Aircraft And Space Vehicle Engineering Official British Standard

BS EN 2650:1997

Discover the compliance benefits of BS EN 2650:1997 for pan head screws in aerospace applications, ensuring safety and quality in critical environments.

Overview

BS EN 2650:1997 specifies the requirements for pan head screws that are slotted and threaded to the head, manufactured from corrosion resisting steel and passivated. These screws are classified for use in environments with a maximum tensile strength of 600 MPa at ambient temperature and 425°C. This standard is crucial for ensuring the reliability and safety of components used in aircraft and space vehicle engineering.

Key Requirements

The standard outlines several key specifications that must be adhered to during the manufacturing process:

  • Material Specification: The screws must be made from corrosion resisting steel, which ensures durability and longevity in harsh environments.
  • Mechanical Properties: The screws are classified to withstand a tensile strength of up to 600 MPa at ambient temperature, ensuring they can handle significant loads.
  • Temperature Resistance: The screws are rated for use at temperatures up to 425°C, making them suitable for high-temperature applications.
  • Passivation: The passivation process enhances corrosion resistance, providing additional protection against environmental factors.

Implementation Benefits

Adhering to BS EN 2650:1997 provides several practical benefits for manufacturers and compliance professionals:

  • Enhanced Safety: Using screws that meet this standard ensures that components are reliable and safe for use in critical applications, reducing the risk of failure.
  • Quality Assurance: Compliance with this standard demonstrates a commitment to quality and reliability, which can enhance the reputation of manufacturers in the aerospace sector.
  • Streamlined Processes: By following the specifications outlined in the standard, manufacturers can streamline their production processes, leading to increased efficiency and reduced waste.
  • Regulatory Compliance: Meeting the requirements of BS EN 2650:1997 helps organisations comply with broader regulatory frameworks governing aerospace manufacturing.

Compliance Value

Compliance with BS EN 2650:1997 is not just about meeting technical specifications; it is also about ensuring that products are fit for purpose in the demanding field of aircraft and space vehicle engineering. The standard provides a benchmark for quality and performance, which is essential for maintaining safety standards in aviation and aerospace applications.

Furthermore, adherence to this standard can facilitate easier access to international markets, as it aligns with European norms and regulations. This can be particularly beneficial for manufacturers looking to expand their reach and establish credibility in the global aerospace industry.

In conclusion, BS EN 2650:1997 is a vital standard for the production of pan head screws in corrosion resisting steel. Its implementation not only enhances product quality and safety but also supports compliance with regulatory requirements, ultimately contributing to the advancement of aerospace engineering.

Technical Information

Aircraft And Space Vehicle Engineering
BSI Group
0 580 26903 5
Specification Details
  • Screws, pan head, slotted, threaded to head, in corrosion resisting steel, passivated
  • Classification: 600 MPa (at ambient temperature) /425°C
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