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Match each fatigue load source in List I with its frequency in List II.

List I

A. Cabin pressurisation cycle

B. Ground-air-ground cycle

C. Gust encounters in cruise

D. Ultimate load application

List II

1. Once per flight, a full bending reversal

2. Once per flight, a full pressure cycle

3. Never expected in service

4. Many small cycles throughout each flight

Select the correct match.

  • A.A-3, B-1, C-4, D-2
  • B.A-2, B-1, C-4, D-3
  • C.A-1, B-2, C-4, D-3
  • D.A-2, B-4, C-1, D-3

Answer: B

The spectrum a transport is assessed against is dominated by the two once-per-flight cycles and filled in by the gust content. Ultimate load, by contrast, is a strength requirement that the aircraft is never expected to meet in service at all.

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