SAE Aerospace Material Specifications

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  • Titanium Alloy Bars, Forgings, and Forging Stock 4Al - 2.5V - 1.5 Fe Single Hearth Melted, Annealed

    Standard [CURRENT] 2022-10-26

    SAE AMS 6950A:2022-10-26

    Titanium Alloy Bars, Forgings, and Forging Stock 4Al - 2.5V - 1.5 Fe Single Hearth Melted, Annealed

    This specification covers a titanium alloy in the form of bars and forgings 14.000 inches (355.60 mm) and under in nominal diameter or least distance between parallel sides and stock for forging ...

    92.10 EUR VAT included

    86.07 EUR VAT excluded

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  • Titanium Alloy, Sheet 5Al - 4V - 0.75Mo - 0.5Fe Annealed

    Standard [CURRENT] 2022-05-16

    SAE AMS 6951A:2022-05-16

    Titanium Alloy, Sheet 5Al - 4V - 0.75Mo - 0.5Fe Annealed

    This specification covers a titanium alloy in the form of sheet 0.025 through 0.100 inch (0.63 through 2.54 mm), inclusive, in thickness (see 8.7).

    86.30 EUR VAT included

    80.65 EUR VAT excluded

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  • Titanium Alloy, Forgings 5.8Al - 4.0Sn - 3.5Zr - 2.8Mo - 0.7Nb - 0.35Si - 0.06C Solution and Precipitation Heat Treated

    Standard [CURRENT] 2023-09-07

    SAE AMS 6952A:2023-09-07

    Titanium Alloy, Forgings 5.8Al - 4.0Sn - 3.5Zr - 2.8Mo - 0.7Nb - 0.35Si - 0.06C Solution and Precipitation Heat Treated

    This specification covers a titanium alloy in the form of forgings 4.400 inches (111.76 mm) and under in nominal diameter or least distance between parallel sides and a maximum cross-sectional ...

    86.30 EUR VAT included

    80.65 EUR VAT excluded

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  • Titanium Alloy Sheet, 6Al - 4Sn - 3Nb - 0.5Mo - 0.3Si, Duplex Annealed

    Standard [CURRENT] 2022-05-24

    SAE AMS 6953A:2022-05-24

    Titanium Alloy Sheet, 6Al - 4Sn - 3Nb - 0.5Mo - 0.3Si, Duplex Annealed

    This specification covers a titanium alloy in the form of sheet 0.020 to 0.1874 inch (0.51 to 4.760 mm), inclusive, in nominal thickness. (see 8.7)

    92.10 EUR VAT included

    86.07 EUR VAT excluded

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  • Laser-Powder Bed Fusion (L-PBF) Produced Parts, Nickel Alloy, Corrosion- and Heat-Resistant, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb Stress Relieved, Hot Isostatic Pressed and Solution Annealed

    Standard [CURRENT] 2022-05-16

    SAE AMS 7000A:2022-05-16

    Laser-Powder Bed Fusion (L-PBF) Produced Parts, Nickel Alloy, Corrosion- and Heat-Resistant, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb Stress Relieved, Hot Isostatic Pressed and Solution Annealed

    This specification covers a corrosion and heat-resistant nickel alloy in the form of parts produced by laser-powder bed fusion (L-PBF) that are subjected to post-deposition stress relief (SR), hot ...

    92.10 EUR VAT included

    86.07 EUR VAT excluded

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  • Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb

    Standard [CURRENT] 2018-06-08

    SAE AMS 7001:2018-06-08

    Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb

    This specification covers a corrosion and heat-resistant nickel alloy in the form of pre-alloyed powder.

    86.30 EUR VAT included

    80.65 EUR VAT excluded

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  • Process Requirements for Production of Metal Powder Feedstock for Use in Additive Manufacturing of Aerospace Parts

    Standard [CURRENT] 2022-05-16

    SAE AMS 7002A:2022-05-16

    Process Requirements for Production of Metal Powder Feedstock for Use in Additive Manufacturing of Aerospace Parts

    This specification is to prescribe process requirements for production (from raw materials through preparation for shipment, see 8.6) of metal powder feedstock for use in additive manufacturing of ...

    138.80 EUR VAT included

    129.72 EUR VAT excluded

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  • Laser Powder Bed Fusion Process

    Standard [CURRENT] 2022-08-05

    SAE AMS 7003A:2022-08-05

    Laser Powder Bed Fusion Process

    This specification establishes process controls for the repeatable production of aerospace parts by Laser Powder Bed Fusion (L-PBF). It is intended to be used for aerospace parts manufactured ...

    120.10 EUR VAT included

    112.24 EUR VAT excluded

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  • Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate, Ti-6Al-4V, Stress Relieved

    Standard [CURRENT] 2019-01-31

    SAE AMS 7004:2019-01-31

    Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate, Ti-6Al-4V, Stress Relieved

    This specification covers preforms fabricated up through 5.5 inches (140 mm) inclusive in deposition width thickness (see 8.2.5) using a Plasma Arc Directed Energy Deposition (PA-DED) additive ...

    101.50 EUR VAT included

    94.86 EUR VAT excluded

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  • Wire Fed Plasma Arc Directed Energy Deposition Additive Manufacturing Process

    Standard [CURRENT] 2019-01-31

    SAE AMS 7005:2019-01-31

    Wire Fed Plasma Arc Directed Energy Deposition Additive Manufacturing Process

    This specification establishes process controls for the repeatable production of preforms by Wire Fed Plasma Arc Directed Energy Deposition (PA-DED). It is intended to be used for aerospace parts ...

    114.30 EUR VAT included

    106.82 EUR VAT excluded

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