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The CDIF Family of Standards is primarily designed to be used as a description of a mechanism for transferring information between CASE tools. It facilitates a successful transfer when the authors of the importing and exporting tools have nothing in common except an agreement to conform to CDIF. The language that is defined for the Transfer Format also has applicability as a general language for Import/Export from repositories. The CDIF Integrated Meta-model defined for CASE also has applicability as the basis of standard definitions for use in repositories. The standards which form the complete family of CDIF Standards are documented in EIA/IS-106 CDIF - CASE Data Interchange Format - Overview. These standards cover the overall framework, the transfer format and the CDIF Integrated Meta-model. The diagram in Figure 1 depicts the various standards that comprise the CDIF Family of Standards. The shaded box depicts this Standard and its position in the CDIF Family of Standards. This
Systems Management Council
This specification covers a butyl (IIR) rubber in the form of sheet, strip, extrusions, and molded shapes
AMS CE Elastomers Committee
This is the Microsoft Word® version of AS9101C, which defines the content and the presentation of the Assessment Report for the AS9100 standard. AS9101CW is an historical document; a newer version, AS9101DW, exists
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
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 Aerospace Standard establishes the diameter-pitch combinations of ISO metric 60° screw threads recommended for use in the aerospace industry for metric module bolts and nuts
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips, and a viscous mixture (paste) of powder in a suitable binder
AMS D Nonferrous Alloys Committee
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips, and a viscous mixture (paste) of powder in a suitable binder
AMS D Nonferrous Alloys Committee
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips and a viscous mixture (paste) of powder in a suitable binder
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate
AMS F Corrosion and Heat Resistant Alloys Committee
This specification details requirements and procedures for the detection of defects in aircraft structural and engine components during maintenance and overhaul operations
AMS K Non Destructive Methods and Processes Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles (shapes), and tubing 0.040 to 4.000 inches (1.00 to 100.00 mm) in nominal diameter, least dimension, or wall thickness (see 8.7
AMS D Nonferrous Alloys Committee
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips and a viscous mixture (paste) of powder in a suitable binder
AMS D Nonferrous Alloys Committee
This specification covers a corrosion and heat-resistant cobalt alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a melt-processible, copolymer resin of ethylene and tetrafluoroethylene (ETFE) in the form of molded sheet
AMS P Polymeric Materials Committee
This specification covers an aluminum alloy in the form of permanent mold castings
AMS D Nonferrous Alloys Committee
This specification has been declared "CANCELLED " by the Aerospace materials Division, SAE, as of April 2009, and has been superseded by AMS3138D. The requirements of the latest issue of AMS3138D shall be fulfilled whenever reference is made to the cancelled AMS3138/1B. 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 AMS3138D. Cancelled specifications are available from SAE
AMS G8 Aerospace Organic Coatings Committee
This specification presents requirements for the heat treatment of parts and components fabricated from wrought (plate, sheet, strip, bar, rod, wire extrusions and tube and forgings) copper alloys, numbers C17000, C17200, C17300, C17500, and C17510 (see 6.7). This specification also covers “bright hardening
AMS D Nonferrous Alloys Committee
This specification has been declared "CANCELLED " by the Aerospace materials Division, SAE, as of April 2009, and has been superseded by AMS3138D. The requirements of the latest issue of AMS3138D shall be fulfilled whenever reference is made to the cancelled AMS3138/1B. 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 AMS3138D. Cancelled specifications are available from SAE
AMS G8 Aerospace Organic Coatings Committee
This specification covers one width and one strength of integral locking slot nylon webbing
AMS P Polymeric Materials Committee
This specification covers one width and one strength of integral locking slot nylon webbing
AMS P Polymeric Materials Committee
This specification covers a coating consisting of tungsten disulfide without binders and not requiring a curing process
AMS B Finishes Processes and Fluids Committee
This specification covers a nitrile rubber (NBR) in the form of molded compression seals such as O-rings, T-seals, and molded-in-place gaskets for aeronautical and aerospace applications. For sheet, strip, tubing, extrusions, and molded shapes, use the AMS3786 specification, which is intended for that use
AMS CE Elastomers Committee
This specification covers a corrosion resistant steel in the form of bars, wire, forgings, flash welded rings, and extrusions in the solution heat treated condition (see 8.3), 12 inches (305 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides, and having a maximum cross-sectional area of 144 in2 (930 cm2), and stock of any size for forging, flash welded rings, or extruding
AMS F Corrosion and Heat Resistant Alloys Committee
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements and procedures for three classes of gas, vacuum, liquid, and low pressure (LPC) carburizing and related heat treatment of parts fabricated from carburizing grade steels. Parts made from steels other than those specified in the detail specifications may be heat treated in accordance with the applicable requirements using processing temperatures, times, and other parameters recommended by the material producer unless otherwise specified by the purchaser. This specification does not cover pack carburizing
AMS B Finishes Processes and Fluids Committee
This specification covers high temperature, compression set, and fluid resistant fluorocarbon (FKM) elastomer in the form of molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications
AMS CE Elastomers Committee
This specification covers a corrosion and heat resistant steel in the form of forgings and forging stock
AMS F Corrosion and Heat Resistant Alloys Committee
This Aeronautical Standard covers terms frequently applied to aircraft gas turbine engines and their operation but does not include names of particular parts, the latter being covered by AS 341, Drawing Title Rules and Nomenclature for Aircraft Engine Parts
AGE-4 Packaging, Handling and Transportability Committee
These products have been used typically for electrodeposited nickel plating on steel, copper and copper alloys, and zinc and zinc alloys, but usage is not limited to such applications
AMS B Finishes Processes and Fluids Committee
This specification covers the engineering requirements for electrodeposition of AMS 3109 epoxy primer on aluminum alloy surfaces and the properties of the deposit
AMS P Polymeric Materials Committee
This specification covers a premium grade titanium alloy in the form of investment castings
AMS G Titanium and Refractory Metals Committee
This specification covers the requirements of inhibited 1,1,1 trichloroethane for vapor degreasing
AMS B Finishes Processes and Fluids Committee
This specification covers a methyl or methyl vinyl silicone rubber material that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded in place gaskets for aeronautical and aerospace applications, use the AMS7000 series specification
AMS CE Elastomers Committee
This specification covers a leaded red brass alloy in the form of sand and centrifugal castings
AMS D Nonferrous Alloys Committee
This PS, AMS2980/4, specifies the batch release and delivery requirements for epoxy resin systems (base resin and curing agent) used for wet lay-up repair purposes
AMS CACRC Commercial Aircraft Composite Repair Committee
This specification covers one weight and strength of para-aramid thread
AMS P Polymeric Materials Committee
This specification has been designated as "SUPERSEDED" by the Aerospace Materials Division, SAE, as of May 17, 1993. The requirements of this specification are embodied in the latest issue of AMS 1431
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers two styles of glass cloth impregnated with a polyester resin system, the resin being processed to a “B” stage condition. Either style of glass may be used
AMS P17 Polymer Matrix Composites Committee
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 5532, ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT (30Fe 21Cr 20Ni 20Co 3.0Mo 2.5W - 1.0(Cb+Ta) 0.15N). The requirements of the latest issue of AMS 5532 shall be fulfilled whenever reference is made to this specification
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a barrier coating in the form of a ready-to-be applied liquid with a consistency suitable for brush, spray, or dip application to exterior surfaces of aircraft
AMS G8 Aerospace Organic Coatings Committee
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of March, 1991
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a low-alloy steel in the form of investment castings
AMS E Carbon and Low Alloy Steels Committee
This specification covers the specific requirements for aluminum alloy 7178-T76 bar, rod, shapes, and wire produced by extrusion
AMS D Nonferrous Alloys Committee
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