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The technical architecture defined in this document outlines mandatory, emerging, and needed standards to provide interoperability at key interfaces in the aircraft/store system (including an associated NATO Network Enabled Capability environment), as required to support a future plug-and-play aircraft/store integration capability. These standards relate to services and protocols associated with the subject interfaces. Modeling standards to facilitate the Model Driven Architecture® (MDA®) approach to system definition and implementation are also included. Note that the status of referenced standards as reflected in this document is as of August 2007, and document users should check to see if there has been a subsequent change of status relative to applicable standards
AS-1B Aircraft Store Integration Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading procured in SI (metric) units. AMS 5706 is the inch/pound version of this MAM. These products have been used typically for parts, such as fasteners, flanges, and rings, requiring high strength up to 815 degrees C and oxidation resistance up to 955 degrees C, particularly those parts which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units. AMS 5536 is the inch/pound version of this MAM. These products have been used typically for parts requiring oxidation resistance up to 1205 degrees C and relatively high strength up to 815 degrees C, but usage is not limited to such applications
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and foil up to 0.38 millimeters in nominal thickness procured in SI (Metric) units. AMS 5914 is the inch/pound version of this MAM. These products have been used typically for the fabrication of bellows, diaphragms, and other components requiring a combination of high strength, resistance to heat and corrosion, leak tightness, and maximum fatigue life, but usage is not limited to such applications
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder and procured in metric units. AMS 4778 is the inch/pound version of this MAM. This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications. Also may be used as a corrosion and oxidation resistant hard coating
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant, vacuum melted, nickel alloy in the form of investment castings. AMS 5401 is the inch/pound version of this MAM. These castings have been used typically for structural parts requiring moderate strength up to 870 degrees C and oxidation and corrosion resistance up to 980 degrees C, but usage is not limited to such applications
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers established metric manufacturing tolerances applicable to low-alloy steel sheet, strip, and plate ordered to metric dimensions. These tolerances apply to all conditions unless otherwise noted. The term 'excl' is used to apply only to the higher figure of the specified range
AMS E Carbon and Low Alloy Steels Committee
This specification covers established metric manufacturing tolerances applicable to aluminum alloy and magnesium alloy extruded bar, rod, wire, shapes, and tubing ordered to metric dimensions. Tolerances greater than standard may be necessary for some shapes; tolerances closer than standard may be possible for others. Tolerances shown herein, however, apply unless otherwise agreed upon by purchaser and vendor and apply to all tempers, unless otherwise noted
AMS D Nonferrous Alloys Committee
This specification covers established metric manufacturing tolerances applicable to aluminum alloy standard structural shapes ordered to metric dimensions. Standard structural shapes are shapes in certain standard alloys, tempers, sizes, and sections such as angles, channels, Tees, Zees, I-Beams, and H-Beams commonly used for structural purposes. These tolerances apply to all conditions, unless otherwise noted. This specification has been declared 'NONCURRENT' by the Aerospace Materials Division, SAE, as of September 1994. It is recommended, therefore, that this specification not be specified for new designs
AMS D Nonferrous Alloys Committee
The scope of this SAE Standard is the definition of the functional, environmental, and life cycle test requirements for electrically operated backup alarm devices primarily intended for use on off-road, self-propelled work machines as defined by SAE J1116 (limited to categories of (1) construction, and (2) general purpose industrial
OPTC3, Lighting and Sound Committee
SAE J3072 establishes requirements for a grid support inverter system function that is integrated into a plug-in electric vehicle (PEV), which connects in parallel with an electric power system (EPS) by way of conductively coupled, electric vehicle supply equipment (EVSE). This standard also defines the communication between the PEV and the EVSE required for the PEV onboard inverter function to be configured and authorized by the EVSE for discharging at a site. The requirements herein are intended to be used in conjunction with IEEE 1547-2018 and IEEE 1547.1-2020 or later versions
Hybrid - EV Committee
A technical committee shall be responsible for a field of endeavor, as defined by its scope. In cases where projects overlap areas of interest of another council’s committee, the originating committee shall submit the project(s) for review and approval to the other concerned committee and its council prior to issuance. A committee is established when a new major project area is to be undertaken and no existing committee is available. A committee is discharged when the assigned work is completed and there is no further need for its services. The councils retain responsibility for periodic review of technical reports developed by their disbanded committees
Executive Standards Committee
This SAE Standard describes a method for measuring the weighted sound pressure levels at prescribed microphone positions in the proximity of a device or machine for outdoor use, in order to determine compliance with noise limits. The A-weighted sound power level of the source is calculated from the measured values
SLTC - Earth Moving Machinery Sound Level
