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Which of the following is NOT a valid reason riveted joints persist in metal airframes?

  • A.Repairs can be made with simple equipment in the field
  • B.Rivet holes introduce no stress concentration
  • C.Individual fasteners can be inspected and replaced
  • D.Their fatigue behaviour is supported by extensive data

Answer: B

Correct answer: Rivet holes introduce no stress concentration

A rivet hole is a stress concentration - a factor of about three for a circular hole in a wide plate - and rivet holes are among the commonest fatigue origins in an airframe. Riveting persists in spite of that, for the three genuine reasons given: field repairability, individual inspection and replacement, and decades of fatigue data behind the design allowables.

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