Aerospace Material Specifications (AMS) Explained

AMS (Aerospace Material Specifications) outlines a set of specifications and standards that dictate the characteristics required for materials used in aerospace purposes. These guidelines are broad-ranging and encompass various materials such as metals, alloys, plastics, composite structures and coatings.

To guarantee quality, performance, and safety in aerospace materials, AMS standards exist. This includes all elements from material components and methods of preparation to examinations and certifications.

AMS specifications Details

Alloy Metals is a distributor of a variety of stainless steel, Titanium, alloy steel and nickel products for the aerospace industry. Here are some details about the materials covered by various AMS specifications and we can supply, Contact us today:

AMS 5643: This specification covers corrosion-resistant stainless steel bars, wire, forgings, and extrusions. The steel is designated as Type 316 and is used in applications that require high strength and corrosion resistance.

AMS 5662: This specification covers a high-strength, corrosion-resistant stainless steel alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 4928: This specification covers a titanium alloy known as Ti 6Al-4V, which is widely used in aerospace applications due to its high strength-to-weight ratio and excellent corrosion resistance. It is used in components such as aircraft frames, engine components, and landing gear.

AMS 5596: This specification covers a nickel-based alloy known as Inconel 625, which is used in applications that require high strength and excellent corrosion resistance. It is used in components such as aircraft engine ducting, combustion liners, and turbine shrouds.

AMS 5659: This specification covers a high-strength, corrosion-resistant stainless steel alloy known as 15-5 PH. It is used in applications that require high strength, corrosion resistance, and good toughness, such as aircraft components and landing gear.

AMS 4911: This specification covers a titanium alloy known as Ti-6Al-4V ELI, which is a variant of Ti-6Al-4V that has enhanced fracture toughness and resistance to fatigue crack growth. It is used in applications such as aircraft landing gear and structural components.

AMS 5604: This specification covers a precipitation-hardening stainless steel alloy known as 17-4 PH. It is used in applications that require high strength, corrosion resistance, and good toughness, such as aircraft components, landing gear, and structural parts.

AMS 5663: This specification covers a high-strength, corrosion-resistant nickel-based alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 5666: This specification covers a high-strength, corrosion-resistant nickel-based alloy known as Inconel 625. It is used in applications that require high strength and excellent corrosion resistance, such as aircraft engine ducting, combustion liners, and turbine shrouds.

AMS 5536: This specification covers a nickel-based alloy known as Inconel X-750. It is used in applications that require high strength and good corrosion resistance, such as aircraft engine components, gas turbines, and rocket motors.

AMS 5599: This specification covers a nickel-based alloy known as Inconel 625. It is used in applications that require high strength and excellent corrosion resistance, such as aircraft engine ducting, combustion liners, and turbine shrouds.

AMS 5629: This specification covers a precipitation-hardening stainless steel alloy known as 17-7 PH. It is used in applications that require high strength and good corrosion resistance, such as aircraft components and landing gear.

AMS 5731: This specification covers a precipitation-hardening nickel-based alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 6414: This specification covers a low-alloy steel known as 4130. It is used in applications that require high strength and good weldability, such as aircraft structural components and landing gear.

AMS 5862: This specification covers a corrosion-resistant stainless steel alloy known as 15-7 PH. It is used in applications that require high strength and good corrosion resistance, such as aircraft components and landing gear.

AMS 5528: This specification covers a corrosion-resistant nickel-based alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 5616: This specification covers a corrosion-resistant stainless steel alloy known as 440C. It is used in applications that require high strength and good corrosion resistance, such as aircraft bearings and other high-load components.

AMS 6265: This specification covers a low-alloy steel known as 9310. It is used in applications that require high strength and good fatigue resistance, such as aircraft landing gear components and other high-load parts.

AMS 5622: This specification covers a corrosion-resistant stainless steel alloy known as 15-5 PH. It is used in applications that require high strength, corrosion resistance, and good toughness, such as aircraft components and landing gear.

AMS 5653: This specification covers a low-alloy steel known as 300M. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 6260: This specification covers a low-alloy steel known as 4330M. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 6931: This specification covers a titanium alloy known as Ti-6Al-4V. It is used in applications that require high strength and good corrosion resistance, such as aircraft structural components and landing gear.

AMS 4965: This specification covers a titanium alloy known as Ti-6Al-6V-2Sn. It is used in applications that require high strength and good corrosion resistance, such as aircraft structural components and landing gear.

AMS 5664: This specification covers a nickel-based alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 5665: This specification covers a nickel-based alloy known as Inconel 625. It is used in applications that require high strength and excellent corrosion resistance, such as aircraft engine ducting, combustion liners, and turbine shrouds.

AMS 6411: This specification covers a low-alloy steel known as 4340. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 6419: This specification covers a low-alloy steel known as 4140. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 6484: This specification covers a low-alloy steel known as 300M. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 6532: This specification covers a low-alloy steel known as 8620. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 4340: This specification covers a low-alloy steel known as 4340. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 4919: This specification covers a titanium alloy known as Ti-6Al-4V ELI. It is used in applications that require high strength and good corrosion resistance, such as medical implants and surgical instruments.

