ICS 49.025.10
Steels
Standards in This Category
LVS EN 2446:2009
Aerospace series - Steel FE-PL1503 (35CrMo4) - 1100 MPa ≤ Rm ≤ 1300 MPa - Bars - De ≤ 25 mm
This technical specification establishes the requirements for seamless steel bars within the aerospace materials portfolio, specifically addressing grades such as 35CrMo4. The document defines
LVS EN 2467:2024
Aerospace series - Steel X2CrNi18-9 (1.4307) - Air melted - Softened - Plates, sheets and strips - 0,4 mm ≤ a ≤ 20 mm - 520 MPa ≤ Rm ≤ 670 MPa
This technical document establishes comprehensive specifications for steel grades designated as X2CrNi18-9, produced via electric furnace melting and delivered in the annealed condition. The material
LVS EN 2466:2009
Aerospace series - Steel FE-PA3901 (X2CrNi19-11) - Softened - Forgings - De ≤ 100 mm
This document outlines technical specifications for a specific grade of stainless steel used in aerospace applications. The material, identified by its chemical composition of 18% chromium and 8%
LVS EN 2448:2009
Aerospace series - Steel FE-PL1503 (35CrMo4) - 900 MPa <kleiner => R<(Index)m> <kleiner => 1100 MPa - Bars - D<(Index)e> <kleiner => 40 mm
This technical specification establishes comprehensive requirements for the mechanical properties of round steel bars intended for aerospace applications. The document focuses on a specific grade of
LVS EN 2470:2019
Aerospace series - Steel FE-PA11 - Softened and cold drawn - Wires for rivets - 1 mm ≤ D ≤ 10 mm
This technical document outlines specific requirements for stainless steel wire intended for the manufacturing of rivets used in aerospace applications. The material covered is identified as steel
LVS EN 2502:2020
Aerospace series - Steel X5CrNoMoCuNb14-5 (1.4594) - 930 MPa ≤ Rm ≤ 1 080 MPa - Bars - De ≤ 150 mm
This document establishes specific technical requirements for a particular grade of stainless steel, identified by the chemical designation X5CrNoMoCuNb14-5 and material number 1.4594. It focuses
LVS EN 2482:2011
Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤Rm ≤1 300 MPa - Bars - De ≤100 mm
This technical specification addresses a specific category of high-strength alloy steel bars utilized within the aerospace industry, focusing on material grade 35NiCrMo16. The document establishes
LVS EN 2475:2018
Aerospace series - Steel 30CrNiMo8 (1.6580) - Air melted - Hardened and tempered - Bar for machining - De ≤ 100 mm - 1 100 MPa ≤ Rm ≤ 1 300 MPa
This document establishes technical specifications for a specialized grade of aerospace-grade steel designated as 30CrNiMo8, corresponding to material number 1.6580. The standard applies specifically
LVS EN 2483:2011
Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤Rm ≤1 300 MPa - Forgings - De ≤ 100 mm
This specification defines the technical requirements for a specific grade of steel designed for aeronautical and aerospace applications. The material in question, identified by the designation
LVS EN 2480:2026
Aerospace series - Steel 36NiCrMo16 (1.6773) - 1 250 MPa ≤ Rm ≤ 1 400 MPa - Bars - De ≤ 75 mm
This document establishes technical specifications for a specific grade of alloy steel designated as 36NiCrMo16, corresponding to material number 1.6773, intended for aerospace applications. The
LVS EN 2476:2020
Aerospace series - Steel 30CrNiMo8 (1.6580) - 1 100 MPa ≤ Rm ≤ 1 300 MPa - Forgings - De ≤ 100 mm
This standard specifies technical requirements for forged components manufactured from 30CrNiMo8 steel within the aerospace sector. The material is defined by a specific tensile strength range
LVS EN 2478:2008
Aerospace series - Steel FE-PL2107 (30NiCrMo16) - 1220 Mpa ≤ Rm ≤ 1370 Mpa- Bars - De ≤ 40 mm
This document outlines the technical specifications for a high-strength alloy steel bar designated as FE-PL2107, corresponding to the material grade 30NiCrMo16. Developed within the framework of
LVS EN 2481:2011
Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 250 MPa ≤ Rm ≤ 1 400 MPa - Forgings - De ≤ 75 mm
This specification outlines the technical requirements for a specific high-strength steel grade utilized extensively in aviation and aerospace sectors. The document defines the material properties
LVS EN 2503:2020
Aerospace series - Steel X5CrNoMoCuNb14-5 (1.4594) - 930 MPa ≤ Rm ≤ 1 080 MPa - Forgings - De ≤ 150 mm
This document specifies the technical requirements for forged components made from a particular stainless steel alloy, designated as X5CrNoMoCuNb14-5 (1.4594). The standard applies to products with
LVS EN 2573:2023
Aerospace series - Steel X6CrNiTi18-10 (1.4541) - Air melted - Softened - Wires - 0,25 mm ≤ De ≤ 3 mm - Rm ≤ 780 MPa
This document establishes specific technical requirements for vacuum-melted stainless steel wires designated as X6CrNiTi18-10, identified by the numerical designation 1.4541. Designed within the
LVS EN 2542:2009
Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Bar and wire - D<(Index)e> <kleiner => 40 mm - For prevailing torque nuts
This document establishes technical specifications for a specific steel grade designated as 25CrMo4 in its annealed condition. It covers the production and requirements for both bar and wire forms,
LVS EN 2543:2009
Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Sheet and strip - 0,3 mm ≤ a ≤ 2 mm - For prevailing torque nuts
This technical specification addresses the requirements for sheet and strip products manufactured from FE-PL1502 steel, also known as 25CrMo4, in the annealed condition. The document covers material
LVS EN 2540:2018
Aerospace series - Steel X7CrNiAl17-7 (1.4568) - Air melted - Solution treated and precipitation hardened - Sheet and strip - a ≤ 6 mm - 1 240 MPa ≤ Rm ≤ 1 450 MPa
This technical specification defines the requirements for flat products made from X7CrNiAl17-7 (1.4568) steel, processed through air melting, solution treatment, and precipitation hardening. The
LVS EN 2590:2017
Aerospace series - Steel - Sheets and plates, hot rolled - Dimensions
This document establishes comprehensive requirements and testing methods for hot-rolled steel strips and sheets used in aviation and aerospace applications. It focuses on defining precise dimensional
LVS EN 2541:2018
Aerospace series - Steel FE-PA18 - Quenched and cold drawn - Wire for spring - D ≤ 4,0 mm
This technical specification establishes the technical requirements for cold-drawn spring wire made of steel, specifically within the diameter range of up to 4.0 millimeters. The document outlines