Transcription of Corrosion and Inspection of General Aviation Aircraft - CAA
{{id}} {{{paragraph}}}
Corrosion and Inspection of General Aviation Aircraft CAP 1570 Published by the Civil Aviation Authority, 2017 Civil Aviation Authority Aviation House Gatwick Airport South West Sussex RH6 0YR You can copy and use this text but please ensure you always use the most up to date version and use it in context so as not to be misleading, and credit the CAA. First published July 2017 Enquiries regarding the content of this publication should be addressed to: The latest version of this document is available in electronic format at CAP 1570 Contents July 2017 Page 3 Contents chapter 1 6 Introduction 6 chapter 2 8 Theory of Corrosion 8 Types of Corrosion 9 Direct Chemical Attack 10 Electrochemical Attack 10 chapter 3 13 Types of corrosi
Chapter 13 57 Categories and limits of corrosion 57 Chapter 14 58 Bibliography 58 Chapter 15 59 Design references 59. CAP 1570 Chapter 1: Introduction ... light aircraft landing gear components, where a mixture of exfoliation and pitting corrosion on the flash line initiated stress corrosion cracking that then lead to
Domain:
Source:
Link to this page:
Please notify us if you found a problem with this document:
{{id}} {{{paragraph}}}