Introduction
Back in the day, aircraft were simple. Instruments were mechanical and not interconnect, many were not required to fly but merely “indicated” to the pilot. Modern avionics employs many complex and interconnected systems, many of which are responsible for high level (aircraft level) function and play a huge role in modern aircraft safety. As instrumentation became more complex, they ran out of space in the cockpit, therefore units became multi-functional or “glass cockpits” were utilised to ensure that the right information is available to the pilot at the right time.
As these systems became more complex and more responsible for aircraft function and safety; the architectures and risks associated with these systems became more complex, novel and diverse. Due to the nature of aviation, in-depth failure mode analysis is required for each component/system in order to identify a wide variety of potential failures using existing knowledge. From this, the risks are assessed for their severity, likelihood and detectability and prioritised from there.
ARP4754A – Guidelines for Development of Civil Aircraft and Systems
This is a document which describes the the validation of requirements and verification of design implementation in the development of aircraft systems. It is a framework for a company to develop their own internal standards.
See also:
- Title 14 Code of Federal Regulations (14CFR) Part 25 (Airworthiness Standards: Transport Category Airplanes)
- European Aviation Safety Agency (EASA) Certification Specification (CS) CS-25 (Certification Specifications for Large Aeroplanes)
