Search Results

Standard

USCAR INFLATOR TECHNICAL REQUIREMENTS AND VALIDATION

2013-04-30

HISTORICAL

USCAR24-2

This specification establishes the performance, and validation requirements for the inflator assembly used in airbag modules. Seatbelt Pretensioners are covered as a reference only.

Standard

10 Megabit/sec Network Configuration Digital Time Division Command/Response Multiplex Data Bus

2013-04-29

HISTORICAL

AS5652

This SAE Aerospace Standard (AS) contains requirements for a digital time division command/response multiplex data bus, for use in systems integration that is functionally similar to MIL-STD-1553B with Notice 2 but with a star topology and some deleted functionality. Even with the use of this document, differences may exist between multiplex data buses in different system applications due to particular application requirements and the options allowed in this document. The system designer must recognize this fact and design the multiplex bus controller (BC) hardware and software to accommodate such differences. These designer selected options must exist to allow the necessary flexibility in the design of specific multiplex systems in order to provide for the control mechanism, architectural redundancy, degradation concept, and traffic patterns peculiar to the specific application requirements.

Standard

Test Plan/Procedure for AS5643 IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications

2013-04-29

CURRENT

AS5657

This document establishes test plans/procedures for the AS5643 Standard that by itself defines guidelines for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. This test specification defines procedures and criteria for testing device compliance with the AS5643 Standard.

Standard

TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, GROUNDING MODULES, STUD TYPE MOUNTING, SERIES I

2013-04-29

HISTORICAL

AS81714/27

Standard

CRIMPING TOOL, TYPE 2, ELECTRICAL, WIRE SPLICING, HAND ACTUATED, TYPE II, FOR ENVIRONMENTAL SPLICES, WIRE RANGE 26-12 AWG

2013-04-29

HISTORICAL

AS22520/37

Standard

Event Data Recorder - Output Data Definition

2013-04-29

HISTORICAL

J1698/1_201304

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 and EDR record format as applicable for light-duty motor vehicle Original Equipment applications.

Standard

IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications

2013-04-29

HISTORICAL

AS5643A

This SAE Aerospace Standard (AS) establishes the requirements for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. It defines the concept of operations and information flow on the network. As discussed in 1.4, this specification contains extensions/restrictions to “off-the-shelf” IEEE-1394 standards, and assumes that the reader already has a working knowledge of IEEE-1394. This document is referred to as the “base” specification, containing the generic requirements that specify data bus characteristics, data formats and node operation. It is important to note that this specification is not stand-alone - several requirements provide only example implementations and delegate the actual implementation to be specified by the network architect/integrator for a particular vehicle application. This information is typically contained in a “network profile” slash sheet that is subservient to this base specification.

Standard

Validation Testing of Electric Fuel Pumps for Gasoline Fuel Injection Systems

2013-04-29

HISTORICAL

J1537_201304

This SAE Recommended Practice defines the minimum design verification testing required to verify the suitability of in-tank mounted electric motor driven fuel pumps used for pumping gasoline or gasoline blend fuels. Additional tests not specified in SAE J1537 will be required for frame mounted pump applications or pumps intended for use on aircraft, motorcycles, or marine equipment.

Standard

STRAPS, CLAMPS, AND MOUNTING HARDWARE, PLASTIC AND METAL FOR CABLE HARNESS TYING AND SUPPORT STRAP, TIE DOWN, ADJUSTABLE, CORROSION RESISTANT STEEL, TYPE VI, CLASS 1

2013-04-29

HISTORICAL

AS23190/3A

Standard

Mechanical and Material Requirements for Externally Threaded Fasteners

2013-04-29

HISTORICAL

J429_201304

This SAE Standard covers the mechanical and material requirements for inch-series steel bolts, screws, studs, screws for sems1, and U-bolts2 in sizes to 1-1/2 in. inclusive. The term “stud” as referred to herein applies to a cylindrical rod of moderate length threaded on either one or both ends or throughout its entire length. It does not apply to headed, collared, or similar products which are more closely characterized by requirements shown herein for bolts. The mechanical properties included in Table 1 were compiled at an ambient temperature of approximately 20 °C (68 °F). These properties are valid within a temperature range which depends upon the material grade used and thermal and mechanical processing.

