A rejected nose wheel hub with loose race at the bearing housing area was sent to this laboratory for investigation. Based on the signatures on the axle, and the outer and inner surfaces of the bearing, it appeared that the looseness of the race was due to inadequate fitment of the bearing at the bearing seating area of the wheel hub. There were no evidences to suggest that there was excessive axial load on the bearing in the outward direction which could lead to detachment/looseness of the bearing race. It is, therefore, stated that this failure is not similar to the one that was investigated in this laboratory earlier (refer NAL Report No. MT-FA-1205-05-2010 dated May 14, 2010). In the earlier case, the dislodgement of the bearing was by...
During 100 h servicing of an aeroengine, chips were noticed in the oil system. Strip examination of ...
Investigation showed that the turbine front bearing has failed by true brinelling followed by severe...
A few components belonging to the engine accessory gearbox (EAGB) of an aeroengine, bearing serial N...
Damaged components of the nose wheel assembly of an aircraft were sent to this laboratory for invest...
A failed nose wheel of an aircraft was forwarded to the laboratory for analysis. Examination reveale...
Damaged parts of bearings of a wheel hub of an aircraft were sent to the laboratory for analysis. Th...
Evidences suggest that the indentation marks on the rollers and the cracks on the bearing cup were r...
A failed main wheel hub of an aircraft was forwarded to the laboratory for analysis. Examination rev...
The wheel hub in question has failed by fatigue. Three fatigue cracks were identified and all of the...
A fractured retainer ring of wheel hub of an aircraft was sent to the laboratory for identifying the...
Item part No. R35/001-150-35002(A) LH main gear assembly Sl. No. 106L of an aircraft was sent to the...
The failure of the left wheel hub assembly was due to fatigue cracking of the rear half hub. The sha...
A number of failures in the main wheel hubs of a specific aircraft were analyzed. Metallography and ...
Examination revealed that misalignment in the assembly of the bearing resulted in the failure. Evide...
Frctorgaphic study showed that the wheel hub has failed by static overload. There were no evidences ...
During 100 h servicing of an aeroengine, chips were noticed in the oil system. Strip examination of ...
Investigation showed that the turbine front bearing has failed by true brinelling followed by severe...
A few components belonging to the engine accessory gearbox (EAGB) of an aeroengine, bearing serial N...
Damaged components of the nose wheel assembly of an aircraft were sent to this laboratory for invest...
A failed nose wheel of an aircraft was forwarded to the laboratory for analysis. Examination reveale...
Damaged parts of bearings of a wheel hub of an aircraft were sent to the laboratory for analysis. Th...
Evidences suggest that the indentation marks on the rollers and the cracks on the bearing cup were r...
A failed main wheel hub of an aircraft was forwarded to the laboratory for analysis. Examination rev...
The wheel hub in question has failed by fatigue. Three fatigue cracks were identified and all of the...
A fractured retainer ring of wheel hub of an aircraft was sent to the laboratory for identifying the...
Item part No. R35/001-150-35002(A) LH main gear assembly Sl. No. 106L of an aircraft was sent to the...
The failure of the left wheel hub assembly was due to fatigue cracking of the rear half hub. The sha...
A number of failures in the main wheel hubs of a specific aircraft were analyzed. Metallography and ...
Examination revealed that misalignment in the assembly of the bearing resulted in the failure. Evide...
Frctorgaphic study showed that the wheel hub has failed by static overload. There were no evidences ...
During 100 h servicing of an aeroengine, chips were noticed in the oil system. Strip examination of ...
Investigation showed that the turbine front bearing has failed by true brinelling followed by severe...
A few components belonging to the engine accessory gearbox (EAGB) of an aeroengine, bearing serial N...