Question 1: In the airworthiness certification process, why is the "Fuel System Certification" necessary?
Which action should you take?
Question 2: How do you evaluate the prototype's performance under extreme weather conditions, such as ice or heavy turbulence?
Which action should you take?
Question 3: When assessing the aircraft's engine performance during flight testing, what key parameters should be evaluated?
Which action should you take?
Question 4: What is the primary advantage of using a fly-by-wire control system compared to traditional mechanical linkages in aircraft design?
Which action should you take?
Question 5: In airworthiness certification, which document would detail the required structural tests for an aircraft's fuselage design?
Which action should you take?
Question 6: What is the role of redundancy in aircraft systems, and how does it contribute to overall system reliability and safety?
Which action should you take?