HOUMA, LA, USA
N2784E
MBB 105
A FATIGUE FAILURE IN A MAIN ROTOR BLADE PITCH CHANGE LINK RESULTED IN THE LOSS OF CONTROL OF ONE BLADE, LEADING TO AN IN FLIGHT SEPARATION OF THE TAIL BOOM. THE HELICOPTER WAS UNCONTROLLABLE AND PITCHED FORWARD, IMPACTING THE GROUND INVERTED.
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports
