Add to ORKGFailed tail rotor control cables of a helicopter were analyzed. Fractographic features suggest that the cables failed under overload. There were no indications of deterioration of the cable material. There were no evidences of progressive failure either. The breaking load of the cables was determined to be in the range 1100-1340 kg was required for fracturing of the cables. Evidences suggest that the cables have broken under sudden tensile overloa
There was an accident to a helicopter during ground run on July 28, 2008 wherein one upper and lower...
There was an accident to a helicopter during ground run on July 28, 2008 wherein one upper and lower...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
Failed tail rotor control cables of a helicopter were analyzed. Fractographic features suggest that ...
Tail rotor cables of a helicopter were sent to the laboratory for identifying the mode of failure. V...
Tail rotor cables of a helicopter were sent to the laboratory for identifying the mode of failure. V...
Visual, stereo-binocular and scanning electron microscopic examination revealed that the tail rotor ...
Damaged components from an accidented helicopter were sent to the laboratory for metallurgical exami...
Damaged components from an accidented helicopter were sent to the laboratory for metallurgical exami...
A broken tail gearbox (TGB) housing and failed pitch link assemblies of a helicopter were sent to th...
A few components retrieved from the wreckage of a helicopter were sent to the laboratory for investi...
A broken tail gearbox (TGB) housing and failed pitch link assemblies of a helicopter were sent to th...
The control tube has failed by rotating bending fatigue. Fretting was observed on the contacting sur...
The control tube has failed by rotating bending fatigue. Fretting was observed on the contacting sur...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
There was an accident to a helicopter during ground run on July 28, 2008 wherein one upper and lower...
There was an accident to a helicopter during ground run on July 28, 2008 wherein one upper and lower...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
Failed tail rotor control cables of a helicopter were analyzed. Fractographic features suggest that ...
Tail rotor cables of a helicopter were sent to the laboratory for identifying the mode of failure. V...
Tail rotor cables of a helicopter were sent to the laboratory for identifying the mode of failure. V...
Visual, stereo-binocular and scanning electron microscopic examination revealed that the tail rotor ...
Damaged components from an accidented helicopter were sent to the laboratory for metallurgical exami...
Damaged components from an accidented helicopter were sent to the laboratory for metallurgical exami...
A broken tail gearbox (TGB) housing and failed pitch link assemblies of a helicopter were sent to th...
A few components retrieved from the wreckage of a helicopter were sent to the laboratory for investi...
A broken tail gearbox (TGB) housing and failed pitch link assemblies of a helicopter were sent to th...
The control tube has failed by rotating bending fatigue. Fretting was observed on the contacting sur...
The control tube has failed by rotating bending fatigue. Fretting was observed on the contacting sur...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
There was an accident to a helicopter during ground run on July 28, 2008 wherein one upper and lower...
There was an accident to a helicopter during ground run on July 28, 2008 wherein one upper and lower...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...