AMS 4943: This specification covers a magnesium alloy known as AZ31B. It is used in applications that require good strength-to-weight ratio and good corrosion resistance, such as aerospace and automotive components.

AMS 4975: This specification covers a titanium alloy known as Ti-6Al-2Sn-4Zr-2Mo. It is used in applications that require high strength and good corrosion resistance, such as aircraft structural components and landing gear.

AMS 5529: This specification covers a corrosion-resistant nickel-based alloy known as Inconel 625. It is used in applications that require high strength and excellent corrosion resistance, such as aircraft engine ducting, combustion liners, and turbine shrouds.

AMS 5617: This specification covers a corrosion-resistant stainless steel alloy known as 416. It is used in applications that require high strength and good corrosion resistance, such as aircraft bearings and other high-load components.

AMS 5644: This specification covers a stainless steel alloy known as 17-4PH. It is used in applications that require high strength and good corrosion resistance, such as aircraft engine and structural components.

AMS 5864: This specification covers a nickel-based alloy known as Inconel 625. It is used in applications that require high strength and excellent corrosion resistance, such as aircraft engine ducting, combustion liners, and turbine shrouds.

AMS 4945: This specification covers a titanium alloy known as Ti-6Al-2Sn-4Zr-6Mo. It is used in applications that require high strength and good corrosion resistance, such as aircraft structural components and landing gear.

AMS 4976: This specification covers a titanium alloy known as Ti-6Al-2Sn-4Zr-2Mo-0.1Si. It is used in applications that require high strength and good corrosion resistance, such as aircraft structural components and landing gear.

AMS 5542: This specification covers a nickel-based alloy known as Inconel X-750. It is used in applications that require high strength and good corrosion resistance at high temperatures, such as gas turbine engines and aircraft structural components.

AMS 5667: This specification covers a nickel-based alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 6257: This specification covers a low-alloy steel known as 4130. It is used in applications that require high strength and good toughness, such as aircraft structural components and landing gear.

AMS 6409: This specification covers a low-alloy steel known as 4340. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 6417: This specification covers a low-alloy steel known as 4130. It is used in applications that require high strength and good toughness, such as aircraft structural components and landing gear.

AMS 6512: This specification covers a low-alloy steel known as 4330M. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 4201: This specification covers a copper-nickel-tin alloy known as C70600. It is used in applications that require good corrosion resistance in marine environments, such as heat exchangers and seawater piping systems.

AMS 4347: This specification covers a brazing filler metal known as silver-copper-zinc-nickel. It is used in applications that require a high-strength, high-temperature braze joint, such as aerospace and automotive components.

AMS 4930: This specification covers a titanium alloy known as Ti-6Al-4V. It is used in applications that require high strength and good corrosion resistance, such as aircraft structural components and landing gear.

AMS 5598: This specification covers a nickel-based alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 5668: This specification covers a nickel-based alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 5825: This specification covers a cobalt-based alloy known as Haynes 25. It is used in applications that require high strength and good corrosion resistance at high temperatures, such as gas turbine blades and combustion chambers.

AMS 6415: This specification covers a low-alloy steel known as 4340. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 6431: This specification covers a low-alloy steel known as 4330M. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 2303: This specification covers a low-alloy steel known as 8740. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 4015: This specification covers an aluminum alloy known as 6061-T6. It is used in applications that require good strength and good corrosion resistance, such as aircraft structural components and other high-stress parts.

AMS 4025: This specification covers an aluminum alloy known as 6061-T651. It is used in applications that require good strength and good corrosion resistance, such as aircraft structural components and other high-stress parts.

AMS 4035: This specification covers an aluminum alloy known as 2024-T3. It is used in applications that require high strength and good fatigue resistance, such as aircraft structural components and other high-stress parts.

AMS 4050: This specification covers an aluminum alloy known as 7050-T7451. It is used in applications that require high strength and good fatigue resistance, such as aircraft structural components and other high-stress parts.

AMS 4101: This specification covers a low-alloy steel known as 4340. It is used in applications that require high strength and good toughness, such as aircraft landing gear components and other high-load parts.

AMS 4914: This specification covers a titanium alloy known as Ti-6Al-4V. It is used in applications that require high strength and good corrosion resistance, such as aircraft structural components and landing gear.

AMS 4981: This specification covers a titanium alloy known as Ti-6Al-6V-2Sn. It is used in applications that require high strength and good corrosion resistance, such as aircraft structural components and landing gear.

AMS 5532: This specification covers a nickel-based alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 5597: This specification covers a nickel-based alloy known as Inconel 718. It is used in applications that require high strength and good corrosion resistance, such as jet engine components and gas turbine blades.

AMS 6345: This specification covers a low-alloy steel known as 4130. It is used in applications that require high strength and good toughness, such as aircraft structural components and landing gear.

AMS 6348: This specification covers a low-alloy steel known as 4140. It is used in applications that require high strength and good toughness, such as aircraft structural components and landing gear.

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