Skip to Main Content

Abstract

This chapter discusses the failure of an aileron control cable in an aircraft and explains how investigators determined the cause. Based on their observations and the results of SEM fractography, investigators concluded that the cable had been damaged by a shearing tool, leading to its failure.

You do not currently have access to this chapter.
Don't already have an account? Register

Failure of an Aileron Control Cable in an Aircraft, Failure Analysis of Engineering Structures: Methodology and Case Histories, By V. Ramachandran, A.C. Raghuram, R.V. Krishnan, S.K. Bhaumik, ASM International, 2005, p 152–153, https://doi.org/10.31399/asm.tb.faesmch.t51270152

Download citation file:


Close
Close Modal

or Create an Account

Close Modal
Close Modal