Standard

Guidance on Selecting a Ground-based Icing Simulation Facility

2013-04-24

WIP

AIR6247

This document is intended to serve two purposes: (1) provide a list of topics for potential customers to ask of the facility to aid their selection decision-making, and (2) provide a list of icing wind tunnel and engine test stand facilities that simulate flight through icing or ice crystal clouds.

Standard

Glossary - Automatic Belt Tensioner

2013-04-24

HISTORICAL

J2198_201304

This glossary was written to provide a consistent and uniform definition of terms used in describing an automatic belt tensioner as it applies to an automotive accessory drive system.

Standard

Shot Peening Coverage Determination

2013-04-24

HISTORICAL

J2277_201304

This SAE recommended practice provides some procedure for determining shot peening coverage and relating coverage to part exposure to the media stream. Effectiveness of shot peening is directly dependent on coverage. Either incomplete or excessive coverage can be detrimental to fatigue strength and life.

Standard

Aircraft Inflight Icing Terminology

2013-04-23

CURRENT

ARP5624

This SAE Aerospace Recommended Practice (ARP) provides recommended definitions for terms commonly used in aircraft inflight icing system design and analysis, research, and operations. Some general thermodynamic terms are included that are frequently used in icing analysis, but this document is not meant to be an inclusive list of such terms.

Standard

Rotor Blade Electrothermal Ice Protection Design Considerations

2013-04-23

CURRENT

AIR1667A

This SAE Aerospace Information Report (AIR) identifies and summarizes the various factors that should be considered during design, development, certification, or testing of helicopter rotor blade ice protection systems. Although various concepts of ice protection are mentioned in this report, the text is limited generally to those factors associated with design and substantiation of cyclic electrothermal ice protection systems as applicable to the protection of helicopter rotor blades. Other systems are described briefly in Appendix A. Applications consider main rotor blades, conventional tail rotor blades, and other types of antitorque devices. The information contained in this report is also limited to the identification of factors that should be considered and why the factor is important. Specific design, analysis and test methodologies are not included. For additional information refer to the references listed in 2.1.

Standard

Droplet Sizing Instrumentation Used in Icing Facilities

2013-04-23

CURRENT

AIR4906

A review of droplet sizing instruments used for icing research is presented. These instruments include the Forward Scattering Spectrometer Probe, the Optical Array Probe, the Phase Doppler Particle Analyzer, the Malvern Particle Size Analyzer, the oil slide technique, and the rotating multicylinder. The report focuses on the theory of operation of these instruments and practical considerations when using them in icing facilities.

Standard

O-RING, MOLDED FROM AMS7379 RUBBER FOR USE WITH AS5202 PORTS

2013-04-23

HISTORICAL

AS6203

Standard

Information on Brake-By-Wire (BBW) Brake Control Systems

2013-04-22

HISTORICAL

AIR5372

A panel of the SAE A-5A Committee prepared this SAE Aerospace Information Report (AIR). The document describes the design approaches used for current applications of Brake-by-Wire (BBW) control systems that are used on commercial and military airplanes. The document also discusses the experience gained during service in the commercial and military environments, and covers system, ergonomic, hardware, and development aspects. The treatment includes the lessons that have been learned during application of the technology. Although there are a variety of approaches that have been used in the design of BBW systems, the main focus of this document is on systems that use the electro-hydraulic method of control. The overall range of implementations is briefly described in 2.3. Sections 3, 4, and 5 describe the electro-hydraulic method in detail.

Standard

J1349 Certified Power Engine Data for GM LFX as used in 2014 Cadillac CTS (Alpha A1LL) ISOPOWER adjusted based on 2013 Cadillac ATS - Level 1

2013-04-22

CURRENT

CPGM1_14LFXCTS

This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.

Standard

J1349 Certified Power Engine Data for GM LFX as used in 2013 Cadillac ATS (ISOPOWER adjusted based on 2012 Chevrolet Camaro LFX) - Level 1

2013-04-22

CURRENT

CPGM1_13LFXATS

This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.