbar spine are laterally notched to reduce lateral stiffness The shoulders have flesh support for durability and human-like performance in areas where seatbelt webbing may be placed. In addition, rubber elements are used in each joint to improve biofidelity and to give the CRABI infant-like range of motion. The CRABI Six-Month-Old design meets all the SAE Infant Dummy Task Group anthropometry, biomechanical and instrumentation requirements.
2017-11-02
Magazine
700 miles, hands-free! GM's Super Cruise turns Cadillac drivers into passengers in a well-engineered first step toward greater vehicle autonomy. Toyota rethinks the Flagship The 2018 Lexus LS moves to twin-turbo V6 power and piles on the takumi. Honda 2018 Accord: Antidote for crossover fever The all-new, tenth-generation Accord is Honda's best-ever-and makes the case for why crossovers shouldn't take over the planet. Autonomy testing: Simulation to the rescue Autonomous technology development injects new rigors on vehicle-development testing.
2017-10-26
WIP Standard
ARP6812
This SAE Aerospace Recommended Practice (ARP) covers the functional, design, construction, and test requirements for Brake Temperature Monitoring Systems (BTMS), and sometimes referred to as Brake Temperature Indication Systems (BTIS). The BTMS is limited to aircraft where a dispatch indication and brake temperature indication is required. The scope of this BTMS equipment shall be limited to the 1) brake temperature sensor or indicator, 2) temperature reference measurement, if required, and 3) processing and communication of brake temperature. This recommended practice will not address cockpit ergonomics and aircraft operating procedures.
CURRENT
2017-10-26
Standard
J2267_201710
This SAE standard applies to all forestry machines exposed to the hazard of objects penetrating the front of the operator station (other than the roof). This would include:
2017-10-25
WIP Standard
ARP1840C
This document establishes two types of engine transport devices: Type A: For split engine pack transport (mainly lower deck) Type B: For full engine transport (mainly main deck)
2017-10-25
WIP Standard
ARP4166A
This Aerospace Recommended Practice (ARP) defines and establishes design, construction, and performance requirements for a flexible, reusable, water-vaporproof cover for environmental protection of internal combustion engines, major components, and other military and commercial items.
2017-10-25
WIP Standard
ARP4898A
This SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage stands for aircraft engines. An optional hard cover (enclosure) is also specified.
2017-10-25
WIP Standard
ARP4732A
This SAE Aerospace Recommended Practice (ARP) defines and establishes design, construction, and performance requirements for a flexible nonreuseqble waterproof cover for shipment of aircraft engines, major components, and other military and commercial items not intended for storage; items to be removed within fourteen (14) days.
2017-10-25
WIP Standard
AS18013A
No scope available.
2017-10-25
WIP Standard
AS5135A
This SAE Aerospace Standard (AS) describes the characteristics of a desiccant port installed through the flat wall of a shipping and storage container. With the cover removed, the desiccant port shall provide access to the interior of the container for installation and removal of desiccant.
CURRENT
2017-10-25
Standard
J3087_201710
Develop and propose an SAE Recommended Practice for AEB system performance testing which: 1. Establishes uniform vehicle level test procedures 2. Identifies target equipment, test scenarios, and measurement methods 3. Identifies and explains the performance data of interest 4. Does not exclude any particular system or sensor technology 5. Identifies the known limitations of the information contained within (assumptions and "gap") 6. Intended to be a guide toward standard practice and is subject to change on pace with the technology 7. Limited to "Vehicle Front to Rear, In-lane Scenarios" for initial release
2017-10-25
WIP Standard
AS5017A
This SAE Aerospace Standard (AS) describes the characteristics of an air filling valve used in reusable shipping and storage containers.
2017-10-25
WIP Standard
ARP726B
This recommended practice covers a self-contained detection system which is capable of pressurizing a closed system up to 70 psig with halogen (tracer) gas and up to 3500 psig with nitrogen. An external tracer gas supply may be used to increase the capacity of the system. The detector shall be capable of detecting leaks as small as .05 ounce of tracer gas per year, with a system pressure of 70 psig or less. The purpose of this document is to provide a recommended practice for the design of a universal leak detector which will pressurize a closed system with a mixture of inert and tracer gas and provide a probe and detector to indicate location and rate of system leakage with a high degree of accuracy.
CURRENT
2017-10-25
Standard
ARP60493
This guide provides detailed information, guidance, and methods for demonstrating electromagnetic compatibility (EMC) on civil aircraft. This guide addresses aircraft EMC compliance for safety and functional performance of installed electrical and electronic systems. The EMC guidance considers conducted and radiated electromagnetic emissions and transients generated by the installed electrical and electronic systems which may affect other installed electrical and electronic systems on the aircraft. Application of appropriate electrical and electronic equipment EMC requirements are discussed. Methods for aircraft EMC tests and analysis are described. This guide does not address aircraft compatibility with the internal electromagnetic environments of portable electronic devices (PED) or with the external electromagnetic environments, such as high-intensity radiated fields (HIRF), lightning, and precipitation static.
2017-10-25
WIP Standard
J2915
This Information Report documents the problems with the 2002 regulated version of the spine box, and defines a recommended solution to resolve the problem.
2017-10-23
WIP Standard
AMS1435D
This specification covers deicing and anti-icing materials in the form of a fluid. This deicing/anti-icing fluid has been used typically on runways, taxiways, and other aircraft maneuvering areas for the prevention and removal of frozen deposits of frost and ice. Fluids must not be used to deice/anti-ice aircraft.
2017-10-22
WIP Standard
ARP6001A
This SAE Aerospace Recommended Practice (ARP) provides general requirements for a generic “passive” side stick that could be used for fly by wire transport and business aircraft. It addresses the following: - The functions to be implemented - The geometric and mechanical characteristics - The mechanical and electrical interfaces - The safety and certification requirements
2017-10-20
WIP Standard
AS4108C
This specification defines the requirements for A286 cres T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160000 psi, for use with clamps and V-band couplings at 1000 °F maximum ambient temperature.
2017-10-20
WIP Standard
AIR5128B
This SAE Aerospace Information Report (AIR) is limited to the subject of aircraft fuel systems and the questions concerning the requirements for electrical bonding of the various components of the system as related to Static Electric Charges, Fault Current, Electromagnetic Interference (EMI) and Lightning Strikes (Direct and Indirect Effects). This AIR contains engineering guidelines for the design, installation, testing (measurement) and inspection of electrical bonds.
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