Damaged components-starboard turnbuckle engine attachment support and hydraulic reservoir guard belonging to an aircraft were analyzed. Analysis showed that the hydraulic reservoir guard material had suffered severe heat effects and as a result, the guard material got cracked/fractured. There were no evidences of progressive failure such as fatigue or corrosion or stress corrosion cracking. Also, no material defects were found responsible for the failure. Evidences suggest that the engine attachment support had deformed due to overload. A detailed analysis of the failure is presented in this report
A failed suspension device fitted with the antenna of a helicopter was forwarded to this laboratory ...
A failed engine fitted on an aircraft which met with an incident was forwarded to National Aerospace...
Components of an aircraft which met with an accident immediately after take off were forwarded to th...
Damaged components-starboard turnbuckle engine attachment support and hydraulic reservoir guard belo...
There was an incidence to an aircraft wherein the pilot heard a loud bang on accelerating throttle t...
There was an incidence to an aircraft wherein the pilot heard a loud bang on accelerating throttle t...
A failed engine mount frame of an aircraft was sent to the laboratory for investigation. The engine ...
A fractured tie rod of the engine rear attachment was analyzed. Fractographic features suggest that ...
During 100 h servicing of an aeroengine, chips were noticed in the oil system. Strip examination of ...
During 100 h servicing of an aeroengine, chips were noticed in the oil system. Strip examination of ...
Evidences suggest that the LH top root fitting of the aircraft has failed by stress corrosion cracki...
Evidences suggest that the LH top root fitting of the aircraft has failed by stress corrosion cracki...
A failed engine fitted on an aircraft which met with an incident was forwarded to National Aerospace...
A failed suspension device fitted with the antenna of a helicopter was forwarded to this laboratory ...
Components of an aircraft which met with an accident immediately after take off were forwarded to th...
A failed suspension device fitted with the antenna of a helicopter was forwarded to this laboratory ...
A failed engine fitted on an aircraft which met with an incident was forwarded to National Aerospace...
Components of an aircraft which met with an accident immediately after take off were forwarded to th...
Damaged components-starboard turnbuckle engine attachment support and hydraulic reservoir guard belo...
There was an incidence to an aircraft wherein the pilot heard a loud bang on accelerating throttle t...
There was an incidence to an aircraft wherein the pilot heard a loud bang on accelerating throttle t...
A failed engine mount frame of an aircraft was sent to the laboratory for investigation. The engine ...
A fractured tie rod of the engine rear attachment was analyzed. Fractographic features suggest that ...
During 100 h servicing of an aeroengine, chips were noticed in the oil system. Strip examination of ...
During 100 h servicing of an aeroengine, chips were noticed in the oil system. Strip examination of ...
Evidences suggest that the LH top root fitting of the aircraft has failed by stress corrosion cracki...
Evidences suggest that the LH top root fitting of the aircraft has failed by stress corrosion cracki...
A failed engine fitted on an aircraft which met with an incident was forwarded to National Aerospace...
A failed suspension device fitted with the antenna of a helicopter was forwarded to this laboratory ...
Components of an aircraft which met with an accident immediately after take off were forwarded to th...
A failed suspension device fitted with the antenna of a helicopter was forwarded to this laboratory ...
A failed engine fitted on an aircraft which met with an incident was forwarded to National Aerospace...
Components of an aircraft which met with an accident immediately after take off were forwarded to th...