Failure analysis of main undercarriage fitting of Main landing gear of an aircraft

Madan, M and Bhuvana, R and Sujata, M and Venkataswamy, MA and Bhaumik, SK (2009) Failure analysis of main undercarriage fitting of Main landing gear of an aircraft. Project Report. National Aerospace Laboratories, Bangalore, India.

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Abstract

A fractured main undercarriage fitting of an aircraft was analyzed. Analysis revealed that there was excessive loading on the hollow member of the undercarriage leading to overload fracture of the main fitting. There were no evidences of progressive failure anywhere on the component and the material of the undercarriage was found to conform to the specification.

Item Type: Proj.Doc/Technical Report (Project Report)
Uncontrolled Keywords: Aircraft;Main landing gear;Overload
Subjects: AERONAUTICS > Aeronautics (General)
CHEMISTRY AND MATERIALS > Chemistry and Materials (General)
Division/Department: Materials Science Division, Materials Science Division, Materials Science Division, Materials Science Division, Materials Science Division
Depositing User: Ms. Alphones Mary
Date Deposited: 18 Jul 2011 11:55
Last Modified: 18 Jul 2011 11:55
URI: http://nal-ir.nal.res.in/id/eprint/9407

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