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Question 1: What role do "Environmental Testing" and "Flight Testing" play in the process of obtaining airworthiness certification for a new aircraft?

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Question 2: During prototype development, which is the most effective way to verify the aircraft's weight and balance distribution?

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Question 3: How is safety factor defined in airworthiness certification, and how does it affect structural design?

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Question 4: When performing a load analysis for an aircraft landing gear, what is the primary factor in determining the design of the shock absorbers?

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Question 5: In a climb performance test, which factor is most critical to ensure the aircraft's climb rate at maximum weight?

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Question 6: When testing a new prototype, what method is typically used to assess its aerodynamic properties before flight?

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