Add to ORKGA fractured lever assembly of an aircraft was analyzed. Fractographic analysis showed that the assembly has failed by overload. Microstructural study and compositional analysis revealed that the lever assembly was made of cast Al-Mg-Fe alloy. The reason(s) for overload needs to be established
Frctorgaphic study showed that the wheel hub has failed by static overload. There were no evidences ...
A prematurely fractured main wheel hub of an aircraft was sent to the laboratory for investigation. ...
A prematurely fractured main wheel hub of an aircraft was sent to the laboratory for investigation. ...
A fractured lever assembly of an aircraft was analyzed. Fractographic analysis showed that the assem...
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...
A failed undercarriage door-operating lever of an aircraft was sent to the laboratory for analysis. ...
A failed undercarriage door-operating lever of an aircraft was sent to the laboratory for analysis. ...
Failed plate assemblies from two aircrafts were analyzed. Fractographic study showed that in both th...
Failed plate assemblies from two aircrafts were analyzed. Fractographic study showed that in both th...
A fractured kinematic linkage of the landing gear assembly of an aircraft was analyzed. Fractographi...
A fractured kinematic linkage of the landing gear assembly of an aircraft was analyzed. Fractographi...
The main fitting subassembly of main landing gear of an aircraft was sent to the laboratory for ana...
The main fitting subassembly of main landing gear of an aircraft was sent to the laboratory for ana...
A broken pin assembly of an aircraft was forwarded to the laboratory for analysis. Examination reve...
Frctorgaphic study showed that the wheel hub has failed by static overload. There were no evidences ...
A prematurely fractured main wheel hub of an aircraft was sent to the laboratory for investigation. ...
A prematurely fractured main wheel hub of an aircraft was sent to the laboratory for investigation. ...
A fractured lever assembly of an aircraft was analyzed. Fractographic analysis showed that the assem...
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...
A failed undercarriage door-operating lever of an aircraft was sent to the laboratory for analysis. ...
A failed undercarriage door-operating lever of an aircraft was sent to the laboratory for analysis. ...
Failed plate assemblies from two aircrafts were analyzed. Fractographic study showed that in both th...
Failed plate assemblies from two aircrafts were analyzed. Fractographic study showed that in both th...
A fractured kinematic linkage of the landing gear assembly of an aircraft was analyzed. Fractographi...
A fractured kinematic linkage of the landing gear assembly of an aircraft was analyzed. Fractographi...
The main fitting subassembly of main landing gear of an aircraft was sent to the laboratory for ana...
The main fitting subassembly of main landing gear of an aircraft was sent to the laboratory for ana...
A broken pin assembly of an aircraft was forwarded to the laboratory for analysis. Examination reve...
Frctorgaphic study showed that the wheel hub has failed by static overload. There were no evidences ...
A prematurely fractured main wheel hub of an aircraft was sent to the laboratory for investigation. ...
A prematurely fractured main wheel hub of an aircraft was sent to the laboratory for investigation. ...