Aerospace series - Steel FE-PM1505 (X1CrNiMoAITi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation hardened - Bar - a or D ≤ 150 mm - Rₘ ≥ 1300 MPa; German and English version EN 4468:2007
Edition 2007-10

Aerospace series - Steel X3CrNiMoAl (1.4534) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars for machining - a or D ≤ 200 mm - 1 200 MPa ≤ Rm ≤ 1 350 MPa; German and English version EN 4884:2022
Edition 2023-03

Aerospace series - Steel 36NiCrMo16 (1.6773) - 1 000 MPa ≤ Rₘ ≤ 1 200 MPa - Bars - 100 mm ≤ D ≤ 250 mm; German and English version EN 4904:2022
Edition 2023-03

Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D ≤ 200 mm - Rₘ ≥ 1310 MPa; German and English version EN 2821:2007
Edition 2007-06

Aerospace series - Steel X5CrNoMoCuNb14-5 (1.4594) - 930 MPa ≤ Rₘ ≤ 1080 MPa - Bars; German and English version EN 2502:2019
Edition 2020-02

Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Bar for machining - D ≤ 75 mm; German and English version EN 3314:2019
Edition 2019-07

Aerospace series - Steel FE-PM1503 (X3CrNiMoAl 13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D ≤ 150 mm - 1 200 MPa ≤ Rₘ ≤ 1 400 MPa; German and English version EN 3357:2019
Edition 2019-10

Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De ≤ 200 mm; German and English version EN 4376:2016
Edition 2016-08

Aerospace series; aluminium alloy AL-P7075-T73511; drawn bars 6 mm ≤ a or D ≤ 75 mm; German version EN 2128:1992
Edition 1993-12

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