Criteria

Text:
Content:
Display:

Results

Viewing 1 to 30 of 5839
CURRENT
2017-07-21
Standard
J1699/3_201707
The main purpose of this Recommended Practice is to verify that vehicles are capable of communicating a minimum subset of information, in accordance with the diagnostic test services specified in SAE J1979: E/E Diagnostic Test Modes, or the equivalent document ISO 15031-5: Communication Between Vehicle and External Equipment for Emissions-Related Diagnostics – Part 5: Emissions-related diagnostic services. Any software meeting these specifications will utilize the vehicle interface that is defined in SAE J2534, Recommended Practice for Pass-Thru Vehicle Programming.
2017-07-20
WIP Standard
ARP5873B
This document presents minimum criteria for the design and installation of LED passenger reading light assemblies in commercial aircraft. The use of “shall” in this specification expresses provisions that are binding. Non-mandatory provisions use the term “should.”
2017-07-19
WIP Standard
J1939DA_201707
This document is intended to supplement the J1939 documents by offering the J1939 information in a form that can be sorted and search for easier use. The J1939 Digital Annex, introduced in August 2013, offers key J1939 technical data in an Electronic Spreadsheet that can be easily searched, sorted, and adapted to other formats. J1939DA contains all of the SPNs (parameters), PGNs (messages), and other J1939 data previously published in the SAE J1939 top level document. J1939DA also contains all of the SLOTs, Manufacturer ID Codes, NAME Functions, and Preferred Addresses previously published in the SAE J1939 top level and the J1939-71 document. J1939DA contains the complete technical details for all of the SPNs and PGNs previously published in the SAE J1939-71 document. It also includes the supporting descriptions and figures previously published in the SAE J1939-71 document.
CURRENT
2017-07-19
Standard
ARP798B
This SAE Aerospace Recommended Practice (ARP) covers the general requirements and test procedures recommended for use with white incandescent integrally lighted instruments. Its use should provide uniformity of illumination from instrument to instrument and legibility under daylight operation. An appendix is provided to familiarize the designer with some of the techniques used to obtain uniformity of color and illumination in various types of instruments.
2017-07-18
WIP Standard
ARP6505
This AIR intends to better document and tabulate electrical load dynamics that influence power source capacity, power quality and stabiltiy.
CURRENT
2017-07-12
Standard
AIR5451A
The landing gear system is a major and safety critical airframe system that needs to be integrated efficiently to meet the overall aircraft program goals of minimizing the penalties of weight, cost, dispatch reliability and maintenance. As the landing gear system business develops and large-scale teaming arrangements and acquisitions become increasingly common, it may be desirable in some instances to procure an Integrated Landing Gear System. This document provides guidelines and useful references for developing an integrated landing gear system for an aircraft. The document structure is divided into four sections: • Landing Gear System Configuration Requirements (Section 3) • Landing Gear System Functional Requirements (Section 4) • Landing Gear System Integrity Requirements (Section 5) • Landing Gear System Program Requirements (Section 6) The landing gear system encompasses all landing gear structural and subsystem elements.
2017-07-12
WIP Standard
J759
This SAE Recommended Practice provides the lighting function identification codes for use on all passenger vehicles, trucks, trailers, motorcycles, and emergency vehicles.
2017-07-11
WIP Standard
AS4111A
This SAE Aerospace Standard (AS) contains a sample test plan for AS 15531 or MIL-STD-1553B Remote Terminals (RT) that may serve several different purposes. This document is intended to be contractually binding when specifically called out in a specification, Statement of Work (SOW), or when required by a Data Item Description (DID). Any and all contractor changes, alterations, or testing deviations to this section shall be separately listed for easy review. The purpose of these tests is to verify that the Unit Under Test (UUT) responds properly in accordance with the requirements of the governing standard. The tests are not intended to verify the mission aspects stated in the equipment specification. The pass criteria is defined in each test paragraph. If any test fails, record the UUT response to that test. This general test plan is intended for design verification of remote terminals designed to meet the requirements of AS 15531 and MIL-STD-1553B with Notice 2.
2017-07-11
WIP Standard
J1608
Provide standard shift pattern guidelines for manual transmission shift controls in light, medium, and heavy trucks and buses.
