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Fuselage bending stress arises principally from

  • A.Wing torsion alone
  • B.Tail loads and payload distribution
  • C.Cabin pressurisation alone
  • D.Engine thrust alone

Answer: B

The fuselage acts as a beam supported at the wing, carrying the tail loads at one end and the nose structure at the other, with payload distributed between. The resulting bending combines with the pressurisation stresses at every point.

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