Discussion
An aircraft weighing \( 60 \) kN pulls a manoeuvre at a load factor of \( 2.5 \). The lift being produced is
Answer: B
Correct answer: 150 kN
\[ L = n W = 2.5 \times 60 = 150\ \mathrm{kN}. \] The load factor is by definition the lift divided by the weight, so at 2.5 g the wing is carrying two and a half times the aircraft’s weight - and everything the wing supports feels the same multiple.
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