2017-07-11
WIP Standard
AS4112A
This test plan is broken into two major sections for the production testing of remote terminals: Electrical and Protocol. This production test plan defines the test requirements for verifying that Remote Terminals meet the requirements of MIL-STD-1553B, 'Digital Time Division Command/Response Multiplex Data Bus.'
2017-07-11
WIP Standard
AS4117A
This test plan defines the requirements of data bus components which comply with the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus.
2017-07-11
WIP Standard
AS4114A
This test plan consists of two major sections for the production testing of bus controllers: Electrical tests and Protocol tests. This production test plan defines the test requirements for determining that bus controllers meet the requirements of MIL-STD-1553B, 'Digital Time Division Command/Response Multiplex Data Bus.'
2017-07-11
WIP Standard
AS4116A
This Aerospace Standard (AS) defines the test requirements for determining that bus monitors meet the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus.
2017-07-11
WIP Standard
AS4115A
This test plan consists of two major sections for testing of MIL-STD-1553B data bus systems: Bus Network and System Integration Tests. This test plan defines the test requirements for: a) verifying that the bus network, (that is, cabling, couplers, connectors and terminators) when in the final system design configuration, complies with the requirements of MIL-STD-1553B and b) ensuring that when the bus system (that is, bus network, remote terminals and bus controllers) is integrated, it meets the specific requirements of MIL-STD-1553B, and provides for reliable communications within its system environment.
2017-07-11
WIP Standard
AS4113A
This test plan is broken into three major sections for the testing of bus controllers: Electrical, Protocol and Noise tests. This validation test plan defines the test requirements for verifying that the design of bus controllers meets the requirements of MIL-STD-1553B, 'Digital Time Division Command/Response Multiplex Data Bus.'
CURRENT
2017-07-10
Standard
J3109_201707
The intention of this standard is to establish a framework to measure the efficiency of PWM HVAC Blower Controllers and Brushless DC Motor Controllers and define a usage based overall efficiency. This result can then be used by vehicle OEMs to demonstrate compliance towards requirements or benchmarks established by regulatory agencies.
CURRENT
2017-07-10
Standard
AIR5565
This aerospace information report (AIR) provides historical design information for various aircraft landing gear and actuation/control systems that may be useful in the design of future systems for similar applications. It presents the basic characteristics, hardware descriptions, functional schematics, and discussions of the actuation mechanisms, controls, and alternate release systems.
CURRENT
2017-07-07
Standard
AS81714/10A
Scope not available.
CURRENT
2017-07-07
Standard
AS7974/5A
SCOPE IS UNAVAILABLE.
CURRENT
2017-07-07
Standard
AS85848/2A
SCOPE IS UNAVAILABLE.
CURRENT
2017-07-06
Standard
AS85848A
This specification establishes the requirements for various types of identification sleeving that will shrink to a predetermined size upon the application of heat after it has been marked. Continuous operating temperature ratings range from -55° to 175°C (-67° to 347°F). (See 6.1).
2017-07-05
WIP Standard
AS85049/151
This AS85049 product will accommodate the user demand for a metal version of the AS85049/103 style accessory.
2017-07-05
WIP Standard
AS85049/152
This AS85049 product will accommodate the user demand for a metal version of the AS85049/104 style accessory.
2017-07-05
WIP Standard
AS85049/153
This AS85049 product will accommodate the user demand for a metal version of the AS85049/105 style accessory.
2017-07-05
WIP Standard
J3146
This document has been issued to provide a reference or overview of some current practices which could be utilized for securing the vehicle’s interface with the Data Link Connector (DLC) from cybersecurity risks associated with external test equipment connections (e.g. diagnostics scan tools) or remotely connected applications (e.g. telematics devices). The practices outlined in this report are examples of some secured in-vehicle data access methods which might be used in the automotive industry. Note that In-vehicle network protocol descriptions and data format details are not included in this report.
CURRENT
2017-06-28
Standard
AS47641A
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies.
CURRENT
2017-06-28
Standard
AS47642B
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760C. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies. For validation of aircraft designed to MIL-STD-1760B Notice 3 AS47641 Issued 1999-08 applies.
Viewing 1 to 30 of 5839