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In-flight upset - 154 km west of Learmonth, WA, 7 October 2008,

In-flight upset - 154 km west of Learmonth, WA, 7 October 2008,

In-flight upset - 154 km west of Learmonth, WA, 7 October 2008,

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mode with the ADIRU that had not been previously identified by the ADIRUmanufacturer. Given the increasing complexity <strong>of</strong> such systems, this investigationhas <strong>of</strong>fered an insight into the types <strong>of</strong> issues that will become relevant for futureinvestigations. It also identified a number <strong>of</strong> specific lessons or reminders for themanufacturers <strong>of</strong> new complex, safety-critical systems to consider. These include:• System safety assessments (SSAs) and other design evaluation activities shouldrecognise that ADIRUs and similar types <strong>of</strong> equipment can generate a widerange <strong>of</strong> patterns <strong>of</strong> incorrect data, including patterns not previouslyexperienced.• Failure mode effects analyses (FMEAs) have a limited ability to identify allequipment failure modes, particularly for complex, highly-integrated systems.• Where practicable for safety-critical functions, SSA and other design evaluationactivities should consider the effects <strong>of</strong> different values <strong>of</strong> system inputs in eachmode <strong>of</strong> operation, particularly during transitions between modes.• The BITE for ADIRUs and similar types <strong>of</strong> equipment should check the results<strong>of</strong> each key stage in the processing <strong>of</strong> output data.• SEEs are a potential hazard to aircraft systems that contain high-densityintegrated circuits. Designers should consider the risk <strong>of</strong> SEE and includespecific features in the system design to mitigate the effects <strong>of</strong> such events,especially in systems with a potentially significant influence on <strong>flight</strong> safety.• The in-service performance records for safety-critical line-replaceable unitsshould include all reported performance problems, not just those that result inthe removal <strong>of</strong> the unit from the aircraft.• The records for the key components within safety-critical systems shouldinclude details such as production or batch codes as well as the part numberwhere practicable.A broader lesson concerns the safety assessment activities needed for complexsystems. <strong>In</strong> recent years there have been developments in the guidance material forsystem development processes and research into new approaches for SSA.However, design engineers and safety analysts also perform a safety-criticalfunction, yet the investigation found little published research that has examined thehuman factors issues affecting such personnel. <strong>In</strong> other words, there has beenlimited research that has systematically evaluated how these personnel conduct theirevaluations <strong>of</strong> systems, and how the design <strong>of</strong> their tasks, tools, training andguidance material can be improved so that the likelihood <strong>of</strong> design errors isminimised. The need for further research and development in this area will becomemore important as system complexity increases over time.- 211 -

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