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An engine of mass \( 6000 \) kg is mounted \( 9.0 \) m outboard. Its bending relief moment on the wing at 1 g is approximately

  • A.5300 kN m
  • B.530 kN m
  • C.54 kN m
  • D.265 kN m

Answer: B

Correct answer: 530 kN m

Convert the mass to weight and multiply by the arm:

\[ W = 6000 \times 9.81 = 58.9\ \mathrm{kN} \]

\[ M = 58.9 \times 9.0 = 530\ \mathrm{kN\,m} \]

This moment acts downward at 1 g, opposing the upward bending the lift produces, so it relieves the wing root and allows a lighter structure. The relief grows with load factor, since both the lift and the engine's inertia scale together, which is why the benefit is greatest exactly where the structure is most highly loaded.

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