BS EN 3489 is a metallic material standard covering technical specifications for the Aerospace series: Steel X8CrNiTi18-10 (1.4878/1.4544) tubes for structures that enhance structural stability and corrosion resistance.
BS EN 3489 specifies the requirements relating to Steel X8CrNiTi18-10 (1.4878/1.4544) tubes for structures in softened delivery conditions.
BS EN 3489 specifies a tensile strength range of 500 ≤ Rm ≤ 750 MPa and a limit dimension range of 0.5 ≤ a ≤ 5 mm for aerospace applications.
BS EN 3489 is a standard prepared and approved by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). Its ASD-STAN designation is FE-PA13.
BS EN 3489 on Aerospace series: Steel X8CrNiTi18-10 (1.4878/1.4544) tubes for structures applies to:
Stainless steel is one of the most commonly used metals in aerospace equipment. Steel has mechanical properties such as corrosion resistance, strength and toughness, making it a reliable option for use in the aerospace industry. Steel tubing sections have a higher strength-to-weight ratio, ensuring structural integrity in aerospace applications.
BS EN 3489 provides you guidance on chemical composition, method of melting, form, method of production, limit dimension and technical specifications, which allows you to ensure corrosion resistance and heat resistance in aircraft structures.
BS EN 3489 provides you guidance on delivery condition, heat treatment, delivery condition code, use condition and heat treatment that facilitates transportation condition, storage and usability for steel tubes.
BS EN 3489 provides you guidance on testing, which includes heat treatment, dimensions, thickness of cladding, temperature, proof stress, strength, elongation, hardness, shear strength and bending, ensuring structural integrity and longevity of the aerospace structures.
Guidance in BS EN 3489 enables you to develop and assess Steel X8CrNiTi18-10 (1.4878/1.4544) tubes that ensures structural integrity and corrosion resistance in aerospace applications.
EN 3489