This SAE Standard describes a method for determining the noise emitted by earthmoving machinery at the operator's position in terms of the equivalent continuous A-weighted sound pressure level while the machine is in a stationary test condition. This SAE Standard is a special test code for specific types of earthmoving machinery. It is an extension of ISO 6081 which contains the general requirements for many types of machinery and equipment. Specific requirements are provided in this special test code to enable the sound pressure level at the operator's position, with the machine in a stationary test condition, to be determined in a manner which is repeatable. Attachments (bucket, dozer, etc.) for the manufacturer's production version shall be fitted since this is the configuration most likely to exist when the machine is in actual use. This document will enable compliance with noise limits to be determined. It can also be used for evaluation purposes in noice reduction investigations
SLTC - Earth Moving Machinery Sound Level
AMS2980/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures
AMS CACRC Commercial Aircraft Composite Repair Committee
This specification covers a melt-processible, copolymer resin of ethylene and tetrafluoroethylene (ETFE) in the form of extruded rods, tubes, and shapes
AMS P Polymeric Materials Committee
This specification covers procedures for marking bare wire for welding to provide positive identification of cut lengths, regardless of length, and of spools, and to ensure that the wire is clean and free from foreign materials and corrosion
AMS B Finishes Processes and Fluids Committee
This specification covers two types of semi-processed silicon steel in the form of sheet and strip supplied in coils or cut lengths
AMS E Carbon and Low Alloy Steels Committee
This SAE Recommended Practice applies to a production dynamometer test procedure which can be used to measure the smoke and gaseous emission characteristics of vehicular diesel engines. This procedure describes the smoke emission test method, smoke test cycle, gaseous emission test method, steady-state gaseous emission test cycle, equipment, instrumentation, calibration, data analysis, and correlation of results for comparison of production engine emission performance to the requirements of current or past Federal regulations. Variations in engines, instrumentation, and test equipment may require modifications to these procedures or data reduction methods. The acceptability of this procedure is dependent upon documented statistical data appropriate to correlate all tests, data reduction techniques, and special instrumentation to the required Federal tests. When using the audit test procedure to assess the emissions performance of production engines, considerations should be given to
SAE IC Powertrain Steering Committee
This specification covers a low-modulus aramid in the form of tape
AMS P Polymeric Materials Committee
This specification covers cored and uncored open cell latex foam rubber sheets, molded and hand- built shapes having good shock-absorbing, vibration-damping, and comfort cushioning characteristics (see 6.1
AMS P Polymeric Materials Committee
This specification covers a magnesium alloy in the form of permanent mold castings
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet and plate
AMS D Nonferrous Alloys Committee
This specification covers a magnesium alloy in the form of permanent mold castings
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat-resistant nickel-iron alloy in the form of welding wire
AMS F Corrosion and Heat Resistant Alloys Committee
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996
AMS P Polymeric Materials Committee
This specification covers the requirements for silver deposited on metal parts with a copper strike between the basis metal and the silver deposit
AMS B Finishes Processes and Fluids Committee
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 AMS3100/2A. 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
AMS G9 Aerospace Sealing Committee
This specification covers a magnesium alloy in the form of sheet and plate
AMS D Nonferrous Alloys Committee
This specification covers a magnesium alloy in the form of sheet and plate
AMS D Nonferrous Alloys Committee
This specification covers balls made of a low-chromium, high-carbon steel
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aluminum alloy procured in the form of extruded bars, rods, and profiles (shapes) with nominal thickness up to 3.000 inch (76.20 mm), inclusive, and having a cross-sectional area of 26.3 square inches (170 cm2) maximum and circle size of 15.3 inches (389 mm) maximum (see 8.7
AMS D Nonferrous Alloys Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock
AMS E Carbon and Low Alloy Steels Committee
This specification covers a titanium alloy in the form of sheet, strip, and plate up to 1.000 inch (25.40 mm) inclusive
AMS G Titanium and Refractory Metals Committee
This specification covers four classes of tungsten heavy metal in the form of sintered and annealed shapes
AMS G Titanium and Refractory Metals Committee
Primarily for preservation, during extended periods of shipment and/or storage, of miscellaneous metal parts, tools, subassemblies, and equipment where the compound is readily accessible for removal and removal does not damage the parts
AMS B Finishes Processes and Fluids Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
AMS P Polymeric Materials Committee
This specification covers a biodegradable, formaldehyde-base material, containing additives, in the form of a concentrated liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
AMS P Polymeric Materials Committee
This specification establishes requirements for aerosol packaging
AMS B Finishes Processes and Fluids Committee
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996
AMS P Polymeric Materials Committee
AMS P Polymeric Materials Committee
This specification covers the engineering requirements for selective (brush) electrodeposition of nickel and the properties of the deposit. This process has been used typically to provide good wear resistance and dimensional build-up and restoration of parts which may operate in service up to 450 degrees F (232 degrees C), where low tensile stress in the deposit is required, but usage is not limited to such applications. Diffusion heat treatment of the deposit is not required
AMS B Finishes Processes and Fluids Committee
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