Add to ORKGA fractured M2 screw of a brake parachute actuator was sent to the laboratory for analyzing the cause of failure. Fractographic study showed that the screw had failed by torsional overload. As understood from the function of the screw, it appears that over-tightening of the screw was responsible for the failure
A failed tachometer generator bolt was analyzed. Fractographic features revealed that the bolt has f...
AbstractFailure analysis in mechanical components has been investigated in many studies in the last ...
Following an incidence to an aircraft, a few components of the main undercarriage assembly were sent...
A fractured plunger of brake parachute release mechanism of an aircraft was analyzed. Fractographic ...
The plunger of an aircraft was found to have fractured by overload. It appears that the fracturing ...
Item part No. R35/001-150-35002(A) LH main gear assembly Sl. No. 106L of an aircraft was sent to the...
The purpose of this study was to investigate the main causes of the co-fracture of sixteen connectin...
Two fractured bolts belonging to an aircraft engine removal ground equipment were brought to the lab...
A failed bearing (No.4) of aeroengine was sent to the laboratory for investigation. Fractographic st...
AbstractThe purpose of this study was to investigate the main causes of the co-fracture of sixteen c...
Fractographic studies indicated that the collared studs of an aeroengine have failed by over load. B...
A fractured eyering shaft (port) of the cargo door assembly of an aircraft was sent to the laborator...
A failed undercarriage door-operating lever of an aircraft was sent to the laboratory for analysis. ...
The plunger spring in question has failed by overload. There were no evidences of progressive failu...
A fractured main undercarriage fitting of an aircraft was analyzed. Analysis revealed that there was...
A failed tachometer generator bolt was analyzed. Fractographic features revealed that the bolt has f...
AbstractFailure analysis in mechanical components has been investigated in many studies in the last ...
Following an incidence to an aircraft, a few components of the main undercarriage assembly were sent...
A fractured plunger of brake parachute release mechanism of an aircraft was analyzed. Fractographic ...
The plunger of an aircraft was found to have fractured by overload. It appears that the fracturing ...
Item part No. R35/001-150-35002(A) LH main gear assembly Sl. No. 106L of an aircraft was sent to the...
The purpose of this study was to investigate the main causes of the co-fracture of sixteen connectin...
Two fractured bolts belonging to an aircraft engine removal ground equipment were brought to the lab...
A failed bearing (No.4) of aeroengine was sent to the laboratory for investigation. Fractographic st...
AbstractThe purpose of this study was to investigate the main causes of the co-fracture of sixteen c...
Fractographic studies indicated that the collared studs of an aeroengine have failed by over load. B...
A fractured eyering shaft (port) of the cargo door assembly of an aircraft was sent to the laborator...
A failed undercarriage door-operating lever of an aircraft was sent to the laboratory for analysis. ...
The plunger spring in question has failed by overload. There were no evidences of progressive failu...
A fractured main undercarriage fitting of an aircraft was analyzed. Analysis revealed that there was...
A failed tachometer generator bolt was analyzed. Fractographic features revealed that the bolt has f...
AbstractFailure analysis in mechanical components has been investigated in many studies in the last ...
Following an incidence to an aircraft, a few components of the main undercarriage assembly were sent...