1. You are designing a new airplane (the Whizbang 550) under the new Part 23 of the Federal Aviation Regulations. Since this is going to be a speedy 4 seater with the ability to do somewhat aggressive maneuvering, you are designing to limit loads of + 5.5g / -4.0g. 2. Assuming a coordinated turn, what is the bank angle for a 5.5g turn? 3. Using the 1.5 safety factor for ultimate load, what is the corresponding bank angle? Show your work