BS EN 2319 is a metallic material standard that covers technical specifications for the Aerospace series: Aluminium alloy 2024 T3510, which ensures safety, performance and stable operability in aerospace applications.
BS EN 2319 specifies the requirements for Aluminium alloy 2024 for aerospace applications. BS EN 2319 specifies the delivery condition as T3510 and drawn bar as the method of production. It also sets the limit dimension (a) ≤ 75 mm for aerospace applications.
BS EN 2319 on Aerospace series: Aluminium alloy 2024 T3510 applies to:
Aluminium has a long history and variety of applications in the aerospace industry. Aluminium is utilised to create the frames and components of aeroplanes, demonstrating its lightweight, strength, and corrosion resistance. Aluminium alloy is a high-grade alloy with outstanding fatigue resistance and high yield strength.
BS EN 2319 provides you guidance on chemical composition, method of melting, form, method of production, limit dimensions and technical specifications, which allows you to standardize the application of aluminium alloys for aerospace applications.
BS EN 2319 provides you guidance on delivery conditions, heat treatment, use condition that facilitates transportation condition, storage and usability for aluminium alloy drawn bars for aerospace applications.
BS EN 2319 also provides you guidance on testing, including heat treatment, dimensions, cladding thickness, temperature, proof stress, strength, elongation, hardness, shear strength and bending that ensures mechanical strength, performance and longevity of aluminium alloys for aerospace applications.
Guidance in BS EN 2319 enables you to develop and assess Aluminium alloy 2024 T3510 bars that ensure safety and structural stability in aerospace applications.EN 2319:2018
EN 2319:2018