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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.
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.
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
2017-10-23
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.
2017-10-19
WIP Standard
J2980
This SAE Recommended Practice presents a method and example results for determining the Automotive Safety Integrity Level (ASIL) for automotive electrical and electronic (E/E) systems. This activity is required by ISO 26262-3:2011 [1], and it is intended that the process and results herein are consistent with ISO 26262:2011 [1]. The technical focus of this document is on vehicle motion control systems. It is limited to passenger cars weighing up to 3.5 metric tons. Furthermore, the scope of this recommended practice is limited to collision-related hazards. ISO 26262:2011 [1] has a wider scope than SAE J2980, covering other functions and accidents (not just motion control or collisions as in SAE J2980).
2017-10-16
Article
The hand-over warning comes 15-20 s before it is required and the system uses a sophisticated infrared driver monitoring system to ensure the driver is capable of taking back the vehicle.
2017-10-16
WIP Standard
J2838
This SAE standard provides test procedures, performance requirements, design guidelines and installation guidelines for full adaptive forward lighting systems (AFS).
2017-10-16
WIP Standard
ARP6448A
This document provides an industry-recommended framework for establishing agreements to ensure that seats with integrated electronic components (e.g., actuation system, reading light, inflatable restraint, IFE, etc.) meet the seat TSO Minimum Performance Standard. These agreements will allow Seat Suppliers to build and ship completed, integrated and approved seat assemblies under TSOA with electronics included. The document presents the roles, responsibilities and accontibilities of the Electronics Manufacturer, the Seat Supplier, and the Seat Installer/Electronics Activator in the context of AC 21-49 Section 7.b ‘ Type Certification using TSO-approved seat with electronic components defined in TSO design’. This document applies to all FAA seat TSOs (C39(), C127()…etc).
2017-10-13
WIP Standard
AS7516A
SCOPE IS UNAVAILABLE.
2017-10-12
WIP Standard
J1814
General criteria are presented as guidelines for: control device location, resistance, and actuation of hand and foot controls by the machine's operator. The criteria are based upon physical limitations as defined by human factors engineering principles. This SAE Recommended Practice applies to upright seated operators of Road Building and Maintenance, and Specialized Mining Machinery categories of off-road, self-propelled work machines as identified in SAE J1116. The criteria presented should apply to most situations. Each situation, however, must be evaluated as to its own function and its relationship to other functions to achieve the desired operation action in normal and emergency situations with high probability. The values for control displacement and resistance apply only to what is required to achieve the desired performance of the function being controlled for the 5th through the 95th percentile person as defined in ISO 3411.
2017-10-12
White Paper
WP-0005
Annie Chang, Nicolas Saunier, Aliaksei Laureshyn
To date, the universal metric for road safety has been historical crash data, specifically, crash frequency and severity, which are direct measures of safety. However, there are well-recognized shortcomings of the crash-based approach; its greatest drawback being that it is reactive and requires long observational periods. Surrogate measures of safety, which encompass measures of safety that do not rely on crash data, have been proposed as a proactive approach to road safety analysis. This white paper provides an overview of the concept and evolution of surrogate measures of safety, as well as the emerging and future methods and measures. This is followed by the identification of the standards needs in this discipline as well as the scope of SAE’s Surrogate Measures of Safety Committee.
CURRENT
2017-10-11
Standard
J2858_201710
This user's manual covers the Hybrid III 10-year old child test dummy. The manual is intended for use by technicians who work with this test device. It covers the construction and clothing, assembly and disassembly, available instrumentation, external dimensions and segment masses, as well as certification and inspection test procedures. It includes guidelines for handling accelerometers, guidelines for flesh repair, and joint adjustment procedures. Finally, it includes drawings for some of the test equipment that is unique to this dummy.
CURRENT
2017-10-10
Standard
ARP5945A
The purpose of this Aerospace Recommended Practice (ARP) is to provide the sample selection criteria and endurance time test procedures for SAE Type I aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G-12 Holdover Time Committee. A significant body of previous research and testing has indicated that all Type I fluids formulated with conventional glycols, as defined in 3.1.1 of AMS1424, perform in a similar manner from an endurance time perspective. This applies to Type I deicing/anti-icing fluids formulated with propylene glycol, ethylene glycol, and diethylene glycol only. As a result, Type I deicing/anti-icing fluids containing these glycol bases no longer require testing for endurance times.
