Discussion on Airworthiness Requirement of Widespread Fatigue Damage - Safe-life Methodology or Damage-tolerance Methodology

被引：0

作者：

Feng Zhenyu ^{[1
]}

Mao Keyi ^{[1
]}

Zou Tianchun ^{[1
]}

Yang Yaning ^{[1
]}

机构：

[1] Civil Aviat Univ China, Tianjin Key Lab Civil Aircraft Airworthiness & Ma, Tianjin 300300, Peoples R China

来源：

3RD INTERNATIONAL SYMPOSIUM ON AIRCRAFT AIRWORTHINESS (ISAA 2013) | 2014年 / 80卷

关键词：

Widespread fatigue damage; damage-tolerance; safe life; airworthiness requirement; limit of validity;

D O I：

10.1016/j.proeng.2014.09.096

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Regulatory action and research conducted by FAA and industries to preclude widespread fatigue damage occurring in transport airplane fleet is introduced, especially the milestones in the rulemaking course. This article gives an interpretation of the current airworthiness requirement relating to widespread fatigue damage and limit of validity based on analysis of the widespread fatigue damage characteristics. The conclusion is made that the methodology of the current airworthiness requirement is a methodology both safe-life and damage-tolerance since that MSD/MED cracks are difficult to detect. (C) 2014 Published by Elsevier Ltd.

引用

页码：392 / 398

页数：7

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