Add to ORKGA 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
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...
A failed jack attachment bolt belonging to an aircraft was sent to the laboratory for investigation....
A failed jack attachment bolt belonging to an aircraft was sent to the laboratory for investigation....
A failed pipe fastener assembly of an aircraft was analyzed. Failure pattern suggest that the two ha...
A cracked pipe assembly of hydraulic system-II of an aircraft was forwarded to this laboratory for e...
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...
The SS tube of the lubricating pipeline has failed by fatigue. The fatigue was of high cycle-low str...
The SS tube of the lubricating pipeline has failed by fatigue. The fatigue was of high cycle-low str...
A fractured rod assembly of an aircraft was sent to the laboratory for analysis. The component is ma...
A fractured rod assembly of an aircraft was sent to the laboratory for analysis. The component is ma...
The normal hose assembly of LH undercarriage of an aircraft has failed by cracking at the ferrule ed...
A failed pipeline of an aircraft was forwarded to the laboratory for analysis. The pipeline was foun...
The normal hose assembly of LH undercarriage of an aircraft has failed by cracking at the ferrule ed...
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...
A failed jack attachment bolt belonging to an aircraft was sent to the laboratory for investigation....
A failed jack attachment bolt belonging to an aircraft was sent to the laboratory for investigation....
A failed pipe fastener assembly of an aircraft was analyzed. Failure pattern suggest that the two ha...
A cracked pipe assembly of hydraulic system-II of an aircraft was forwarded to this laboratory for e...
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...
The SS tube of the lubricating pipeline has failed by fatigue. The fatigue was of high cycle-low str...
The SS tube of the lubricating pipeline has failed by fatigue. The fatigue was of high cycle-low str...
A fractured rod assembly of an aircraft was sent to the laboratory for analysis. The component is ma...
A fractured rod assembly of an aircraft was sent to the laboratory for analysis. The component is ma...
The normal hose assembly of LH undercarriage of an aircraft has failed by cracking at the ferrule ed...
A failed pipeline of an aircraft was forwarded to the laboratory for analysis. The pipeline was foun...
The normal hose assembly of LH undercarriage of an aircraft has failed by cracking at the ferrule ed...
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...
A cracked starboard outrigger strut assembly of an aircraft was sent to the laboratory to analyze th...
A failed jack attachment bolt belonging to an aircraft was sent to the laboratory for investigation....
A failed jack attachment bolt belonging to an aircraft was sent to the laboratory for investigation....