Add to ORKGDamaged components from an accidented helicopter were sent to the laboratory for metallurgical examination. Investigation revealed that all the components failed by overload. The tail rotor cables have failed under tensile overload. Pitch change link, pulley assembly and the tail rotor control rod were found damaged/fractured due to impact
A broken tail gearbox (TGB) housing and failed pitch link assemblies of a helicopter were sent to th...
Failed tail rotor control cables of a helicopter were analyzed. Fractographic features suggest that ...
Failed tail rotor control cables of a helicopter were analyzed. Fractographic features suggest that ...
Damaged components from an accidented helicopter were sent to the laboratory for metallurgical exami...
A few components retrieved from the wreckage of a helicopter were sent to the laboratory for investi...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
A few damaged components pertaining to the incident helicopter were sent to this laboratory for anal...
A few damaged components pertaining to the incident helicopter were sent to this laboratory for anal...
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 components retrieved from the wreckage of a helicopter were forwarded to the laboratory for as...
A few components retrieved from the wreckage of a helicopter were forwarded to the laboratory for as...
Visual, stereo-binocular and scanning electron microscopic examination revealed that the tail rotor ...
A broken tail gearbox (TGB) housing and failed pitch link assemblies of a helicopter were sent to th...
A broken tail gearbox (TGB) housing and failed pitch link assemblies of a helicopter were sent to th...
Failed tail rotor control cables of a helicopter were analyzed. Fractographic features suggest that ...
Failed tail rotor control cables of a helicopter were analyzed. Fractographic features suggest that ...
Damaged components from an accidented helicopter were sent to the laboratory for metallurgical exami...
A few components retrieved from the wreckage of a helicopter were sent to the laboratory for investi...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
A few damaged components pertaining to the incident helicopter were sent to this laboratory for anal...
A few damaged components pertaining to the incident helicopter were sent to this laboratory for anal...
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 components retrieved from the wreckage of a helicopter were forwarded to the laboratory for as...
A few components retrieved from the wreckage of a helicopter were forwarded to the laboratory for as...
Visual, stereo-binocular and scanning electron microscopic examination revealed that the tail rotor ...
A broken tail gearbox (TGB) housing and failed pitch link assemblies of a helicopter were sent to th...
A broken tail gearbox (TGB) housing and failed pitch link assemblies of a helicopter were sent to th...
Failed tail rotor control cables of a helicopter were analyzed. Fractographic features suggest that ...
Failed tail rotor control cables of a helicopter were analyzed. Fractographic features suggest that ...