Discussion
Which of the following would NOT increase the load factor an aircraft experiences?
Answer: B
Correct answer: Rolling out of a turn to wings level
Rolling out reduces the bank angle, so \( n = 1/\cos\phi \) falls back towards 1 - the load factor decreases. A gust, a steeper bank and an abrupt elevator pull all raise it, the last being the case that VA exists to protect against.
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