SAE Aerospace Material Specifications

2,602 search results

  • Nickel-Copper Alloy, Corrosion Resistant, Tubing, Seamless 67Ni - 31Cu Annealed

    Standard [CURRENT] 2022-02-03

    SAE AMS 4574F:2022-02-03

    Nickel-Copper Alloy, Corrosion Resistant, Tubing, Seamless 67Ni - 31Cu Annealed

    This specification covers a corrosion-resistant nickel-copper alloy in the form of seamless tubing.

    80.30 EUR VAT included

    75.05 EUR VAT excluded

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  • Nickel-Copper Alloy Tubing, Brazed, Corrosion Resistant, 67Ni - 31Cu, Annealed

    Standard [CURRENT] 2017-02-09

    SAE AMS 4575F:2017-02-09

    Nickel-Copper Alloy Tubing, Brazed, Corrosion Resistant, 67Ni - 31Cu, Annealed

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Extrusions, Nickel-Aluminum Bronze, Martensitic 78.5Cu - 10.5Al - 5.1Ni - 4.8Fe Quenched and Tempered (TQ50)

    Standard [CURRENT] 2021-12-01

    SAE AMS 4590D:2021-12-01

    Extrusions, Nickel-Aluminum Bronze, Martensitic 78.5Cu - 10.5Al - 5.1Ni - 4.8Fe Quenched and Tempered (TQ50)

    This specification covers one type of nickel-aluminum bronze in the form of extruded bars, rods, and tubes.

    80.30 EUR VAT included

    75.05 EUR VAT excluded

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  • Copper-Nickel-Tin Alloy Plate, 77Cu - 15Ni - 8Sn, Solution Annealed and Spinodal Hardened (TX02, formerly TX00)

    Standard [CURRENT] 2025-11-13

    SAE AMS 4595A:2025-11-13

    Copper-Nickel-Tin Alloy Plate, 77Cu - 15Ni - 8Sn, Solution Annealed and Spinodal Hardened (TX02, formerly TX00)

    This specification covers a copper-nickel-tin alloy in the form of plate over 0.188 to 4.50 inches (4.77 to 114.3 mm) in nominal thickness (see 8.8).

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Copper Nickel Tin Alloy, Bars and Rods, 77Cu - 15Ni - 8Sn, Solution Annealed and Spinodal Hardened (TX02, formerly TX00)

    Standard [CURRENT] 2025-10-20

    SAE AMS 4596C:2025-10-20

    Copper Nickel Tin Alloy, Bars and Rods, 77Cu - 15Ni - 8Sn, Solution Annealed and Spinodal Hardened (TX02, formerly TX00)

    This specification covers a copper-nickel-tin alloy in the form of bars and rods up to 8.500 inches (216 mm), inclusive, in nominal thickness. When tube is ordered to AMS4596, it shall be supplied ...

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Copper-Nickel-Tin Alloy, Bars and Rods 77Cu - 15Ni - 8Sn Solution Annealed, Cold Finished and Spinodal Hardened (TX TS)

    Standard [CURRENT] 2019-04-30

    SAE AMS 4597A:2019-04-30

    Copper-Nickel-Tin Alloy, Bars and Rods 77Cu - 15Ni - 8Sn Solution Annealed, Cold Finished and Spinodal Hardened (TX TS)

    This specification covers a copper-nickel-tin alloy in the form of bars and rods.

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Copper-Nickel-Tin Alloy, Mechanical Tube 77Cu - 15Ni - 8Sn Solution Annealed and Spinodal Hardened (TX02, formerly TX00)

    Standard [CURRENT] 2022-08-05

    SAE AMS 4598B:2022-08-05

    Copper-Nickel-Tin Alloy, Mechanical Tube 77Cu - 15Ni - 8Sn Solution Annealed and Spinodal Hardened (TX02, formerly TX00)

    This specification covers a copper-nickel-tin alloy in the form of mechanical tube 1.100 to 13.6 inches (28 to 346 mm) in outer diameter (see 8.11).

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Aluminum Alloy, Sheet, and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution and Precipitation Heat Treated (2219 -T81/-T851)

    Standard [CURRENT] 2023-05-10

    SAE AMS 4599B:2023-05-10

    Aluminum Alloy, Sheet, and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution and Precipitation Heat Treated (2219 -T81/-T851)

    This specification covers an aluminum alloy in the form of sheet and plate from 0.020 to 6.000 inches (0.51 to 152.40 mm), inclusive, in thickness (see 8.5).

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Aluminum Alloy, Sheet and Plate, 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr, Solution Heat Treated, Cold Worked (8%) and Naturally Aged (2219 -T37)

    Standard [CURRENT] 2024-03-01

    SAE AMS 4600B:2024-03-01

    Aluminum Alloy, Sheet and Plate, 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr, Solution Heat Treated, Cold Worked (8%) and Naturally Aged (2219 -T37)

    This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 5.000 inches (0.51 to 127.00 mm) in nominal thickness (see 8.5).

    91.00 EUR VAT included

    85.05 EUR VAT excluded

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  • Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution Heat Treated, Cold Worked and Naturally Aged (2219 -T31/-T351)

    Standard [CURRENT] 2025-07-09

    SAE AMS 4601B:2025-07-09

    Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution Heat Treated, Cold Worked and Naturally Aged (2219 -T31/-T351)

    This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 6.000 inches (0.551 to 152.4 mm), inclusive, in thickness (see 8.6).

    91.00 EUR VAT included

    85.05 EUR VAT excluded

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