CURRENT AIRWORTHINESS REGULATIONS FOR DAMAGE-TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE

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Published: 2017-03-30

Page: 72-84


DAWEI JIA *

Engineering R&D Center, AVIC SAC Commercial Aircraft Company Ltd., Shenyang, China.

XU LIU

Engineering R&D Center, AVIC SAC Commercial Aircraft Company Ltd., Shenyang, China.

*Author to whom correspondence should be addressed.


Abstract

Airworthiness regulations pertaining to the fatigue and damage tolerance (F&DT) evaluation of civil transport aircraft structure have been extensively modified and broadened in scope over the past sixty years. These changes to the regulations resulted from investigations of major accidents and in-service structural failures due to fatigue damage. New design concepts and philosophies were developed which led to improvements in the F&DT evaluation. This paper presents a review of the current airworthiness regulations for F&DT evaluation of civil transport aircraft structure and provides an overview of an acceptable means of compliance with those regulations for new type certificates. The analyses and scope of testing for certification are addressed.

Keywords: Airworthiness regulations, fatigue, damage tolerance, means of compliance, certification


How to Cite

JIA, DAWEI, and XU LIU. 2017. “CURRENT AIRWORTHINESS REGULATIONS FOR DAMAGE-TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE”. Journal of Basic and Applied Research International 21 (2):72-84. https://ikprress.org/index.php/JOBARI/article/view/4025.

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