Browse Topic: Materials testing

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Iron and Steel Castings Engineering GuideB-ASM-05502/28/2024
This engineering guide, an accompanying guide to Aluminum Castings Engineering Guide (ASM International, 2018), explains the interactions of product design (for function and manufacturability), materials engineering (for the best choice of alloy and microstructure), and process engineering practices (to achieve the properties and integrity of a component at the most comprehensive cost).
Reference
Cadmium Plate Cyclic Corrosion Test . AIR6130A (Current)01/25/2023
14-day material test to determine the cyclic effects of runway deicing compounds on cadmium plated parts.
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Information Report
Steel, Sheet, Strip, and Plate 0.95Cr - 0.22V (0.48 - 0.53C) (SAE 6150)AMS6455M-TEST-REC (Historical)11/09/2021
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Performance Testing of PK Section V-Ribbed BeltsJ2432_202111 (Current)11/09/2021
The following information covers accessory drive belt testing methods and includes test configurations, pulley diameters, power loads, and guidance for interpreting test data. Belt construction definitions are also documented. This information has been prepared from existing literature, including standards and data supplied by producers and users of V-ribbed belts.
Belt Drive (Automotive) Systems Committee
Recommended Practice
Performance Testing of PK Section V-Ribbed BeltsJ2432_202111-TEST-REC (Historical)11/09/2021
The following information covers accessory drive belt testing methods and includes test configurations, pulley diameters, power loads, and guidance for interpreting test data. Belt construction definitions are also documented. This information has been prepared from existing literature, including standards and data supplied by producers and users of V-ribbed belts.
Belt Drive (Automotive) Systems Committee
Recommended Practice
Steel, Sheet, Strip, and Plate 0.95Cr - 0.22V (0.48 - 0.53C) (SAE 6150)AMS6455M (Current)11/09/2021
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Brake Lining Quality Test ProcedureJ661_202110 (Current)10/26/2021
The purpose of this SAE Recommended Practice is to establish a uniform laboratory procedure for securing and reporting the friction and wear characteristics of brake linings. The performance data obtained can be used for in-plant quality control by brake lining manufacturers and for the quality assessment of incoming shipments by the purchasers of brake linings.
Brake Linings Standards Committee
Recommended Practice
Steel, Sheet, Strip, and Plate 0.75Si - 0.62Cr - 0.20Mo - 0.10Zr (0.10 - 0.17C)AMS6354G-TEST-REC (Historical)09/29/2021
This specification covers a low-alloy steel in the form of sheet, strip, and plate 4.00 inches (101.6 mm) and under in thickness.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Steel, Sheet, Strip, and Plate 0.75Si - 0.62Cr - 0.20Mo - 0.10Zr (0.10 - 0.17C)AMS6354G (Current)09/29/2021
This specification covers a low-alloy steel in the form of sheet, strip, and plate 4.00 inches (101.6 mm) and under in thickness.
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 1 - General RequirementsAMS2980/1B (Current)09/23/2021
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
Material Specification
Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 0 - IntroductionAMS2980B (Current)09/23/2021
This document (Technical Specification) gives information about qualification rules and the relation between the different specification parts involved, such as Technical Specification (TS), Material Specification (MS), and Purchasing Specification (PS). The link to material qualification and qualified products is presented.
AMS CACRC Commercial Aircraft Composite Repair Committee
Material Specification
Test Method for Determining Cold Cracking of Flexible Plastic MaterialsJ323_202109 (Current)09/15/2021
This SAE Recommended Practice is applicable for determining the cold characteristics of flexible plastic materials, as applicable. It consists of three different methods for determining low-temperature properties of materials depending on type of material and end use. The method used shall be as specified by the contractual parties.
Textile and Flexible Plastics Committee
Recommended Practice
Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V 1800 °F (982 °C) Solution Heat TreatedAMS5525L-TEST-REC (Historical)09/01/2021
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate 0.0010 inch (0.025 mm) and above in nominal thickness (see 8.6).
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V 1800 °F (982 °C) Solution Heat TreatedAMS5525L (Current)09/01/2021
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate 0.0010 inch (0.025 mm) and above in nominal thickness (see 8.6).
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Foil 62Ni - 21.5Cr - 9.0Mo - 3.7Cb (Nb) Cold Rolled and AnnealedAMS5879E-TEST-REC (Historical)08/19/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.100 inch (2.54 mm) and under in nominal thickness.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Foil 62Ni - 21.5Cr - 9.0Mo - 3.7Cb (Nb) Cold Rolled and AnnealedAMS5879E (Current)08/19/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.100 inch (2.54 mm) and under in nominal thickness.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Wire, Electrical, Stranded, Uninsulated Copper, Copper Alloy, or Aluminum, or Thermocouple Extension, General Specification forAS29606B (Current)08/18/2021
This specification covers concentric lay stranded and rope-lay stranded round electrical conductor fabricated from copper, copper alloy or aluminum. This specification also covers thermocouple extension conductor fabricated from nickel/chromium or nickel/aluminum/manganese. The conductors in this specification are suitable for use in insulated wires used in aerospace and other applications.
