The SS tube of the lubricating pipeline has failed by fatigue. The fatigue was of high cycle-low stress type. Analysis shows that the failure was due to presence of assembly stresses. It appears that anchoring of the pipeline has resulted in the assembly stresses. No metallurgical and/or mechanical abnormalities were found responsible for the failure. Anchoring of the pipeline of the type in question is not a general engineering practice and hence should be avoided. Also, care must be taken to avoid any assembly stresses during fixing of the pipeline
A fractured ‘Support clamp RH’ installed on an aircraft was sent to the laboratory for analysis. Exa...
A fractured ‘Support clamp RH’ installed on an aircraft was sent to the laboratory for analysis. Exa...
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...
The SS tube of the lubricating pipeline has failed by fatigue. The fatigue was of high cycle-low str...
A failed pipeline of an aircraft was forwarded to the laboratory for analysis. The pipeline was foun...
Both the fuel pipelines of an aeroengine have failed in similar fashion at identical location. Fract...
Both the fuel pipelines of an aeroengine have failed in similar fashion at identical location. Fract...
A cracked pipe assembly of hydraulic system-II of an aircraft was forwarded to this laboratory for e...
Pipelines play significant roles in the major phases of petroleum exploration, drilling, refining an...
A fractured drain pipe-port installed in an aircraft was forwarded to the laboratory for analyzing m...
A fractured drain pipe-port installed in an aircraft was forwarded to the laboratory for analyzing m...
A failed pipe fastener assembly of an aircraft was analyzed. Failure pattern suggest that the two ha...
A failed pipe fastener assembly of an aircraft was analyzed. Failure pattern suggest that the two ha...
The normal hose assembly of LH undercarriage of an aircraft has failed by cracking at the ferrule ed...
The normal hose assembly of LH undercarriage of an aircraft has failed by cracking at the ferrule ed...
A fractured ‘Support clamp RH’ installed on an aircraft was sent to the laboratory for analysis. Exa...
A fractured ‘Support clamp RH’ installed on an aircraft was sent to the laboratory for analysis. Exa...
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...
The SS tube of the lubricating pipeline has failed by fatigue. The fatigue was of high cycle-low str...
A failed pipeline of an aircraft was forwarded to the laboratory for analysis. The pipeline was foun...
Both the fuel pipelines of an aeroengine have failed in similar fashion at identical location. Fract...
Both the fuel pipelines of an aeroengine have failed in similar fashion at identical location. Fract...
A cracked pipe assembly of hydraulic system-II of an aircraft was forwarded to this laboratory for e...
Pipelines play significant roles in the major phases of petroleum exploration, drilling, refining an...
A fractured drain pipe-port installed in an aircraft was forwarded to the laboratory for analyzing m...
A fractured drain pipe-port installed in an aircraft was forwarded to the laboratory for analyzing m...
A failed pipe fastener assembly of an aircraft was analyzed. Failure pattern suggest that the two ha...
A failed pipe fastener assembly of an aircraft was analyzed. Failure pattern suggest that the two ha...
The normal hose assembly of LH undercarriage of an aircraft has failed by cracking at the ferrule ed...
The normal hose assembly of LH undercarriage of an aircraft has failed by cracking at the ferrule ed...
A fractured ‘Support clamp RH’ installed on an aircraft was sent to the laboratory for analysis. Exa...
A fractured ‘Support clamp RH’ installed on an aircraft was sent to the laboratory for analysis. Exa...
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...