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Engine failure on a wing-mounted installation produces a structural load case because

  • A.Asymmetric thrust loads the fin
  • B.The wing immediately loses all its lift
  • C.Cabin pressure is lost
  • D.The undercarriage extends automatically

Answer: A

The remaining engine's thrust must be balanced by rudder, and that side load is reacted through the fin, its attachment and the rear fuselage in torsion. The case is checked at the critical speed and is frequently what sizes the fin.

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