BS A 334:1999, ISO 3221:1998
Discover BS A 334:1999, ISO 3221:1998, a key standard for aircraft and space vehicle engineering. Ensure safety and compliance in material testing.
BS A 334:1999, ISO 3221:1998 - Comprehensive Overview
BS A 334:1999, incorporating ISO 3221:1998, establishes crucial standards within the arena of aircraft and space vehicle engineering. This British Standard is pivotal for professionals within the aerospace domain, ensuring that materials and components are benchmarked against the highest safety and performance standards.
Published on February 15, 1999, this standard specifies the methodology for the determination of the flammability of aircraft materials due to accumulation of test runs and evaluations. By adhering to the principles outlined in this document, engineers and technicians can comprehensively assess the fire performance characteristics of materials intended for use in aircraft and aerospace applications. This includes thorough guidance on test environments and operational parameters needed to replicate real-world scenarios.
The significance of BS A 334:1999 lies in its alignment with international standards. As an identical national standard to ISO 3221:1998, it serves as a vital reference point for compliance with global best practices in material testing. This congruity not only promotes consistency across international borders but also eases collaboration between global aerospace manufacturers and regulatory bodies.
The standard details various testing protocols, ensuring they are methodical and reproducible, thus leading to results that stakeholders can trust. It elucidates the criteria required for successful evaluations and denotes the acceptable performance parameters for materials subjected to evaluation. Such structured guidelines are essential in mitigating risks related to material selection and usage in aerospace applications, directly influencing safety and regulatory adherence.
Purchasing BS A 334:1999 is an investment in quality assurance for aerospace components. At a price of £134.00, it provides access to vital content intended to fortify safety and enhance operational reliability in both commercial and private aviation sectors. By implementing the practices detailed within this standard, organizations can demonstrate their commitment to excellence and responsibility in aerospace engineering.
Furthermore, this standard is available in both PDF and hardcopy formats, catering to various preferences for documentation retention. Whether utilized as a reference for ongoing engineering projects or as a basis for developing new materials, BS A 334:1999 is an essential tool for any organization entrenched in the aerospace industry. For those looking to enhance their material engineering protocols, adopting this standard is a crucial step to align with industry standards and fortify safety measures.
Technical Information
Specification Details
- Nuts, anchor, self-locking, fixed, 90° corner, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235°C, 1100 MPa (at ambient temperature)/315°C and 1100 MPa (at ambient temperature)/425°C
- Dimensions