Aerospace series - Titanium Ti10V2Fe3Al - Bars - D < 110 mm - Rₘ ≥ 1 240 MPa; German and English version EN 4685:2011
Edition 2011-12

Aerospace series - Titanium TI-P99002 - Annealed - Bar for machining - a or D ≤ 150 mm - Rₘ ≥ 390 MPa; German and English version EN 3460:2019
Edition 2019-08

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rₘ ≥ 1310 MPa; German and English version EN 3160:2007
Edition 2007-11

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rₘ ≥ 930 MPa; German and English version EN 3161:2007
Edition 2007-11

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, sheet and strip a ≤ 6 mm, Rₘ ≥ 930 MPa; German and English version EN 3162:2007
Edition 2007-11

Aerospace series - Steel X6CrNiTi18-10 (1.4541) - Air melted - Softened - Wires - 0,25 mm ≤ Dₑ ≤ 3 mm - Rₘ ≤ 780 MPa; German and English version EN 2573:2022
Edition 2023-04

Aerospace series - Steel X5CrNiCu17-4 (1.4542) - Air melted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rₘ ≥ 1310 MPa; English version prEN 3677:2024
Edition 2024-08

Aerospace series - Steel X5CrNiCu17-4 (1.4542) - Air melted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rₘ ≥ 930 MPa; English version prEN 3678:2024
Edition 2024-08

Aerospace series - Steel FE-CM3801 (GX5CrNiCuNb16-4) - Homogenized, solution treated and precipitation hardened, investment casting Dₑ ≤ 50 mm, Rₘ ≥ 900 MPa; German and English version EN 4216:2007
Edition 2008-03

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rₘ ≥ 900 MPa; German and English version EN 4315:2007
Edition 2008-03