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Viewing 241 to 270 of 712
HISTORICAL
2009-06-29
Standard
ARP5660
The purpose of this document is to provide guidelines for the standardization of safe operating procedures to be used in performing the services and maintenance at Designated Deicing Facilities (Central Deicing Facilities/Remote Deicing Facilities) that are necessary for proper de-icing/anti-icing of aircraft on the ground and performing of associated checks in accordance with the various approved ground icing programs, while considering applicable local environmental, operational and economic requirements. This document should be used by regulators and airport authorities to develop and standardize approvals and permits for the establishment and operation of a DDF. Operating procedures must be agreed to, in writing, by all air operators, airport authorities, regulators and service providers prior to commencing deicing operations.
HISTORICAL
2009-06-29
Standard
J551/15_200906
This SAE Standard specifies the ESD test methods and procedures necessary to evaluate electronic modules intended for vehicle use. It describes test procedures for evaluating electronic modules in complete vehicles. A procedure for verifying the simulator that is used to generate the electrostatic discharges is given in Appendix A. Functional status classifications for immunity to ESD are given in Appendix B.
CURRENT
2009-06-05
Standard
AIR1204A
This Aerospace Information Report (AIR) outlines the design considerations and criteria for the control of water carryover from the environmental control system (ECS) with respect to causes and indicated corrective or preventative action. In addition, condensation on structure will be reviewed with possible preventative action described.
HISTORICAL
2009-04-22
Standard
ARP4260A
This SAE Aerospace Recommended Practice (ARP) contains methods used to measure the optical performance of airborne electronic flat panel display (FPD) systems. The methods described are specific to the direct view, liquid crystal matrix (x-y addressable) display technology used on aircraft flight decks. The focus of this document is on active matrix, liquid crystal displays (LCD). The majority of the procedures can be applied to other display technologies, however, it is cautioned that some techniques need to be tailored to different display technologies. The document covers monochrome and color LCD operation in the transmissive mode within the visual spectrum (the wavelength range of 380 to 780 nm). These procedures are adaptable to reflective and transflective displays paying special attention to the source illumination geometry. Photometric and colorimetric measurement procedures for airborne direct view CRT (cathode ray tube) displays are found in SAE ARP1782.
HISTORICAL
2009-02-25
Standard
AS5420E
This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, integrally heated silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and is primarily intended for use in aircraft potable water systems with an environmental operating temperature range of -65 °F (-54 °C) to +160 °F (+71 °C).
CURRENT
2009-02-16
Standard
J2766_200902
This recommended best practice outlines a method for estimating CO2-Equivalent emissions using the GREEN-MAC-LCCP© (Global Refrigerants Energy and ENvironmental – Mobile Air Conditioning – Life Cycle Climate Performance) model (also referred to as “the model” in this standard).
CURRENT
2008-12-15
Standard
AMS3100/3A
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS3100B. The requirements of the latest issue of AMS3100B shall be fulfilled whenever reference is made to the cancelled AMS3100/3. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS3100B.
HISTORICAL
2008-12-02
Standard
J1351_200812
This test applies to various materials used for insulation and other applications.
CURRENT
2008-11-25
Standard
J1718_200811
This SAE Recommended Practice describes a procedure for measuring gaseous hydrogen emissions from the aqueous battery system of a battery-powered passenger car or light truck. The purpose of this procedure is to determine what concentrations of hydrogen gas an electric vehicle together with its charger will generate while being charged in a residential garage. Gaseous emissions are measured during a sequence of vehicle tests and laboratory tests that simulate normal and abnormal conditions during operational use. The results of this test may be used to determine whether or not forced air ventilation is required when a particular electric vehicle and its associated battery and charging system are used in a residential garage.
HISTORICAL
2008-10-21
Standard
AMS3006G
This specification covers mixtures of methyl alcohol and/or ethyl alcohol with water in the form of liquids.
CURRENT
2008-10-02
Standard
J2190_200810
This SAE Recommended Practice describes the implementation of Enhanced Diagnostic Test Modes, which are intended to supplement the legislated Diagnostic Test Modes defined in SAE J1979. Modes are defined for access to emission related test data beyond what is included in SAE J1979, and for non-emission related data. This document describes the data byte values for diagnostic messages transmitted between diagnostic test equipment, either on-vehicle or off-vehicle, and vehicle electronic control modules. No distinction is made between test modes for emission related and non-emission related diagnostics. These messages can be used with a diagnostic serial data link such as described in SAE J1850 or ISO 9141-2. For each test mode, this document includes a functional description of the test mode, request and report message data byte content, and an example if useful for clarification.
HISTORICAL
2008-08-28
Standard
J2727_200808
The original SAE J2727 "Emission Chart" provided a rating system for comparing mobile A/C systems and was not intended to define mobile A/C system refrigerant emission. It had been developed from industry experience of expected system refrigerant emission based upon currently available technologies. The "System Emissions Chart" now contained in this revision is intended to serve as a means of estimating the annual refrigerant emissions rate (grams per year) from new production A/C systems equipped with specified component technologies. It provides emission values for various component technologies that are currently available, and can be expanded as new technologies are commercialized. This document provides the information to develop an Excel file template "System Emissions Chart" for system emission analysis. The chart includes automotive compressor technologies for conventional mobile air conditioning systems as well as those using semi-hermetic compressors.
HISTORICAL
2008-08-21
Standard
AS5420D
This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, integrally heated silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and is primarily intended for use in aircraft potable water systems with an environmental operating temperature range of -65 °F (-54 °C) to +160 °F (+71 °C).
CURRENT
2008-08-06
Standard
AS31091B
Scope unavailable.
