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The Practical Implementation of Fatigue Requirements to Military Aircraft and Helicopters in the United Kingdom

Rebekah Maxwell

Abstract

The methods adopted in the United Kingdom to ensure the structural integrity of military aeroplanes and helicopters from the fatigue point of view are described. The procedure adopted from the writing of the specification to the monitoring of fatigue life in service are presented along with the requirements to be met and the way in which they are satisfied. Some of the outstanding problems that remain to be solved are indicated.

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Key concepts: Aeronautics, Service (business), Point (geometry), Military service, Engineering, Computer science, Business, Political science