CURRENT
2017-10-10
Standard
ARP5485B
The purpose of this Aerospace Recommended Practice (ARP) is to provide the sample selection and endurance time test procedures for SAE Type II, III, and IV aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G-12 Holdover Time Committee. The related standard ARP5718 provides the process by which endurance time data is converted to holdover times for publication by regulators and subsequent use by aircraft operators.
CURRENT
2017-10-10
Standard
ARP6207
This document describes: the preparatory steps to test experimental Type I fluids according to AMS1424; the recommendations for the preparation of samples for endurance time testing according to ARP5945; a short description of the recommended field spray test; the protocol to demonstrate that Type I fluid can be used with the Type I holdover time guidelines published by the FAA and Transport Canada, including endurance time data obtained from ARP5945; the protocol for inclusion of Type I fluids on the FAA and Transport Canada lists of fluids; the protocol for updating the FAA and Transport Canada lists of fluids; the role of the SAE G-12 Aircraft Deicing Fluids Committee; the role of the SAE G-12 Holdover Time Committee; and the process for the publication of Type I holdover time guidelines. This document does not describe laboratory-testing procedures. This document does not include the qualification requirements for AMS1428 Type II, III, and IV fluids (these are provided in ARP5718).
CURRENT
2017-10-10
Standard
ARP6385
The requirements presented in this document address the key considerations for mechanical and electrical 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
2017-10-09
Standard
J220_201710
This SAE Recommended Practice applies to the boomstop for the main boom of all mobile construction type cranes having rope supported booms, equipped for hook work, clamshell, magnet, grapple, or concrete bucket attachments.
2017-10-05
WIP Standard
AIR6811
Provide guidance for applying aircraft equipment electromagnetic, electrical, and mechanical qualification standards, including RTCA/DO-160, MIL-STD-461, MIL-STD-810, and MIL-STD-704, to civil aircraft certification intended for military use and for military aircraft equipment installed on civil aircraft. The guidance will identify where the equipment environmental qualification standards meet the intent of the civil or military aircraft certification requirements. Conversely, the guidance will identify where the equipment environmental qualification standards have differences that do not meet the intent of the civil or military aircraft certification requirements and when these differences matter based on equipment criticality.
2017-10-05
Magazine
ICE Breaker! Mazda's Skyactiv-X beats the big guys to market with a promising new production engine that marries Otto and Diesel attributes. Testing mmWave radars in the loop University of Texas researchers develop a real-time HIL testbed that beats the incumbents on cost, time and flexibility. Driverless cars and freeway traffic flow Analysis shows platooning and wave damping can reduce congestion. Editorial: EVs lack a robust charging grid SAE Standards News Mobility for everyone: Automated Driving Systems Supplier Eye The future on stage at Frankfurt The Navigator Time for standard naming of safety features Developing high-energy-density batteries for EVs U.S.
2017-10-03
WIP Standard
J1015
This SAE Standard establishes the Tonne Kilometer Per Hour Test Procedure for off-the-road tires. This document is applicable to only those tires used on certain earthmoving machines referenced in SAE J1116.
2017-10-03
WIP Standard
J3157
The scope of this task force is to gather information of all bicyclist targets known to the task force members and analyzed the state of the art features of these targets. The goal of the Bicyclist Test Target Task Force is to develop standard specifications/requirements for bicyclist test targets that are representative of real bicyclists to the sensors used in Forward Looking Pedestrian Detection systems and can be used for performance assessment of such in-vehicle systems (including warning and/or braking) in real world test scenarios/conditions.
CURRENT
2017-10-03
Standard
AS1055E
This SAE Aerospace Standard (AS) establishes uniform requirements and procedures for the fire testing of flexible hose assemblies and rigid tube assemblies (including coiled tubes) to be used in aircraft or aerospace vehicle fluid systems. These procedures may also be followed for fire tests on other piping components as specified by the customer. It also refers to standard fire test equipment to be used in conducting "referee" fire tests.
Viewing 31 to 60 of 17408

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