Discussion
An aircraft is certificated to \( +3.8 \) g in the normal category. Its ultimate design load factor is
Answer: C
Correct answer: 5.7
\[ 3.8 \times 1.5 = 5.7. \] The certificated figure of \( +3.8 \) g is the limit load factor; multiplying by the standard 1.5 factor of safety gives the ultimate design load factor at which the structure must not fail.
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