AE-8D Wire and Cable Committee
Technical Standard
Wire, Electrical, Stranded, Uninsulated Copper, Copper Alloy, or Aluminum, or Thermocouple Extension, General Specification forAS29606B-TEST-REC (Historical)08/18/2021
This specification covers concentric lay stranded and rope-lay stranded round electrical conductor fabricated from copper, copper alloy or aluminum. This specification also covers thermocouple extension conductor fabricated from nickel/chromium or nickel/aluminum/manganese. The conductors in this specification are suitable for use in insulated wires used in aerospace and other applications.
AE-8D Wire and Cable Committee
Technical Standard
Steel, Corrosion Resistant, Sheet, Strip, and Plate 15Cr - 6.5Ni - 0.75Mo - 0.60Cb - 1.5Cu Solution Heat Treated, Precipitation HardenableAMS5863F-TEST-REC (Historical)07/23/2021
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Steel, Corrosion-Resistant, Sheet, Strip, and Plate 19Cr - 9.2Ni (SAE 30304) Solution Heat TreatedAMS5513K (Historical)07/23/2021
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Steel, Corrosion and Heat-Resistant, Sheet, Strip, Foil, and Plate 15Cr - 7.1Ni - 2.5Mo - 1.1Al Solution Heat Treated, Precipitation HardenableAMS5520H-TEST-REC (Historical)07/23/2021
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, foil, and plate 0.0015 inch (0.038 mm) and greater in nominal thickness.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Steel, Corrosion Resistant, Sheet, Strip, and Plate 15Cr - 6.5Ni - 0.75Mo - 0.60Cb - 1.5Cu Solution Heat Treated, Precipitation HardenableAMS5863F (Current)07/23/2021
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Steel, Corrosion and Heat-Resistant, Sheet, Strip, Foil, and Plate 15Cr - 7.1Ni - 2.5Mo - 1.1Al Solution Heat Treated, Precipitation HardenableAMS5520H (Current)07/23/2021
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, foil, and plate 0.0015 inch (0.038 mm) and greater in nominal thickness.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Nickel Alloy, Corrosion and Heat-Resistant, Plate 54Ni - 22Cr - 12.5Co - 9.0Mo - 1.2Al AnnealedAMS5888D-TEST-REC (Historical)07/19/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of plate nominally 2.00 inches (50.8 mm) and under in thickness, inclusive.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Nickel Alloy, Corrosion and Heat-Resistant, Plate 54Ni - 22Cr - 12.5Co - 9.0Mo - 1.2Al AnnealedAMS5888D (Current)07/19/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of plate nominally 2.00 inches (50.8 mm) and under in thickness, inclusive.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Remover, Paint Epoxy and Polyurethane Paint System Non-Chlorinated SolventAMS1377-TEST-REC (Historical)07/13/2021
This specification covers a non-phenolic, non-chromated, thickened paint remover in the form of a solvent-base liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Material Specification
Remover, Paint Epoxy and Polyurethane Paint SystemsAMS1375B (Current)07/13/2021
This specification covers an alkaline-type, thickened paint remover in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Material Specification
Remover, Paint Epoxy and Polyurethane Paint System Non-Chlorinated SolventAMS1377 (Current)07/13/2021
This specification covers a non-phenolic, non-chromated, thickened paint remover in the form of a solvent-base liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Material Specification
Steel, Corrosion-Resistant, Sheet, Strip, and Plate 17Cr (SAE 51430) AnnealedAMS5503G (Current)06/10/2021
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Recommended Practice for Determining Material Properties of Li-Battery Cathode Active MaterialsJ3021_202105-TEST-REC (Historical)05/28/2021
This SAE Recommended Practice provides a set of test methods and practices for the characterization of lithium ion battery cathode active material. It is beyond the scope of this document to establish criteria for the test results, as these are usually established between the vendor and customer. It should be noted that materials properties can vary substantially between classes of materials (e.g., LNO and LFP) and caution should be exercised when attempting to directly compare their chemical and physical properties. While these distinctions are important for the manufacturer, this document focuses on the techniques to measure the materials properties and not their absolute or relative values. Future materials such as solid-state batteries and sulfides are beyond the scope of this document. It is beyond the scope of this document to examine the rheological properties of the cathode material dispersed in a coating slurry since such properties are influenced by the conductive additive
Battery Materials Testing Committee
Recommended Practice
Recommended Practice for Determining Material Properties of Li-Battery Cathode Active MaterialsJ3021_202105 (Current)05/28/2021
