BS 2HC 211:1989
Comprehensive British Standard for aircraft and space vehicle engineering. Ensure compliance and safety with this essential technical specification.
BS 2HC 211:1989 - The Essential Standard for Aircraft and Space Vehicle Engineering
Developed by the British Standards Institution (BSI), BS 2HC 211:1989 is a crucial technical specification for the design, manufacture, and maintenance of aircraft and space vehicles. This comprehensive standard covers a wide range of engineering requirements, ensuring the safety, reliability, and performance of these complex and mission-critical systems.
Key Features and Benefits:
- Comprehensive Scope: Covers a broad range of engineering disciplines, including structures, materials, systems, and testing procedures, ensuring a holistic approach to aircraft and space vehicle design.
- Compliance and Safety: Adherence to BS 2HC 211:1989 helps organizations demonstrate compliance with industry regulations and safety standards, mitigating risks and liability.
- Quality Assurance: The standard provides detailed guidelines for quality control and assurance, enabling manufacturers to deliver high-quality products that meet stringent performance requirements.
- Interoperability: The standard promotes standardization, facilitating the integration of components and systems from different suppliers, enhancing overall system compatibility.
- Maintenance and Lifecycle Management: The standard includes provisions for maintenance, repair, and overhaul (MRO) procedures, ensuring the long-term reliability and serviceability of aircraft and space vehicles.
Technical Specifications and Requirements:
BS 2HC 211:1989 covers a wide range of technical specifications and requirements, including:
- Structural Design: Guidelines for the design and analysis of airframes, wings, and other structural components, ensuring structural integrity and airworthiness.
- Materials and Processes: Specifications for the selection, testing, and processing of materials used in aircraft and space vehicle construction, including metals, composites, and advanced materials.
- Systems and Equipment: Requirements for the design, integration, and testing of aircraft and space vehicle systems, such as propulsion, avionics, electrical, and environmental control systems.
- Testing and Certification: Detailed procedures for the testing and certification of aircraft and space vehicle components and systems, ensuring compliance with regulatory requirements.
- Maintenance and Repair: Guidelines for the maintenance, repair, and overhaul of aircraft and space vehicles, including inspection, troubleshooting, and component replacement procedures.
Ensure Compliance and Safety with BS 2HC 211:1989
As a leading British Standard, BS 2HC 211:1989 is an essential reference for organizations involved in the design, manufacture, and maintenance of aircraft and space vehicles. By adhering to this comprehensive standard, companies can demonstrate their commitment to quality, safety, and compliance, positioning themselves as trusted partners in the highly regulated aerospace industry.
Whether you're an aircraft manufacturer, a space exploration company, or a maintenance service provider, investing in BS 2HC 211:1989 can help you navigate the complex technical and regulatory landscape, optimize your operations, and deliver superior products and services to your customers.
Technical Information
Specification Details
- Specification for nickel-chromium-cobalt-molybdenum-aluminium-titanium alloy castings (Nickel base Cr 15
- 5, Co 10
- 0, Mo 8,3, Al 4
- 2, Ti 3
- 6)