Aircraft And Space Vehicle Engineering Official British Standard

BS A 361:2000, ISO 12281:1999

Ensure compliance with BS A 361:2000 for solid rivets, enhancing safety and performance in aircraft and space vehicle engineering.

Overview

BS A 361:2000, which is identical to ISO 12281:1999, specifies the requirements for solid rivets with a 100° normal countersunk head, manufactured from metallic materials. These rivets may be supplied with or without surface treatment, depending on the application needs. This standard is crucial for ensuring the reliability and performance of riveted joints in aircraft and space vehicle engineering.

Key Requirements

The standard outlines specific dimensions and mechanical properties for solid rivets, which include:

  • Head Configuration: 100° normal countersunk head design for optimal aerodynamic performance.
  • Material Specifications: Rivets must be made from suitable metallic materials that meet defined strength and durability criteria.
  • Surface Treatment: Options for surface treatment are provided to enhance corrosion resistance and longevity.
  • Dimensional Tolerances: Precise measurements are specified to ensure compatibility and performance in assembly.

Implementation Benefits

Adhering to BS A 361:2000 offers several practical benefits for manufacturers and engineers in the aerospace sector:

  • Enhanced Safety: Compliance with this standard ensures that rivets used in critical applications meet rigorous safety and performance criteria.
  • Quality Assurance: The standard provides a framework for quality control during the manufacturing process, reducing the risk of defects.
  • Interchangeability: Standardised dimensions and specifications facilitate the interchangeability of rivets, simplifying maintenance and repairs.
  • Regulatory Compliance: Meeting the requirements of this standard helps organisations comply with national and international regulations governing aerospace engineering.

Compliance Value

Compliance with BS A 361:2000 not only enhances the integrity of aircraft and space vehicle structures but also provides a competitive advantage in the aerospace market. By ensuring that rivets meet established standards, organisations can:

  • Reduce Liability: Adhering to recognised standards mitigates risks associated with structural failures.
  • Improve Customer Confidence: Demonstrating compliance can enhance customer trust and satisfaction, leading to increased business opportunities.
  • Facilitate Audits: Compliance with recognised standards simplifies the audit process, making it easier to demonstrate adherence to quality and safety protocols.

In conclusion, BS A 361:2000 is an essential standard for the aerospace industry, providing clear guidelines for the use of solid rivets. By following this standard, organisations can ensure the safety, reliability, and performance of their products, ultimately contributing to the advancement of aerospace technology.

Technical Information

Aircraft And Space Vehicle Engineering
BSI Group
0 580 34012 0
Specification Details
  • Rivets, solid, 100° normal countersunk head, in metallic material, with or without surface treatment
  • Dimensions
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