This SAE Recommended Practice provides a set of test methods and practices for the characterization of lithium ion battery cathode active material. It is beyond the scope of this document to establish criteria for the test results, as these are usually established between the vendor and customer. It should be noted that materials properties can vary substantially between classes of materials (e.g., LNO and LFP) and caution should be exercised when attempting to directly compare their chemical and physical properties. While these distinctions are important for the manufacturer, this document focuses on the techniques to measure the materials properties and not their absolute or relative values. Future materials such as solid-state batteries and sulfides are beyond the scope of this document. It is beyond the scope of this document to examine the rheological properties of the cathode material dispersed in a coating slurry since such properties are influenced by the conductive additive
Battery Materials Testing Committee
Recommended Practice
Molded or Extruded Bar, Rod, and Shapes Made from Polyamide-Imide (PAI) Plastic Material Both Filled and Unfilled Grades for High-Impact Strength and Mechanical Strength Applications in High Temperature EnvironmentsAMS3670C-TEST-REC (Historical)05/19/2021
This specification and its supplementary detail specifications cover molded or extruded bar, rod, and shapes made from filled and unfilled polyamide-imide (PAI) polymer.
AMS P Polymeric Materials Committee
Material Specification
Molded or Extruded Bar, Rod, and Shapes Made from Polyamide-Imide (PAI) Plastic Material Both Filled and Unfilled Grades for High-Impact Strength and Mechanical Strength Applications in High Temperature EnvironmentsAMS3670C (Current)05/19/2021
This specification and its supplementary detail specifications cover molded or extruded bar, rod, and shapes made from filled and unfilled polyamide-imide (PAI) polymer.
AMS P Polymeric Materials Committee
Material Specification
Steel Bars, Wire, Forgings and Forging Stock, Mechanical Tubing, Rings, and Extrusions, Corrosion-Resistant 11.8Cr - 2.5Ni - 1.8Mo - 0.33V (0.08 - 0.15C) Annealed, Vacuum Arc or Electroslag RemeltedAMS5719E-TEST-REC (Historical)05/18/2021
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and extrusions 7.00 inches (177.8 mm) and under in nominal diameter or least distance between parallel sides, and stock of any size for forging, flash welded rings, or extruding (see 8.8).
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Steel Bars, Wire, Forgings and Forging Stock, Mechanical Tubing, Rings, and Extrusions, Corrosion-Resistant 11.8Cr - 2.5Ni - 1.8Mo - 0.33V (0.08 - 0.15C) Annealed, Vacuum Arc or Electroslag RemeltedAMS5719E (Current)05/18/2021
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and extrusions 7.00 inches (177.8 mm) and under in nominal diameter or least distance between parallel sides, and stock of any size for forging, flash welded rings, or extruding (see 8.8).
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Temporary Protective Coating and RemoverAMS7202-TEST-REC (Historical)05/13/2021
This specification establishes requirements for a temporary protective coating (TPC) intended to protect aluminum surfaces from damage and corrosion. This specification also establishes requirements for an alkaline remover used to strip the specified TPCs.
AMS G8 Aerospace Organic Coatings Committee
Material Specification
Temporary Protective Coating and RemoverAMS7202 (Current)05/13/2021
This specification establishes requirements for a temporary protective coating (TPC) intended to protect aluminum surfaces from damage and corrosion. This specification also establishes requirements for an alkaline remover used to strip the specified TPCs.
AMS G8 Aerospace Organic Coatings Committee
Material Specification
High-Cycle Fatigue of Polyamide-6,6 and Glass Fiber-Based Short Fiber Composite Using Finite Element Analysis2021-01-505105/11/2021
As the automotive industry strives for an increased fuel economy, lightweighting is a key factor and can be realized through composite materials. Composites have better strength-to-weight ratio as compared to metals. In this paper, static and fatigue analysis is performed on an oil pan made of polyamide-6,6 and 50% glass fiber (PA66-GF50). PA66 has a glass transition temperature of 170°C; therefore, it is suitable for automotive applications where the operating range is −40°C to 150°C. Long glass fiber (LGF) composite has an aspect ratio of 30-50 in the oil pan. Fibers break in the molding process but are still considerably longer than with conventionally compounded short glass fiber (SGF) composite, where the aspect ratio of fiber is between 10 and 20. However, the computer-aided engineering (CAE) procedure for life prediction of short glass fiber-reinforced (SGFR) plastic versus LGF-reinforced plastic is the same. CAE simulations have been performed for both static and fatigue
Singh, Sushil, Wys, Dennis
Technical Paper
Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Multiple Melted, 1800 °F (982 °C) Solution Heat Treated, Welding Grade Precipitation HardenableAMS5858E-TEST-REC (Historical)04/27/2021
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Multiple Melted, 1800 °F (982 °C) Solution Heat Treated, Welding Grade Precipitation HardenableAMS5858E (Current)04/27/2021
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 13Cr - 2.0Ni - 3.0W AnnealedAMS5508G (Current)03/16/2021
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 62Ni - 21.5Cr - 9.0Mo - 3.7Cb Solution Heat TreatedAMS5869D-TEST-REC (Historical)03/05/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate up to 1.000 inch (25.40 mm) in nominal thickness (see 8.7).
