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Question 1: How do you evaluate the trade-offs between system complexity and reliability when designing critical systems like flight controls?

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Question 2: What is the primary challenge when testing an aircraft's control response during a steep climb?

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Question 3: When designing an aircraft structure to resist buckling, what is the primary consideration in ensuring that the structure is stable?

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Question 4: What is the primary factor affecting the buckling strength of a thin-walled aerospace structure?

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Question 5: How does prototype development differ for military versus commercial aircraft?

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Question 6: What is the purpose of the compliance documentation in the airworthiness certification process?

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