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If my factor of safety is 2 and design load of my aircraft is 1000N then, at which value of ultimate load my aircraft can withstand without breaking?

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If my factor of safety is 2 and design load of my aircraft is 1000N then, at which value of ultimate load my aircraft can withstand without breaking?

(a) 2KN

(b) 9N

(c) 1208KN

(d) 1.208KN

This question was addressed to me in an interview for job.

My question is taken from Loads Categories topic in chapter Structures and Loads of Aircraft Design

1 Answer

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Correct option is (a) 2KN

To explain: Ultimate load without breaking = factor of safety * design load = 2*1000 = 2KN.

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