Aircraft And Space Vehicle Engineering Official British Standard

BS EN 2866:2009

Ensure compliance and reliability with BS EN 2866:2009 for aerospace self-locking nuts. Key specifications and benefits for manufacturers detailed.

Overview

BS EN 2866:2009 is a critical standard within the aerospace sector, specifically addressing the specifications for self-locking anchor nuts with a floating design. These components are essential in ensuring the integrity and reliability of aircraft and space vehicle assemblies. The standard outlines the requirements for nuts made of steel, which are cadmium plated and lubricated with MoS2. The classification of these nuts is 1110 MPa at ambient temperature, with a maximum operating temperature of 235°C.

Key Requirements

The standard specifies several key requirements for the manufacturing and testing of self-locking anchor nuts:

  • Material Specifications: The nuts must be constructed from high-strength steel, ensuring durability and resistance to mechanical stress.
  • Surface Treatment: A cadmium plating process is mandated to enhance corrosion resistance, which is vital for components used in harsh aerospace environments.
  • Lubrication: MoS2 lubrication is required to reduce friction and wear, thereby extending the lifespan of the nuts.
  • Dimensional Tolerances: The standard includes precise dimensional tolerances to ensure compatibility with corresponding components in aerospace assemblies.
  • Testing Procedures: Rigorous testing methods must be employed to verify the mechanical properties and performance of the nuts under specified conditions.

Implementation Benefits

Adhering to BS EN 2866:2009 provides numerous benefits for manufacturers and compliance professionals:

  • Enhanced Safety: By using components that meet stringent standards, manufacturers can significantly reduce the risk of failure in critical aerospace applications.
  • Improved Reliability: The use of high-quality materials and manufacturing processes ensures that the nuts perform consistently under varying operational conditions.
  • Streamlined Compliance: Implementing this standard simplifies the compliance process with regulatory bodies, as it aligns with international aerospace quality requirements.
  • Market Competitiveness: Compliance with recognised standards enhances a manufacturer’s reputation and can lead to increased market opportunities.

Compliance Value

Compliance with BS EN 2866:2009 is not merely a regulatory requirement; it is a strategic advantage. The aerospace industry is governed by stringent safety and quality regulations, and adherence to this standard demonstrates a commitment to excellence. It assures stakeholders, including regulatory bodies and customers, that the products meet the highest levels of safety and performance.

Furthermore, compliance can lead to reduced liability and insurance costs, as well as improved customer satisfaction through reliable product performance. In an industry where the consequences of failure can be catastrophic, the value of compliance cannot be overstated.

In conclusion, BS EN 2866:2009 serves as a vital framework for the production of self-locking anchor nuts in aerospace applications. By following this standard, manufacturers can ensure that their products are safe, reliable, and compliant with industry expectations.

Technical Information

Aircraft And Space Vehicle Engineering
BSI Group
978 0 580 68568 2
Specification Details
  • Aerospace series
  • Nuts, anchor, self-locking, floating, one lug, with counterbore, in steel, cadmium plated, MoS2 lubricated
  • Classification: 1110 MPa (at ambient temperature)/235°C
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