A few components retrieved from the wreckage of a helicopter were sent to the laboratory for investigation. Examination revealed that all these components have failed by overload, probably under impact forces. None of the failed components showed evidences of delayed or progressive failure such as fatigue or stress corrosion cracking. The damage marks observed on the leading edge of the main rotor blade suggests that it had impacted with metallic wire rope or cable
A sample pertaining to the mounting lug of ‘A’ frame at cluster 8D of body structure of accident hel...
The wreckage of a helicopter which met with an accident on September 02, 2009 was examined. General ...
A sample pertaining to the mounting lug of ‘A’ frame at cluster 8D of body structure of accident hel...
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...
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...
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...
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...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
Visual, stereo-binocular and scanning electron microscopic examination revealed that the tail rotor ...
AbstractA military helicopter crash was investigated. The aircraft was flying at cruise speed in cle...
A sample pertaining to the mounting lug of ‘A’ frame at cluster 8D of body structure of accident hel...
The wreckage of a helicopter which met with an accident on September 02, 2009 was examined. General ...
A sample pertaining to the mounting lug of ‘A’ frame at cluster 8D of body structure of accident hel...
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...
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...
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...
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...
A few damaged components from the CAT-I accidented helicopter were analyzed. Detailed analysis showe...
Visual, stereo-binocular and scanning electron microscopic examination revealed that the tail rotor ...
AbstractA military helicopter crash was investigated. The aircraft was flying at cruise speed in cle...
A sample pertaining to the mounting lug of ‘A’ frame at cluster 8D of body structure of accident hel...
The wreckage of a helicopter which met with an accident on September 02, 2009 was examined. General ...
A sample pertaining to the mounting lug of ‘A’ frame at cluster 8D of body structure of accident hel...