CURRENT
2008-06-30
Standard
J2288_200806
This SAE Recommended Practice defines a standardized test method to determine the expected service life, in cycles, of electric vehicle battery modules. It is based on a set of nominal or baseline operating conditions in order to characterize the expected degradation in electrical performance as a function of life and to identify relevant failure mechanisms where possible. Accelerated aging is not included in the scope of this procedure, although the time compression resulting from continuous testing may unintentionally accelerate battery degradation unless test conditions are carefully controlled. The process used to define a test matrix of accelerated aging conditions based on failure mechanisms, and to establish statistical confidence levels for the results, is considered beyond the scope of this document. Because the intent is to use standard testing conditions whenever possible, results from the evaluation of different technologies should be comparable.
HISTORICAL
2008-06-19
Standard
J1212_200806
This document applies to off-road forestry work machines defined in SAE J1116 or ISO 6814.
CURRENT
2008-06-01
Standard
SUBDECSTDPKG
SAE has published three documents on the subject of Declarable Substances for the Aerospace Industry. This family of documents is designed to: Assist aerospace and defense industry experts in making product and process decisions to support regulatory compliance. mitigate business risks such as supply chain disruption. Pricing is for single user (without distribution to suppliers) The standard and spreadsheet package includes: AS9535 Substance Declaration Standard - provides for a consistent approach to collection of chemicals throughout the supply chain. Among other things this document provides instructions for filling out the related Substance Declaration Form as well as a representation of some parts of the Form. ARP9536 The Declarable Substances Recommended Practice - Provides a Declarable Substances Chemical List including, a glossary of chemical family identifier abbreviations, chemical family names, CAS number, and EU Index number for associated chemicals.
CURRENT
2008-03-28
Standard
ARP9536
This standard applies to the aerospace and defense industries and their supply chain.
CURRENT
2008-03-28
Standard
AS9535
This standard applies to the aerospace and defense industries and their supply chains.
HISTORICAL
2008-03-20
Standard
AS5901A
This document establishes the minimum requirements for an environmental test chamber, and test procedures to carry out anti-icing performance tests according to the current materials specification for aircraft deicing/anti-icing fluids. The primary purpose for such a test method is to determine the anti icing endurance under controlled laboratory conditions of AMS1424 Type I and AMS1428 Type II, III, and IV.
CURRENT
2008-03-05
Standard
AMS1531D
This specification covers a water-soluble cleaner containing suspended abrasive solids in the form of a ready-to-use liquid.
HISTORICAL
2008-03-04
Standard
ARP5718
This document describes: the preparatory steps to test experimental Type II, III and IV fluids according to AMS1428; the recommendations for the preparation of samples for endurance time testing according to ARP5485; a short description of recommended field spray test; the protocol to generate draft holdover time guidelines from endurance time data as obtained from ARP5485; the role of the SAE G-12 Fluids Subcommittee; the role of the SAE G-12 Holdover Time Subcommittee; the process for the publication of holdover time guidelines and list of qualified Type II, III and IV fluids. This document does not describe laboratory testing procedures. This document does not include the qualification process for AMS1424 Type I fluids.
CURRENT
2008-02-26
Standard
AMSD81956A
This specification covers a water soluble, oil dispersing nonionic detergent used for cleaning aircraft removable fuel tanks.
CURRENT
2008-01-11
Standard
J1885_200801
This test method specifies the operating procedures for a controlled irradiance, water cooled xenon-arc apparatus used for the accelerated exposure of various automotive interior trim components. Test durations, as well as any exceptions to the sample preparation and performance evaluation procedures contained in this document, are covered in material specifications of the different automotive manufacturers. This standard is limited to the models of xenon arc test apparatus specified in the Section on Equipment. All other models of xenon arc test apparatus must use SAE J2412 to perform the test conditions specified in SAE J1885. SAE J2412 is the performance standard based on the test parameters of SAE J1885. Use of xenon arc test apparatus to perform SAE J2412 must be agreed upon by contractual parties.
CURRENT
2008-01-11
Standard
J1960_200801
This test method specifies the operating procedures for a controlled irradiance, water-cooled xenon arc apparatus used for the accelerated exposure of various automotive exterior materials. This standard is limited to the models of xenon arc test apparatus specified in the Section on Apparatus. All other models of xenon arc test apparatus must use SAE J2527 to perform the test conditions specified in SAE J1960. SAE J2527 is the performance standard based on the test parameters of SAE J1960. Use of xenon arc test apparatus to perform SAE J2527 must be agreed upon by contractual parties.
CURRENT
2007-11-19
Standard
ARP496D
The scope of this Aerospace Recommended Practice (ARP) is to establish the criteria for aircraft installations which shall ensure rapid and effective use of emergency flotation equipment in the event of ditching.
CURRENT
2007-11-16
Standard
J1332_200711
This SAE Recommended Practice applies to cranes when used in lifting crane service which are equipped with rope drum rotation indicating devices.
HISTORICAL
2007-11-15
Standard
J2641_200711
This SAE Information Report provides basic information about the issues surrounding the administration of stationary, infield sound testing of snowmobiles. The information provided herein is meant to enhance safety, improve the environment and promote uniform testing.
CURRENT
2007-10-09
Standard
ARP4043B
This ARP provides the rationale and theory of charges being present on aircraft while on the ground. The necessary implementation of safety practices are explained and defined.
HISTORICAL
2007-09-26
Standard
AS5681
This SAE Aerospace Standard (AS)/Minimum Operational Performance Specification (MOPS) specifies the minimum performance requirements of Remote On-Ground Ice Detection Systems (ROGIDS). These systems are ground-based. They provide information that indicates whether frozen contamination is present on aircraft surfaces.
Viewing 241 to 270 of 712