Failure analysis of pipe fastener (RH) of an aircraft

Madan, M and Bhuvana, R and Sujata, M and Venkataswamy, MA and Bhaumik, SK (2009) Failure analysis of pipe fastener (RH) of an aircraft. Project Report. National Aerospace Laboratories, Bangalore, India.

Full text not available from this repository. (Request a copy)


A failed pipe fastener assembly of an aircraft was analyzed. Failure pattern suggest that the two haves of the pipe fastener got detached by deforming the sheet material at the bolted region due to forces exerted from inside. Examination revealed that surfaces of a few other parts of the assembly were in touch with the sheet material. However, it was not possible to establish whether or not any assembly related issues were responsible for the failure. Evidences do not suggest any metallurgical abnormalities in the material of construction as the cause of failure.

Item Type: Monograph (Project Report)
Uncontrolled Keywords: Aircraft;Pipe fastener;Overload
Subjects: AERONAUTICS > Aeronautics (General)
CHEMISTRY AND MATERIALS > Chemistry and Materials (General)
Depositing User: Ms. Alphones Mary
Date Deposited: 18 Jul 2011 05:37
Last Modified: 18 Jul 2011 05:37

Actions (login required)

View Item View Item