Aerospace series - Nut, anchor, self-locking, fixed, 90° corner, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C; English version prEN 3750:2024
Edition 2024-11

Aerospace series - Screw, 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C; English version prEN 4162:2024
Edition 2024-11

Aerospace series - Screw, 100° countersunk normal head, offset cruciform recess, threaded to head, in titanium alloy, anodized, with aluminium pigmented coating, metric series - Classification: 1 100 MPa (at ambient temperature)/315 °C; English version prEN 4509:2024
Edition 2024-12

Aerospace series - Screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature) / 235 °C; English version prEN 4163:2024
Edition 2025-02

Aerospace series - Nuts, self-locking, MJ threads, in heat resisting steel FE-PA2601 (A286), classification: 1100 MPa (at ambient temperature)/650 °C - Technical specification; English version prEN 3004:2024
Edition 2025-01

Aerospace series - Nuts, self-locking, MJ threads, in heat-resisting nickel base alloy NI-PH2601 (Inconel 718), MoS₂coated - Classification: 1550 MPa (at ambient temperature)/425 °C - Technical specification; English version prEN 4048:2024
Edition 2025-01

Aerospace series - Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), Classification: 1 275 MPa (at ambient temperature)/650 °C - Technical specification; English version prEN 2583:2024
Edition 2025-02

Oil and gas industries including lower carbon energy - Site-specific assessment of mobile offshore units - Part 1: Jack-ups: elevated at a site (ISO 19905-1:2023); English version EN ISO 19905-1:2023
Edition 2024-04

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

Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D ≤ 200 mm - 690 MPa ≤ R ₘ ≤ 880 MPa; German and English version EN 4262:2013
Edition 2014-01