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Insulating Compound, Electrical, Embedding, Reversion Resistant SiliconeAS81550B (Current)03/05/2021
This specification covers the requirements for two types of a two-part, transparent, reversion resistant flexible insulating compound, to provide resilient, environmental, and electrical insulation of components in systems in temperature range -85 to 392 °F (-65 to 200 °C). These insulating compounds are intended for embedding, potting or encapsulation of electrical and electronic components in systems where tear resistance is not critical, but their use is not limited to such applications. These transparent compounds allow visual circuit and part identification and facilitate part replacement and repairs. The insulating compound shall cure in sections of unlimited thickness, either exposed to air or completely sealed.
AMS G9 Aerospace Sealing Committee
Technical Standard
Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 62Ni - 21.5Cr - 9.0Mo - 3.7Cb Solution Heat TreatedAMS5869D (Current)03/05/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate up to 1.000 inch (25.40 mm) in nominal thickness (see 8.7).
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Insulating Compound, Electrical, Embedding, Reversion Resistant SiliconeAS81550B-TEST-REC (Historical)03/05/2021
This specification covers the requirements for two types of a two-part, transparent, reversion resistant flexible insulating compound, to provide resilient, environmental, and electrical insulation of components in systems in temperature range -85 to 392 °F (-65 to 200 °C). These insulating compounds are intended for embedding, potting or encapsulation of electrical and electronic components in systems where tear resistance is not critical, but their use is not limited to such applications. These transparent compounds allow visual circuit and part identification and facilitate part replacement and repairs. The insulating compound shall cure in sections of unlimited thickness, either exposed to air or completely sealed.
AMS G9 Aerospace Sealing Committee
Technical Standard
Steel, Corrosion Resistant, Sheet, Strip, and Plate 9.0Mn - 20Cr - 6.5Ni - 0.28N Solution Heat TreatedAMS5595H-TEST-REC (Historical)03/01/2021
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Steel, Corrosion Resistant, Sheet, Strip, and Plate 9.0Mn - 20Cr - 6.5Ni - 0.28N Solution Heat TreatedAMS5595H (Current)03/01/2021
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Material Specification
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 0 - IntroductionAMS6885 (Current)02/23/2021
This document (Technical Specification) gives information about qualification rules and the relation between the different specification parts involved, such as the Technical Specification (TS), the Material Specification (MS), and the Purchasing Specifications (PS).
AMS CACRC Commercial Aircraft Composite Repair Committee
Material Specification
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 1 - General RequirementsAMS6885/1 (Current)02/23/2021
AMS6885/1 gives information about the technical requirements and qualification procedure for unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The repair system includes an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
AMS CACRC Commercial Aircraft Composite Repair Committee
Material Specification
Jet Reference Fluid Study for Fuel Tank SealantsAIR4275B (Current)02/03/2021
This information report covers two distinct projects to formulate Jet Refrence Fluids (JRF) for testing of material compatibility. The first effort began in 1978 and focused on producing a formulation (JRF-2) that simulated JP-4 and included composition with metallic ions that reproduced chalking of fuel tank sealants. This effort resulted in the preparation of AMS2629 that defined the formulation of JRF-2 (Type 1) and the same formulation with metallic ions (Type 2). The second effort began in 2002 and focused on preparing a JRF that simulated Jet A, JP-5 and JP-8. This effort went through multiple iterations, but eventually resulted in a JRF-3 formulation composed of Jet A plus military additives spiked to 25% aromatic content and high levels of sulfur experienced in the global fuel supply. Since the metallic ions added to JRF-2 demonstrated their ability to simulate a chalking reaction, chalking was not tested with the ions added to JRF-3. AMS2629 was changed multiple times to
AMS G9 Aerospace Sealing Committee
Information Report
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