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Assertion (A): The structure must show no detrimental permanent deformation at ultimate load.

Reason (R): Ultimate load is 1.5 times the limit load in civil design.

Select the correct answer from the options below.

  • A.Both A and R are true, and R is the correct explanation of A
  • B.Both A and R are true, but R is not the correct explanation of A
  • C.A is true but R is false
  • D.A is false but R is true

Answer: D

The assertion is false and the reason is true. The no-permanent-deformation requirement applies at limit load. At ultimate the structure must merely not fail, and permanent set there is entirely acceptable since the aircraft is not expected to fly again.

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