BS EN 2125 is a metallic material standard that covers technical specifications for use of aluminium alloy which ensures safety, performance and stable operability in aerospace applications.
BS EN 2125 specifies the requirements relating to: Aluminium alloy Al-P16-T6151 plates with limit dimension range of 6 mm < a ≤ 120 mm for aerospace applications.
BS EN 2125 on aluminium alloy plate requirements for aerospace applications 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 light weight, strength, and corrosion resistance. Aluminium alloy is a high-grade alloy with outstanding fatigue resistance and a high yield strength.
BS EN 2125 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 2125 also provides you guidance on delivery conditions, heat treatment, use condition which allows you to ensure the quality and performance of aluminium alloys for aerospace applications.
Guidance in BS EN 2125 allows you to test aluminium alloys for different physical attributes such as temperature, proof stress, strength, elongation, reduction of area, hardness, shear strength, bending and impact strength that allows you to ensure the safety and structural integrity of aluminium plates.
EN 2125