SAE Aerospace Material Specifications

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  • Aluminum Alloy, Plate (7065-T7451), 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr, Solution Heat Treated, Stress-Relieved, and Overaged

    Standard [CURRENT] 2024-12-10

    SAE AMS 4361B:2024-12-10

    Aluminum Alloy, Plate (7065-T7451), 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr, Solution Heat Treated, Stress-Relieved, and Overaged

    This specification covers an aluminum alloy in the form of plate.

    96.30 EUR VAT included

    90.00 EUR VAT excluded

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  • Forgings, Magnesium Alloy, 5.5Zn - 0.45Zr (ZK60A-T5), Precipitation Heat Treated

    Standard [CURRENT] 2019-12-16

    SAE AMS 4362H:2019-12-16

    Forgings, Magnesium Alloy, 5.5Zn - 0.45Zr (ZK60A-T5), Precipitation Heat Treated

    This specification covers a magnesium alloy in the form of die forgings 3 inches (76 mm) and under in nominal thickness at time of heat treatment, hand forgings 6 inches (152 mm) and under in ...

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Aluminum Alloy, Plate, 7.9Zn - 1.8Cu - 2.0Mg - 0.10Zr (7099-T7651) Solution Heat Treated, Stress Relieved, and Overaged

    Standard [CURRENT] 2021-09-15

    SAE AMS 4364A:2021-09-15

    Aluminum Alloy, Plate, 7.9Zn - 1.8Cu - 2.0Mg - 0.10Zr (7099-T7651) Solution Heat Treated, Stress Relieved, and Overaged

    This specification covers an aluminum alloy in the form of plate from 1.000 to 6.000 inches (25.40 to 152.40 mm) in thickness (see 8.6).

    91.00 EUR VAT included

    85.05 EUR VAT excluded

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  • Aluminum Alloy, Plate 7.9Zn - 1.2Cu - 2.1Mg - 0.10Zr (7097-T7651) Solution Heat Treated, Stress Relieved, and Overaged

    Standard [CURRENT] 2022-12-16

    SAE AMS 4365A:2022-12-16

    Aluminum Alloy, Plate 7.9Zn - 1.2Cu - 2.1Mg - 0.10Zr (7097-T7651) Solution Heat Treated, Stress Relieved, and Overaged

    This specification covers an aluminum alloy in the form of plate from 3.000 to 8.000 inches (76.20 to 203.20 mm) in thickness (see 8.5).

    91.00 EUR VAT included

    85.05 EUR VAT excluded

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  • Aluminum Alloy, Extruded Profiles (2065-T84), 4.2Cu - 1.2Li - 0.52Mg - 0.32Mn - 0.32Ag - 0.1Zr, Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged

    Standard [CURRENT] 2026-04-21

    SAE AMS 4366B:2026-04-21

    Aluminum Alloy, Extruded Profiles (2065-T84), 4.2Cu - 1.2Li - 0.52Mg - 0.32Mn - 0.32Ag - 0.1Zr, Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged

    This specification covers an aluminum-lithium alloy in the form of extruded profiles with a maximum cross-sectional area of 19 square inches (123 cm2) and a maximum circle size of 11 inches (279 ...

    80.30 EUR VAT included

    75.05 EUR VAT excluded

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  • Aluminum Alloy, Extruded Profiles, 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T74511), Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

    Standard [CURRENT] 2022-11-02

    SAE AMS 4367A:2022-11-02

    Aluminum Alloy, Extruded Profiles, 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T74511), Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

    This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) 0.040 to 4.500 inches (1.02 to 114.30 mm), inclusive, in thickness produced with maximum cross ...

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Aluminum Alloy, Discontinuously Reinforced Hot Isostatically Pressed Shapes 6061B/SiC/40p (3 μm) (T1P)

    Standard [CURRENT] 2023-03-08

    SAE AMS 4368A:2023-03-08

    Aluminum Alloy, Discontinuously Reinforced Hot Isostatically Pressed Shapes 6061B/SiC/40p (3 μm) (T1P)

    This specification covers discontinuously reinforced aluminum alloy (DRA) metal matrix composites (MMC) made by mechanical alloying of 6061B aluminum powder and SiC particulate, which is then ...

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Aluminum Alloy, Discontinuously Reinforced Extruded Bar, Rod, Wire and Shapes, (2124A/SiC/25p (0.7 µm) (T1P)

    Standard [CURRENT] 2024-10-28

    SAE AMS 4369A:2024-10-28

    Aluminum Alloy, Discontinuously Reinforced Extruded Bar, Rod, Wire and Shapes, (2124A/SiC/25p (0.7 µm) (T1P)

    This specification covers a discontinuously reinforced aluminum alloy (DRA) made by mechanical alloying 2124A aluminum powder and silicon carbide particulate (SiC). It is produced in the form of ...

    80.30 EUR VAT included

    75.05 EUR VAT excluded

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  • Magnesium Alloy, Plate 4.0Y - 2.25Nd - 0.5Zr (WE43C - T5) Precipitation Heat Treated

    Standard [CURRENT] 2023-12-13

    SAE AMS 4371C:2023-12-13

    Magnesium Alloy, Plate 4.0Y - 2.25Nd - 0.5Zr (WE43C - T5) Precipitation Heat Treated

    This specification covers a magnesium alloy in the form of rolled plate from 0.500 up to 6.0 inches (12.7 to 152.4 mm), inclusive (see 8.5).

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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  • Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T34) Solution Heat Treated and Stress Relieved

    Standard [CURRENT] 2022-08-05

    SAE AMS 4372B:2022-08-05

    Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T34) Solution Heat Treated and Stress Relieved

    This specification covers an aluminum-lithium alloy in the form of plate 0.500 to 6.500 inches (12.70 to 165.00 mm) in nominal thickness (see 8.6).

    84.50 EUR VAT included

    78.97 EUR VAT excluded

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